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School of Civil and Environmental Engineering Structural Engineering, Mechanics and Materials Research Report No. 09-10 Literature Review of Punching Shear in Reinforced Concrete Slabs for CEE 8956, Special Research Problem by Eva Lantsoght August 2009 Summary This literature review describes the four different methods to study the problem of punching shear in reinforced concrete bridge deck slabs and the ACI 318 and EN 1992-1-1 code provisions regarding punching shear. The first chapter of this literature review is an introduction to the problem of punching shear in reinforced concrete bridge deck slabs. The lay-out of bridge deck slabs in Dutch and North-American practice is introduced, as well as the wheel loading model used in the European and North-American design codes. Punching shear failure in slabs is described and the difference with shear failure in beams is explained. The second chapter introduces the shear stress theory. This theory is the basis of the currently used design codes. The influence of the concrete strength, the flexural reinforcement, the support and loading conditions, the side length of the loaded area, the size effect, the restraints and the column shape are studied and compared to experimental data. The third chapter introduces the solutions based on plate theory and finite element methods. The fourth chapter introduces the beam analogy method. The currently used beam analogy method as well as the method used before 1960 are briefly explained. The fifth chapter introduces the strut and tie model as developed by Alexander and Simmonds (1986). Consequently, the bond model developed by Alexander and Simmonds (1992) is introduced. In the sixth chapter, the code provisions of ACI 318-08 and EN 1992-1-1:2004 are cited and consequently compared to experimental data. The seventh chapter is the discussion of the literature review. Critique on the introduced theories is given and possible future work is pointed out. The last chapter contains the conclusions of this literature review. A distinction is made between the design practice based on the code equations and the analysis practice which requires a thorough understanding of the mechanics at the basis of the punching shear problem. ii Acknowledgements First and foremost I would like to thank Dr. Lawrence Kahn for his guidance during my reading of the literature on punching shear and during the writing of this report and for advising me during my master’s studies. I also would like to thank Prof. Joost Walraven, Dr. Cor van der Veen and Ir. Joop den Uijl, Technical University of Delft, for sending information and literature during my reading and Xuying Wei and Gert Jan Bakker for answering my questions regarding their MSc theses. Funding for my master’s studies has been provided by the Belgian American Educational Foundation and the Fulbright program. I am very grateful for the received sponsorship. iii Table of Contents Summary ................................................................................................................................... ii Acknowledgements.................................................................................................................. iii Table of Contents ..................................................................................................................... iv List of Tables ............................................................................................................................ v List of Figures .......................................................................................................................... vi 1. Introduction........................................................................................................................... 1 1.1. Purpose and objectives................................................................................................... 1 1.2. Shear in slabs ................................................................................................................. 6 1.3. Comparison with shear in beams ................................................................................... 7 2. Shear Stress Theory ............................................................................................................ 10 2.1. Shear stress on critical perimeter ................................................................................. 10 2.2. Critical shear crack theory ........................................................................................... 20 2.3. Influence of concrete strength...................................................................................... 23 2.4. Influence of flexural reinforcement ............................................................................. 26 2.5. Influence of support and loading conditions................................................................ 31 2.6. Influence of the side length of the loaded area ............................................................ 31 2.7. Size effect..................................................................................................................... 33 2.8. Influence of restraints .................................................................................................. 37 2.9. Influence of the shape of the loaded area..................................................................... 41 2.10. Discussion of shear stress theory ............................................................................... 42 3. Plate Theory and Finite Elements ....................................................................................... 44 3.1. Material modeling........................................................................................................ 44 3.2. 3D solids model ........................................................................................................... 44 3.3. Axi-symmetric model .................................................................................................. 