i TECHNOLOGICAL INSTITUTE OF THE PHILIPPINES 938 Aurora BLVD. Cubao, Quezon City COLLEGE OF ENGINEERING AND ARCHITECTURE CIVIL ENGINEERING DEPARTMENT CE 502 REINFORCED CONCRETE DESIGN A DESIGN OF A FIVE-STOREY REINFORCED CONCRETE COMMERCIAL BUILDING IN MARAWI CITY Submitted By: AMER, AHMAD BASHIR D. Submitted To: ENGR. ALLAN B. BENOGSUDAN December 11, 2021 ii ABSTRACT This project is entitled as “A Design of a Five Storey Reinforced Concrete Commercial Building in Marawi City” is presented by Ahmad Bashir D. Amer, as partial fulfillment for the requirements for CE 502 (Reinforced Concrete Design). The project is about the structural analysis and design of the identified parts for the five storey reinforced concrete commercial building utilizing the moment resisting frames, namely Ordinary Moment Resisting Frame and Special Moment Resisting Frame. Design specifications, inputs and other considerations from NBCP and NSCP were used in the design process of the project. The analyzed parts and designed included: beams, columns and slabs. The most critical part were considered to be chosen due to its highest result computed from STAAD pro CONNECT Edition, considering all the load combinations. The details and schedule of the member of the structure were created for the final design of the project. The software used in the analyzation and concrete design of the structure was STAAD.Pro CONNECT Edition. As for the detailing of the members designed was AutoCAD. iii LIST OF TABLES TABLE 1. AREAS AND FUNCTIONS PER FLOOR ...................................................................................... 6 TABLE 2. SUMMARY OF INITIAL ESTIMATES OF VALUES ..................................................................... 31 TABLE 3. RAW DESIGNER'S RANKING .................................................................................................... 37 TABLE 4. RAW INITIAL DATA .................................................................................................................... 38 TABLE 5. NORMALIZED INITIAL DATA ..................................................................................................... 38 TABLE 6. FIRST WEIGHTED SUM OF VARIOUS PERCENTAGE FOR INITIAL DATA ............................ 38 TABLE 7. SECOND WEIGHTED SUM OF VARIOUS PERCENTAGE FOR INITIAL DATA ....................... 39 TABLE 8. THIRD WEIGHTED SUM OF VARIOUS PERCENTAGE FOR INITIAL DATA............................ 39 TABLE 9. MINIMUM DENSITIES FOR DESIGN LOADS FROM MATERIALS ........................................... 54 TABLE 10. MINIMUM UNIFORM CONCENTRATED LIVE LOADS ............................................................ 54 TABLE 11. SEISMIC IMPORTANCE FACTORS ......................................................................................... 55 TABLE 12. SOIL PROFILE TYPES ............................................................................................................. 55 TABLE 13. SEISMIC ZONE FACTOR ......................................................................................................... 55 TABLE 14. NEAR-SOURCE FACTOR ........................................................................................................ 55 TABLE 15. NEAR-SOURCE FACTOR ........................................................................................................ 56 TABLE 16. SEISMIC COEFFICIENT, CA..................................................................................................... 56 TABLE 17. SEISMIC COEFFICIENT, CV..................................................................................................... 56 TABLE 18. EARTHQUAKE FORCE –RESISTING STRUCTURAL SYSTEMS OF CONCRETE ................ 57 TABLE 19. WIND ZONE FOR THE DIFFERENT PROVINCES OF THE PHILIPPINES ............................. 57 TABLE 20. WIND DIRECTIONALITY FACTOR........................................................................................... 57 TABLE 21. IMPORTANCE FACTOR, IW...................................................................................................... 58 TABLE 22. VELOCITY PRESSURE EXPOSURE COEFFICIENTS ............................................................ 58 TABLE 23. DESIGN LIVE LOADS ............................................................................................................... 58 TABLE 24. MINIMUM DESIGN DEAD LOADS............................................................................................ 59 TABLE 25. SEISMIC LOADING PARAMETER FOR ORDINARY MOMENT RESISTING FRAME – ONE WAY SLAB AND TWO WAY SLAB ..................................................................................................... 59 TABLE 26. SEISMIC LOADING PARAMETER FOR SPECIAL MOMENT RESISTING FRAME – ONE WAY SLAB AND TWO WAY SLAB .............................................................................................................. 60 TABLE 27. LOAD CASES COMBINATIONS ............................................................................................... 61 TABLE 28. BEAM END FORCES SUMMARY............................................................................................. 75 TABLE 29. NODE DISPLACEMENTS SUMMARY...................................................................................... 75 TABLE 30. SUPPORT REACTIONS SUMMARY ........................................................................................ 76 TABLE 31. BEAM END FORCES SUMMARY............................................................................................. 90 TABLE 32. NODE DISPLACEMENTS SUMMARY...................................................................................... 90 TABLE 33. SUPPORT REACTIONS SUMMARY ........................................................................................ 91 TABLE 34. BEAM END FORCES SUMMARY........................................................................................... 105 TABLE 35. NODE DISPLACEMENT SUMMARY ...................................................................................... 105 TABLE 36. SUPPORT REACTIONS SUMMARY ...................................................................................... 106 TABLE 37. BEAM END FORCES SUMMARY........................................................................................... 120 iv TABLE 38. NODE DISPLACEMENTS SUMMARY.................................................................................... 120 TABLE 39. SUPPORT REACTIONS SUMMARY ...................................................................................... 121 TABLE 40. FINAL ESTIMATE OF TRADEOFFS ....................................................................................... 122 TABLE 41. COMPARISON OF INITIAL AND FINAL ESTIMATE OF TRADEOFFS .................................. 122 TABLE 42. FINAL DESIGNER’S RANKING .............................................................................................. 129 TABLE 43. RAW FINAL DATA. ................................................................................................................. 129 TABLE 44. NORMALIZED FINAL DATA ................................................................................................... 130 TABLE 45. FIRST WEIGHTED SUM OF VARIOUS PERCENTAGE FOR FINAL DATA .......................... 130 TABLE 46. SECOND WEIGHTED SUM OF VARIOUS PERCENTAGE FOR FINAL DATA ..................... 130 TABLE 47. THIRD WEIGHTED SUM OF VARIOUS PERCENTAGE FOR FINAL DATA.......................... 131 TABLE 48.SLAB SCHEDULE .................................................................................................................... 132 TABLE 49. BEAM SCHEDULE .................................................................................................................. 132 TABLE 50. COLUMN SCHEDULE ............................................................................................................ 136 v LIST OF FIGURES FIGURE 1. MAP LOCATION OF THE FIVE-STOREY COMMERCIAL BUILDING ....................................... 2 FIGURE 2. PROJECT DEVELOPMENT PROCESS ..................................................................................... 4 FIGURE 3. GEOMETRIC MODEL ................................................................................................................. 5 FIGURE 4. GROUND FLOOR PLAN............................................................................................................. 7 FIGURE 5. SECOND FLOOR PLAN ............................................................................................................. 8 FIGURE 6. THIRD FLOOR PLAN.................................................................................................................. 9 FIGURE 7. FOURTH FLOOR PLAN............................................................................................................ 10 FIGURE 8. FIFTH FLOOR PLAN ................................................................................................................ 11 FIGURE 9. FRONT ELEVATION ................................................................................................................. 12 FIGURE 10. LEFT SIDE ELEVATION ......................................................................................................... 12 FIGURE 11. RIGHT SIDE ELEVATION ....................................................................................................... 13 FIGURE 12. REAR ELEVATION ................................................................................................................. 13 FIGURE 13. ONE WAY SLAB SYSTEM ..................................................................................................... 26 FIGURE 14. TWO WAY SLAB SYSTEM ..................................................................................................... 26 FIGURE 15. ORDINARY MOMENT RESISTING FRAME ........................................................................... 27 FIGURE 16. SPECIAL MOMENT RESISTING FRAME .............................................................................. 28 FIGURE 17. RANKING SCALE FOR IMPORTANCE FACTOR .................................................................. 30 FIGURE 18. RANKING SCALE FOR SATISFACTORY FACTOR ............................................................... 30 FIGURE 19. COST DIFFERENCE OF TRADE-OFFS 1 AND 4 .................................................................. 31 FIGURE 20. COST DIFFERENCE OF TRADE-OFFS 2 AND 4 .................................................................. 32 FIGURE 21. COST DIFFERENCE OF TRADE-OFFS 3 AND 4 .................................................................. 33 FIGURE 22. CONSTRUCTABILITY DIFFERENCE OF TRADE-OFFS 1 AND 4 ........................................ 33 FIGURE 23. CONSTRUCTABILITY DIFFERENCE OF TRADE-OFFS 2 AND 4 ........................................ 34 FIGURE 24. CONSTRUCTABILITY DIFFERENCE OF TRADE-OFFS 3 AND 4 ........................................ 35 FIGURE 25. SAFETY/SERVICEABILITY DIFFERENCE OF TRADE-OFFS 1 AND 3 ................................ 35 FIGURE 26. SAFETY/SERVICEABILITY DIFFERENCE OF TRADE-OFFS 2 AND 3 ................................ 36 FIGURE 27. SAFETY/SERVICEABILITY DIFFERENCE OF TRADE-OFFS 4 AND 3 ................................ 36 FIGURE 28. DESIGN METHODOLOGY ..................................................................................................... 41 FIGURE 29. ONE WAY SLAB FRAMING PLAN ......................................................................................... 43 FIGURE 30. TWO WAY SLAB FRAMING PLAN ......................................................................................... 44 FIGURE 31. STRESS-STRAIN DIAGRAM FOR SINGLY REINFORCED BEAM........................................ 46 FIGURE 32. FLOW CHART OF SHEAR COMPUTATION .......................................................................... 47 FIGURE 33. FLOW CHART OF DESIGN OF SINGLY REINFORCED BEAM ............................................ 48 FIGURE 34. FLOW CHART OF DESIGN OF DOUBLY REINFORCED BEAM........................................... 49 FIGURE 35. FLOW CHART OF COLUMN REINFORCEMENT .................................................................. 51 FIGURE 36. DESIGN OF SLAB .................................................................................................................. 52 FIGURE 37. GENERAL DESIGN PROCESS .............................................................................................. 53 FIGURE 38. DESIGN PROCESS FLOW CHART FOR TRADE-OFF ONE (ONE WAY SLAB – ORDINARY MOMENT RESISTING FRAME) .......................................................................................................... 62 vi FIGURE 39. GEOMETRIC MODEL OF ORDINARY MOMENT RESISTING FRAME - ONE WAY SLAB .. 63 FIGURE 40. LOAD DIAGRAM FOR DEAD LOADS .................................................................................... 64 FIGURE 41. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT X ............................................................. 64 FIGURE 42. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT -X ........................................................... 65 FIGURE 43. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT Z ............................................................. 65 FIGURE 44. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT -Z............................................................ 66 FIGURE 45. LOAD DIAGRAM FOR LIVE LOADS ...................................................................................... 66 FIGURE 46. SHEAR DIAGRAM AT X ......................................................................................................... 67 FIGURE 47. SHEAR DIAGRAM AT Y ......................................................................................................... 67 FIGURE 48. SHEAR DIAGRAM AT Z ......................................................................................................... 68 FIGURE 49. MOMENT DIAGRAM AT X ...................................................................................................... 68 FIGURE 50. MOMENT DIAGRAM AT Y ...................................................................................................... 69 FIGURE 51. MOMENT DIAGRAM AT Z ...................................................................................................... 69 FIGURE 52. WIND LOAD DIAGRAM AT X ................................................................................................. 70 FIGURE 53. WIND LOAD DIAGRAM AT –X ............................................................................................... 70 FIGURE 54. WIND LOAD DIAGRAM AT Z ................................................................................................. 71 FIGURE 55. WIND LOAD DIAGRAM AT -Z ................................................................................................ 71 FIGURE 56. GRAVITY LOAD (1.2DL + 1.6LL) – LONGITUDINAL DIRECTION ......................................... 72 FIGURE 57. GRAVITY LOAD (1.2DL + 1.6LL) – TRANSVERSE DIRECTION ........................................... 72 FIGURE 58. MOMENT DUE TO SEISMIC LOAD - LONGITUDINAL DIRECTION ..................................... 73 FIGURE 59. MOMENT DUE TO SEISMIC LOAD – TRANSVERSE DIRECTION....................................... 73 FIGURE 60. WIND LOAD – LONGITUDINAL ............................................................................................. 74 FIGURE 61. WIND LOAD – TRANSVERSE................................................................................................ 74 FIGURE 62. DESIGN PROCESS FLOW CHART FOR TRADE-OFF ONE (ONE WAY SLAB – SPECIAL MOMENT RESISTING FRAME) .......................................................................................................... 77 FIGURE 63. GEOMETRIC MODEL OF SPECIAL MOMENT RESISTING FRAME - ONE WAY SLAB ...... 78 FIGURE 64. LOAD DIAGRAMS FOR DEAD LOAD .................................................................................... 79 FIGURE 65. LOAD DIAGRAMS FOR LIVE LOAD ...................................................................................... 79 FIGURE 66. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT X ............................................................. 80 FIGURE 67. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT -X ........................................................... 80 FIGURE 68. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT Z ............................................................. 81 FIGURE 69. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT –Z ........................................................... 81 FIGURE 70. SHEAR DIAGRAM AT X ......................................................................................................... 82 FIGURE 71. SHEAR DIAGRAM AT Y ......................................................................................................... 82 FIGURE 72. SHEAR DIAGRAM AT Z ......................................................................................................... 83 FIGURE 73. MOMENT DIAGRAM AT X ...................................................................................................... 83 FIGURE 74. MOMENT DIAGRAM AT Y ...................................................................................................... 84 FIGURE 75. MOMENT DIAGRAM AT Z ...................................................................................................... 84 FIGURE 76. WIND LOAD DIAGRAM AT X ................................................................................................. 85 FIGURE 77. WIND LOAD DIAGRAM AT –X ............................................................................................... 85 FIGURE 78. WIND LOAD DIAGRAM AT Z ................................................................................................. 86 vii FIGURE 79. WIND LOAD DIAGRAM AT -Z ................................................................................................ 86 FIGURE 80. GRAVITY LOAD (1.2DL + 1.6LL) – LONGITUDINAL DIRECTION ......................................... 87 FIGURE 81. GRAVITY LOAD (1.2DL + 1.6LL) – TRANSVERSE DIRECTION ........................................... 87 FIGURE 82. MOMENT DUE TO SEISMIC LOAD - LONGITUDINAL DIRECTION ..................................... 88 FIGURE 83. MOMENT DUE TO SEISMIC LOAD - TRANSVERSE DIRECTION ....................................... 88 FIGURE 84. WIND LOAD – LONGITUDINAL ............................................................................................. 89 FIGURE 85. WIND LOAD – TRANSVERSE................................................................................................ 89 FIGURE 86. DESIGN PROCESS FLOW CHART FOR TRADE-OFF TWO (TWO WAY SLAB – ORDINARY MOMENT RESISTING FRAME) .......................................................................................................... 92 FIGURE 87. GEOMETRIC MODEL OF ORDINARY MOMENT RESISTING FRAME - TWO WAY SLAB .. 93 FIGURE 88. LOAD DIAGRAMS FOR DEAD LOAD .................................................................................... 94 FIGURE 89. LOAD DIAGRAMS FOR LIVE LOAD ...................................................................................... 94 FIGURE 90. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT X ............................................................. 95 FIGURE 91. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT –X........................................................... 95 FIGURE 92. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT Z ............................................................. 96 FIGURE 93. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT –Z ........................................................... 96 FIGURE 94. SHEAR DIAGRAM AT X ......................................................................................................... 97 FIGURE 95. SHEAR DIAGRAM AT Y ......................................................................................................... 97 FIGURE 96. SHEAR DIAGRAM AT Z ......................................................................................................... 