46 3.4. Discussion of plate theory and finite elements solutions............................................. 49 4. Beam Analogy .................................................................................................................... 50 4.1. Currently used beam analogy....................................................................................... 50 4.2. Design based on the equivalent width of a beam strip................................................. 50 4.3. Discussion of beam analogy methods.......................................................................... 51 5. Strut and Tie models ........................................................................................................... 52 5.1. Strut and tie model ....................................................................................................... 52 5.2. Bond model .................................................................................................................. 57 5.3. Discussion of strut and tie models ............................................................................... 61 6. Code Provisions .................................................................................................................. 62 6.1. ACI 318-08 .................................................................................................................. 62 6.2. EN 1992-1-1: 2004 ...................................................................................................... 62 6.3. Comparison of code provisions ................................................................................... 64 6.3.1. Comparison of ACI 318 and EN 1992-1-1 ........................................................... 64 6.3.2. Size effect.............................................................................................................. 67 6.3.3. Influence of concrete strength............................................................................... 68 6.3.4. Influence of reinforcement ratio ........................................................................... 69 7. Discussion ........................................................................................................................... 71 8. Conclusions......................................................................................................................... 73 9. References........................................................................................................................... 75 Appendix A: Notations ........................................................................................................... 78 A.1. List of notations by symbol......................................................................................... 78 A.2. Table of notations by parameter.................................................................................. 82 iv List of Tables Table 1: Shear stresses at the inclined cracking load, Moe (1961)......................................... 13 Table 2: Conversion factors for compressive concrete strength, Dilger, Birkle and Mitchell (2005)...................................................................................................................................... 26 Table 3: Test values with the analytical (Pa), experimental (Pe) and predicted (Pp) solutions, Bakker (2008). ........................................................................................................................ 39 Table 4: List of test results and calculated results, Wei (2008). ............................................. 41 Table 5: Comparison of test results reported by Taylor, Ranking, Cleland and Kirckpatrick (2007) and finite element modeling, Bakker (2008)............................................................... 49 Table 6: Overview of the notations by parameter................................................................... 82 v List of Figures Fig. 1: Punching shear failure of a bridge deck, Ngo (2001).................................................... 1 Fig. 2: Traffic load according to the NEN-EN 1991-2, Bakker (2008). ................................... 2 Fig. 3: Dimension of the ZIP profile and the edge beam, Bakker (2008)................................. 3 Fig. 4: Cross-section of the bridge and one span of the compression layer zoomed into, Bakker (2008). .......................................................................................................................... 4 Fig. 5: Characteristics of the design truck, US customary units, AASHTO (2007). ................ 5 Fig. 6: Characteristics of the design truck, SI units, AASHTO (2007). ................................... 5 Fig. 7: Typical North-American cross-section of a bridge, PCI (2003). .................................. 6 Fig. 8: Crack formation in column area of slab, ASCE-ACI Committee 426 (1974). ............. 8 Fig. 9: Horizontal forces on sections near inclined cracks, ASCE-ACI committee 426 (1974). ................................................................................................................................................... 8 Fig. 10: Testing arrangement, Moe (1961). ........................................................................... 11 Fig. 11: Inclined cracking observed by Moe (1961)............................................................... 11 Fig. 12: Response curves for flexural and punching failure, Menétry (1998), taken from Menétry (2002). ...................................................................................................................... 12 Fig. 13: Punching cone with different inclinations: 30°, 45° and 60°, Menétry (1998), taken from Menétry (2002)............................................................................................................... 12 Fig. 14: Stresses after inclined cracking, Moe (1961). ........................................................... 13 Fig. 15: Schematic presentation of cracking, Theodorakopoulos and Swamy (2002). .......... 