98 FIGURE 97. MOMENT DIAGRAM AT X ...................................................................................................... 98 FIGURE 98. MOMENT DIAGRAM AT Y ...................................................................................................... 99 FIGURE 99. MOMENT DIAGRAM AT Z ...................................................................................................... 99 FIGURE 100. WIND LOAD DIAGRAM AT X ............................................................................................. 100 FIGURE 101. WIND LOAD DIAGRAM AT –X ........................................................................................... 100 FIGURE 102. WIND LOAD DIAGRAM AT Z ............................................................................................. 101 FIGURE 103. WIND LOAD DIAGRAM AT –Z ........................................................................................... 101 FIGURE 104. GRAVITY LOAD (1.2DL + 1.6LL) – LONGITUDINAL DIRECTION ..................................... 102 FIGURE 105. GRAVITY LOAD (1.2DL + 1.6LL) – TRANSVERSE DIRECTION ....................................... 102 FIGURE 106. MOMENT DUE TO SEISMIC LOAD - LONGITUDINAL DIRECTION ................................. 103 FIGURE 107. MOMENT DUE TO SEISMIC LOAD - TRANSVERSE DIRECTION ................................... 103 FIGURE 108. WIND LOAD – LONGITUDINAL.......................................................................................... 104 FIGURE 109. WIND LOAD – TRANSVERSE ............................................................................................ 104 FIGURE 110. DESIGN PROCESS FLOW CHART FOR TRADE-OFF TWO (TWO WAY SLAB – SPECIAL MOMENT RESISTING FRAME) ........................................................................................................ 107 FIGURE 111. GEOMETRIC MODEL OF SPECIAL MOMENT RESISTING FRAME - TWO WAY SLAB.. 108 FIGURE 112. LOAD DIAGRAMS FOR DEAD LOAD ................................................................................ 109 FIGURE 113. LOAD DIAGRAMS FOR LIVE LOAD .................................................................................. 109 FIGURE 114. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT X ......................................................... 110 FIGURE 115. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT –X....................................................... 110 FIGURE 116. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT Z ......................................................... 111 FIGURE 117. LOAD DIAGRAM FOR EARTHQUAKE LOADS AT -Z........................................................ 111 viii FIGURE 118. SHEAR DIAGRAM AT X ..................................................................................................... 112 FIGURE 119. SHEAR DIAGRAM AT Y ..................................................................................................... 112 FIGURE 120. SHEAR DIAGRAM AT Z ..................................................................................................... 113 FIGURE 121. MOMENT DIAGRAM AT X .................................................................................................. 113 FIGURE 122. MOMENT DIAGRAM AT Y .................................................................................................. 114 FIGURE 123. MOMENT DIAGRAM AT Z .................................................................................................. 114 FIGURE 124. WIND LOAD DIAGRAM AT X ............................................................................................. 115 FIGURE 125. WIND LOAD DIAGRAM AT –X ........................................................................................... 115 FIGURE 126. WIND LOAD DIAGRAM AT Z ............................................................................................. 116 FIGURE 127. WIND LOAD DIAGRAM AT –Z ........................................................................................... 116 FIGURE 128. GRAVITY LOAD (1.2DL + 1.6LL) – LONGITUDINAL DIRECTION ..................................... 117 FIGURE 129. GRAVITY LOAD (1.2DL + 1.6LL) – TRANSVERSE DIRECTION ....................................... 117 FIGURE 130. MOMENT DUE TO SEISMIC LOAD - LONGITUDINAL DIRECTION ................................. 118 FIGURE 131. MOMENT DUE TO SEISMIC LOAD - TRANSVERSE DIRECTION ................................... 118 FIGURE 132. WIND LOAD – LONGITUDINAL.......................................................................................... 119 FIGURE 133. WIND LOAD - TRANSVERSE ............................................................................................ 119 FIGURE 134. COST DIFFERENCE OF TRADE-OFFS 1 AND 4 .............................................................. 123 FIGURE 135. COST DIFFERENCE OF TRADE-OFFS 2 AND 4 .............................................................. 124 FIGURE 136. COST DIFFERENCE OF TRADE-OFFS 3 AND 4 .............................................................. 125 FIGURE 137. CONSTRUCTABILITY DIFFERENCE OF TRADE-OFFS 1 AND 4 .................................... 125 FIGURE 138. CONSTRUCTABILITY DIFFERENCE OF TRADE-OFFS 2 AND 4 .................................... 126 FIGURE 139. CONSTRUCTABILITY DIFFERENCE OF TRADE-OFFS 3 AND 4 .................................... 127 FIGURE 140. SAFETY/SERVICEABILITY DIFFERENCE OF TRADE-OFFS 1 AND 2 ............................ 127 FIGURE 141. SAFETY/SERVICEABILITY DIFFERENCE OF TRADE-OFFS 3 AND 2 ............................ 128 FIGURE 142. SAFETY/SERVICEABILITY DIFFERENCE OF TRADE-OFFS 4 AND 2 ............................ 128 FIGURE 143. BEAM DETAILS (A) ............................................................................................................ 141 FIGURE 144. BEAM DETAILS (B) ............................................................................................................ 142 FIGURE 145. COLUMN DETAILS (A) ....................................................................................................... 143 FIGURE 146. COLUMN DETAILS (B) ....................................................................................................... 143 ix CHAPTER 1: PROJECT BACKGROUND 1.1 The Project The project is a commercial building constituted of five stories containing all the necessary rooms for offices and grocery store at the ground floor. It is intended to be built in Marawi City. As a city with many businesses and many professionals who will go to nearby cities or most will go to metro manila, constructing a commercial building is appropriate. The designed structure is composed of five floors with a basic floor area of 893.09 sq.m. The entire building comprises of state-of-the-art facilities on offices, a lobby, a lounge, a pantry, a comfort room in every floor, a conference rooms, and an open-plan offices common in an office building topped by a roof deck. Each floor has a height of 3 meters. It is designed with the principles of Reinforced Concrete Design and under the standard and specifications of National Building Code of the Philippines (NBCP) and National Structural Code of the Philippines (NSCP), 2015, Volume 1, 7th Edition. 1 1.2 Project Location Figure 1. Map Location of the Five-Storey Commercial Building 1.3 Project Objectives 1.4.1 General Objective 1. The purpose of this project is to design a 5-storey commercial building and to analyze the structure using reinforced concrete design in accordance with the NSCP 2010 principles. 1.4.2 Specific Objectives 1) To design a 5-storey school building made of reinforced concrete materials. 2) To provide detailed plans and programmed design of the project 3) To evaluate the effect of multiple constraints, trade-offs and standards in the final design. 2 4) To provided structural analysis of the project. 1.4 The Client The client of this project is the mayor of Marawi City which is Atty. Majul Gandamra, which he will be the one to accept the funding to create a commercial building that will lead to a better Marawi City after it had a devastating collapse in economy due to the siege. 1.5 Project Scope and Limitations The following are the scope covered by the project: • The project is designed in accordance with the National Structural Code of the Philippines 2015 Volume 1, National Building Code of the Philippines and other applicable codes. • Analysis of structural elements using STAADPro CONNECT v22 program. • Detailed illustrations of structural member and design • Design by reinforced concrete materials The following are the limitations of the design project: • The detailed activities within the span of construction of the project. • The project does not include Architectural, Mechanical, Plumbing and Electrical Works. • The project does not include the cost estimation for Architectural, Mechanical, Plumbing and Electrical Works. • The interior perspective each floor of the school building project. • The maintenance and alterations of the project. 3 1.6 Project Development The following stages shown in Figure 1-3 takes place in design in a 5-storey commercial building. Conceptualization Location/Vicinity Map Identifying the project objectives, target client and scope and limitations Determining design standards and parameters Architectural and Structural Plans Identification of Constraints and TradeOffs Weighing of constraints and trade-offs based on standard capstone procedures Loadings and Structural Analysis Final Design Output Figure 2. Project Development Process 4 CHAPTER 2: DESIGN INPUT 2.1 Description of Structure The figure below shows geometric model of the main frame system of the five-storey building. It is modeled through STAAD.Pro CONNECT software and used for structural analysis. Figure 3. Geometric Model 2.2 Classification of Structure In designing a structure, the designer/s should be able to classify the structure itself using National Structural Code of the Philippines (NSCP- 2015). The structure which is commercial building classified as essential facility according to the occupancy category based on the NSCP-2015. It also classified as Special Moment Resisting Frame (SMRF) for the structural components but there is also Ordinary Moment Resisting Frame. From these classifications, the designer will identify all the parameters involve in designing the structure especially for seismic and earthquake analysis. 5 2.3 Floor Area Table 1. Areas and Functions per Floor FUNCTION AREA (m2) First Floor Store Office-2 Employee Break Rm. Storage Rm. C.R. Stairs Hallway TOTAL 725 25 25 50 25 25 25 900 Second Floor Office-1 Office-2 Conference Rm. Open-Plan Office Lobby Hallway Pantry C.R. Stair TOTAL 100 150 50 250 175 100 25 25 25 900 Third Floor Office-1 Office-2 Conference Rm. Open-Plan Office Lounge Hallway Pantry C.R Stair TOTAL 100 150 50 400 75 50 25 25 25 900 Fourth Floor Office-1 Office-2 Conference Rm. Open-Plan Office Hallway Pantry C.R Stair 100 150 50 450 75 25 25 25 6 TOTAL 900 Fifth Floor Office-1 Office-2 Conference Rm. Open-Plan Office Hallway Pantry C.R Stair TOTAL 2.4 100 150 50 450 75 25 25 25 900 Architectural Plans 2.4.1 Floor Plans Figure 4. Ground Floor Plan 7 Figure 5. Second Floor Plan 8 Figure 6. Third Floor Plan 9 Figure 7. Fourth Floor Plan 10 Figure 8. Fifth Floor Plan 11 2.4.2 Elevations Figure 9. Front Elevation Figure 10. Left Side Elevation 12 Figure 11. Right Side Elevation Figure 12. Rear Elevation 13 2.5 Review of Related Literature and Studies 2.5.1 Seismic Resistance of Buildings The conceptual design and the detailing of the structural elements (walls, columns, slabs) and the non-structural elements (partition walls, façades) plays a central role in determining the structural behaviour (before failure) and the earthquake vulnerability (sensitivity to damage) of buildings. Errors and defects in the conceptual design cannot be compensated for in the following calculations and detailed design of the engineer. A seismically correct conceptual design is furthermore necessary in order to achieve a good earthquake resistance without incurring significant additional costs. (Hugo Bachmann, January 2002). 2.5.2 Floor Slab Analysis Floor Slab Analysis (Case Study: One Residence Apartment Batam Center) Reinforced concrete slab are widely used in civil buildings, including as building floors, roof floors, bridge floors and dock floors. The load acting on the slab is generally calculated against gravitational loads. This study aims to analyse floor slab in One Residence Batam Center Apartment Construction Project. The moment method is used to predict the magnitude of frame and shrinkage values that refer to 2002 of SNI. Loading is carried out from dead loads and live loads with a two-way reinforcement system. Reinforcement is done using steel with a diameter of 10 mm. So that the minimum area is 313 mm square with a distance of 250 mm and is in the safe category. From the calculation results obtained the concrete elastic modulus obtained by 250 MPa with a reinforcement ratio of 0.0025. Checking the time dependency factor for dead loads is carried out within 3 months, 6 months, 14 12 months and more than 5 years. Long-term deflection due t frame and shrinkage is still in the safe category. (Yayuk Setyaning Astutik, 2019) 2.5.2.1 One Way Slab Behaviour and Strength of One Way Reinforced Concrete Slabs There would be a variety of slab systems which can be used to reduce the slab self-weight, such as the hollow slab, to cope with the increase in the height and dimensions of building structures which results in turn in self weight structure increase. In this study, one directional hollow slabs were experimented to investigate the behavior of the reinforced concrete slab containing cavities. The cavities filled with styropor as insulation material which were inserted at the middle zone of the slab thickness between the tension cord (lower zone) and the compression cord (upper zone). They will reduce the slab weight rather than the insulation properties as compared to the solid slab (reference slab). (Amer Izzet, March 2014) Enhancing the Behavior of One-Way Reinforced Concrete Slabs by Using Laced Reinforcement This paper studies experimentally the behavior of laced reinforced concrete one-way slabs under monotonic load. The experimental program included testing three simply supported one-way slabs of dimensions (1500 mm length, 600 mm width, and thickness 130mm. One of these slabs was the control specimen which was designed without lacing reinforcement steel and the other two specimens designed were with two variable lacing reinforcement ratio (0.27% and 0.52%). All specimens were cast with normal of 22 MPa compressive strength. Specimens were 15 tested under two equal line loads applied at the third parts of the slab (monotonic load) gradually applying up to failure. The specimens showed an enhanced in ultimate load capacity up to 40% as a result of increasing the lacing steel ratio to 0.52 %. Also, decreasing in deflection at service and at ultimate load levels by 42% and %57 respectively. In addition, the results showed that specimen with lacing reinforcement are more ductility than specimen without lacing reinforcement so using of lacing steel reinforcement leads to significant improvements in ductility index which reached to about 49% with increasing the lacing steel ratio to (0.52%). (Ali Faiq Hallawi et al., 2019) 2.5.2.2 Two Way Slab Maximum bending moments in a RC two-way slab subjected to wall loads With the purpose to characterize the behavior of a transfer slab system, a slab-wall full-scale specimen was designed, build and tested to cyclic loads in the Laboratory of Structures at UAM. The prototype slab-wall was subjected to three load patterns: 1) gravitational load; 2) horizontal load only; and 3) a combination of gravitational and lateral loads. The specimen consists of a masonry wall placed on top of a squared two-way slab of 4.25 m by side, thickness of 12 cm, on four reinforced concrete beams. The most important results presented herein are the resistance capacity of the slab supporting a load-bearing wall subjected to vertical and horizontal load. Analytical finite element slab-wall models were used. (Alonso Gómez Bernal et al., 2017) AN EXPERIMENTAL STUDY ON FLEXURAL BEHAVIOUR OF RCC TWO WAY SLABS 16 Concrete is the most commonly used material in various types of constructions. The demand of aggregate and cement used in concrete is increasing worldwide every year due to rapid industrialization and urban development. The excessive utilization of aggregate for concrete production leads to excessive exploitation of natural aggregate and environmental degradation from quarrying activities. This has resulted in renewed interest in Recycled Aggregate (RA) as a viable source of concrete ingredient. Study carries casting and testing of two way slab specimens by using natural coarse aggregate and 50% replacement with recycled aggregate. The concrete grade considered for study is M25. In the experimental study the concrete mix has been designed as per the guidelines given in IS: 10262-2009 published by Bureau of Indian Standards. In slab specimens, the steel reinforcement varies from 0.3%, 0.4%, 0.5% in both the cases (natural and recycled) by using 6mm and 8mm diameter rebars. The size of two way slab is 600mm × 800mm × 90mm. The value of modulus of elasticity (E) is evaluated from the load vs. deflection curve of slab specimens. The modulus of elasticity of concrete is a very important parameter reflecting the ability of concrete to deform elastically. Deflections and crack widths are the parameters that gives us warning that the structure is about to fail so that there will be time to counter act. The aim of study is to verify the influence of steel reinforcement on the modulus of elasticity of reinforced concrete members. (Dr. B. Madhusudana Reddy et al., December 2017) 17 2.5.2.3 Computational Analysis of RCC Slab (Simply Supported) using C Software Language Slab design is done mainly by manual method or using design and analysis software. In this article, a C coding has been done for the design of a simply supported reinforced concrete slab. The design of slabs will differ depending upon the support conditions and also on end conditions. The load condition can also be a variable factor. The design criteria will change with the grade of concrete used, the exposure conditions. These criteria have not taken into account in the coding procedure. Indian standard design procedure has been followed, and the clauses in the IS456-2000, has been followed during the coding. This coding has done to overcome the delay in the manual calculations, to obtain the accuracy in the result calculations. As slab is an import element in the structural design aspect, it has to be designed very carefully. As an input value, the steel area calculation has to be done manually in this procedure. Also the unit conversion is not allowed in the coding, and all the dimensions are to be submitted in meters only. (S.Suchithra et al., November 2019) A Comparative Study on Structural Analysis of High-Rise Buildings With the developing technology, the high-level structures provide innovative solutions that enable many functions to coexist together. In addition, high-rise buildings are an advertising tool for countries, cities and large companies to show their power and prestige. From their design to operation, these structures take place in the city skyline with their advanced technology. Formerly human’s life was near to nature, which human beings have been accustomed for centuries. However today, they have been tried to rise their structures with the help of developments in technology, construction techniques and with the limitations brought by urbanization day by day. These 18 structures, which are defined as multi storey buildings in the literature, have taken the name of skyscraper together with the desire to reach higher and higher. As technology has advanced, the desire to build higher has brought different structure system solutions and proposals. In this context, the investigation of the positive/negative effects of these structures to the function of the structure, which are the new living spaces of people, constitutes the main point of the study. It has been found that the functions are limited and the spaces cannot be used efficiently in the structure system solutions of the prestige buildings in this study. With the development of the construction materials, it will be provided that hybrid or steel construction system buildings formed by taking advantage of the steel structure with slender columns and beams. Thus, creating a more flexible and efficient use of interior spaces of extraordinary forms can be designed. (Şule Yılmaz Erten et al., 2018). Structural Framing Analysis They presented an advanced structural framing system, which can construct cost-efficient high-rise office buildings with high additional value. Main components are comprised of, (1) earthquake-resisting core walls with boundary beams, which can bear almost all of the earthquake forces, (2) outer frames and (3) the inversed haunch beams of office areas released from earthquake force. These characteristics give flexibility to building planning and future possible renovations. The seismic response analysis results illustrated that the earthquake-resistance standards of Japan, as a severely seismic country, could be satisfied, and the boundary beams reduced the seismic response. The loading tests confirmed that the shear strength and bending characteristics of the earthquake-resisting walls with built-in steel could be evaluated by conventional design equations for reinforced concrete earthquake-resisting walls. It was also verified that the boundary beams proposed had a large equivalent damping factor and could decrease damage compared with boundary beams of normal cross-sections. (Naoki Niwa et. al., 2004) 19 Ordinary Moment Resisting Frame In this study behaviour of the structure having various structural configurations like OMRF (Ordinary Moment Resisting Frames), SMRF (Special Moment Resisting Frames). The poor performance of Ordinary Moment Resisting Frame (OMRF) in past earthquakes suggested that, the special design and detailing to require arresting a ductile behaviour in seismic zones of high earthquake (zone III, IV & V). For this purpose, a G+7 storey R.C.C. regular building are analyzed for OMRCF, SMRCF framing configurations in Seismic Zone II, III & IV according to Indian codes. For OMRF structures the guide lines of I.S. 456-2000 and the design, detailing of reinforcement are executed as per which make the structure less tough and ductile in comparison of SMRF structures. The earthquake resistant design should be based on lateral strength as well as deformability and ductility capacity of structure. For adequate toughness and ductility to resist the severe earthquake shocks without collapse, in the SMRF structures Beams, columns, and beam-column joints are proportioned and detailed as per I.S. code 13920(2002). Thus it has been studied and observed that SMRF structures behave well in earthquake than OMRF structures. (Anupam S. Hirapure et. al., 2017) Special Moment Resisting Frames This performance-based study was conducted to investigate the effects of seismic coefficients on performance of concrete special moment frames of 5,7, and 10-storey buildings located in Tehran, Iran. The structures are designed three-dimensionally by ETABS 2016 software according to ACI-318-08. Fifteen specimens were designed with different base shears having seismic coefficients of 0.7, 0.85, 1, 1.15, and 1.30 times the proposed value of Iranian Standard 2800, (i.e. decreased by 70 and 85%, and increased by 115 and 130%). Endurance time method (ETA20in series of ET acceleration function) as well as three real earthquake records was employed 20 to evaluate the seismic performance of the modeled structures. The performance of structures was compared by the time of the first plastic hinges formation in beams and columns, the time of entering to nonlinear region and the time of experiencing storey drift of 2% corresponding to the life safety performance level. It was observed that the results of ET records and real records were similar to each other. A procedure was proposed for finding optimum structure with lower weight using ET method through defining efficient ratio (ER) and cost ratio (CR). Based on the results of ER/CR ratio and considering the importance of collapse prevention performance level, optimum structure was a 7-storey structure with lower weight or cost whose seismic coefficient had been reduced by 70%. It was concluded that high safety can not be achieved simply by increasing the seismic coefficient of structures. (Hadi Radmanesh et. al., 2018) Comparative Analysis on Moment Resisting Frames The comparative study of SMRF and OMRF buildings has been done by performing pushover analysis for 12 storey and 16 storey RC buildings and their response is monitored. The comparative observations are, 1. It is observed that the base shear capacity of OMRF buildings is 80% to 85% more than that of SMRF buildings. 2. And the ductility of SMRF buildings is 55% to 140% more than that of OMRF buildings. 3. This is due to the use of more number of stirrups as ductile reinforcement and heavy confinement of concrete due to splicing. 4. It is observed that SMRF buildings perform much better compared to OMRF buildings. 5. The ductility and magnitude of base shear that can be resisted increases with increase in number of storeys. (Shinde M.S. et. al., 2018). A Comparative Study on Structural Analysis of High-Rise Buildings 21 With the developing technology, the high-level structures provide innovative solutions that enable many functions to coexist together. In addition, high-rise buildings are an advertising tool for countries, cities and large companies to show their power and prestige. From their design to operation, these structures take place in the city skyline with their advanced technology. Formerly human’s life was near to nature, which human beings have been accustomed for centuries. However today, they have been tried to rise their structures with the help of developments in technology, construction techniques and with the limitations brought by urbanization day by day. These structures, which are defined as multi storey buildings in the literature, have taken the name of skyscraper together with the desire to reach higher and higher. As technology has advanced, the desire to build higher has brought different structure system solutions and proposals. In this context, the investigation of the positive/negative effects of these structures to the function of the structure, which are the new living spaces of people, constitutes the main point of the study. It has been found that the functions are limited and the spaces cannot be used efficiently in the structure system solutions of the prestige buildings in this study. With the development of the construction materials, it will be provided that hybrid or steel construction system buildings formed by taking advantage of the steel structure with slender columns and beams. Thus, creating a more flexible and efficient use of interior spaces of extraordinary forms can be designed. (Şule Yılmaz Erten et al., 2018). Study of OMRF and SMRF structures for different earthquake zones of India The increase in the rate of earthquake every year and thereby increasing loss of life and property has led to necessity of comparing the methods of analyzing/designing of building structures. The study of the building structures was done by classifying them into two methods i.e. Ordinary RC Moment Resisting Frames (OMRF) structures and Special RC Moment Resisting Frame (SMRF) Structures. In these study two comparisons has been done. First comparison is between OMRF and 22 SMRF structures. Second comparison is the behavior of a building structure in different earthquake zones of India. STAAD Pro software is used for designing structures, for four Earthquake zones. In this study the variation in the structure was done while designing, considering OMRF and SMRF Structures. For that purpose fixed dimensions of beams and columns was taken, so as to co-relate the variation in the displacement of OMRF and SMRF Structure due to lateral force generated by the earthquake in x and z direction. In conclusion, the comparison of study output is done for following the suitable method of designing the structure for safety purpose, to prevent the loss of life, infrastructure and to meet the better serviceability criteria during the earthquake. (J. Bhattacharjee, 2017). 23 CHAPTER 3: CONSTRAINTS, TRADE-OFFS AND STANDARDS 3.1 Design Constraints Design constraints are the factors that will limit the range of potential design solutions that can be adopted. In the early stage of a project only some of these constraints may be known, while others become evident as the design progresses. Constraints are divided into two, the Quantitative Constraints which refers to those that can be measured by applying of engineering principles and one of this is estimation method. Qualitative Constraints, refers to those constraints that are not measurable anymore but it can be classified by designer through perception. The following are the constraints to be considered: 3.1.1 Quantitative Constraints 1. Economic. The cost of the structure is highly considerable and important in terms of fund of the client, and it is also highly significant to the designer due to the fact that the client will be happy if the designer considers the least reasonable cost. 2. Constructability. The constructability is also called as buildability, which is a new term in construction industry. But the concept of buildability has existed from past. This will also be an important quantitative constraints because it will determine the duration of construction, schedules, number of workers and laborers, equipments needed and materials to be used. If the desired schedule to finish the project are not met, it will take a lot of time and more money to spend on the project. 3. Safety/Serviceability. Safety of the structure should and always a priority for the occupants to use. It makes the structure function effectively overtime. There are times it will accidentally damage but we cannot deny the fact of the importance of safety. 24 3.1.2 Qualitative Constraints 1. Aesthetics. This will depend on a person’s perception whether which design is more presentable and pleasing. This constraint will depend on the taste of a person and therefore it is considered as a qualitative constraint. 2. Sustainability. Sustainability refers to which how durable will be the structure as time pass by and how the building will still be considered useful and safe at the same time. Should these limit states be exceeded, it will be considered unsustainable. 3.2 Trade-Offs Considering the design constraints, trade-offs will have a significant effect on the structural design of the structure that were provided by the designer. As a trade-off, the designer will have to evaluate and check which is more effective considering the given constraints. Trade-off in the design are always present in the design process. The following are the trade-offs that were chosen by the designer because it will be most fitted to the given constraints. 3.2.1 One Way Slab 25 Figure 13. One Way Slab System One-way slabs are those slabs with an aspect ratio in plan of 2:1 or greater, in which bending is primarily about the long axis. In heavily loaded slabs, the thickness is often governed by shear or flexure, while in lightly-loaded slabs, the thickness is generally chosen based on deflection limitations. Both lightly and heavily loaded slabs are typically dimensioned so that no shear reinforcement is required, as placing stirrups in slabs is perceived to be difficult and costly. One-way slabs are designed for flexure and shear on a per meter width basis, assuming that they act as a series of independent strips. Thus one-way shear in slabs is often referred to as beam shear, and design for flexure and shear is carried out using a beam analogy 3.2.2 Two Way Slab Figure 14. Two Way Slab System When a rectangular slab is supported on all the sides and the length-to-breadth ratio is less than two, it is considered to be a two-way slab. The slab spans in both the orthogonal directions. In 26 general, a slab which is not falling in the category of one-way slab is considered to be a two-way slab. 3.2.3 Ordinary Moment Resisting Frame Ordinary Moment Resisting Frames (OMRF) do not meet special detailing requirements for ductile behavior under National Structural Code of the Philippines (NSCP 2015). Ordinary Moment Resisting Frames is stiffer and attracts higher base shear (seismic force) but less capable to redistribute forces from member to joint and joint to member due to its limitations of detailing. Typically used in non/low-seismic regions. Figure 15. Ordinary Moment Resisting Frame 3.2.4 Special Moment Resisting Frame NSCP specifies using Special moment resisting frames for analysis and study on lateral loads. NSCP uses moment-resisting frames, particularly special moment resisting frames. Special Moment Resisting Frame (SMRF) is expected to withstand significant inelastic deformations and it must sustain inter-story drift angle of at least 0.04 radians. Intermediate moment resisting frame is typically used in mid/high-seismic regions. 27 Figure 16. Special Moment Resisting Frame 3.3 Significance of Chosen Tradeoffs to the Quantitative Design Constraints In this section, the constraints enlisted in the beginning of the chapter will be related to the tradeoffs chosen by the designer. The final decision of choosing the tradeoff that will be used for the structure lies on the client. Thus, the significance of the tradeoffs to the constraints is needed. Economic. For the cost effectiveness of the structure, the tradeoffs chosen will be designed to be compared whether of the two will be more economical. Clients do not have the same state of living and thus might give priority to this constraint. Some might choose the tradeoff that have lower price but might not give way to the positivity of other tradeoffs. 28 Constructability. Time measures is significant in the construction of the structure. Knowing which of the difference in the period of construction two tradeoffs might be significant for a client. Some clients need shorter period of time and thus give priority to this constraint. Safety/Serviceability. The magnitudes of deflection for concrete members are also important. Any structure used by the people should be quite rigid and relatively-vibration free so as to provide security. Designing these two tradeoffs will give different results. Thus, one tradeoff might be safer than the other. A safer structure known to a client might be given priority. Through the consideration of multiple constraints, the designer will have to choose what particular design among the tradeoffs will be used. The tradeoff is very significant in the design for it will solve the problem regarding the concern of client considering the constraints. 3.4 Method of Measurements for Quantitative Constraints The main method of measurement that will be used in this design is estimation. For the economic constraint, the cost of the whole building. This includes the materials that will be used for the construction of the beams, slabs, and columns. It also includes the cost of the reinforcements that will be used for the structure. For the constructability of the structure, the period of time that will be utilized to construct the building will be estimated, together with the number of workers that will work on that period of time. The number of workers will be constant for both tradeoffs. The difference between the days will give the result for each tradeoff. For the last constraint, the deflection of the most critical beam will be computed for each tradeoff and will then be compared. 3.5 Ranking Scale The ranking scale that will be used in the design will be based on the model on tradeoff strategies that is formulated by Otto and Antonsson (1991). The importance factors in every constraint is scaled from 0 29 to 5, while the capacity to satisfy the constraints will be scaled from -5 to 5, 5 being the highest for both. After obtaining the results, the product of the importance and the capacity to satisfy the criteria will be summed of from every constraint. The result will be the overall ranking of the trade-off. Figure 17. Ranking Scale for Importance Factor Figure 18. Ranking Scale for Satisfactory Factor Computation of ranking for ability to satisfy criterion of materials: Percent Difference () = Higher Value-Lower Value Higher Value Subordinate Rank = Governing rank - x10; Equation 1 Percent Difference 10 ; Equation 2 The above equations will be used for the manipulation of the rankings of each constraint given to the tradeoffs. The governing rank is the highest possible value set by the designer. The subordinate rank in second equation is a variable that corresponds to its percentage difference from the governing rank along the ranking scale. 3.6 Initial Estimate and Ranking Computation To determine the difference between the two tradeoffs, certain methods were used by the designer. For the economic constraint, a cost estimate was provided. For the constructability constraint, an estimate of the number of working days was provided, given that there will be 50 workers. For the safety/serviceability constraint, the deflection of the most critical beam was considered. 30 In this part, a rough computation of the estimates was utilized. The values written in the table below were just assumed by the designer whose basis came from experience. Table 2. Summary of Initial Estimates of Values CONSTRAINT Economic Constructability Safety/Serviceability ESTIMATED VALUE One-Way Slab Two-Way Slab SMRF OMRF Php 16,000,000 Php 17,500,000 550 Days 575 Days 5% of allowable 3.5% of allowable One-Way Slab OMRF Php 18,000,000 600 Days 4% of allowable Two-Way Slab SMRF Php 15,500,000 525 Days 4.5% of allowable Computation of ranking for Economic Constraint of Trade-Offs one (1) and four (4) % Difference = Higher Value-Lower Value % Difference = Higher Value 18000000-15500000 18000000 x100 x100 % Difference = 13.88 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 1.389 Subordinate rank = 3.599 Figure 19. Cost Difference of Trade-Offs 1 and 4 31 Computation of ranking for Economic Constraint of Trade-Offs two (2) and four (4) % Difference = Higher Value-Lower Value Higher Value % Difference = 16000000-15500000 16000000 x100 x100 % Difference = 3.125 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 0.3125 Subordinate rank = 4.6875 Figure 20. Cost Difference of Trade-Offs 2 and 4 Computation of ranking for Economic Constraint of Trade-Offs three (3) and four (4) % Difference = Higher Value-Lower Value % Difference = Higher Value 17500000-15500000 17500000 x100 x100 % Difference = 11.429 Subordinate rank = Governing rank - % difference 10 32 Subordinate rank = 5 – 1.43 Subordinate rank = 3.57 Figure 21. Cost Difference of Trade-Offs 3 and 4 Computation of ranking for Constructability Constraint of Trade-Offs one (1) and four (4) % Difference = Higher Value-Lower Value Higher Value % Difference = 600-525 600 x100 x100 % Difference = 12.5 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 1.25 Subordinate rank = 3.75 Figure 22. Constructability Difference of Trade-Offs 1 and 4 Computation of ranking for Constructability Constraint of Trade-Offs two (2) and four (4) % Difference = Higher Value-Lower Value Higher Value x100 33 % Difference = 550-525 550 x100 % Difference = 4.545 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 0.454 Subordinate rank = 4.546 Figure 23. Constructability Difference of Trade-Offs 2 and 4 Computation of ranking for Constructability Constraint of Trade-Offs three (3) and four (4) % Difference = Higher Value-Lower Value Higher Value % Difference = 575-525 575 x100 x100 % Difference = 8.695 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 0.869 Subordinate rank = 4.131 34 Figure 24. Constructability Difference of Trade-Offs 3 and 4 Computation of ranking for Safety/Serviceability Constraint for Trade-Offs one (1) and three (3) % Difference = Higher Value-Lower Value Higher Value % Difference = 4 - 3.5 4 x100 x100 % Difference = 12.5 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 1.25 Subordinate rank = 3.75 Figure 25. Safety/Serviceability Difference of Trade-Offs 1 and 3 Computation of ranking for Safety/Serviceability Constraint for Trade-Offs two (2) and three (3) % Difference = Higher Value-Lower Value Higher Value % Difference = 5 - 3.5 5 x100 x100 % Difference = 30 Subordinate rank = Governing rank - % difference 10 35 Subordinate rank = 5 – 3 Subordinate rank = 2 Figure 26. Safety/Serviceability Difference of Trade-Offs 2 and 3 Computation of ranking for Safety/Serviceability Constraint for Trade-Offs four (4) and three (3) % Difference = Higher Value-Lower Value Higher Value % Difference = 4.5 - 3.5 4 x100 x100 % Difference = 22.222 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 2.222 Subordinate rank = 2.778 Figure 27. Safety/Serviceability Difference of Trade-Offs 4 and 3 3.7 Raw Designer’s Ranking and Assessment After making an initial estimate of the structure considering the constraints, the design came up with the raw rankings on the one-way slab and two-way slab. The values computed in the latter section is tabulated. 