14 Fig. 16: Strain and stress distribution in concrete section, Theodorakopoulos and Swamy (2002)...................................................................................................................................... 15 Fig. 17: Interaction between shearing and flexural strength, Moe (1961).............................. 16 Fig. 18: Comparison of test results and Eq. 8, Moe (1961). ................................................... 17 Fig. 19: Elimination of the possibility of shear failure in slab, Moe (1961)........................... 18 Fig. 20: Eq. 9, Moe (1961)..................................................................................................... 19 Fig. 21: Influence of relative shearing strength (Eq. 10) Elstner and Hognestad (1956). ...... 20 Fig. 22: Test by Guandalini and Muttoni: (a) cracking pattern of slab after failure; (b) theoretical strut developing across the critical shear crack; (c) elbow-shaped strut; and (d) plots of measured radial strains in soffit of slab as function of applied load, Muttoni (2008). ................................................................................................................................................. 21 Fig. 23: Slab deflection during punching test: (a) measured values of w at top and bottom face of a slab tested by Guandalini, Burdet and Muttoni (2009); and (b) inpterpretation of measurements according to critical shear crack theory. ......................................................... 22 Fig. 24: Design procedure to check the punching strength of a slab, Muttoni (2008)............ 23 Fig. 25: Influence of concrete strength, Elstner and Hognestad (1956). ................................ 24 Fig. 26: Effect of concrete strength on shear strength (tests by Elstner and Hognestad, (1956), figure by Mitchell, Cook and Dilger (2005). .......................................................................... 25 Fig. 27: Comparison of square root and cube root functions with test results reported by Ghannoum (1998) and McHarg et al. (2000), figure by Mitchell, Cook and Dilger (2005). . 26 Fig. 28: Failure load vs. flexural reinforcement ratio (h ≈ 150 mm ≈ 6 in ), from Dilger, Birkle and Mitchell (2005)...................................................................................................... 27 Fig. 29: Test results from Vanderbilt (1972), from Dilger, Birkle and Mitchell (2005). ....... 28 Fig. 30: Test results from Mardouk and Hussein (1991) from Dilger, Birkle and Mitchell (2005)...................................................................................................................................... 28 Fig. 31: Test results from Hallgren (1996), from Dilger, Birkle and Mitchell (2005). .......... 28 Fig. 32: Test results from Richart (1948), from Dilger, Birkle and Mitchell (2005).............. 28 vi Fig. 33: Influence of flexural reinforcement ratio on punching shear strength according to ACI 318-08 and EN 1992-1-1 (fck = 30 MPa = 4350 psi, fyk = 414 MPa = 60 ksi, c/d=1, l/d=25, l1=l2), Guandalini, Burdet and Muttoni (2009)........................................................... 29 Fig. 34: Normalized load-deflection curve for all 11 specimens (deflection w was measured between center of column and reaction points at perimeter), Guandalini, Burdet and Muttoni (2009)...................................................................................................................................... 30 Fig. 35: Results of 99 punching tests analyzed by Guandalini, Burdet and Muttoni (2009) and 88 tests taken from the literature compared with the failure criterion of the critical shear crack theory: (b) 99 tests with identification of the reinforcement ratio; and (c) 99 tests with identification of effective depth. ............................................................................................. 31 Fig. 36: Effect of large c/d values on shear strength, ASCE-ACI committee 426 (1974)...... 32 Fig. 37: Beam and slab effect as function of r/d, Moe (1961). ............................................... 32 Fig. 38: Effect of the ratio bo/d on the punching shear strength of slab-column connections, from Sherif, Emara, Ibrahim and Magd (2005). ..................................................................... 33 Fig. 39: Normalized punching shear stress ( v / f c' ) vs. average effective depth for tests reported by Li (2000), Mitchell, Cook and Dilger (2005). ..................................................... 34 Fig. 40: Normalized punching shear stress ( v / f c' ) vs. average effective depth for tests reported by Nylander and Sundquist (1972), from Mitchell, Cook and Dilger (2005). ......... 35 Fig. 41: Normalized punching shear stress ( v / f c' ) vs. average effective depth for tests reported by Regan (1986) and Birkle (2004), from Mitchell, Cook and Dilger (2005). ........ 35 Fig. 42: Influence of slab thickness on failure stress in slabs without shear reinforcement, Birkle and Dilger (2008). ........................................................................................................ 36 Fig. 43: Idealized restrained slabs: forces and stress distributions, Hewitt and Batchelor (1975)...................................................................................................................................... 37 Fig. 44: Punching shear failure model, taking compressive membrane action into account, Bakker (2008). ........................................................................................................................ 38 Fig. 45: Modified Hallgren model considering boundary restraint, Wei (2008). ................... 40 Fig. 46: Effect of column rectangularity on shear strength, ASCE-ACI committee 426 (1974). ................................................................................................................................................. 41 Fig. 47: Influence of rectangularity of column on shear strength from tests by Hawkins et al. (1971), Leong and Teng (2000) and Oliveira et al. (2004), figure by Mitchell, Cook and Dilger (2005)........................................................................................................................... 