36 Table 3. Raw Designer's Ranking CONSTRAINT (CRITERIA) IMPORTANCE (on a scale of 0 to 5) Economic 5 Constructability 4 Safety/Serviceability 3 Overall Ranking ABILITY TO SATISFY THE CRITERION (on a scale of 0 to 5) One-Way One-Way Two-Way Two-Way Slab OMRF Slab SMRF Slab OMRF Slab SMRF 3.599 4.6875 3.57 5 3.75 4.546 4.131 5 3.75 2 5 2.778 44.245 47.6215 49.374 53.334 These tabulated values are just subjective, especially the importance factors. These values will still go on with the validation after making a final estimate and final ranking. Knowing the significance of the constraints to the tradeoffs, the ranks in its importance are given as 5, for economic, 4, for constructability, and 3, for safety/serviceability. As for economic constraint, it turned out that the initial cost for the two-way slab SMRF is cheaper than the other three, considering only the volume of concrete that will be used. As for the constructability constraint, it turned out that the labor constituting of 50 workers will have to work for longer time for the construction of the one-way slab OMRF. As for the safety/serviceability constraint, the deflection of the critical member in the two-way slab is quite greater than that of the one-way slab. Overall, it turned out that the two-way slab SMRF tradeoff outranked the other three tradeoff for the raw designer’s ranking. 3.8 Normalization of Initial Data The normalization of data are based on the initial estimate of the two mandatory tradeoffs namely, One-Way Slab and Two-Way Slab, and based on the three constraints, namely Economic, Constructability and Serviceability. 37 3.8.1 Raw Data Table 4. Raw Initial Data Design 1. OMRF (One-Way) 2. OMRF (Two-Way) 3. SRMF (One-Way) 4. SMRF (Two-Way) PC1 (Cost in pesos) 18000000 16000000 17500000 15500000 PC2 (Duration in days) 600 550 575 525 PC3 (Safety/Serviceability in percent) 4 5 3.5 4.5 Table 4 shows the raw data gathered from previous studies and used it as a basis to determine which trade-off offers the best in a particular constraint, and in general scale. 3.8.2 Normalized Data Table 5. Normalized Initial Data Design 1. OMRF (One-Way) 2. OMRF (Two-Way) 3. SRMF (One-Way) 4. SMRF (Two-Way) PC1 (Cost in pesos) 1 8.2 2.8 10 PC2 (Duration in days) 1 7 4 10 PC3 (Safety/Serviceability in percent) 7 1 10 4 Normalization of rating means adjusting values measured on different scales to a noitionally common scale, prior to averaging. Table 5 shows the normalized data from the raw data. 3.8.3 Weighted Sum of Various Percentage Weight Table 6. First weighted sum of various percentage for initial data PC 1 2 3 Weighted Sum Weight (%) 0.5 0.3 0.2 1 D1 1 1 7 2.2 D2 8.2 7 1 6.4 D3 2.8 4 10 4.6 D4 10 10 4 8.8 38 Table 6 shows the first weighted sum of various percentage where constraints one (1), two (2) and three (3) have given a percentage of 0.5, 0.3 and 0.2 respectively. Table 7. Second weighted sum of various percentage for initial data PC 1 2 3 Weighted Sum Weight (%) 0.44 0.3 0.26 1 D1 1 1 7 2.56 D2 8.2 7 1 5.968 D3 2.8 4 10 5.032 D4 10 10 4 8.44 Table 7 shows the first weighted sum of various percentage where constraints one (1), two (2) and three (3) have given a percentage of 0.44, 0.3 and 0.26 respectively. Table 8. Third weighted sum of various percentage for initial data PC 1 2 3 Weighted Sum Weight (%) 0.3 0.4 0.3 1 D1 1 1 7 2.8 D2 8.2 7 1 5.56 D3 2.8 4 10 5.44 D4 10 10 4 8.2 Table 8 shows the first weighted sum of various percentage where constraints one (1), two (2) and three (3) have given a percentage of 0.3, 0.4 and 0.3 respectively. 3.9 Design Standards To come up with the final design of the structure, the designer utilized the codes and standards written in the following: 1. National Building Code of the Philippines (NBCP) 2. National Structure Code of the Philippines (NSCP 2015) 39 The National Building Code of the Philippines (NBCP), enacted into law on August 26, 1972, provides for all buildings and structures a framework of minimum standards and requirements by guiding and controlling location, siting, and design. The NBCP also establishes standards for quality of materials, construction, use, occupancy, and maintenance, including environment, utilities, fixtures, equipments, and mechanical, electrical, and other systems and installations. One of the main reasons why the National Building Code is created is to ensure public safety. All buildings must abide to certain principles of construction. All materials that are needed must also be environmental friendly. The National Structural Code of the Philippines (NSCP) is created to provide minimum standards to safeguard life, health, property, and public welfare, consistent with the principles of sound environmental management and control. It is also the purpose of this code is to provide a framework of minimum standards and requirements to regulate and controlling their location, site, deign, quality of materials, construction, use, occupancy and maintenance for all buildings that will be built. The current version of it is the NSCP 2015 7th Edition (Vol.1). 40 CHAPTER 4: DESIGN OF STRUCTURE 4.1 Design Methodology In designing the Reinforced Concrete Structure, the designer will conform to the codes and standards of National Structural Code of the Philippines 2015. The figure below shows the step by step process of the design. STRUCTURAL PLANS FRAMING PLANS NBCP DESIGN SPECIFICATIONS NSCP COMPRESSIVE STRENGTH MATERIAL PROPERTIES MODULUS OF ELASTICITY STRUCTURAL MEMBER DIMENSIONS STRUCTURAL MODEL GEOMETRIC MODELING DEAD LOAD AND LIVE LOAD LOAD MODELS SEISMIC LOAD AND WIND LOAD LOAD COMBINATIONS SHEAR DIAGRAMS STRUCTURAL ANALYSIS MOMENT DIAGRAMS REACTIONS AND DEFLECTIONS STRUCTURAL DESIGN DESIGN SCHEDULES DETAILING Figure 28. Design Methodology 41 The first process in design methodology was the creation of structural plans. The structural plans included the framing plans of the two trade-offs. The next step was to know the design specifications. These specifications are the codes and standards needed for the structure’s classification and description. The National Building Code and National Structural Code of the Philippines are the main books used for design specifications. The third step in the process was the identification of the material properties. The compressive stresses and modulus of elasticity of the concrete and steel to be used were determined. Also, the structural member dimensions (b, d, etc.) were assumed. The fourth step was the creation of the structural model. These models included geometric modelling, which showed the positioning of the structural members (beams, columns, slabs) in 3D form. The fifth step was the presentation of load models. In this part, the loads acting on the structure were computed. These loads were the dead load, live load, wind load, and seismic (earthquake) load, applying also the load combinations. After computing for these loads, load models was presented also in 3D form. The sixth step was the structural analysis. In structural analysis, member (beams and columns) forces and reactions were determined. The member forces included were the axial force, shear force, and moment acting on the member. The last part was the structural design. The structural design did not include the design of footings. The values from the structural analysis was utilized to design the structural members of the structures, mainly the beams and columns. The maximum moment acting on a beam was used to design the beam, and the maximum value of the axial force acting on a column was used to design the column. To design the slab, the total load on the floors was utilized. 42 4.1.1 Structural Plans Figure 29. One Way Slab Framing Plan 43 Figure 30. Two Way Slab Framing Plan 44 4.1.2 Structural Design In this section, the beams, columns, and slabs were designed. The main goal of the structural design of the members is to know the number of bars and their spacing, and check if the assumed dimensions are adequate for the structure. For beams and columns, only the most critical parts were designed. For one-way slab, only one slab was considered both in longitudinal and transverse directions was designed. For two-way slab, only one strip was designed also considering both longitudinal and transverse directions. For convenience, a sample procedure of computation for a structural member will be shown. The manual computations of the members is shown in the appendices. 4.1.2.1 Design of Beams Due to forces acting on the beam, the whole structure experiences flexure, and thus the whole length of the beam have moments within them. Also due to these forces, the beam experiences a shearing stress, which makes a part of the beam to be compressed (top), and another part to be tensed (bottom). To design the beams of the entire structure, the beam which had the highest moment was picked and the resulting design for that beam will be applied to all other beams in the structure. The dimensions of the beam (b,t) and the stresses (f’c,fy) were provided by the designer. The parts of the beam to be designer are the supports, which experience negative moment, and the midspan, which experience positive moment. Moreover, the stress strain diagram of the cross-sectional of the beam was used for the design. The following flow charts present the step by step process of designing a beam. 45 Figure 31. Stress-Strain Diagram for Singly Reinforced Beam Given: b,d,f’c and fy Vu = R-Wud Vc = 1/6ξf'cbd YES Vu = 1/3 ΦVc YES No shear reinforcement is required Vu = 1/3 ΦVc Vn = Vu/Φ NO Av = bs/3fy S=d/2 Vs = Vn - Vc Vs ≤ 2/3 ξf'cbd 46 YES NO S = Avfyd/Vs Adjust the size of beam Vs ≤ 1/3 ξf'cbd Smax = d/2 Smax = d/4 End End Figure 32. Flow Chart of Shear Computation Given: f’c,fy,b,d and ω Calculate Mumax=Φf’cbd ω(1-.59 ω) MT=Mload+Mwt of beam MT<Mumax MT<Mumax YES NO MT>Mumax MT<Mumax Design as Doubly Design as Singly 47 Ru = Mu/Φbd2 ρact = (0.85f’c/fy)(1-1-2Ru/0.85f’c) YES ρmin < ρ <ρmax NO Ast = ρact(bd) Change Section π No. of bars = Ast/(4 D2 ) Check if steel yield, a =Asfy/0.85f’cb c = a/β εs = 0.003(d-c)/c εy = fy/Es YES εs > εy NO εs > εy, Steel Yield εs > εy, Steel not Yield End End Figure 33. Flow Chart of Design of Singly Reinforced Beam 48 Given: f’c,fy,b,d and ω Calculate Mumax = Φf’cbd2ω(1-.59ω) MT = Mload + Mwt of beam YES MT > Mumax NO MT > Mumax, Design as Doubly MT < Mumax, Design as Singly As1 = ρmaxbd Check if Compression steel yield Mu1 = Mumax a = As1 / 0.85f’cb Mu2 = Mu-Mu1 c = a/β As2 = Mu2/Φfy(d-d’) YES f’s ≥ fy NO f’s = fy f’s < fy A’s = As2 A’s = As2fy/f’s π No. of bars = A’s/( 4 D2 ) π No. of bars = A’s/( 4 D2 ) End End Figure 34. Flow Chart of Design of Doubly Reinforced Beam 49 4.1.2.2 Design of Columns From the structural analysis, the column that experienced the greatest axial forces was designed. The designer started the design of the column in determining the number of bars and its positioning within the gross area of the column. Knowing the position of bars in the column, the designer then computed for the axial force capacity column due to the eccentric load. The flow chart below shows the step by step process done by the designer. The second flow chart is applicable only in this design (eccentricity on one side only). Given: Pcap,fy,f’c,Φ; Assume: ρg = 0.01-0.08 Ast = 0.01Ag Pcap = 0.8Φ[(0.85f’c(Ag-0.01Ag)+fy(0.01Ag)], Compute for Ag t = Ag Solve for ex = Pux(d)/Pu ex = Puy(d)/Pu Check for column capacity YES S ρg < 0.08, OK ρg < 0.08 NO ρg > 0.08 adjust ρg (Assume) 50 Check for column capacity Pu=0.8Φ[(0.85f’c(Ag-0.01Ag)+fy(0.01Ag)] Pcap > Pu Pcap < Pu Pcap > Pu, OK Adjust dimension End Figure 35. Flow Chart of Column Reinforcement 4.1.2.3 Design of Slabs To design a slab, we always consider the longer and shorter span of the slab since the bending is experience by the whole. For One-way slabs, the process is quite the same in designing a singly reinforced concrete beam. The only difference is that we assume that we get a strip from the whole length of the slab. The width of that strip is 1 meter with thickness. Following the procedure of solving for the reinforcement of singly reinforced beams, the desired number of bars for one-way slab was computed. For the spacing of bars, the width, b (1 m) was divided by the diameter of the bar times the quantity of bars. Since the two-way slab transmits the load to the supports in trapezoidal form, the method used for one-way slab is not applicable. For the two-way slab, the equivalent frame method was used. The two-way slab was designed considering the positive and negative 51 moments passed through the column strip and middle strip. The flow chart below shows the procedure of equivalent frame method. Flat Plate Slab L/S One-Way Slab Two-Way Slab Step 1: Estimate the slab thieckness to meet the code requirements Step 1: Estimate the slab thieckness to meet the code requuirements Step 2: Calculate the factored moment to be carried by the slab Step 2: Determine the depth required from shear Step 3: Compute for the Required Steel Ratio Step 3: Calculate the total static moments to be resisted in the two direction Step 4: Compute for the Steel Area Step 5: Compute for the required main bar spacing Step 4: Estimate the percentages of the static moments that are positive and negative, and proportion the resulting values between the column and middle strips. Step 5: Select the reinforcing End End Figure 36. Design of Slab 52 4.2 General Design Process of the Structure START Design of Reinforced Concrete Data Gathering Design Codes and Consideration Trade-Offs Design One-Way Slab Design Two-Way Slab Evaluations of Results Evaluation of Results Final Design of Beams, Columns and Slabs Final Design of Beams, Columns and Slabs END END Figure 37. General Design Process 53 Figure 31 shows the flow chart of process activities for the designer. The design process will start with planning what type structure must be designed and getting the data and assumptions that the project might need. The data and assumptions were computed through the use of computer software aid like STAAD and MS Excel, and the results will be tabulated by the designer for the evaluation of what result may be fit in the constraints and what might be economical. 4.2.1 Design Loads and Inputs The following are the tables used in each design computations: 4.2.1.1 Materials Table 9. Minimum Densities for Design Loads from Materials Stone Concrete Fill Gypsum Board Suspended Steel Channel Mechanical Duct Allowance Terrazo Grout CHB Clay Dry Water Proofing Cement Finish 1.53 Kpa 0.2 Kpa 0.1 Kpa 0.2 Kpa 1.53 Kpa 0.11 Kpa 1.65 Kpa 0.6435 Kpa 0.05 Kpa 1.53 Kpa Table 204-1 Minimum Densities for Design Loads from Materials (NSCP 2015) Table 10. Minimum Uniform Concentrated Live Loads Material Masonry, Concrete Density (KN/m3) 16.5 Table 205-1 Minimum Uniform Concentrated Live Loads (NSCP 2015) 54 4.2.1.2 Earthquake Load Parameters Table 11. Seismic Importance Factors Occupancy Category I. Essential facilities II. Hazardous facilities III. Special Occupancy Structures IV. Standard Occupancy Strutures V. Miscellaneous Structures Seismic Importance Factor I 1.5 1.25 1 Seismic Importance Factor Ip 1.5 1.5 1 1 1 1 1 Table 208-1 Seismic Importance Factors (NSCP 2015) Table 12. Soil Profile Types Soil Profile Soil Profile Name Ave. Properties for Top 30 m Soil Profile Shear Wave Velocity SPT Undrained Shear Strenght SA Hard Rock >1500 SB Rock 760 to 1500 Sc Very Dense Soil 360 to 760 >50 >100 SD Stiff Soil Profile 180 to 360 15 to 50 50 to 100 SE Soft Soil Profile <180 <15 <50 SF Soil Requiring Site-Specific Evaluation See Section 208.4.3.1 Table 208-2 Soil Profile Types (NSCP 2015) Table 13. Seismic Zone Factor Zone Z 2 0.2 4 0.4 Table 208-3 Seismic Zone Factor, Z Table 14. Near-Source factor Seismic Source Type A Closest Distance to Known Seismic Source ≤ 5 Km ≥10 Km 1.2 1 55 B C 1 1 1 1 Table 208-4 Near-Source factor, Na (NSCP 2015) Table 15. Near-Source factor Seismic Source Type A B C Closest Distance to Known Seismic Source ≤ 5 Km 10 Km 1.6 1.2 1.2 1 1 1 ≥15 Km 1 1 1 Table 208-5 Near-Source factor, Nv (NSCP 2015) Table 16. Seismic Coefficient, Ca Soil Profile Type Seismic Zone 4 Z=0.4 .32Na SA 2 Z=0.2 0.16 SB 0.2 .40Na Sc 0.24 .40Na SD 0.28 .44Na SE 0.34 .44Na SF See Footnote 1 of Table 208-8 Table 208-7 Seismic Coefficient, Ca (NSCP 2015) Table 17. Seismic Coefficient, Cv SA Seismic Zone 2 Z=0.2 0.16 4 Z=0.4 .32Na SB 0.20 .40Na Sc 0.32 .56Na SD 0.40 .64Na SE 0.64 .96Na SF See Footnote 1 of Table 208-8 Soil Profile Type 56 Table 208-8 Seismic Coefficient, Cv (NSCP 2015) Table 18. Earthquake Force –Resisting Structural Systems of Concrete Basic Seismic Force Resisting System R Ω0 System Limitation and Building Limitation Zone 2 Zone 4 C. Moment Resisting Frame Special reinforced concrete moment frames 8.5 2.8 NL NL Table 208-11A Earthquake Force –Resisting Structural Systems of Concrete (NSCP 2015) 4.2.1.3 Wind Loads Table 19. Wind Zone for the Different Provinces of the Philippines Zone Classification (Basic Wind Speed) Zone 2 V=200 kph Province National Capital Region Table 207-1 Wind Zone for the Different Provinces of the Philippines (NSCP 2015) Table 20. Wind Directionality factor Structural Type Directionality factor Kd Buildings °Main Wind Force Resisting System °Components and Cladding Arched Roof Chimneys, Tanks, and Similar Structures °Square °Hexagonal °Round Soild Signs Open Signs and Lattice Framework Trussed Towers °Triangular. Square, rectangular °All other cross sections 0.85 0.85 0.9 0.95 0.95 0.85 0.85 0.85 0.95 57 Table 207-2 Wind Directionality factor (NSCP 2015) Table 21. Importance factor, Iw Occupancy Category I II III IV V Description Iw Essential Hazardous Special Occupancy Standard Occupancy Miscellaneous 1.15 1.15 1.15 1 0.87 Table 207-3 Importance factor Iw (NSCP 2015) Table 22. Velocity Pressure Exposure Coefficients Exposure (Note 1) B Height above Ground Level (m) Case 1 Case 2 0-4.5 0.7 0.57 6 0.7 0.62 7.5 0.7 0.66 9 0.7 0.7 12 0.76 0.76 15 0.81 0.81 18 0.85 0.85 C Cases 1& 2 0.85 0.9 0.94 0.98 1.04 1.09 1.13 D Cases 1&2 1.03 1.08 1.12 1.16 1.22 1.27 1.31 Table 207-4 Velocity Pressure Exposure Coefficients (NSCP 2015) 4.2.1.4 Live Loads The following Live Loads are to be used in the analysis of the structure. Table 23. Design Live Loads Occupancy Office Open Plan Office Call Centers and Business Processing Lobbies Lounge Pantry Uniform Load (kPa) 2.4 4.8 2.9 4.8 4.8 2.4 58 Hallway Comfort Room 1.9 1.9 4.2.1.5 Dead Loads The following Dead Loads are to be used in the analysis of the structure. Table 24. Minimum Design Dead Loads Materials Cement Finish (25mm) on stone concrete fill Suspended Steel Channel System Mechanical duct allowance Gypsum Board (per mm) CHB wall full grout (19.6 kN/m3) (200mm) Plaster (both sides) Design Loads (kPa) 1.53 0.1 0.2 0.008 3.88 0.48 4.2.1.6 Seismic Loading Parameters The following values are the inputs used in the parameters for Earthquake loadings. Table 25. Seismic Loading Parameter for Ordinary Moment Resisting Frame – One Way Slab and Two Way Slab 59 Table 26. Seismic Loading Parameter for Special Moment Resisting Frame – One Way Slab and Two Way Slab 60 4.2.1.7 Load Combinations The following table defines the different types of load combination used in the structural analysis of the building. All these combinations will be applied, and the designer will determine the load combination that will produce the maximum stress in the building. This governing load combination will then be used to calculate the member forces for the design. Table 27. Load Cases Combinations 61 4.3 Design Analysis for Trade-Off One (One Way Slab – Ordinary Moment Resisting Frame) The following are the analysis that is based on the modelling of the structure using the software – STAAD.Pro CONNECT. The values are taken depending on the design loads and inputs. 4.3.1 Design Methodology for Trade-Off One (One-Way Slab – Ordinary Moment Resisting Frame) GEOMETRIC AND FRAME MODELLING ANALYSIS AND INITIAL DESIGN ESTIMATION OF COST DESIGNER’S FINAL RANKING FINAL DESIGN Figure 38. Design Process Flow Chart for Trade-Off One (One Way Slab – Ordinary Moment Resisting Frame) 62 4.3.2 Geometric Modeling To simulate all the possible effects of different loadings to the structure with different load combinations, the designer use Staad Pro CONNECT to have a thorough analysis for this first tradeoff. Figure 39. Geometric Model of Ordinary Moment Resisting Frame - One Way Slab 63 4.3.3 Load Diagrams of Trade-Off One (One Way Slab) Figure 40. Load Diagram for Dead Loads Figure 41. Load Diagram for Earthquake Loads at X 64 Figure 42. Load Diagram for Earthquake Loads at -X Figure 43. Load Diagram for Earthquake Loads at Z 65 Figure 44. Load Diagram for Earthquake Loads at -Z Figure 45. Load Diagram for Live Loads 66 Figure 46. Shear Diagram at X Figure 47. Shear Diagram at Y 67 Figure 48. Shear Diagram at Z Figure 49. Moment Diagram at X 68 Figure 50. Moment Diagram at Y Figure 51. Moment Diagram at Z 69 Figure 52. Wind Load Diagram at X Figure 53. Wind Load Diagram at –X 70 Figure 54. Wind Load Diagram at Z Figure 55. Wind Load Diagram at -Z 71 4.3.4 Frame Staad Analysis Figure 56. Gravity Load (1.2DL + 1.6LL) – Longitudinal direction Figure 57. Gravity Load (1.2DL + 1.6LL) – Transverse direction 72 Figure 58. Moment due to Seismic Load - Longitudinal direction Figure 59. Moment due to Seismic Load – Transverse direction 73 Figure 60. Wind Load – Longitudinal Figure 61. Wind Load – Transverse 74 4.3.5 Structural Analysis Results The following results are presented in the table below. These are the results of the design loads and inputs using the software STAAD.Pro CONNECT Edition. 4.3.5.1 Beam End Forces Table 28. Beam End Forces Summary Max Fx Min Fx Max Fy Min Fy Max Fz Min Fz Max Mx Min Mx Max My Min My Max Mz Min Mz Beam 1140 12173 12173 52215 1144 1145 52250 52250 1145 1144 1128 1128 L/C 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 6 EQ +Z -E 1 EQ +X +E 219 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (4) 6 EQ +Z -E 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 4 EQ -X -E Beam End Forces Node Fx (kN) 131 2250.67 6 -967.885 6 720.797 20 511.587 135 1343.185 136 13.726 221 0 221 -44.815 136 13.726 135 1343.185 119 1494.325 119 -0.008 Fy (kN) 270.794 -54.991 303.122 -335.117 3.548 6.609 0 -90.263 6.609 3.548 290.511 -287.57 Fz (kN) Mx (kN-m) My (kN-m) 14.401 -3.413 -52.024 0.542 -2.415 -0.678 -1.937 8.626 2.421 -0.391 0.652 -0.489 303.253 -3.234 -616.068 -299.329 3.265 595.559 -51.646 85.995 64.554 51.982 -86.555 -64.974 -299.329 3.265 595.559 303.253 -3.234 -616.068 -14.508 -3.413 -1.899 0 3.444 0 Mz (kN-m) 645.516 -124.239 377.581 441.342 -13.945 16.5 0 -141.376 16.5 -13.945 686.221 -681.714 4.3.5.2 Node Displacements Table 29. Node Displacements Summary Max X Min X Max Y Min Y Max Z Min Z Max rX Min rX Max rY Min rY Max rZ Min rZ Max Rst Node 498 498 84 286 420 504 7 86 414 420 231 225 504 Node Displacement Horizontal Vertical Horizontal Resultant L/C X (mm) Y (mm) Z (mm) mm 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 48.988 -0.616 -0.2 48.992 4 EQ -X -E -48.544 -0.359 -3.25 48.654 6 EQ +Z -E -0.561 1.708 6.595 6.835 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 0.639 -4.655 -24.856 25.296 6 EQ +Z -E 3.033 0.449 31.67 31.818 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 3.306 -0.45 -35.047 35.205 6 EQ +Z -E 0.67 0.199 6.595 6.631 223 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (8) -0.521 -0.313 -6.679 6.706 224 ULC, 1.38 DEAD + 1 SEISMIC (1) 42.321 -0.383 1.017 42.335 219 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (4) -41.708 -0.575 0.064 41.712 219 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (4) -22.72 -0.324 0.567 22.729 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 22.95 -0.38 0.537 22.959 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 48.791 -1.257 -6.63 49.256 rX (rad) 0 0 0.001 -0.001 0.001 -0.001 0.002 -0.002 0 0 0 0 0 Rotational rY (rad) 0 0 0 0 0 0 0 0 0 0 0 0 0 rZ (rad) -0.001 0.001 0 0 0 0 0 0 -0.001 0.001 0.004 -0.004 -0.001 75 4.3.5.3 Support Reactions Table 30. Support Reactions Summary Max Fx Min Fx Max Fy Min Fy Max Fz Min Fz Max Mx Min Mx Max My Min My Max Mz Min Mz Node 125 118 131 127 135 136 135 136 92 92 119 119 Support Reactions Horizontal Vertical Horizontal Moment L/C Fx (kN) Fy (kN) Fz (kN) Mx (kN-m) My (kN-m) Mz (kN-m) 227 ULC, 1.38 DEAD + 1 SEISMIC (4) 292.628 1566.054 -10.113 -9.018 3.425 -675.38 109 ULC, 1.2 DEAD + 1 LIVE + 1 SEISMIC (1) -292.932 1494.751 -4.417 8.193 -3.407 678.042 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) -270.794 2250.67 14.401 52.024 -3.413 645.516 6 EQ +Z -E -22.71 -579.503 -228.339 -513.016 3.265 52.608 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) -3.548 1343.185 303.253 616.068 -3.234 -13.945 6 EQ +Z -E -6.609 13.726 -299.329 -595.559 3.265 16.5 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) -3.548 1343.185 303.253 616.068 -3.234 -13.945 6 EQ +Z -E -6.609 13.726 -299.329 -595.559 3.265 16.5 112 ULC, 1.2 DEAD + 1 LIVE + 1 SEISMIC (4) 203.839 1246.519 38.509 83.538 3.481 -532.128 224 ULC, 1.38 DEAD + 1 SEISMIC (1) -184.36 356.005 -12.977 -32.859 -3.462 514.802 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) -290.511 1494.325 -14.508 1.899 -3.413 686.221 4 EQ -X -E 287.57 -0.008 0 0 3.444 -681.714 76 4.4 Design Analysis for Trade-Off Two (One Way Slab – Special Moment Resisting Frame) The following are the analysis that is based on the modelling of the structure using the software – STAAD.Pro CONNECT. The values are taken depending on the design loads and inputs. 4.4.1 Design Methodology for Trade-Off One (One-Way Slab – Special Moment Resisting Frame) GEOMETRIC AND FRAME MODELLING ANALYSIS AND INITIAL DESIGN ESTIMATION OF COST DESIGNER’S FINAL RANKING FINAL DESIGN Figure 62. Design Process Flow Chart for Trade-Off One (One Way Slab – Special Moment Resisting Frame) 77 4.4.2 Geometric Modelling Figure 63. Geometric Model of Special Moment Resisting Frame - One Way Slab 78 4.4.3 Load Diagrams of Trade-Off One (One way Slab – Special Moment Resisting Frame) Figure 64. Load Diagrams for Dead Load Figure 65. Load Diagrams for Live Load 79 Figure 66. Load Diagram for Earthquake Loads at X Figure 67. Load Diagram for Earthquake Loads at -X 80 Figure 68. Load Diagram for Earthquake Loads at Z Figure 69. Load Diagram for Earthquake Loads at –Z 81 Figure 70. Shear Diagram at X Figure 71. Shear Diagram at Y 82 Figure 72. Shear Diagram at Z Figure 73. Moment Diagram at X 83 Figure 74. Moment Diagram at Y Figure 75. Moment Diagram at Z 84 Figure 76. Wind Load Diagram at X Figure 77. Wind Load Diagram at –X 85 Figure 78. Wind Load Diagram at Z Figure 79. Wind Load Diagram at -Z 86 4.4.4 Frame Staad Analysis Figure 80. Gravity Load (1.2DL + 1.6LL) – Longitudinal direction Figure 81. Gravity Load (1.2DL + 1.6LL) – Transverse direction 87 Figure 82. Moment due to Seismic Load - Longitudinal direction Figure 83. Moment due to Seismic Load - Transverse direction 88 Figure 84. Wind Load – Longitudinal Figure 85. Wind Load – Transverse 89 4.4.5 Structural Analysis Results The following results are presented in the table below. These are the results of the design loads and inputs using the software STAAD.Pro CONNECT Edition. 4.4.5.1 Beam End Forces Table 31. Beam End Forces Summary Max Fx Min Fx Max Fy Min Fy Max Fz Min Fz Max Mx Min Mx Max My Min My Max Mz Min Mz Beam 1140 12173 22166 52250 2144 2141 52256 52244 1144 1144 1128 1128 L/C 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 220 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (5) 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 112 ULC, 1.2 DEAD + 1 LIVE + 1 SEISMIC (4) 6 EQ +Z -E 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 4 EQ -X -E Beam End Forces Node Fx (kN) 131 1816.167 6 -357.342 214 126.438 228 255.203 21 861.683 76 1332.153 222 -3.665 220 -6.184 135 11.831 135 1135.974 119 1240.01 119 -0.002 Fy (kN) 84.251 51.779 156.722 -174.917 22.45 -1.573 -78.769 -56.375 4.987 12.638 98.13 -94.315 Fz (kN) Mx (kN-m) My (kN-m) Mz (kN-m) 0.238 -1.852 -43.49 305.323 -0.226 1.529 0.282 37.603 0.157 -1.062 -0.196 180.639 -0.372 0.906 -0.465 218.135 105.584 -3.066 -185.841 42.198 -107.868 3.215 174.864 -4.288 -7.992 19.453 9.989 -104.18 8.082 -19.673 -10.102 -74.803 -98.166 1.812 247.483 16.959 102.278 -1.762 -284.181 5.452 -10.486 -1.852 -22.073 331.704 0 1.902 0 -324.271 4.4.5.2 Node Displacements Table 32. Node Displacements Summary Max X Min X Max Y Min Y Max Z Min Z Max rX Min rX Max rY Min rY Max rZ Min rZ Max Rst Node 498 498 224 221 420 504 147 230 432 433 231 225 504 Node Displacement Horizontal Vertical Horizontal Resultant L/C X (mm) Y (mm) Z (mm) mm 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 42.393 -0.745 -6.74 42.932 4 EQ -X -E -41.221 -0.12 -2.732 41.312 6 EQ +Z -E -1.01 1.61 11.357 11.515 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 1.323 -8.432 -13.244 15.757 6 EQ +Z -E 2.585 0.153 25.433 25.564 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 3.576 -0.629 -34.734 34.924 6 EQ +Z -E 1.202 0.111 11.357 11.421 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 1.519 -0.614 -14.028 14.124 224 ULC, 1.38 DEAD + 1 SEISMIC (1) 37.363 -1.016 -7.147 38.054 112 ULC, 1.2 DEAD + 1 LIVE + 1 SEISMIC (4) -35.759 -1.164 -5.33 36.173 227 ULC, 1.38 DEAD + 1 SEISMIC (4) -16.16 -0.347 -0.793 16.183 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 16.708 -0.492 -1.845 16.817 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 42.188 -0.901 -12.036 43.881 rX (rad) 0 0 0.001 -0.002 0.001 -0.001 0.002 -0.003 0 0 0 -0.001 -0.001 Rotational rY (rad) 0 0 0 0 0 0 0 0 0 0 0 0 0 rZ (rad) -0.002 0.001 0 0 0 0 0 0 -0.001 0.001 0.003 -0.004 -0.001 90 4.4.5.3 Support Reactions Table 33. Support Reactions Summary Max Fx Min Fx Max Fy Min Fy Max Fz Min Fz Max Mx Min Mx Max My Min My Max Mz Min Mz Node 125 119 131 127 135 132 135 135 92 92 119 119 Support Reactions Horizontal Vertical Horizontal Moment L/C Fx (kN) Fy (kN) Fz (kN) Mx (kN-m) My (kN-m) Mz (kN-m) 227 ULC, 1.38 DEAD + 1 SEISMIC (4) 98.554 1245.34 -1.267 15.131 1.851 -319.599 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) -98.13 1240.01 -10.486 22.073 -1.852 331.704 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) -84.251 1816.167 0.238 43.49 -1.852 305.323 6 EQ +Z -E -8.335 -171.812 -75.194 -218.733 1.812 26.339 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) -12.638 1135.974 102.278 284.181 -1.762 5.452 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 6.636 1718.367 -103.636 -215.452 1.863 -15.059 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) -12.638 1135.974 102.278 284.181 -1.762 5.452 6 EQ +Z -E -4.987 11.831 -98.166 -247.483 1.812 16.959 112 ULC, 1.2 DEAD + 1 LIVE + 1 SEISMIC (4) 74.756 784.652 21.729 64.302 1.971 -262.907 224 ULC, 1.38 DEAD + 1 SEISMIC (1) -56.206 546.336 3.79 9.129 -1.954 249.68 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) -98.13 1240.01 -10.486 22.073 -1.852 331.704 4 EQ -X -E 94.315 -0.002 0 0 1.902 -324.271 91 4.5 Design Analysis for Trade-Off Three (Two Way Slab – Ordinary Moment Resisting Frame) The following are the analysis that is based on the modelling of the structure using the software – STAAD.Pro CONNECT. The values are taken depending on the design loads and inputs. 4.5.1 Design Methodology for Trade-Off Two (Two Way Slab – Ordinary Moment Resisting Frame) GEOMETRIC AND FRAME MODELLING ANALYSIS AND INITIAL DESIGN ESTIMATION OF COST DESIGNER’S FINAL RANKING FINAL DESIGN Figure 86. Design Process Flow Chart for Trade-Off Two (Two Way Slab – Ordinary Moment Resisting Frame) 92 4.5.2 Geometric Modelling Figure 87. Geometric Model of Ordinary Moment Resisting Frame - Two Way Slab 93 4.5.3 Load Diagrams of Trade-Off Two (Two Way Slab – Ordinary Moment Resisting Frame) Figure 88. Load Diagrams for Dead Load Figure 89. Load Diagrams for Live Load 94 Figure 90. Load Diagram for Earthquake Loads at X Figure 91. Load Diagram for Earthquake Loads at –X 95 Figure 92. Load Diagram for Earthquake Loads at Z Figure 93. Load Diagram for Earthquake Loads at –Z 96 Figure 94. Shear Diagram at X Figure 95. Shear Diagram at Y 97 Figure 96. Shear Diagram at Z Figure 97. Moment Diagram at X 98 Figure 98. Moment Diagram at Y Figure 99. Moment Diagram at Z 99 Figure 100. Wind Load Diagram at X Figure 101. Wind Load Diagram at –X 100 Figure 102. Wind Load Diagram at Z Figure 103. Wind Load Diagram at –Z 101 4.5.4 Frame Staad Analysis Figure 104. Gravity Load (1.2DL + 1.6LL) – Longitudinal direction Figure 105. Gravity Load (1.2DL + 1.6LL) – Transverse direction 102 Figure 106. Moment due to Seismic Load - Longitudinal direction Figure 107. Moment due to Seismic Load - Transverse direction 103 Figure 108. Wind Load – Longitudinal Figure 109. Wind Load – Transverse 104 4.5.5 Structural Analysis Results The following results are presented in the table below. These are the results of the design loads and inputs using the software STAAD.Pro CONNECT Edition. 4.5.5.1 Beam End Forces Table 34. Beam End Forces Summary Max Fx Min Fx Max Fy Min Fy Max Fz Min Fz Max Mx Min Mx Max My Min My Max Mz Min Mz Beam 1134 1136 1128 1128 1146 1147 52106 52148 1147 1146 1128 1128 L/C 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 6 EQ +Z -E 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 4 EQ -X -E 7 EQ -Z +E 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 220 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (5) 217 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (2) 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 7 EQ -Z +E 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 4 EQ -X -E Beam End Forces Node Fx (kN) 40 2078.37 6 -554.401 46 1431.457 46 -0.009 28 -0.009 35 1471.231 251 33.259 281 33.385 35 1471.231 28 -0.009 46 1431.457 46 -0.009 Fy (kN) 16.335 23.164 284.324 -282.5 0 10.847 54.819 54.827 10.847 0 284.324 -282.5 Fz (kN) Mx (kN-m) My (kN-m) Mz (kN-m) 257.878 -3.149 -595.045 38.059 -224.328 3.139 572.465 52.02 -14.166 -3.02 16.913 644.7 0 3.01 0 -640.335 283.407 -3.139 -642.427 0 -284.145 3.129 645.489 4.119 2.731 6.026 -5.981 40.634 -2.743 -6.045 6.011 40.638 -284.145 3.129 645.489 4.119 283.407 -3.139 -642.427 0 -14.166 -3.02 16.913 644.7 0 3.01 0 -640.335 4.5.5.2 Node Displacements Table 35. Node Displacement Summary Max X Min X Max Y Min Y Max Z Min Z Max rX Min rX Max rY Min rY Max rZ Min rZ Max Rst Node 288 288 251 285 252 252 105 147 246 288 147 141 252 Node Displacement Horizontal Vertical Horizontal Resultant L/C X (mm) Y (mm) Z (mm) mm 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 44.988 -0.565 3.277 45.111 4 EQ -X -E -44.346 -0.447 -2.869 44.441 6 EQ +Z -E 3.025 0.479 43.996 44.103 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 2.552 -2.03 -42.473 42.598 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 3.42 -0.561 45.131 45.264 7 EQ -Z +E -3.027 -0.447 -44.504 44.609 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 1.785 -0.322 20.774 20.853 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 1.795 -0.284 -20.437 20.518 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) -2.402 -1.476 -37.865 37.969 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) -2.391 -1.461 38.914 39.015 219 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (4) -20.354 -0.284 1.713 20.428 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 20.712 -0.327 1.723 20.786 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 3.42 -0.561 45.131 45.264 rX (rad) 0 0 0.001 -0.001 0.001 -0.001 0.003 -0.003 -0.001 0.001 0 0 0.001 Rotational rY (rad) 0 0 0 0 0 0 0 0 0 0 0 0 0 rZ (rad) -0.001 0.001 0 0 0 0 0 0 0 0 0.003 -0.003 0 105 4.5.5.3 Support Reactions Table 36. Support Reactions Summary Max Fx Min Fx Max Fy Min Fy Max Fz Min Fz Max Mx Min Mx Max My Min My Max Mz Min Mz Node 46 46 40 6 28 35 28 35 1 1 46 46 Support Reactions Horizontal Vertical Horizontal Moment L/C Fx (kN) Fy (kN) Fz (kN) Mx (kN-m) My (kN-m) Mz (kN-m) 4 EQ -X -E 282.5 -0.009 0 0 3.01 -640.335 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) -284.324 1431.457 -14.166 -16.913 -3.02 644.7 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) -16.335 2078.37 257.878 595.045 -3.149 38.059 6 EQ +Z -E -23.164 -554.401 -224.328 -572.465 3.139 52.02 7 EQ -Z +E 0 -0.009 283.407 642.427 -3.139 0 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) -10.847 1471.231 -284.145 -645.489 3.129 4.119 7 EQ -Z +E 0 -0.009 283.407 642.427 -3.139 0 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) -10.847 1471.231 -284.145 -645.489 3.129 4.119 229 ULC, 1.38 DEAD + 1 SEISMIC (6) -9.144 305.738 -181.944 -483.236 3.14 38.986 115 ULC, 1.2 DEAD + 1 LIVE + 1 SEISMIC (7) 29.526 1299.511 202.191 500.614 -3.15 -56.694 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) -284.324 1431.457 -14.166 -16.913 -3.02 644.7 4 EQ -X -E 282.5 -0.009 0 0 3.01 -640.335 106 4.6 Design Analysis for Trade-Off Four (Two Way Slab – Special Moment Resisting Frame) The following are the analysis that is based on the modelling of the structure using the software – STAAD.Pro CONNECT. The values are taken depending on the design loads and inputs. 4.6.1 Design Methodology for Trade-Off Two (Two Way Slab – Ordinary Moment Resisting Frame) GEOMETRIC AND FRAME MODELLING ANALYSIS AND INITIAL DESIGN ESTIMATION OF COST DESIGNER’S FINAL RANKING FINAL DESIGN Figure 110. Design Process Flow Chart for Trade-Off Two (Two Way Slab – Special Moment Resisting Frame) 107 4.6.2 Geometric Modelling Figure 111. Geometric Model of Special Moment Resisting Frame - Two Way Slab 108 4.6.3 Load Diagrams of Trade-Off Two (Two Way Slab – Special Moment Resisting Frame) Figure 112. Load Diagrams for Dead Load Figure 113. Load Diagrams for Live Load 109 Figure 114. Load Diagram for Earthquake Loads at X Figure 115. Load Diagram for Earthquake Loads at –X 110 Figure 116. Load Diagram for Earthquake Loads at Z Figure 117. Load Diagram for Earthquake Loads at -Z 111 Figure 118. Shear Diagram at X Figure 119. Shear Diagram at Y 112 Figure 120. Shear Diagram at Z Figure 121. Moment Diagram at X 113 Figure 122. Moment Diagram at Y Figure 123. Moment Diagram at Z 114 Figure 124. Wind Load Diagram at X Figure 125. Wind Load Diagram at –X 115 Figure 126. Wind Load Diagram at Z Figure 127. Wind Load Diagram at –Z 116 4.6.4 Frame Staad Analysis Figure 128. Gravity Load (1.2DL + 1.6LL) – Longitudinal direction Figure 129. Gravity Load (1.2DL + 1.6LL) – Transverse direction 117 Figure 130. Moment due to Seismic Load - Longitudinal direction Figure 131. Moment due to Seismic Load - Transverse direction 118 Figure 132. Wind Load – Longitudinal Figure 133. Wind Load - Transverse 119 4.6.5 Structural Analysis Results The following results are presented in the table below. These are the results of the design loads and inputs using the software STAAD.Pro CONNECT Edition. 