42 Fig. 48: Models for behavior of concrete in tension: brittle and Hordijk tension softening, Bakker (2008). ........................................................................................................................ 44 Fig. 49: Ideal plastic model used for concrete in compression, Bakker (2008)...................... 44 Fig. 50: Dimensions of the 3D solids model. All the edges are clamped and horizontally restrained. Dimensions are in mm, Bakker (2008). ................................................................ 45 Fig. 51: 3D solid element of DIANA software, Bakker (2008).............................................. 45 Fig. 52: Model of a slab using 3D solid elements. The load is applied to the red zone. Figure by Bakker, personal communication 07-15-2009................................................................... 45 Fig. 53: The load-displacement graphs of the 3D solids model, Bakker (2008). ................... 46 Fig. 54: Axi-symmetric model, Bakker (2008)....................................................................... 47 Fig. 55: CQ16A element from DIANA (2008), used in the axi-symmetric model by Bakker (2008)...................................................................................................................................... 47 Fig. 56: Load-displacement graphs for 4 different models of the axi-symmetric model, Bakker (2008). ........................................................................................................................ 48 Fig. 57: Crack pattern just before (loadstep 16) and after (loadstep 17) failure, Bakker (2008). ................................................................................................................................................. 48 vii Fig. 58: Limiting strength combinations for beam analogy, Park and Gamble (1999). ......... 50 Fig. 59: In-plane or anchoring struts, Alexander and Simmonds (1986)................................ 52 Fig. 60: Comparison of corbel with out-of-plane or shear strut, Alexander and Simmonds (1986)...................................................................................................................................... 53 Fig. 61: Calibration of α, Alexander and Simmonds (1986). ................................................. 55 Fig. 62: Effect of the reinforcement density, Alexander and Simmonds (1986). ................... 56 Fig. 63: Space truss analogy for torsion, MacGregor and Ghoneim (1995)........................... 56 Fig. 64: Layout of radial strips, Alexander and Simmonds (1992). ....................................... 58 Fig. 65: Equilibrium of radial strip, Alexander and Simmonds (1992). ................................. 58 Fig. 66: Free-body diagram of one-half radial strip, Alexander and Simmonds (1992). ....... 60 Fig. 67: Bond model results using ACI one-way shear, Alexander and Simmonds (1992). . 60 Fig. 68: Verification model for punching shear at the ultimate limit state, figure 6.12 from EN 1992-1-1:2004. ................................................................................................................. 63 Fig. 69: Typical basic control perimeters around loaded areas, Figure 6.13 from EN 1992-11: 2004. ................................................................................................................................... 63 Fig. 70: Comparison of test/predicted using ACI 318-05 with rounded corners shear perimeter, by Gardner (2005). ................................................................................................ 65 Fig. 71: Comparison of test/predicted using ACI 318-05 with assumption of square shear perimeter, by Gardner (2005). ................................................................................................ 66 Fig. 72: Comparison of test/predicted using CEB-FIP MC90 and EN 1992-1-1:2003, by Gardner (2005)........................................................................................................................ 66 Fig. 73: Comparison of code expressions with results reported by Li (2000) from Mitchell, Cook and Dilger (2005). ......................................................................................................... 67 Fig. 74: Failure criterion: punching shear strength as function of width of critical shear crack compared with 99 experimental results and ACI 318-05 design equation, Muttoni (2008)... 68 Fig. 75: Comparison of code expressions with test results reported by Ghannoum (1998) and McHarg et al. (2000), figure by Mitchell, Cook and Dilger (2005). ...................................... 69 Fig. 76: Effect of analysis on perceived scatter, Alexander and Hawkins (2005).................. 70 viii 1. Introduction 1.1. Purpose and objectives The purpose of this report is to provide a review of the literature regarding the shear capacity and behavior of bridge decks and two-way structural concrete slab systems. The scope is limited; influence of shear reinforcement, moment transfer and holes in the slab is not included. The notations are kept identical to the notations used in the referenced literature. A list of notations can be found in Appendix A. A typical punching shear failure of a bridge deck can be seen in Fig. 1. Fig. 1: Punching shear failure of a bridge deck, Ngo (2001). Currently, new attention is given to the punching shear problem, as the traffic loads are increased and older bridges might not have enough punching shear resistance. The traffic load model according to the EN 1991-2 is shown in Fig. 2. A typical lay-out of a bridge deck using the ZIP-girder system from the Dutch company Spanbeton is shown in Fig. 3. The area over which the wheel load is spread is 350x600 mm (13.73x23.62 in), as can be seen in Fig. 4. Fig. 2: Traffic load according to the NEN-EN 1991-2, Bakker (2008). 2 Fig. 3: Dimension of the ZIP profile and the edge beam, Bakker (2008). 