4.6.5.1 Beam End Forces Table 37. Beam End Forces Summary Max Fx Min Fx Max Fy Min Fy Max Fz Min Fz Max Mx Min Mx Max My Min My Max Mz Min Mz Beam 1134 1136 22134 22133 2139 2141 2101 2101 1148 1146 1128 1128 L/C 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 6 EQ +Z -E 219 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (4) 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 229 ULC, 1.38 DEAD + 1 SEISMIC (6) 115 ULC, 1.2 DEAD + 1 LIVE + 1 SEISMIC (7) 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 7 EQ -Z +E 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 4 EQ -X -E Beam End Forces Node Fx (kN) 40 1693.314 6 -148.941 137 -0.878 137 -9.304 76 1309.933 90 1250.581 50 413.803 50 610.308 42 1136.043 28 -0.002 46 1140.442 46 -0.002 Fy (kN) 6.704 8.14 136.363 -121.791 -0.312 -0.227 -11.881 -22.534 11.866 0 92.935 -90.151 Fz (kN) 77.558 -74.518 0.011 -0.029 92.974 -93.711 -33.027 66.978 -91.925 89.892 -13.509 0 Mx (kN-m) My (kN-m) Mz (kN-m) -2.029 -280.603 28.186 2.004 290.122 28.236 -0.214 -0.023 158.899 0.583 -0.062 157.435 -3.811 -186.89 2.727 3.727 195.304 -0.1 3.77 90.584 -15.355 -3.812 -143.256 -37.316 1.978 320.57 6.942 -2.004 -311.617 0 -1.92 20.993 340.461 1.894 0 -329.472 4.6.5.2 Node Displacements Table 38. Node Displacements Summary Max X Min X Max Y Min Y Max Z Min Z Max rX Min rX Max rY Min rY Max rZ Min rZ Max Rst Node 288 288 251 285 252 252 105 105 254 282 141 141 252 Node Displacement Horizontal Vertical Horizontal Resultant L/C X (mm) Y (mm) Z (mm) mm 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 48.723 -0.728 5.29 49.015 4 EQ -X -E -46.197 -0.143 -3 46.295 6 EQ +Z -E 3.228 0.154 47.629 47.738 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 4.584 -1.759 -44.102 44.375 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 5.419 -0.721 50.79 51.083 7 EQ -Z +E -3.231 -0.144 -48.259 48.367 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 2.051 -0.46 19.259 19.374 7 EQ -Z +E -1.406 -0.095 -18.585 18.639 115 ULC, 1.2 DEAD + 1 LIVE + 1 SEISMIC (7) -0.175 -1.093 -41.215 41.23 229 ULC, 1.38 DEAD + 1 SEISMIC (6) -0.597 -1.018 44.739 44.755 4 EQ -X -E -17.346 -0.093 -1.324 17.397 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) 18.024 -0.467 2.031 18.144 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 5.419 -0.721 50.79 51.083 rX (rad) 0 0 0.002 -0.001 0.002 -0.002 0.004 -0.004 -0.001 0.002 0 0 0.002 Rotational rY (rad) 0 0 0 0 0 0 0 0 0 0 0 0 0 rZ (rad) -0.002 0.002 0 0 0 0 0 0 0 0 0.004 -0.004 0 120 4.6.5.3 Support Reactions Table 39. Support Reactions Summary Max Fx Min Fx Max Fy Min Fy Max Fz Min Fz Max Mx Min Mx Max My Min My Max Mz Min Mz Node 39 46 40 6 27 41 28 42 1 1 46 46 Support Reactions Horizontal Vertical Horizontal Moment L/C Fx (kN) Fy (kN) Fz (kN) Mx (kN-m) My (kN-m) Mz (kN-m) 227 ULC, 1.38 DEAD + 1 SEISMIC (4) 92.519 999.463 -0.072 -4.092 1.895 -321.155 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) -92.935 1140.442 -13.509 -20.993 -1.92 340.461 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) -6.704 1693.314 77.558 280.603 -2.029 28.186 6 EQ +Z -E -8.14 -148.941 -74.518 -290.122 2.004 28.236 222 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (7) 0.224 1672.22 91.753 300.954 -2.029 7.657 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) 4.074 1587.325 -93.516 -316.629 1.978 -9.385 7 EQ -Z +E 0 -0.002 89.892 311.617 -2.004 0 221 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (6) -11.866 1136.043 -91.925 -320.57 1.978 6.942 229 ULC, 1.38 DEAD + 1 SEISMIC (6) 2.457 527.228 -54.538 -245.286 2.004 21.863 115 ULC, 1.2 DEAD + 1 LIVE + 1 SEISMIC (7) 16.752 778.831 73.396 254.816 -2.029 -30.983 216 ULC, 1.68 DEAD + 1 LIVE + 1 SEISMIC (1) -92.935 1140.442 -13.509 -20.993 -1.92 340.461 4 EQ -X -E 90.151 -0.002 0 0 1.894 -329.472 121 4.7 Normalization of Final Data, Raw Ranking Validation, Comparison of Results, and Final Ranking Assessments In this section, the raw designer’s ranking was validated through the gathered results of the design. The initial and final estimated values was then be compared. With the help of the final designer’s ranking, the final ranking assessments was concluded. 4.7.1 Final Estimates of Tradeoffs The table below shows the result of the estimation of construction cost, man days, and cost of maintenance for each tradeoff. Table 40. Final Estimate of Tradeoffs CONSTRAINT One-Way Slab OMRF TRADE-OFFS One-Way Slab Two-Way Slab SMRF OMRF Two-Way Slab SMRF Economic (Construction Cost) Php 18,179,360.48 Php 16,661,469.14 Php 15,898,110.45 Php 14,349,860.25 Constructability Safety/Serviceability 573 Days 2.81% of allowable 450 Days 2.02% of allowable 553 Days 3.89% of allowable 427 Days 5.65 % of allowable 4.7.2 Validation of Raw Designer’s Ranking Table 41. Comparison of Initial and Final Estimate of Tradeoffs CONSTRAINT One-Way Slab OMRF Economic Php 18,000,000 600 Days Constructabili ty Safety/Servic eability 4% of allowable Initial Estimate One-Way Two-Way Slab SMRF Slab OMRF Php Php 16,000,000 17,500,00 550 Days 575 Days 5% of allowable 3.5% of allowable Final Estimate One-Way Two-Way Slab SMRF Slab OMRF Php Php 16,661,469 15,898,110 Two-Way Slab SMRF Php 15,500,00 525 Days One-Way Slab OMRF Php 18,179,360 Two-Way Slab SMRF Php 14,349,860 573 Days 450 Days 553 Days 427 Days 4.5% of allowable 2.81% of allowable 2.02% of allowable 3.89% of allowable 5.65 % of allowable 122 Looking at the table, there are small discrepancies between the assumed values and the computed values, except for the serviceability of the four. However, the results of the final estimate of values has almost the same outcome with the initial estimate. It turned out that the two way slab is better than the one way slab in terms of both economic and constructability constraint, while one way slab is better than two way slab in terms of safety/serviceability constraint. These results are the same as what was said in the raw ranking, which makes raw design to be quite certain in this project. 4.7.3 Final Designer’s Ranking Computation of ranking for Economic Constraint for Trade-Offs one (1) and four (4) % Difference = % Difference = Higher Value-Lower Value Higher Value x100 18,179,360.48-14,349,860.25 18,179,360.48 x100 % Difference = 21.06509871 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 2.106509871 Subordinate rank = 2.893490129 Figure 134. Cost Difference of Trade-Offs 1 and 4 Computation of ranking for Economic Constraint for Trade-Offs two (2) and four (4) 123 % Difference = % Difference = Higher Value-Lower Value Higher Value x100 16,661,469.14-14,349,860.25 16,661,469.14 x100 % Difference = 13.87397996 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 1.387397996 Subordinate rank = 3.612602004 Figure 135. Cost Difference of Trade-Offs 2 and 4 Computation of ranking for Economic Constraint for Trade-Offs three (3) and four (4) % Difference = % Difference = Higher Value-Lower Value Higher Value x100 15,898,110.45-14,349,860.25 15,898,110.45 x100 % Difference = 9.738579971 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 0.973857997 124 Subordinate rank = 4.026142003 Figure 136. Cost Difference of Trade-Offs 3 and 4 Computation of ranking for Constructability Constraint for Trade-Offs one (1) and four (4) % Difference = Higher Value-Lower Value Higher Value % Difference = 573-427 573 x100 x100 % Difference = 25.47993019 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 2.547993019 Subordinate rank = 2.452006981 Figure 137. Constructability Difference of Trade-Offs 1 and 4 Computation of ranking for Constructability Constraint for Trade-Offs two (2) and four (4) % Difference = Higher Value-Lower Value Higher Value x100 125 % Difference = 450-427 450 x100 % Difference = 5.111111111 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 0.511111111 Subordinate rank = 4.488888889 Figure 138. Constructability Difference of Trade-Offs 2 and 4 Computation of ranking for Constructability Constraint for Trade-Offs three (3) and four (4) % Difference = Higher Value-Lower Value Higher Value % Difference = 553-427 553 x100 x100 % Difference = 22.78481013 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 2.278481013 Subordinate rank = 2.721518987 126 Figure 139. Constructability Difference of Trade-Offs 3 and 4 Computation of ranking for Safety/Serviceability Constraint for Trade-Offs one (1) and two (2) % Difference = Higher Value-Lower Value Higher Value % Difference = 2.81-2.02 2.81 x100 x100 % Difference = 28.113879 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 2.8113879 Subordinate rank = 2.1886121 Figure 140. Safety/Serviceability Difference of Trade-Offs 1 and 2 Computation of ranking for Safety/Serviceability Constraint for Trade-Offs three (3) and two (2) % Difference = Higher Value-Lower Value Higher Value % Difference = 3.89-2.02 3.89 x100 x100 % Difference = 48.07197943 127 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 4.807197943 Subordinate rank = 0.192802057 Figure 141. Safety/Serviceability Difference of Trade-Offs 3 and 2 Computation of ranking for Safety/Serviceability Constraint for Trade-Offs three (3) and two (2) % Difference = Higher Value-Lower Value Higher Value % Difference = 3.89-2.02 3.89 x100 x100 % Difference = 64.24778761 Subordinate rank = Governing rank - % difference 10 Subordinate rank = 5 – 6.424778761 Subordinate rank = -1.424778761 Figure 142. Safety/Serviceability Difference of Trade-Offs 4 and 2 128 Table 42. Final Designer’s Ranking CONSTRAINT (Criteria) Importance (on a scale of 0 to 5) Economic 5 Constructability 4 Safety/Serviceability 3 Overall Rank 4.7.4 Ability to Satisfy the Criterion (on a scale of 0 to 5) One-Way One-Way Two-Way Two-Way Slab OMRF Slab SMRF Slab OMRF Slab SMRF 2.89 3.61 4.03 5 2.45 4.49 2.72 5 2.19 5 0.192 -1.424 30.82 51.01 31.606 40.728 Normalization of Final Data The normalization of data are based on the initial estimate of the two mandatory tradeoffs namely, One-Way Slab and Two-Way Slab, and based on the three constraints, namely Economic, Constructability and Serviceability. 4.7.4.1 Raw Data Table 43. Raw Final Data. Design 1. OMRF (One-Way) 2. OMRF (Two-Way) 3. SRMF (One-Way) 4. SMRF (Two-Way) PC1 (Cost in pesos) 18,179,360.48 16,661,469.14 15,898,110.45 14,349,860.25 PC2 (Duration in days) 573 450 553 427 PC3 (Safety/Serviceability in percent) 2.81 2.02 3.89 5.65 Table 43 shows the raw data gathered from the estimate conducted by the designer that is available to see in the appendix. 129 4.7.4.2 Normalized Data Table 44. Normalized Final Data Design 1. OMRF (One-Way) 2. OMRF (Two-Way) 3. SRMF (One-Way) 4. SMRF (Two-Way) PC1 (Cost in pesos) 1 4.567311983 6.361339349 10 PC2 (Duration in days) 1 8.582191781 2.232876712 10 PC3 (Safety/Serviceability in percent) 8.041322314 10 5.363636364 1 Normalization of rating means adjusting values measured on different scales to a noitionally common scale, prior to averaging. Table 44 shows the normalized data from the raw data. 4.7.4.3 Weighted Sum of Various Percentage Weight Table 45. First weighted sum of various percentage for final data PC 1 2 3 Weighted Sum Weight (%) 0.5 0.3 0.2 1 D1 1 1 8.041322314 2.408264463 D2 4.567311983 8.582191781 10 6.858313526 D3 6.361339 2.232877 5.363636 4.92326 D4 10 10 1 8.2 Table 45 shows the first weighted sum of various percentage where constraints one (1), two (2) and three (3) have given a percentage of 0.5, 0.3 and 0.2 respectively. Table 46. Second weighted sum of various percentage for final data PC 1 2 3 Weighted Sum Weight (%) 0.44 0.3 0.26 1 D1 1 1 8.041322314 2.830743802 D2 4.567311983 8.582191781 10 7.184274807 D3 6.361339 2.232877 5.363636 4.863398 D4 10 10 1 7.66 Table 46 shows the first weighted sum of various percentage where constraints one (1), two (2) and three (3) have given a percentage of 0.44, 0.3 and 0.26 respectively. 130 Table 47. Third weighted sum of various percentage for final data PC 1 2 3 Weighted Sum Weight (%) 0.3 0.4 0.3 1 D1 1 1 8.041322314 3.112396694 D2 4.567311983 8.582191781 10 7.803070307 D3 6.361339 2.232877 5.363636 4.410643 D4 10 10 1 7.3 Table 47 shows the first weighted sum of various percentage where constraints one (1), two (2) and three (3) have given a percentage of 0.3, 0.4 and 0.3 respectively. 4.7.5 Designer’s Final Ranking Assessment In terms of economic constraints, the two-way slab got the rank of 5 considering both the concrete works and rebar works. As for the constructability constraints, the number of man hours needed to construct the structure in one-way slab is larger rather than the two-way slab, thus making the two-way slab gets the rank of 5. For safety/serviceability constraint, the percentage of deflection from allowable in the one way slab is smaller than the two way slab making this trade get a rank of 5 in this constraint. After gathering all data and making the designer’s overall final ranking assessment. Overall, the four tradeoffs had a difference of smaller in tradeoffs one and three, but large in the other tradeoffs. Overall, the one-way slab SMRF outranked the other three tradeoffs. With these information, the designer concluded that the governing tradeoff is One-Way slab SMRF in contrast with the raw designer’s ranking. 131 CHAPTER 5: FINAL DESIGN As what was proven from the previous chapters, the governing tradeoff was the One-Way Slab. After going through all the design processes, the designer can now conclude the final design of the structure which includes the design schedule of the structural members. 5.1 Design Schedules The design schedule of the structural members included the investigated dimensions and designed number of bars with spacing. The following tables below show the design schedule of the project. 5.1.1 Design Schedule of Slabs Table 48.Slab Schedule SLAB (2F - ROOF) t (mm) S-1 S-2 150 150 S-1 S-2 150 150 5.1.2 Spacing (mm) Φ bar (mm) Midspan Continuous Edge Longitudinal Direction 12 250 250 12 250 250 Transverse Direction 12 250 250 12 250 250 Φ tie (mm) 10 10 10 10 Design Schedule of Beams Table 49. Beam Schedule Beam 2F - ROOF B1 B2 B3 B4 B5 B6 Dimension b (mm) 310 310 310 310 310 310 t (mm) 420 420 420 420 420 420 Top (left) 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ Numbers of Bars Bottom (mid) 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ Top (Right) 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 132 B7 B8 B9 B10 B11 B12 B13 B14 B15 B16 B17 B18 B19 B20 B21 B22 B23 B24 B25 B26 B27 B28 B29 B30 B31 B32 B33 B34 B35 B36 B37 B38 B39 B40 B41 B42 B43 B44 B45 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 133 B46 B47 B48 B49 B50 B51 B52 B53 B54 B55 B56 B57 B58 B59 B60 B61 B62 B63 B64 B65 B66 B67 B68 B69 B70 B71 B72 B73 B74 B75 B76 B77 B78 B79 B80 B81 B82 B83 B84 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 134 B85 B86 B87 B88 B89 B90 B91 B92 B93 B94 B95 B96 B97 B98 B99 B100 B101 B102 B103 B104 B105 B106 B107 B108 B109 B110 B111 B112 B113 B114 B115 B116 B117 B118 B119 B120 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 310 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 420 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 5 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 4 - 32Φ 135 5.1.3 Design Schedule of Columns Table 50. Column Schedule Column C1 C2 C3 C4 C5 C6 C7 C8 C9 C10 C11 C12 C13 C14 C15 C16 C17 C18 C19 C20 C21 C22 C23 C24 C25 C26 C27 C28 C29 C30 C31 C32 C33 Dimensions b (mm) t (mm) 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 No. and size of Bars nd 2 Floor 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 20 – 16mmΦ 20 – 16mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 20 – 16mmΦ 8 – 25mmΦ 20 – 16mmΦ 20 – 16mmΦ 20 – 16mmΦ 8 – 25mmΦ 8 – 25mmΦ Tie Wires Φtie (mm) Spacing (mm) 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 400 400 400 400 400 400 400 400 400 400 400 400 400 400 256 256 400 400 400 400 400 400 400 400 400 400 256 400 256 256 256 400 400 136 C34 C35 C36 C37 C38 C39 C40 C41 C42 C43 C44 C45 C46 C47 C48 C49 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 C1 C2 C3 C4 C5 C6 C7 C8 C9 C10 C11 C12 C13 C14 C15 C16 C17 C18 C19 C20 C21 C22 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 8 – 25mmΦ 8 – 25mmΦ 20 – 16mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 20 – 16mmΦ 20 – 16mmΦ 20 – 16mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ rd 3 Floor 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 400 400 256 400 400 400 400 400 400 256 256 256 400 400 400 400 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 137 C23 C24 C25 C26 C27 C28 C29 C30 C31 C32 C33 C34 C35 C36 C37 C38 C39 C40 C41 C42 C43 C44 C45 C46 C47 C48 C49 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 C1 C2 C3 C4 C5 C6 C7 C8 C9 C10 C11 650 650 650 650 650 650 650 650 650 650 650 600 600 600 600 600 600 600 600 600 600 600 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 20 – 16mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 20 – 16mmΦ 20 – 16mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ th 4 Floor 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 400 400 400 400 400 400 400 400 400 400 400 400 256 400 400 400 256 256 400 400 400 400 400 400 400 400 400 10 10 10 10 10 10 10 10 10 10 10 400 400 400 400 400 400 400 400 400 400 400 138 C12 C13 C14 C15 C16 C17 C18 C19 C20 C21 C22 C23 C24 C25 C26 C27 C28 C29 C30 C31 C32 C33 C34 C35 C36 C37 C38 C39 C40 C41 C42 C43 C44 C45 C46 C47 C48 C49 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ th 5 Floor 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 139 C1 C2 C3 C4 C5 C6 C7 C8 C9 C10 C11 C12 C13 C14 C15 C16 C17 C18 C19 C20 C21 C22 C23 C24 C25 C26 C27 C28 C29 C30 C31 C32 C33 C34 C35 C36 C37 C38 C39 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 650 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 600 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 10 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 400 140 C40 C41 C42 C43 C44 C45 C46 C47 C48 C49 5.1.4 650 650 650 650 650 650 650 650 650 650 600 600 600 600 600 600 600 600 600 600 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 8 – 25mmΦ 10 10 10 10 10 10 10 10 10 10 400 400 400 400 400 400 400 400 400 400 Beam Details Figure 143. Beam Details (a) 141 Figure 144. Beam Details (b) 142 5.1.5 Column Details Figure 145. Column Details (a) Figure 146. Column Details (b) 143 APPENDICES APPENDIX A: CODES AND STANDARDS National Building Code of the Philippines (NBC) The following are the sections and codes that are followed in conceptualizing and designing the structural plan of the apartment building: • Section 401. Types of Construction Type I. The structural elements may be any of the materials permitted by this Code. • Section 701. Occupancy Classified. Group E. Business and Mercantile • Section 805. Ceiling Heights. Habitable rooms provided with artificial ventilation have\ ceiling heights not less than 2.40 meters measured from the floor to the ceiling; Provided that for buildings of more than one-storey, the minimum ceiling height of the first storey shall be 2.70 meters and that for the second storey 2.40 meters and succeeding storeys shall have an unobstructed typical head-room clearance of not less than 2.10 meters above the finished floor. Above stated rooms with a natural ventilation shall have ceiling height not less than 2.70 meters. • Section 806. Size and Dimensions of Rooms. Minimum sizes of rooms and their least horizontal dimensions shall be as follows: 1. Rooms for Human Habitations. 6.00 square meters with at least dimensions of 2.00 2. Kitchens. 3.00 square meters with at least dimension of 1.50 meters; 3. Bath and toilet. 1.20 square meters with at least dimension of 0.90 meters. • Section 808. Window Openings. 144 Every room intended for any use, not provided with artificial ventilation system as herein specified in this Code, shall be provided with a window or windows with a total free area of openings equal to at least ten percent of the floor area of room, and such window shall open directly to a court, yard, public street or alley, or open water courses. • Section 1207. Stairs, Exits and Occupant Loads. General. The construction of stairs and exits shall conform to the occupant load requirements of buildings, reviewing stands, bleachers and grandstands: a. Determinations of Occupant Loads. The Occupant load permitted in any building or portion thereof shall be determined by dividing the floor area assigned to that use by the unit area allowed per occupant as determined by the Secretary. b. Exit Requirements. Exit requirements of a building or portion thereof used for different purposes shall be determined by the occupant load which gives the largest number of persons. No obstruction shall be placed in the required width of an exit except projections permitted by this Code. National Structural Code of the Philippines (NSCP) 2015 Notation Ag = gross area of section, mm2. As = area of nonprestressed tension reinforcement, mm2. As ,min = minimum amount of flexural reinforcement, mm2 Ast = total area of nonprestressed longitudinal reinforcement (bars and steel shapes), mm 2. Av = area of shear reinforcement within a distance s, mm2. 