3 Fig. 4: Cross-section of the bridge and one span of the compression layer zoomed into, Bakker (2008). According to AASHTO (2007), either a design truck or a design tandem is used in North-America. The design truck is given in Fig. 5 and Fig. 6. The design tandem consists of a pair of 25 kip axles (110 kN) spaced 4 ft (1200 mm) apart and with a transverse spacing of 6 ft (1800 mm). The tire contact area is taken as a single rectangle with width 20.0 in (510 mm) and length 10.0 in (250 mm). The tire pressure is assumed to be uniformly distributed over the contact area. A typical North-American bridge lay-out is shown in Fig. 7. The girders are spaced at 9 ft on center (2.74 m) and the slab is 8 in thick (20.32 cm). 4 Fig. 5: Characteristics of the design truck, US customary units, AASHTO (2007). Fig. 6: Characteristics of the design truck, SI units, AASHTO (2007). 5 Fig. 7: Typical North-American cross-section of a bridge, PCI (2003). 1.2. Shear in slabs Although the mechanics of punching shear are not entirely understood, many methods have been developed over the years. The first to experimentally study the punching problem was Talbot in 1913. According to Park and Gamble (1999), the behavior of the failure region is extremely complex, because of the combined flexural and diagonal tension cracking and the 3D nature of the problem. However, Moe (1961) stated: “safe design equations apparently can be developed without a full understanding of the fundamental laws governing the phenomenon under consideration”. The methods which have been developed can be divided into 4 categories, according to Park and Gamble (1999): methods which calculate a nominal shear stress on a critical section, beam analogies in which slab strips are calculated as beams under a combination of moment, shear and torsion, methods based on a combination of plate theory and nonlinear finite element methods and truss models. These four methods are studied in this literature review. Alexander and Simmonds (1986) cited the description of Masterson and Long of the four basic stages in the punching failure of a slab-column connection. First, flexural and shear cracks form in the tension zone of the slab near the face of the loaded area. Then, the slab tension steel close to the loaded area yields. Consequently, flexural and shear cracks extend into what was the compression zone of the concrete. Finally, failure occurs before yielding extends beyond the vicinity of the loaded area. A possible reason for punching is rupture of the reduced compression zone in the slab. 6 According to ASCE-ACI committee 426 (1974), most available test data come from slab-column tests. These tests consist of a slab-column specimen with the slab piece up to the line of contraflexure. The behavior of slab-column specimens differs from the real behavior of a slab, since in-plane forces cannot develop. This literature review treats the four previously mentioned categories and the ACI 318 and EN 1992-1-1 code provisions. Most attention is given to methods based on a nominal shear stress on a critical section, as stress methods are most commonly used in design and serve as a basis for the code provisions. 1.3. Comparison with shear in beams The difference between the shear stress theory in beams and slabs is that the nominal ultimate shear stress which can be developed in a slab is higher than in a beam. According to ASCE-ACI committee 426 (1974) this increase is due to the following effects: the location of the inclined crack, the stress conditions at the apex of the crack, the proportionally greater dowel forces, the distribution of moments, the lack of symmetry, the inadequacy of simple static analysis and the in-plane forces generated by restraints provided by the supports and non-yielding portions of the slab. The distribution of moments can be seen from Fig. 8. The radial moment Mr decreases at a rapid rate with distance from the loaded area. It causes yielding to develop first at the perimeter of the loaded area. However, an increasing tangential moment Mθ will restrain any rotation at the inclined crack. Most punching failures do not occur until aggregate interlock effects are markedly diminished by yielding in both the Mr and Mθ direction. When the direction of the principal moment does not match the direction of the layout of the reinforcement, in-plane compression forces are developed to balance the tension force resulting from the reinforcement. The in-plane forces due to this lack of symmetry thus increase the maximum loading. 7 Fig. 8: Crack formation in column area of slab, ASCE-ACI Committee 426 (1974). Fig. 9 shows that statics does not provide a unique value for the compressive force C1 above the inclined crack for a slab. This is the limitation of static analysis. The in-plane forces due to the elastic band around the outer boundary of the yielding portion of the slab which restrains the outward displacement and generates axial compressive forces, increases the flexural and shear capacities. Fig. 9: Horizontal forces on sections near inclined cracks, ASCE-ACI committee 426 (1974). 8 The ability of a slab to resist higher unit shear stresses diminishes as the size of the loaded area increases relative to the slab thickness and as the direction of the reinforcement more closely parallels the direction of the maximum moment when there is essentially oneway action. A slab can then fail as a wide beam. 9 2. Shear Stress Theory 2.1. Shear stress on critical perimeter The shear stress theory compares the shear stress on a critical section with a maximum shear stress. According to Alexander and Simmonds (1986) the shear stress theory is perhaps the simplest approach and is favored by most design codes. Moe (1961) tested 43 slabs (Fig. 10) and investigated the results of 140 footings and 120 slabs tested in the literature. He reported inclined cracking at 60% of the ultimate load (Fig. 11). This inclined cracking started from bending cracks, then rapidly extended up to the proximity of the neutral axis and finally developed rather slowly but leaving only a very narrow depth of compression zone unaffected. Moe (1961) introduced three levels of shear force: Vi = the shear force at which inclined cracks form, Ve = the shear force at which failure in the compression zone above the inclined cracks occurs, Vflex = the shear force at the ultimate flexural strength. With these three forces, he classified four possible types of failure: Vi < Ve < Vflex: shear-compression failure. This type of failure occurs when the compression zone of the critical section (reduced in size due to inclined cracks) fails under a combined action of compressive and shearing stresses. Ve < Vi < Vflex: the slab fails at the moment of formation of inclined cracks, this failure mode is called inclined tension failure. Vi < Vflex < Ve: the slab will fail in flexure after the formation of inclined cracks. Vflex < Vi: the slab will fail in flexure before the formation of inclined cracks. 10 Fig. 10: Testing arrangement, Moe (1961). Fig. 11: Inclined cracking observed by Moe (1961). Menétry (2002) claimed that the distinction between the flexural and punching failure is controlled by the punching crack inclination angle α (Fig. 12 and Fig. 13). For a crack inclination of 30° the failure mode is pure punching and for a crack inclination of 90° the failure mode is pure flexure. Fig. 12 shows a typical lay-out of a slab-column test at the right of the figure. In the test lay-out the loading is applied on the top of the slab, resulting in a compression zone at the top. Fig. 13 displays the column on the bottom as typically seen in flat plates, resulting in a compression zone at the bottom. 11 Fig. 12: Response curves for flexural and punching failure, Menétry (1998), taken from Menétry (2002). Fig. 13: Punching cone with different inclinations: 30°, 45° and 60°, Menétry (1998), taken from Menétry (2002). According to Moe (1961) the periphery of the loaded area is the critical one for a shear-compression failure. For the inclined cracking load, the critical zone is not so clear. A statistical analysis of the data in Table 1 demonstrated that the best agreement between the individual values resulted for a critical perimeter at a distance d/2 away from the periphery of the column or loaded area. Therefore the distance d/2 away from the face of the loaded area was chosen as the location to compute the shear stress for the inclined cracking. 12 Table 1: Shear stresses at the inclined cracking load, Moe (1961). After the inclined cracking, the following stresses occur in the compression zone (Fig. 14): vertical shearing stresses (vo), direct compressive stresses (fc), vertical compressive stresses (f3), which make the shear strength of a slab higher than the shear strength of a beam, and lateral compressive stresses (f2), which increase the compressive strength of a slab as compared to a beam. Fig. 14: Stresses after inclined cracking, Moe (1961). These stresses can be used in theories of failure in concrete under combined stresses. There are two groups of theories: physical theories, based on the internal non-isotropic 13 structure of the material, and phenomenological theories, based on the external behavior under different stress combinations. The physical theories are mathematically complicated and the phenomenological theories, using Mohr’s theory of failure, do not give a reliable criterion of failure. Therefore, Moe (1961) concluded that a better understanding of the stress distribution in the critical zone of the slab and the stress conditions during failure was needed. The depth of the zone above the inclined cracking (Fig. 14) is important for the shear strength, as this zone carries the load after inclined cracking. Theodorakopoulos and Swamy (2002) developed an expression for the depth of the critical section based on the harmonic mean of Xs (depth of the critical section for punching) and Xf (depth of the critical section for flexure) (Fig. 15). Fig. 15: Schematic presentation of cracking, Theodorakopoulos and Swamy (2002). The depth of the shear critical section is found as X s = 0.25d . Eq. 1 The depth of the flexural critical section is found as Xf = ρf s − ρ ' f s' k1 f cu Eq. 2 d with k1 = 0.67 ε cu − Aε o / 3 ε cu Eq. 3 and εo = f cu 4115 (SI units) Eq. 4 14 εo = f cu 49380 (US customary units) in which fs and fs’ = the steel stresses in tension and compression respectively, ρ = the reinforcement ratio of tensile steel, ρ’ = the reinforcement ratio of compression steel, εcu = the ultimate concrete strain (Fig. 16), εo = the concrete strain at the level of the end of the rectangular stress block, A = a coefficient, =1 for normal density concrete, d = the effective depth of the slab, fcu = the ultimate concrete strength in MPa (SI units) or psi (US customary units). Fig. 16: Strain and stress distribution in concrete section, Theodorakopoulos and Swamy (2002). The harmonic mean is then given by 1 1 1 = + . X 2X s 2X f Eq. 5 This method requires iterations and is not very useful for design practice. Alexander and Simmonds (1986) questioned the importance of diagonal cracking, arguing that, although diagonal cracks appear visually important, test observations have shown that these cracks occur at 50-70% of the ultimate loading. The slab in that cracked 15 state is very stable since it can be unloaded and reloaded without affecting the ultimate capacity. As a workable solution to the difficulties encountered, Moe (1961) developed a semiempirical formula for the ultimate strength. The nominal stress is computed as v= V bd Eq. 6 with V = the shear force, b = the width of critical section in shear, d = the effective depth of the slab. Vflex is introduced as a parameter governing the shear strength of slabs, but the magnitude of Vflex has no direct physical relation to the mechanism of failure. Vo is defined as the fictitious shear strength if bending could be eliminated (Fig. 17). Fig. 17: Interaction between shearing and flexural strength, Moe (1961). Considering the influence of the ratio of column size to slab thickness and φo = V/Vflex, Moe (1961) suggested the following relationship: 16 r v = A1 − C − Bφ o f c' (US customary units) d r v = 12 A1 − C − Bφ o f c' d Eq. 7 (SI units) The constants A, B and C from Eq. 7 were obtained with a statistical analysis (Fig. 18). The purpose of the statistical analysis was to determine the specific combination of constants A, B and C which for the available test data yields to an average value of the ratio of tested to calculated ultimate loads (Vtest/Vcalc) equal to one and a minimum standard deviation for Vtest/Vcalc. This analysis led to: r 15(1 − 0.075 ) d = = ' ' f c bd f c bd f c' 1 + 5.25 V flex v V (US customary units) Eq. 8 r 180(1 − 0.075 ) v V d (SI units) = = ' ' f c bd f c bd f c' 1 + 63 V flex Fig. 18: Comparison of test results and Eq. 8, Moe (1961). 