145 Avf = area of shear-friction reinforcement, mm2. A 's = area of compression reinforcement, mm2. b = width of compression face of member, mm. bw = web width, mm. c = distance from extreme compression fiber to neutral axis, mm. cc = clear cover from the nearest surface in tension to the surface of the flexural tension reinforcement, mm. Cm = a factor relating actual moment diagram to an equivalent uniform moment diagram. D = dead loads, or related internal moments and forces. d = distance from extreme compression fiber to centroid of tension reinforcement, mm. d ' = distance from extreme compression fiber to centroid of compression reinforcement, mm. db = nominal diameter of bar, wire, or prestressing strand, mm. dc = thickness of concrete cover measure from extreme tension fiber to center of bar or wire located closest thereto, mm. ds = distance from extreme tension fiber to centroid of tension reinforcement, mm. dt = distance from extreme compression fiber to extreme tension steel, mm. E = load effects of earthquake, or related internal moments and forces. Ec = modulus of elasticity of concrete, MPa. Es = modulus of elasticity of reinforcement, MPa. 146 EI = flexural stiffness of compression member, N-mm2. F = loads due to weight and pressures of fluids with well-defined densities and controllable maximum heights, or related internal moments and forces. f 'c = specified compressive strength of concrete, MPa. f y = specified yield strength of nonprestressed reinforcement, MPa. f yt = specified yield strength fy H = loads due to weight and pressure of soil, water in soil, or other materials, or related internal moments and forces. h = overall thickness of member, mm. I = moment of inertia of section beam about the centroidal axis, mm4. Icr = moment of inertia of cracked section transformed to concrete, mm4. Ie = effective moment of inertia for computation of deflection, mm4. Ig = moment of inertia of gross concrete section about centroidal axis, neglecting reinforcement, mm4. L = live loads, or related internal moments and forces. Ld = development length, mm. ln = length of clear span measured face-to-face of supports, mm. Ma = maximum moment in member at stage deflection is computed. Mcr = cracking moment. Pb = nominal axial load strength at balanced strain conditions 147 Pn = nominal axial load strength at given eccentricity. Vc = nominal shear strength provided by concrete W = wind load, or related integral moments and forces. wc = unit weight of concrete, kN/m3. wu = factored load per unit length of beam or per unit area of slab. αf = ratio of flexural stiffness of beam section to flexural stiffness of a width of slab bounded laterally by center line of adjacent panle, if any on each side of beam. αfm = average value of αf for all beams on edges of a panel. β1 = factor εt = net tensile strain in extreme tension steel at nominal strength. λ = modification factor reflection the reduced mechanical properties of lightweight concrete. λΔ = multiplier for additional long-time deflection ρ = ration of nonprestressed tension reinforcement = As /bd ρ ' = ratio of nonprestressed compression reinforcement = A 's /bd ρb = reinforcement ratio producing balanced strain conditions Φ = strength-reduction factor. The following are the sections and codes that are followed in conceptualizing and designing the structural plan of the apartment building: • Section 203 - Combination of Load 148 a. Minimum densities for design loads from materials b. Minimum design loads c. Minimum uniform and concentrated live loads • Section 206 - Other Minimum Loads a. 206.3 Impact loads b. 206.3.1 Elevators c. 206.3.2 Machinery • Section 207 - Wind Load a. 207B.3.2 Velocity Pressure b. 207C.3.1 Velocity Pressure Exposure Coefficient c. 207A.8 Topographic Factor d. 207A.6 Wind Directionality Factor e. 207 A.7 Exposure • Section 208 - Earthquake Loads a. 208.5.1.1 Design Base Shear b. 208.5.2.2 Structure Period 149 APPENDIX B: RESULTS OF STRUCTURAL ANALYSIS B1 B2 B3 B4 B5 B6 B7 B8 B9 B10 B11 B12 B13 B14 B15 B16 B17 B18 B19 B20 B21 B22 B23 B24 B25 B26 B27 B28 B29 B30 B31 B32 B33 B34 B35 B36 B37 B38 B39 B40 B41 ONE WAY SLAB (SMRF) – 2ND FLOOR ONLY M(+) kN-m M(-) kN-m 62.74 122.46 C1 61.21 121.47 C2 61.10 121.46 C3 61.10 121.45 C4 61.12 121.60 C5 62.36 121.92 C6 63.78 116.18 C7 62.12 115.78 C8 61.99 115.84 C9 61.98 115.80 C10 62.04 116.21 C11 63.55 116.12 C12 62.60 115.03 C13 60.97 115.77 C14 60.84 115.82 C15 60.83 115.80 C16 60.86 116.21 C17 62.34 116.06 C18 61.47 113.91 C19 59.86 114.66 C20 59.74 114.72 C21 59.70 114.82 C22 54.92 131.94 C23 56.36 133.21 C24 63.30 115.82 C25 61.65 116.47 C26 61.53 116.55 C27 61.43 116.98 C28 61.49 112.34 C29 58.03 132.21 C30 65.13 117.75 C31 63.38 117.32 C32 63.34 122.20 C33 58.45 141.62 C34 58.39 140.21 C35 59.91 129.73 C36 64.72 124.81 C37 63.12 123.50 C38 63.05 128.59 C39 63.03 128.61 C40 63.09 128.87 C41 P (Axial) kN 766.43 1009.15 1008.92 1008.56 1008.64 1009.45 749.12 996.12 1184.31 1181.53 1181.20 1181.24 1185.14 1010.49 1094.77 1116.40 1135.03 1134.58 1135.37 1203.76 1024.65 979.67 1136.52 1134.02 1136.85 1142.69 1094.00 1026.52 1093.89 1116.72 1116.71 1334.88 1372.86 1469.24 1024.73 1115.62 1183.25 1185.21 1484.12 1523.17 1520.85 150 B42 B43 B44 B45 B46 B47 B48 B49 B50 B51 B52 B53 B54 B55 B56 B57 B58 B59 B60 B61 B62 B63 B64 B65 B66 B67 B68 B69 B70 B71 B72 B73 B74 B75 B76 B77 B78 B79 B80 B81 B82 B83 B84 MAX 64.17 113.74 112.06 112.10 112.17 112.24 115.76 143.08 143.54 143.60 143.77 143.80 145.90 134.53 136.21 136.18 136.29 136.48 144.64 132.68 134.42 134.42 135.20 135.06 156.08 134.91 136.54 136.75 140.83 142.08 151.89 144.04 145.77 146.37 149.16 148.26 144.50 112.13 111.41 111.72 110.82 109.88 109.30 151.89 119.15 148.59 145.80 145.86 145.93 146.02 148.27 159.68 159.47 159.58 159.75 159.84 160.74 151.32 152.11 152.15 152.26 152.58 158.88 149.11 150.00 150.07 150.77 150.91 180.64 151.80 152.52 152.98 168.58 170.44 165.75 160.93 161.67 162.57 176.91 176.59 159.74 147.50 145.49 145.89 144.97 144.06 142.63 176.91 C42 C43 C44 C45 C46 C47 C48 C49 1013.54 1115.77 1094.59 1115.97 1063.84 1067.07 1065.17 726.18 1523.17 151 B1 B2 B3 B4 B5 B6 B7 B8 B9 B10 B11 B12 B13 B14 B15 B16 B17 B18 B19 B20 B21 B22 B23 B24 B25 B26 B27 B28 B29 B30 B31 B32 B33 B34 B35 B36 B37 B38 B39 B40 B41 B42 B43 TWO WAY SLAB (SMRF) – 2ND FLOOR ONLY M(+) kN-m M(-) kN-m 70.82 133.62 C1 69.35 132.79 C2 69.28 132.79 C3 69.27 132.80 C4 69.30 132.86 C5 70.18 133.28 C6 70.96 131.08 C7 69.50 131.74 C8 69.45 131.73 C9 69.45 131.73 C10 69.51 131.80 C11 70.96 132.30 C12 69.20 129.30 C13 67.77 131.36 C14 67.72 131.35 C15 67.72 131.36 C16 67.78 131.42 C17 69.20 131.89 C18 67.43 127.51 C19 66.03 129.58 C20 65.97 129.58 C21 66.01 129.91 C22 61.18 146.28 C23 62.52 147.96 C24 69.42 129.55 C25 67.98 131.52 C26 67.93 131.52 C27 68.08 132.06 C28 67.96 126.10 C29 64.44 146.70 C30 71.40 131.57 C31 69.99 131.77 C32 65.14 157.36 C33 65.22 158.90 C34 65.09 155.58 C35 66.49 142.80 C36 71.49 134.12 C37 69.96 133.33 C38 69.93 139.59 C39 69.86 139.95 C40 69.98 139.80 C41 70.85 127.57 C42 74.15 136.44 C43 P (Axial) kN 756.05 990.55 989.65 989.55 989.62 990.25 740.98 989.63 1102.78 1100.84 1100.83 1100.85 1102.61 948.71 989.11 1101.25 1099.27 1099.19 1099.36 1169.43 982.15 989.05 1101.24 1099.28 1100.45 1101.63 1171.01 949.18 989.07 1101.19 1100.42 1303.75 1306.97 1406.92 1017.00 989.37 1102.39 1102.58 1407.10 1410.74 1410.74 950.80 740.88 152 B44 B45 B46 B47 B48 B49 B50 B51 B52 B53 B54 B55 B56 B57 B58 B59 B60 B61 B62 B63 B64 B65 B66 B67 B68 B69 B70 B71 B72 B73 B74 B75 B76 B77 B78 B79 B80 B81 B82 B83 B84 MAX 72.30 72.21 72.21 72.24 73.47 74.44 72.61 72.53 72.52 72.58 74.40 72.83 71.03 70.95 70.95 71.06 68.00 71.21 69.45 69.37 69.37 69.48 71.11 73.32 71.52 71.41 66.69 66.86 73.15 75.42 73.57 73.54 68.74 68.81 75.22 75.63 73.73 73.56 73.63 73.67 74.87 75.63 135.49 135.49 135.55 135.66 136.24 134.09 134.60 134.58 134.69 134.83 134.04 132.50 134.41 134.38 134.46 134.25 158.10 130.91 132.84 132.81 132.90 133.05 143.66 133.03 134.91 135.17 151.16 152.27 145.87 135.16 136.99 137.56 151.83 151.23 134.77 137.92 138.40 138.69 137.02 135.71 131.11 158.90 C44 C45 C46 C47 C48 C49 949.15 949.08 1051.90 1116.91 1116.06 726.72 1410.74 153 APPENDIX C: DESIGN OF BEAMS Beam with Maximum Moment was Designed (One-Way Tradeoff) For Support The following are the given data: Mu = Vu = f'c = fy = b= t= d' = d= Φbar = Φtie = 151.89 84.4 21 275 420 310 62.5 247.5 32 10 kN-m kN Mpa Mpa mm mm mm mm mm mm Es = Ec = n= L= 200000 21383.71 10 5 Mpa Mpa m Part 1. Computation of Steel Area and Number of Bars Step 1. Solve for ρmax and Mu(max) ρb = (0.75*0.85*f'c*β1*600)/(fy*(600+fy) β = 0.85, for f'c < 28 MPa ρmax = ρ = 0.75ρb ω = ρ*fy/f'c Mu(max) = Φ*f'c*ω*b*(d^2)*(1-.59ω) Φ = 0.9 * If Mu < Mu(max), design is Singly Reinforced * If Mu > Mu(max), design is Doubly Reinforced Step 2. Using Doubly Reinforcement. Solving As and N bars As1 = ρmax*b*d M2 = Mu/ Φ – M1, Where M1 = Mu(max) As2 = M2/ fy(d-d’) As = As1 + As2 a = As1*fy/0.85f’c*b 154 c = a/ β fsc = 600(c-d’/c) A’s = As2fy/fsc-0.85f’c N = As/Ab, For tensions reinforcement bars N’ = A’s/Ab, For compression reinforcement bars β ρb ρmax ω φ Mumax RESULTS: 0.85 0.028374545 0.021280909 0.278678571 0.9 113.2277631 DOUBLY As 3303.824281 mm2 A's N N' 1585.621017 4 2 mm2 pcs pcs kN-m Part 2. Designing the Vertical Stirrup Step 1. Calculate the Shear Strength by Concrete (Vc) Vc = sqrt(f'c)*b*d/6 * If Vu > ΦVc, stirrups needed, go to Step II * If Vu < ΦVc, but Vu > .5*ΦVc Stirrups needed * If Vu < .5*Φ*Vc, stirrups are not needed Step 2. Calculate the Shear Strength by Stirrup (Vs) Vn = Vu/Φ Vs = Vn – Vc * If Vs < 0.67*sqrt(f'c)*b*d, go to Step 3. * If Vs > 0.67*sqrt(f'c)*b*d, redesign. Step 3. Spacing of Stirrups Si = Av*fy*d/Vs, Av = pi*(Φtie^2)/4 For Smax, 155 * If Vs < 0.33*sqrt(f'c)*b*d, Smax = d/2 or 600mm (get smaller) * If Vs > 0.33*sqrt(f'c)*b*d, Smax = d/4 or 400mm (get smaller) RESULTS: Vc 79.39312392 φVc 71.45381152 0.5φVc 35.72690576 STIRRUPS NEEDED Vn 93.77777778 Vs 14.38465386 Parameter 319.1603581 Av Si Parameter Smax1 Smax2 Sf 78.53981634 371.6193869 157.1983854 123.75 600 130 kN kN kN kN kN kN mm2 mm mm mm mm mm Part 3. Development Length The following are the supplementary data. Cc = 40 mm, Bar Coat = Epoxy Step 1. Determine the Value of the Coefficients (ψt,ψe,ψs,λ) ψt = 1.0 for all other situations ψe = 1.5 for epoxy-coated bars with cover less than 3d or 6d, = 1.2 for all other epoxycoated bars, = 1 for uncoated or zinc coated bars ψt = .8 for 20 mm bars and smaller, = 1 for 25 mm bars and larger λ = 1 for normal weight concrete Step 2. Compute for the development length ld = (fy*ψt*ψe*ψs*d)/(1.1*λ*sqrt(f'c)*((cc+Ktr)/d)) Ktr = 40*Atr/(S*N), Atr = 2*pi*(Φtie^2)/4 ψt = ψe = ψt = λ= RESULTS: 1 1.2 1 1 156 Atr Ktr ld mm2 157.0796327 24.51472131 62.15888111 mm For Midspan The following are the given data: Mu = Vu = f'c = fy = b= t= d' = d= Φbar = Φtie = 176.91 75.05 21 275 420 310 62.5 247.5 32 10 kN-m kN Mpa Mpa mm mm mm mm mm mm Es = Ec = n= L= 200000 21383.71 10 5 Mpa Mpa m Part 1. Computation of Steel Area and Number of Bars Step 1. Solve for ρmax and Mu(max) ρb = (0.75*0.85*f'c*β1*600)/(fy*(600+fy) β = 0.85, for f'c < 28 MPa ρmax = ρ = 0.75ρb ω = ρ*fy/f'c Mu(max) = Φ*f'c*ω*b*(d^2)*(1-.59ω) Φ = 0.9 * If Mu < Mu(max), design is Singly Reinforced * If Mu > Mu(max), design is Doubly Reinforced Step 2. Using Doubly Reinforcement. Solving As and N bars As1 = ρmax*b*d M2 = Mu/ Φ – M1, Where M1 = Mu(max) As2 = M2/ fy(d-d’) 157 As = As1 + As2 a = As1*fy/0.85f’c*b c = a/ β fsc = 600(c-d’/c) A’s = As2fy/fsc-0.85f’c N = As/Ab, For tensions reinforcement bars N’ = A’s/Ab, For compression reinforcement bars β ρb ρmax ω φ Mumax RESULTS: 0.85 0.028374545 0.021280909 0.278678571 0.9 113.2277631 DOUBLY kN-m As 3850.261627 mm2 A's N N' 2379.303669 5 3 mm2 pcs pcs Part 2. Designing the Vertical Stirrup Step 1. Calculate the Shear Strength by Concrete (Vc) Vc = sqrt(f'c)*b*d/6 * If Vu > ΦVc, stirrups needed, go to Step II * If Vu < ΦVc, but Vu > .5*ΦVc Stirrups needed * If Vu < .5*Φ*Vc, stirrups are not needed Step 2. Calculate the Shear Strength by Stirrup (Vs) Vn = Vu/Φ Vs = Vn – Vc * If Vs < 0.67*sqrt(f'c)*b*d, go to Step 3. * If Vs > 0.67*sqrt(f'c)*b*d, redesign. Step 3. Spacing of Stirrups Si = Av*fy*d/Vs, Av = pi*(Φtie^2)/4 158 For Smax, * If Vs < 0.33*sqrt(f'c)*b*d, Smax = d/2 or 600mm (get smaller) * If Vs > 0.33*sqrt(f'c)*b*d, Smax = d/4 or 400mm (get smaller) RESULTS: Vc 79.39312392 φVc 71.45381152 0.5φVc 35.72690576 STIRRUPS NEEDED Vn 83.38888889 Vs 3.995764974 Parameter 319.1603581 Av Si Parameter Smax1 Smax2 Sf 78.53981634 1337.820489 157.1983854 123.75 600 130 kN kN kN kN kN kN mm2 mm mm mm mm mm Part 3. Development Length The following are the supplementary data: Cc = 40 mm, Bar Coat = Epoxy Step 1. Determine the Value of the Coefficients (ψt,ψe,ψs,λ) ψt = 1.0 for all other situations ψe = 1.5 for epoxy-coated bars with cover less than 3d or 6d, = 1.2 for all other epoxycoated bars, = 1 for uncoated or zinc coated bars ψt = .8 for 20 mm bars and smaller, = 1 for 25 mm bars and larger λ = 1 for normal weight concrete Step 2. Compute for the development length ld = (fy*ψt*ψe*ψs*d)/(1.1*λ*sqrt(f'c)*((cc+Ktr)/d)) Ktr = 40*Atr/(S*N), Atr = 2*pi*(Φtie^2)/4 159 RESULTS: ψt = ψe = ψt = λ= 1 1.2 1 1 Atr Ktr ld 157.0796327 16.33715689 71.18149216 mm2 mm Part 4. Checking the Beam in Deflection Step 1. Calculate the Gross Moment of Inertia and the Cracking Moment of the Beam Ig = b(t^3)/12 Mcr = Ig*fr/ϒt, fr = 0.62*λ*sqrt(f'c), ϒt = t/2 Step 2. Calculate the Moment of Inertia of the Cracked Section Icr = b*(c^3)/12 + nAs(d-c)+nAs'(c-d') Step 3. Calculate the Effective Moment of Inertia Ie = ((Mcr/Mu)^3)*Ig + ((1-(Mcr/Mu)^3)*Icr) Step 4. Determine and Check the Deflection Mu = W(L^2)/8, W=____ δ = 5*W*(L^4)/(384*Ec*Ie) δmax = L/360 RESULTS: Ig fr ϒt Mcr 1042685000 2.841196931 155 19.11273175 mm4 Mpa mm kN-m Icr 37088340.7 mm4 Ie W δ δmax 38356386.58 9.04 0.280295746 13.88888889 OK mm4 kN/m mm mm 160 Beam with Maximum Moment was Designed (Two-Way Tradeoff) For Support The following are the given data: Mu = Vu = f'c = fy = b= t= d' = d= Φbar = Φtie = 75.63 101.37 21 275 310 420 62.5 357.5 32 10 kN-m kN Mpa Mpa mm mm mm mm mm mm Es = Ec = n= L= 200000 21383.71 10 5 Mpa Mpa m Part 1. Computation of Steel Area and Number of Bars Step 1. Solve for ρmax and Mu(max) ρb = (0.75*0.85*f'c*β1*600)/(fy*(600+fy) β = 0.85, for f'c < 28 MPa ρmax = ρ = 0.75ρb ω = ρ*fy/f'c ρmax Mu(max) = Φ*f'c*ω*b*(d^2)*(1-.59ω) Φ = 0.9 * If Mu < Mu(max), design is Singly Reinforced * If Mu > Mu(max), design is Doubly Reinforced Step 2. Using Singly Reinforcement. Solving As and N bars As1 = ρmax*b*d N = As/Abar, Abar = pi*(Φbar^2)/4 β ρb ρmax RESULTS: 0.85 0.028374545 0.021280909 161 ω φ Mumax 0.278678571 0.9 174.3680925 SINGLY As N 2358.45675 3 kN-m mm2 pcs Part 2. Designing the Vertical Stirrup Step 1. Calculate the Shear Strength by Concrete (Vc) Vc = sqrt(f'c)*b*d/6 * If Vu > ΦVc, stirrups needed, go to Step II * If Vu < ΦVc, but Vu > .5*ΦVc Stirrups needed * If Vu < .5*Φ*Vc, stirrups are not needed Step 2. Calculate the Shear Strength by Stirrup (Vs) Vn = Vu/Φ Vs = Vn – Vc * If Vs < 0.67*sqrt(f'c)*b*d, go to Step 3. * If Vs > 0.67*sqrt(f'c)*b*d, redesign. Step 3. Spacing of Stirrups Si = Av*fy*d/Vs, Av = pi*(Φtie^2)/4 For Smax, * If Vs < 0.33*sqrt(f'c)*b*d, Smax = d/2 or 600mm (get smaller) * If Vs > 0.33*sqrt(f'c)*b*d, Smax = d/4 or 400mm (get smaller) RESULTS: Vn 84.6439919 Vs 76.17959271 0.5φVc 34.28081672 STIRRUPS NEEDED kN kN kN Vn Vs 112.6333333 27.98934143 kN kN Parameter Av 340.2688474 78.53981634 mm2 mm 162 Si Parameter Smax1 Smax2 Sf 275.8709315 167.595104 178.75 600 180 mm mm mm mm mm Part 3. Development Length The following are the supplementary data. Cc = 40 mm, Bar Coat = Epoxy Step 1. Determine the Value of the Coefficients (ψt,ψe,ψs,λ) ψt = 1.0 for all other situations ψe = 1.5 for epoxy-coated bars with cover less than 3d or 6d, = 1.2 for all other epoxycoated bars, = 1 for uncoated or zinc coated bars ψt = .8 for 20 mm bars and smaller, = 1 for 25 mm bars and larger λ = 1 for normal weight concrete Step 2. Compute for the development length ld = (fy*ψt*ψe*ψs*d)/(1.1*λ*sqrt(f'c)*((cc+Ktr)/d)) Ktr = 40*Atr/(S*N), Atr = 2*pi*(Φtie^2)/4 ψt ψe ψt λ RESULTS: 1 1.2 1 1 Atr Ktr 157.0796327 11.90335223 mm2 ld 161.2012078 mm2 163 For Midspan The following are the given data: Mu = Vu = f'c = fy = b= t= d' = d= Φbar = Φtie = 158.9 97.94 21 275 310 420 62.5 357.5 32 10 kN-m kN Mpa Mpa mm mm mm mm mm mm Es = Ec = n= L= 200000 21383.71 10 5 Mpa Mpa m Part 1. Computation of Steel Area and Number of Bars Step 1. Solve for ρmax and Mu(max) ρb = (0.75*0.85*f'c*β1*600)/(fy*(600+fy) β = 0.85, for f'c < 28 MPa ρmax = ρ = 0.75ρb ω = ρ*fy/f'c ρmax Mu(max) = Φ*f'c*ω*b*(d^2)*(1-.59ω) Φ = 0.9 * If Mu < Mu(max), design is Singly Reinforced * If Mu > Mu(max), design is Doubly Reinforced Step 2. Using Singly Reinforcement. Solving As and N bars As1 = ρmax*b*d N = As/Abar, Abar = pi*(Φbar^2)/4 β ρb ρmax ω φ Mumax RESULTS: 0.85 0.028374545 0.021280909 0.278678571 0.9 174.3680925 kN-m 164 SINGLY As N 2358.45675 3 mm2 pcs Part 2. Designing the Vertical Stirrup Step 1. Calculate the Shear Strength by Concrete (Vc) Vc = sqrt(f'c)*b*d/6 * If Vu > ΦVc, stirrups needed, go to Step II * If Vu < ΦVc, but Vu > .5*ΦVc Stirrups needed * If Vu < .5*Φ*Vc, stirrups are not needed Step 2. Calculate the Shear Strength by Stirrup (Vs) Vn = Vu/Φ Vs = Vn – Vc * If Vs < 0.67*sqrt(f'c)*b*d, go to Step 3. * If Vs > 0.67*sqrt(f'c)*b*d, redesign. Step 3. Spacing of Stirrups Si = Av*fy*d/Vs, Av = pi*(Φtie^2)/4 For Smax, * If Vs < 0.33*sqrt(f'c)*b*d, Smax = d/2 or 600mm (get smaller) * If Vs > 0.33*sqrt(f'c)*b*d, Smax = d/4 or 400mm (get smaller) RESULTS: Vn 84.6439919 Vs 76.17959271 0.5φVc 34.28081672 STIRRUPS NEEDED kN kN kN Vn Vs 108.8222222 24.17823032 kN kN Parameter Av Si Parameter Smax1 Smax2 Sf 340.2688474 78.53981634 319.3552874 167.595104 178.75 600 180 mm2 mm mm mm mm mm mm 165 Part 3. Development Length The following are the supplementary data. Cc = 40 mm, Bar Coat = Epoxy Step 1. Determine the Value of the Coefficients (ψt,ψe,ψs,λ) ψt = 1.0 for all other situations ψe = 1.5 for epoxy-coated bars with cover less than 3d or 6d, = 1.2 for all other epoxycoated bars, = 1 for uncoated or zinc coated bars ψt = .8 for 20 mm bars and smaller, = 1 for 25 mm bars and larger λ = 1 for normal weight concrete Step 2. Compute for the development length ld = (fy*ψt*ψe*ψs*d)/(1.1*λ*sqrt(f'c)*((cc+Ktr)/d)) Ktr = 40*Atr/(S*N), Atr = 2*pi*(Φtie^2)/4 ψt ψe ψt λ RESULTS: 1 1.2 1 1 Atr Ktr 157.0796327 11.90335223 mm2 ld 161.2012078 mm2 Part 4. Checking the Beam in Deflection Step 1. Calculate the Gross Moment of Inertia and the Cracking Moment of the Beam Ig = b(t^3)/12 Mcr = Ig*fr/ϒt, fr = 0.62*λ*sqrt(f'c), ϒt = t/2 Step 2. Calculate the Moment of Inertia of the Cracked Section Icr = b*(c^3)/12 + nAs(d-c)+nAs'(c-d') Step 3. Calculate the Effective Moment of Inertia Ie = ((Mcr/Mu)^3)*Ig + ((1-(Mcr/Mu)^3)*Icr) Step 4. Determine and Check the Deflection Mu = W(L^2)/8, W=____ 166 δ = 5*W*(L^4)/(384*Ec*Ie) δmax = L/360 RESULTS: Ig fr ϒt Mcr 1042685000 2.841196931 155 19.11273175 mm4 Mpa mm kN-m Icr 37088340.7 mm4 Ie W δ δmax 38356386.58 25.29 0.784145953 13.88888889 OK mm4 kN/m mm mm 167 APPENDIX D: DESIGN OF ONE-WAY SLAB Design of S-1 Considering Longer Side The following are the given data: Dead Loads Weight of Slab = 3.6 kPa Stone Concrete Fill = 1.53 kPa Gypsum Board = 0.2 kPa Total = 5.33 kPa Live Loads Basic Floor Area = 1.9 kPa f'c = fy = L= t= b= Φbar = Φtie = d= β= 21 415 5 150 1000 12 10 134 0.850000 Mpa Mpa m mm mm mm mm mm Step 1. Calculate the Factored Loads and the Moment in the Slab W = 1.2DL + 1.6LL For Midspan, M = W*(L^2)/14 For Continuous Edge, M = W*(L^2)/10 Step 2. Calculate the ρ and check for the Midspan R = Mu/(b*(d^2)) ρ = (0.85*f'c/fy)*(1-(sqrt(1-((2*R)/(0.85*f'c)))) ρmax = 0.75*0.85*f'c*β*600/(fy*(600+fy)) ρmin = 1.4/fy * If ρ > ρmax, redesign * If ρmin < ρ < ρmax, ok * If ρmin > ρ, use ρmin Step 3. Calculate the Steel Area and Spacing of Bars As = ρ*b*d S = b*Abar/As, Abar = pi*(Φbar^2)/4 Step 4. Calculate the ρ and check for the Continuous Edge Step 5. Calculate the Steel Area and Spacing of Bars 168 W Mmid Mc.e. R ρi ρmax ρmin ρf As Abar S R ρi ρmax ρmin ρf As Abar S STEP 1 RESULTS: 9.436 16.85 23.59 STEP 2 RESULTS: 0.93840499 0.002324001 0.016208974 0.003373494 0.003373494 STEP 3 RESULTS: 452.0481928 113.0973355 250.1886687 STEP 4 RESULTS: 1.313766986 0.003291657 0.016208974 0.003373494 0.003373494 STEP 5 RESULTS: 452.0481928 113.0973355 250.1886687 kN/m kN-m kN-m mm2 mm2 mm mm2 mm2 mm Considering Shorter Side The following are the given data: Dead Loads Weight of Slab = 3.6 kPa Stone Concrete Fill = 1.53 kPa Gypsum Board = 0.2 kPa Total = 5.33 kPa Live Loads Basic Floor Area = 1.9 kPa f'c = fy = L= t= b= Φbar = Φtie = d= β= 21 415 2.5 150 1000 12 10 134 0.850000 Mpa Mpa m mm mm mm mm mm Step 1. Calculate the Factored Loads and the Moment in the Slab W = 1.2DL + 1.6LL 169 For Midspan, M = W*(L^2)/14 For Continuous Edge, M = W*(L^2)/10 Step 2. Calculate the ρ and check for the Midspan R = Mu/(b*(d^2)) ρ = (0.85*f'c/fy)*(1-(sqrt(1-((2*R)/(0.85*f'c)))) ρmax = 0.75*0.85*f'c*β*600/(fy*(600+fy)) ρmin = 1.4/fy * If ρ > ρmax, redesign * If ρmin < ρ < ρmax, ok * If ρmin > ρ, use ρmin Step 3. Calculate the Steel Area and Spacing of Bars As = ρ*b*d S = b*Abar/As, Abar = pi*(Φbar^2)/4 Step 4. Calculate the ρ and check for the Continuous Edge Step 5. Calculate the Steel Area and Spacing of Bars W Mmid Mc.e. R ρi ρmax ρmin ρf As Abar S R ρi ρmax ρmin STEP 1 RESULTS: 9.436 4.2125 5.8975 STEP 2 RESULTS: 0.234601247 0.000569069 0.016208974 0.003373494 0.003373494 STEP 3 RESULTS: 452.0481928 113.0973355 250.1886687 STEP 4 RESULTS: 0.328441746 0.000798844 0.016208974 0.003373494 kN/m kN-m kN-m mm2 mm2 mm 170 ρf 0.003373494 STEP 5 RESULTS: As 452.0481928 mm2 Abar 113.0973355 mm2 S 250.1886687 mm Design of S-2 Considering Longer Side The following are the given data: Dead Loads Weight of Slab = 3.6 kPa Stone Concrete Fill = 1.53 kPa Gypsum Board = 0.2 kPa Total = 5.33 kPa Live Loads Basic Floor Area = 1.9 kPa f'c = fy = L= t= b= Φbar = Φtie = d= β= 21 415 2.475 150 1000 12 10 134 0.850000 Mpa Mpa m mm mm mm mm mm Step 1. Calculate the Factored Loads and the Moment in the Slab W = 1.2DL + 1.6LL For Midspan, M = W*(L^2)/14 For Continuous Edge, M = W*(L^2)/10 Step 2. Calculate the ρ and check for the Midspan R = Mu/(b*(d^2)) ρ = (0.85*f'c/fy)*(1-(sqrt(1-((2*R)/(0.85*f'c)))) ρmax = 0.75*0.85*f'c*β*600/(fy*(600+fy)) ρmin = 1.4/fy * If ρ > ρmax, redesign * If ρmin < ρ < ρmax, ok * If ρmin > ρ, use ρmin Step 3. Calculate the Steel Area and Spacing of Bars As = ρ*b*d 171 S = b*Abar/As, Abar = pi*(Φbar^2)/4 Step 4. Calculate the ρ and check for the Continuous Edge Step 5. Calculate the Steel Area and Spacing of Bars W Mmid Mc.e. R ρi ρmax ρmin ρf As Abar S R ρi ρmax ρmin ρf As Abar S STEP 1 RESULTS: 9.436 4.12867125 5.78013975 STEP 2 RESULTS: 0.229932683 0.00055767 0.016208974 0.003373494 0.003373494 STEP 3 RESULTS: 452.0481928 113.0973355 250.1886687 STEP 4 RESULTS: 0.321905756 0.0007828 0.016208974 0.003373494 0.003373494 STEP 5 RESULTS: 452.0481928 113.0973355 250.1886687 kN/m kN-m kN-m mm2 mm2 mm mm2 mm2 mm 172 Considering Shorter Side The following are the given data: Dead Loads Weight of Slab = 3.6 kPa Stone Concrete Fill = 1.53 kPa Gypsum Board = 0.2 kPa Total = 5.33 kPa Live Loads Basic Floor Area = 1.9 kPa f'c = fy = L= t= b= Φbar = Φtie = d= β= 21 415 2.3 150 1000 12 10 134 0.850000 Mpa Mpa m mm mm mm mm mm Step 1. Calculate the Factored Loads and the Moment in the Slab W = 1.2DL + 1.6LL For Midspan, M = W*(L^2)/14 For Continuous Edge, M = W*(L^2)/10 Step 2. Calculate the ρ and check for the Midspan R = Mu/(b*(d^2)) ρ = (0.85*f'c/fy)*(1-(sqrt(1-((2*R)/(0.85*f'c)))) ρmax = 0.75*0.85*f'c*β*600/(fy*(600+fy)) ρmin = 1.4/fy * If ρ > ρmax, redesign * If ρmin < ρ < ρmax, ok * If ρmin > ρ, use ρmin Step 3. Calculate the Steel Area and Spacing of Bars As = ρ*b*d S = b*Abar/As, Abar = pi*(Φbar^2)/4 Step 4. Calculate the ρ and check for the Continuous Edge Step 5. Calculate the Steel Area and Spacing of Bars STEP 1 RESULTS: W 9.436 kN/m Mmid 3.56546 kN-m Mc.e. 4.991644 kN-m 173 R ρi ρmax ρmin ρf As Abar S R ρi ρmax ρmin ρf As Abar S STEP 2 RESULTS: 0.198566496 0.000481165 0.016208974 0.003373494 0.003373494 STEP 3 RESULTS: 452.0481928 113.0973355 250.1886687 STEP 4 RESULTS: 0.277993094 0.000675162 0.016208974 0.003373494 0.003373494 STEP 5 RESULTS: 452.0481928 113.0973355 250.1886687 mm2 mm2 mm mm2 mm2 mm 174 APPENDIX E: DESIGN OF TWO-WAY SLAB The following are the given and results for S1: 1 2 3 4 5 1 DESIGN OF SLAB BY LIMIT STATE METHOD (SIMPLY SUPPORTED TWO WAY ) DIMENSIONS OF ROOM Ly 5000 mm LONGER Lx 5000 mm SHORTER THICKNESS OF SUPPORT b' 200 mm q 0.133 GRADE OF CONCRETE fck 20 N/mm^2 LL 4 KN/M^2 GRADE OF STEEL fy 415 N/mm^2 FF 1 KN/M^2 CLEAR COVER d'' 40 mm ALPHA X 0.086 0.058 ASSUMED DATA ALPHA Y DIA. OF BAR FOR ASTx 10 mm b 1000 mm DIA. OF BAR FOR ASTy 10 mm MF 1.3 CALCULATION d=Lx/(20*1. d 192.307692 mm ASSUMPTION FOR EFFECTIVE FOR S.S. 4) DEPTH OF SLAB OVERALL DEPTH 2 EFFECTIVE SPAN d= D= 120 mm 165 mm lx 1 2 5120 mm 5.12 M 1 2 5120 mm 5.12 M lx ly ly 3 0.165 m 5200 mm Lx+b' 5120 mm Lx+d WHICH EVER IS LESSER 5200 mm Ly+b' 5120 mm Ly+d WHICH EVER IS LESSER FOR ONE WAY AND TWO WAY 1 CHECK ly/lx NEED TO DESIGN AS TWO WAY SLAB 4 5 LOADING CALCULATION FOR ONE METER STRIP BENDING MOMENT CALCULATION DEAD LOAD LIVE LOAD FLOAR FINISH TOTAL LOAD TOTAL FACTORED LOAD(wd) Mux Muy Mu max 5.33 KN/M 1.9 KN/M 1 KN/M 8.23 KN/M 12.345 KN/M 27.83104205 KN.M 18.76977254 KN.M 27.83104205 KN.M Dx25X1 LL.x1 FF.x1 DL+LL+FF TLx1.5 (ALPHA X) x( Wd)x(lx^2) (ALPHA Y) x( Wd)x(lx^2) 175 6 CHECK FOR DEPTH 6 dreq. DEPTH REQUIRED Mur max Qxfckxbxdxd d req.= 102.2878183 mm d provided > d required HENCE OK d=√(Mur*10^6)/(fck*10 00*Q) AST CALCULATION 1 ASTx CALCULATION ASTx= 736.473544 mm^2 SPACING OF 10 MM BAR AREA OF ONE BAR= 78.53982 CHECK FOR MIN. SPACING TAKE SPACING = . . ( d 106.6431 mm 1000` 360 mm 300 mm 106.64 mm 3Xd 300 mm LESSER OF ABOVE 3 CHECK FOR AST MIN. ASTmin= 198.00 mm^2 ASTprovided>ASTmin HENCE OK 2 ASTy CALCULATION ASTy= 524.79416 mm^2 SPACING AREA OF ONE BAR= 78.53982 CHECK FOR MIN. SPACING TAKE SPACING = . . ( d 149.658 mm X1000 360.000 3Xd 300.00 300 mm 149.66 mm LESSER OF ABOVE 3 The following are the results for the Design of S1: SLAB SCHEDULE SLAB MARK S1 SLAB SIZE Ly mm 5000 Lx mm 5000 EFFECTIVE SLAB SIZE ly mm 5120 lx mm 5120 DIA OF BAR #1 mm 10 #2 mm 10 DEPTH EFFECTIVE DEPTH D mm 165 d mm 120 ASTx SPACING FOR ASTx ASTy #1 mm^2 #1 mm #2 mm^2 736.47354 106.6431 524.79416 SPACING FOR ASTy #2 mm 149.658 176 The following are the given and results for S2: 1 2 3 4 5 1 DESIGN OF SLAB BY LIMIT STATE METHOD (SIMPLY SUPPORTED TWO WAY ) DIMENSIONS OF ROOM Ly 2475 mm LONGER Lx 2300 mm SHORTER THICKNESS OF SUPPORT b' 230 mm q 0.133 GRADE OF CONCRETE fck 20 N/mm^2 LL 4 KN/M^2 GRADE OF STEEL fy 415 N/mm^2 FF 1 KN/M^2 CLEAR COVER d'' 40 mm ALPHA X 0.086 0.058 ASSUMED DATA ALPHA Y DIA. OF BAR FOR ASTx 16 mm b 1000 mm DIA. OF BAR FOR ASTy 10 mm MF 1.3 CALCULATION d=Lx/(20*1. d 88.4615385 mm ASSUMPTION FOR EFFECTIVE FOR S.S. 4) DEPTH OF SLAB OVERALL DEPTH 2 EFFECTIVE SPAN d= D= 80 mm 128 mm lx 1 2 2380 mm 2.38 M 1 2 2555 mm 2.555 M lx ly ly 3 0.128 m 2530 mm Lx+b' 2380 mm Lx+d WHICH EVER IS LESSER 2705 mm Ly+b' 2555 mm Ly+d WHICH EVER IS LESSER FOR ONE WAY AND TWO WAY 1.073529 CHECK ly/lx NEED TO DESIGN AS TWO WAY SLAB 4 5 LOADING CALCULATION FOR ONE METER STRIP BENDING MOMENT CALCULATION DEAD LOAD LIVE LOAD FLOAR FINISH TOTAL LOAD TOTAL FACTORED LOAD(wd) Mux Muy Mu max 5.33 KN/M 1.9 KN/M 1 KN/M 8.23 KN/M 12.345 KN/M 6.013723548 KN.M 4.055767044 KN.M 6.013723548 KN.M Dx25X1 LL.x1 FF.x1 DL+LL+FF TLx1.5 (ALPHA X) x( Wd)x(lx^2) (ALPHA Y) x( Wd)x(lx^2) 177 6 CHECK FOR DEPTH 6 dreq. DEPTH REQUIRED Mur max Qxfckxbxdxd d req.= 47.54785301 mm d provided > d required HENCE OK d=√(Mur*10^6)/(fck*10 00*Q) AST CALCULATION 1 ASTx CALCULATION ASTx= 220.971564 mm^2 SPACING OF 10 MM BAR AREA OF ONE BAR= 201.0619 CHECK FOR MIN. SPACING TAKE SPACING = . . ( d 909.8996 mm 1000` 240 mm 300 mm 240.00 mm 3Xd 300 mm LESSER OF ABOVE 3 CHECK FOR AST MIN. ASTmin= 153.60 mm^2 ASTprovided>ASTmin HENCE OK 2 ASTy CALCULATION ASTy= 177.502133 mm^2 SPACING AREA OF ONE BAR= 78.53982 CHECK FOR MIN. SPACING TAKE SPACING = . . ( d 442.473 mm X1000 240.000 3Xd 300.00 300 mm 240.00 mm LESSER OF ABOVE 3 The following are the results for the Design of S2: SLAB SCHEDULE SLAB MARK S2 SLAB SIZE Ly mm 2475 Lx mm 2300 EFFECTIVE SLAB SIZE ly mm 2555 lx mm 2380 DIA OF BAR #1 mm 16 #2 mm 10 DEPTH EFFECTIVE DEPTH D mm 128 d mm 80 ASTx SPACING FOR ASTx ASTy #1 mm^2 #1 mm #2 mm^2 220.97156 909.8996 177.50213 SPACING FOR ASTy #2 mm 240.000 178 APPENDIX F: SAMPLE DESIGN OF COLUMNS One-Way Slab Tradeoff The column with the maximum axial force was designed. The following are the given data: P= My = b= t= cc = d= f'c = fy = Φbar = Φtie = 1523.17 283.25 650 600 40 534 21 415 32 10 kN kN-m mm mm mm mm Mpa Mpa mm mm Step 1. Determine the Steel Area and N bars ρg = ____, assumed value from 0.02 - 0.04 As = ρgAg N = As/Abar then determine actual As Get actual ρg, Pcap = Φ*0.8*Ag(0.85*f'c*(1-ρg)+fy*ρg) * If Pcap > P, the dimensions are adequate * If Pcap < P , Redesign ρg Ag As Asactual Abar N Actual ρg Φ Pcap RESULTS 0.02 390000 7800 8042.477 804.2477 10 0.020622 0.65 5280.896 Adequate mm2 mm2 mm2 mm2 pcs kN 179 Two-Way Slab Tradeoff The column with the maximum axial force was designed. The following are the given data: P= My = 1410.74 283.25 kN kN-m b= 650 mm t= 600 mm cc = 40 mm d= f'c = fy = Φbar = Φtie = 534 21 415 32 10 mm Mpa Mpa mm mm Step 1. Determine the Steel Area and N bars ρg = ____, assumed value from 0.02 - 0.04 As = ρgAg N = As/Abar then determine actual As Get actual ρg, Pcap = Φ*0.8*Ag(0.85*f'c*(1-ρg)+fy*ρg) * If Pcap > P, the dimensions are adequate * If Pcap < P , Redesign ρg Ag As Asactual Abar N Actual ρg Φ Pcap RESULTS 0.02 390000 7800 8042.477 804.2477 10 0.020622 0.65 5280.896 Adequate mm2 mm2 mm2 mm2 pcs kN 180 APPENDIX G: COST ESIMATE COST ESTIMATE OF ONE-WAY OMRF TRADEOFF CONCRETE WORKS CEMENT (bags) 4294.125 1732.5 2751.84 8778.465 CEMENT (bags) 5906.25 38.424375 16.858125 5961.5325 MEMBER B-1 B-2 C-1 L (m) 5 2.5 3.2 b (m) 0.55 0.55 0.65 t (m) 0.5 0.5 0.6 pcs 347 280 245 V (m3) 477.125 192.5 305.76 TOTAL SLAB S-1 S-2 S-3 L (m) 5 2.475 0.925 b (m) 2.5 2.3 2.7 t (m) 0.15 0.15 0.15 pcs 350 5 5 V (m3) 656.25 4.269375 1.873125 TOTAL PRICE LABOR 1473999.75 16377.775 524088.8 2014466.325 7050632.138 N - members 347 280 245 300 300 Total W (kg) 65718.33 32365.2 49493.92 7920 7920 ITEM CEMENT SAND GRAVEL TOTAL 14739.9975 bags 818.88875 m3 1637.7775 m3 TOTAL PRICE MEMBER B-1 B-2 C-1 Slonger Sshorter BAR Ø (mm) 32 25 32 12 12 ITEM TOTAL Steel 163417.45 As (mm2) 804.2477 490.8739 804.2477 113.0973 113.0973 per kg 22.7 per pc 250 50 800 ITEM 3684999 40944.44 1310222 5036166 REBAR WORKS L (m) 5 5 3.2 30 30 N bars 6 6 10 PRICE ITEM LABOR 3709576 7419152 TOTAL COST SAND (m) 238.5625 96.25 152.88 487.6925 SAND (m) 328.125 2.1346875 0.9365625 331.19625 GRAVEL (m) 477.125 192.5 305.76 975.385 GRAVEL (m) 656.25 4.269375 1.873125 662.3925 TOTAL TOTAL 11128728.35 18179360.48 181 COST ESTIMATE OF ONE-WAY SMRF TRADEOFF CONCRETE WORKS CEMENT (bags) 2033.073 820.26 2751.84 5605.173 CEMENT (bags) 5906.25 38.424375 16.858125 5961.5325 MEMBER B-1 B-2 C-1 L (m) 5 2.5 3.2 b (m) 0.42 0.42 0.65 t (m) 0.31 0.31 0.6 pcs 347 280 245 V 225.897 91.14 305.76 TOTAL SLAB S-1 S-2 S-3 L (m) 5 2.475 0.925 b (m) 2.5 2.3 2.7 t (m) 0.15 0.15 0.15 pcs 350 5 5 V (m3) 656.25 4.269375 1.873125 TOTAL PRICE LABOR 1156670.55 12851.895 411260.64 1580783.085 5532740.798 N - members 347 280 245 300 300 Total W (kg) 65718.33 32365.2 49493.92 7920 7920 ITEM CEMENT SAND GRAVEL TOTAL 11566.7055 bags 642.59475 m3 1285.1895 m3 TOTAL PRICE MEMBER B-1 B-2 C-1 Slonger Sshorter BAR Ø (mm) 32 25 32 12 12 ITEM TOTAL Steel 163417.45 As (mm2) 804.2477 490.8739 804.2477 113.0973 113.0973 per kg 22.7 per pc 250 50 800 ITEM 2891676 32129.74 1028152 3951958 REBAR WORKS L (m) 5 5 3.2 30 30 N bars 6 6 10 PRICE ITEM LABOR 3709576 7419152 TOTAL COST (m3) SAND (m) 112.9485 45.57 152.88 311.3985 SAND (m) 328.125 2.1346875 0.9365625 331.19625 GRAVEL (m) 225.897 91.14 305.76 622.797 GRAVEL (m) 656.25 4.269375 1.873125 662.3925 TOTAL TOTAL 11128728.35 16661469.14 182 COST ESTIMATE OF TWO-WAY OMRF TRADEOFF CONCRETE WORKS CEMENT (bags) 5346 2751.84 8097.84 CEMENT (bags) 6075 38.424375 16.858125 6130.2825 MEMBER B-1 C-1 L (m) 5 3.2 b (m) 0.6 0.65 t (m) 0.55 0.6 pcs 360 245 V 594 305.76 TOTAL SLAB S-1 S-2 S-3 L (m) 5 2.475 0.925 b (m) 5 2.3 2.7 t (m) 0.15 0.15 0.15 pcs 180 5 5 V (m3) 675 4.269375 1.873125 TOTAL PRICE LABOR 1422812.25 15809.025 505888.8 1944510.075 6805785.263 N - members 360 245 300 300 Total W (kg) 68180.4 49493.92 7920 7920 ITEM CEMENT SAND GRAVEL TOTAL 14228.1225 bags 790.45125 m3 1580.9025 m3 TOTAL PRICE MEMBER B-1 C-1 Slonger Sshorter BAR Ø (mm) 32 32 12 12 ITEM TOTAL Steel 133514.32 As (mm2) 804.2477 804.2477 113.0973 113.0973 per kg 22.7 per pc 250 50 800 ITEM 3557031 39522.56 1264722 4861275 REBAR WORKS L (m) 5 3.2 30 30 N bars 6 10 PRICE ITEM LABOR 3030775 6061550 TOTAL COST (m3) SAND (m) 297 152.88 449.88 SAND (m) 337.5 2.1346875 0.9365625 340.57125 GRAVEL (m) 594 305.76 899.76 GRAVEL (m) 675 4.269375 1.873125 681.1425 TOTAL TOTAL 9092325.192 15898110.45 183 COST ESTIMATE OF TWO-WAY SMRF TRADEOFF CONCRETE WORKS CEMENT (bags) 2109.24 2751.84 4861.08 CEMENT (bags) 6075 38.424375 16.858125 6130.2825 MEMBER B-1 C-1 L (m) 5 3.2 b (m) 0.42 0.65 t (m) 0.31 0.6 pcs 360 245 V 234.36 305.76 TOTAL SLAB S-1 S-2 S-3 L (m) 5 2.475 0.925 b (m) 5 2.3 2.7 t (m) 0.15 0.15 0.15 pcs 180 5 5 V (m3) 675 4.269375 1.873125 TOTAL PRICE LABOR 1099136.25 12212.625 390804 1502152.875 5257535.063 N - members 360 245 300 300 Total W (kg) 68180.4 0 49493.92 7920 7920 ITEM CEMENT SAND GRAVEL TOTAL 10991.3625 bags 610.63125 m3 1221.2625 m3 TOTAL PRICE MEMBER B-1 C-1 Slonger Sshorter BAR Ø (mm) 32 32 12 12 ITEM TOTAL Steel 133514.32 As (mm2) 804.2477 804.2477 113.0973 113.0973 per kg 22.7 per pc 250 50 800 ITEM 2747841 30531.56 977010 3755382 REBAR WORKS L (m) 5 3.2 30 30 N bars 6 10 PRICE ITEM LABOR 3030775 6061550 TOTAL COST (m3) SAND (m) 117.18 152.88 270.06 SAND (m) 337.5 2.1346875 0.9365625 340.57125 GRAVEL (m) 234.36 305.76 540.12 GRAVEL (m) 675 4.269375 1.873125 681.1425 TOTAL TOTAL 9092325.192 14349860.25 184 APPENDIX H: ESTIMATE OF MAN HOURS For Trade-Off One (One-Way Slab OMRF) Beam B-1 B-2 C-1 S-1 S-2 S-3 b (m) 0.5 0.5 0.65 t (m) 0.15 0.15 0.15 ESTIMATE OF MAN HOURS t (m) L (m) Quantity 0.55 5 347 0.55 2.5 280 0.6 3.2 245 s (m) L (m) Quantity 2.5 5 350 2.3 2.475 5 0.925 2.7 5 TOTAL VOLUME Volume (m3) 477.125 192.5 305.76 Volume (m3) 656.25 4.269375 1.873125 1637.7775 Assuming that 500% of Total Volume of Concrete Works is equal to Total Man Days, Adding 200% For Rebar Works and 350% For Finishing TOTAL MAN DAYS = 5 (1637.7775) + 2 (1637.7775) + 3.5 (1637.7775) TOTAL MAN DAYS = 17197 days Given that there will be 30 workers TOTAL MAN DAYS = 573 days 185 For Trade-Off Two (One-Way Slab SMRF) Beam B-1 B-2 C-1 S-1 S-2 S-3 b (m) 0.31 0.31 0.65 t (m) 0.15 0.15 0.15 ESTIMATE OF MAN HOURS t (m) L (m) Quantity 0.42 5 347 0.42 2.5 280 0.6 3.2 245 s (m) L (m) Quantity 2.5 5 350 2.3 2.475 5 0.925 2.7 5 TOTAL VOLUME Volume (m3) 225.897 91.14 305.76 Volume (m3) 656.25 4.269375 1.873125 1285.1895 Assuming that 500% of Total Volume of Concrete Works is equal to Total Man Days, Adding 200% For Rebar Works and 350% For Finishing TOTAL MAN DAYS = 5 (1285.1895) + 2 (1285.1895) + 3.5 (1285.1895) TOTAL MAN DAYS = 13494 days Given that there will be 30 workers TOTAL MAN DAYS = 450 days 186 For Trade-Off Three (Two-Way Slab OMRF) Beam B-1 C-1 S-1 S-2 S-3 b (m) 0.55 0 0.65 t (m) 0.15 0.15 0.15 ESTIMATE OF MAN HOURS t (m) L (m) Quantity 0.6 5 360 0 0 0 0.6 3.2 245 s (m) L (m) Quantity 5 5 180 2.3 2.475 5 0.925 2.7 5 TOTAL VOLUME Volume (m3) 594 0 305.76 Volume (m3) 675 4.269375 1.873125 1580.9025 Assuming that 500% of Total Volume of Concrete Works is equal to Total Man Days, Adding 200% For Rebar Works and 350% For Finishing TOTAL MAN DAYS = 5 (1580.9025) + 2 (1580.9025) + 3.5 (1580.9025) TOTAL MAN DAYS = 16599 days Given that there will be 30 workers TOTAL MAN DAYS = 553 days 187 For Trade-Off Four (Two-Way Slab SMRF) Beam B-1 C-1 S-1 S-2 S-3 b (m) 0.31 0 0.65 t (m) 0.15 0.15 0.15 ESTIMATE OF MAN HOURS t (m) L (m) Quantity 0.42 5 360 0 0 0 0.6 3.2 245 s (m) L (m) Quantity 5 5 180 2.3 2.475 5 0.925 2.7 5 TOTAL VOLUME Volume (m3) 234.36 0 305.76 Volume (m3) 675 4.269375 1.873125 1221.2625 Assuming that 500% of Total Volume of Concrete Works is equal to Total Man Days, Adding 200% For Rebar Works and 350% For Finishing TOTAL MAN DAYS = 5 (1221.2625) + 2 (1221.2625) + 3.5 (1221.2625) TOTAL MAN DAYS = 12823 days Given that there will be 30 workers TOTAL MAN DAYS = 427 days 188 APPENDIX I: PERCENTAGE DEFLECTION FROM ALLOWABLE Tradeoff 1 (One Way Slab OMRF) (Beam with maximum moment was used) Beam Deflection at Midspan 0.39010528 mm Allowable Deflection 13.88888889 mm Percentage of Computed Deflection from Allowable % = (LV/HV)*100% % = (0.39010528/13.88888889)*100% % = 2.808758016 % Tradeoff 2 (One Way Slab SMRF) (Beam with maximum moment was used) Beam Deflection at Midspan 0.280295746 mm Allowable Deflection 13.88888889 mm Percentage of Computed Deflection from Allowable % = (LV/HV)*100% % = (0.280295746/13.88888889)*100% % = 2.018129371 % Tradeoff 3 (Two Way Slab OMRF) (Beam with maximum moment was used) Beam Deflection at Midspan 0.54028932 Allowable Deflection 189 13.88888889 mm Percentage of Computed Deflection from Allowable % = (LV/HV)*100% % = (0.54028932/13.88888889)*100% % = 3.890083104 % Tradeoff 4 (Two Way Slab SMRF) (Beam with maximum moment was used) Beam Deflection at Midspan 0.784145953 Allowable Deflection 13.88888889 mm Percentage of Computed Deflection from Allowable % = (LV/HV)*100% % = (0.784145953 /13.88888889)*100% % = 5.645850861 % 190 APPENDIX J: REFERENCES Books • McCormac, J.C., & Brown, R. H. (2014). Design of Reinforced Concrete 9th Edition. United States: John Wiley & Sons, Inc. • Everrad & Tanner (1996). Theory and Problems of Reinforced Concrete Design. New York: Schaum Publishing Company. • Association of Structural Engineers of the Philippines. National Structural Code of the Philippines 2010. Quezon City, Philippines: Association of Structural Engineers of the Philippines, Inc. • National Building Code of the Philippines (1977). Philippines. Website References • https://iopscience.iop.org/article/10.1088/1742-6596/1230/1/012050/pdf • https://www.sciencedirect.com/science/article/pii/S1877705817336081 • https://www.semanticscholar.org/paper/Active-Control-of-Pendulum-Tuned-Mass-Dampers-forEltaeb/a33b1682592681e0a3d16030938d766be0cc8b5d • https://www.iitk.ac.in/nicee/wcee/article/13_53.pdf • https://www.researchgate.net/publication/303818187_Structural_Analysis_and_Design_of_Comme rcial_Building_for_Earthquake_Resistance • https://www.researchgate.net/publication/317767808_Study_of_OMRF_and_SMRF_structures_for _different_earthquake_zones_of_India • http://www.iitk.ac.in/nicee/wcee/article/13_53.pdf • https://www.researchgate.net/publication/239545693_Seismic_Conceptual_Design_of_Buildings__Basic_principles_for_engineers_architects_building_owners_and_authorities 191 • https://www.northernarchitecture.us/resisting-system/info-ybx.html • https://www.irjet.net/archives/V5/i6/IRJET-V5I6160.pdf • https://recentscientific.com/sites/default/files/10104-A-2018.pdf • http://sknlazoce.blogspot.com/2018/10/how-to-determine-coefficient-of-over.html • https://www.semanticscholar.org/paper/Active-Control-of-Pendulum-Tuned-Mass-Dampers-for Eltaeb/a33b1682592681e0a3d16030938d766be0cc8b5d • www.wikipedia.com • www.google.com 192