17 A shear failure is not desirable in a slab, and therefore Moe (1961) limited the stress such that a slab fails in flexure (Fig. 19). The shear failures in Fig. 19 are calculated by Eq. 8. The point of balanced design is chosen as point B, where V =1.1Vflex. In order to be sure of obtaining a flexural failure, the shear stress should be limited to: r v = (9.23 − 1.12 ) f c' d for r/d ≤ 3 (US customary units) Eq. 9 d v = (2.5 + 10 ) f c' r for r/d > 3 (US customary units) r v = (110.76 − 13.44 ) f c' d for r/d ≤ 3 (SI units) d v = (30 + 120 ) f c' r for r/d > 3 (SI units) The equation for r/d > 3 was derived theoretically based on the fact that for a value of r/d approaching infinity, the value for the shear stress should approach the corresponding shearing strength of a beam and because test data were only available for values of r/d up to 3.1. Fig. 19: Elimination of the possibility of shear failure in slab, Moe (1961). 18 Fig. 20: Eq. 9, Moe (1961). Elstner and Hognestad (1956) used a shearing stress, v2, computed at zero distance from the column face or loaded area and used an equation based on statistical analysis: v2 P 333 0.046 = shear = ' + (US customary units) ' ϕ fc 7 fc ' o bdf c 8 Eq. 10 v2 P 2.296 0.046 = shear = + (SI units) ' 7 ϕ fc f c' ' o bdf c 8 with fc’ = the cylinder strength (psi for US customary units, MPa for SI units), φo = Pshear/Pflex, Pshear = the ultimate shear capacity, and Pflex = the ultimate flexural capacity of the slab computed by the yield-line theory without regard to a shear failure (Fig. 21). No resistance factor is used. 19 Fig. 21: Influence of relative shearing strength (Eq. 10) Elstner and Hognestad (1956). 2.2. Critical shear crack theory The critical shear crack theory describes the relationship between the punching shear strength of a slab and its rotation at failure. Muttoni (2008) gave the following evidence supporting the role of the shear critical crack in the punching shear strength. After reaching a maximum level, the radial compressive strain decreases; and shortly before punching, tensile strains may be observed. These strains can be explained by the development of an elbowshaped strut (Fig. 22) with a horizontal tensile member along the soffit due to the development of the critical shear crack. Also, experimental results on slabs with a particular lay-out of circular reinforcement in which only radial cracks form and in which the formation of circular cracks is avoided, confirmed the role of the critical shear crack. 20 Fig. 22: Test by Guandalini and Muttoni: (a) cracking pattern of slab after failure; (b) theoretical strut developing across the critical shear crack; (c) elbow-shaped strut; and (d) plots of measured radial strains in soffit of slab as function of applied load, Muttoni (2008). The critical shear crack theory is described in Guandalini, Burdet and Muttoni (2009). This theory is based on the assumption that the shear strength of members without transverse reinforcement is governed by the width and roughness of an inclined shear crack that develops through the inclined compression strut carrying shear. In two-way slabs the width wc of the critical shear crack is assumed proportional to the slab rotation ψ and the effective depth d of the member (Fig. 23). The following failure criterion was obtained: VR b0 d f c VR b0 d f c = 3/ 4 1 + 15 1 + 15 Eq. 11 d g0 + d g 9 = (SI units) ψd ψd (US customary units) d g0 + d g in which VR = the shear strength, b0 = a control perimeter at d/2 from the edge of the column, d = the effective depth of the member, fc = the compressive strength of the concrete, 21 dg = the maximum size of the aggregate (accounting for the roughness of the lips of the cracks), dg0 = a reference aggregate size equal to 16 mm = 0.63 in. Fig. 23: Slab deflection during punching test: (a) measured values of w at top and bottom face of a slab tested by Guandalini, Burdet and Muttoni (2009); and (b) inpterpretation of measurements according to critical shear crack theory. The failure load is obtained at the intersection (Fig. 24) of the failure criterion (Eq. 11) with the load-rotation curve of the slab, which for practical purposes can be approximated by: r f V ψ = 1.5 s . y d E s V flex 3/ 2 Eq. 12 with rs = the radius of the slab, Vflex can be estimated with the yield-line method. 22 According to Muttoni (2008), the load-rotation relationship can, in a more general case, be obtained from a nonlinear numerical simulation of the flexural behavior of the slab, or in the axi-symmetric case by a numerical integration of the moment-curvature relationship. An advantage of this method is that it finds the value of the rotation capacity of the slab, and thus of its ductility. Due to the relation between the shear carried across a crack and the depth of a section, this method takes the size effect into account. An earlier treatment of this method can be found in Muttoni (2003). Fig. 24: Design procedure to check the punching strength of a slab, Muttoni (2008). 2.3. Influence of concrete strength The shear strength is related to the concrete strength fc’. It is not clear however if this relationship is a square root or cubic root dependence. Early research did not consider a square or cube root dependence. Elstner and Hognestad (1956) used the concrete strength fc’ in their study and tested slabs with concrete strengths fc’ ranging from 2000 to 7000 psi. 23 Fig. 25: Influence of concrete strength, Elstner and Hognestad (1956). Moe (1961) used the square root for the following two reasons. First, a shear failure is of a splitting type, comparable to the type of failure observed in specimens under tension. The tensile strength was generally assumed to be proportional to f c' . Second, f c' approaches zero when fc’ approaches zero. A function a + bf c' which fits test results would not approach zero and therefore would not be satisfactory. Mitchell, Cook and Dilger (2005) compared the influence of the square and cube root of the concrete strength with experimental data. Fig. 26 compares test results to ( f c' ) with n n=1/2, 1/3 and 2/3. These figures show that the overall trend is reasonably presented by n=1/3 as well as by n=1/2. 24 Fig. 26: Effect of concrete strength on shear strength (tests by Elstner and Hognestad, (1956), figure by Mitchell, Cook and Dilger (2005). Fig. 27 shows test results compared by Mitchell, Cook and Dilger (2005) to the square root and cube root of the concrete strength. The two functions were normalized to give a value of 1.0 at a concrete strength of 30 MPa. For each of the tests, the normalized shear ratio is taken as the failure load divided by the failure load for the case with a concrete compressive strength of 30 MPa. Based on Fig. 27, the cube root function appears to fit the data for high strength concrete in a more conservative manner. However, Mitchell, Cook and Dilger (2005) concluded that it is not clear whether the punching strength is proportional to the square or cube root of the concrete strength and that additional research is needed to enable the development of design expressions for punching shear that are applicable to a wide range of concrete strengths, especially high strength concrete. 25 Fig. 27: Comparison of square root and cube root functions with test results reported by Ghannoum (1998) and McHarg et al. (2000), figure by Mitchell, Cook and Dilger (2005). 2.4. Influence of flexural reinforcement ASCE-ACI committee 426 (1974) collected different methods to calculate the shear strength and divided them into two categories: expressions dependent primarily on the concrete strength and expressions dependent primarily on flexural effects. Tensile reinforcement was advised to improve the flexural behavior of the slab in the service load range. Compression reinforcement was advised because it acts like a suspension net, supplying an alternate load path that holds the slab together even after a punching failure. Elstner and Hognestad (1956) tested the influence of compression reinforcement on the ultimate shearing strength and concluded that it did not have an effect on the ultimate shearing strength of slabs. They did not include the influence of reinforcement in the expression they developed (Eq.10). Dilger, Birkle and Mitchell (2005) studied the influence of the reinforcement ratio on the ultimate shearing strength. Fig. 28 shows the comparison of test results from a variety of researchers. The stresses at failure were adjusted for varying concrete strength and the reinforcement ratio was taken as the average reinforcement ratio in both directions. The concrete strength was adjusted as 30 v adj = vtest f' c 1/ 3 4350 v adj = vtest f' c (SI units) Eq. 13 1/ 3 (US customary units) in which fc’ is the concrete strength measured in MPa (SI units) or psi (US customary units) and adjusted according to Table 2. 26 Table 2: Conversion factors for compressive concrete strength, Dilger, Birkle and Mitchell (2005). Fig. 28 indicated a tendency of increasing punching strength with increasing reinforcement ratio, but the data showed a lot of scatter. Therefore the data were studied per researcher. Fig. 28: Failure load vs. flexural reinforcement ratio (h ≈ 150 mm ≈ 6 in ), from Dilger, Birkle and Mitchell (2005). The test results per researcher are shown in Fig. 29, Fig. 30, Fig. 31 and Fig. 32. Dilger, Birkle and Mitchell (2005) concluded from these test series that with an increase in flexural reinforcement ratio the stresses along the punching cone and, hence, the load carrying capacity in shear were increased. Dilger, Birkle and Mitchell (2005) cited an explanation given by Richart (1948), who found that significant yielding of the flexural reinforcement produced large cracks, which decreased the effective area resisting the shear. Assuming that little or no shear can be transferred through the portion of the depth of the slab that is cracked, it is easy to conclude that the width and, hence, the depth of the crack, which are controlled by the amount of flexural reinforcement, have a significant influence on the shear capacity. 27 Fig. 29: Test results from Vanderbilt (1972), from Dilger, Birkle and Mitchell (2005). Fig. 30: Test results from Mardouk and Hussein (1991) from Dilger, Birkle and Mitchell (2005). Fig. 31: Test results from Hallgren (1996), from Dilger, Birkle and Mitchell (2005). Fig. 32: Test results from Richart (1948), from Dilger, Birkle and Mitchell (2005). 28 Guandalini, Burdet and Muttoni (2009) investigated the punching strength of slabs with low reinforcement ratios. The scope of their research was slabs with low reinforcement ratios, because there was not much data available for slabs with low reinforcement ratios failing in shear, as researchers tried to avoid flexural failures, and because the code provisions differ significantly (Fig. 33). The results were recorded as load-deflection curves (Fig. 34) which shows unexpectedly low strengths for slabs with low reinforcement ratios. The results were compared to results form the literature (Fig. 35). Guandalini, Burdet and Muttoni (2009) concluded that future research is needed to investigate this observation and that special attention should be given to the cases in which the code provisions significantly underestimate the punching shear strength. Fig. 33: Influence of flexural reinforcement ratio on punching shear strength according to ACI 318-08 and EN 1992-1-1 (fck = 30 MPa = 4350 psi, fyk = 414 MPa = 60 ksi, c/d=1, l/d=25, l1=l2), Guandalini, Burdet and Muttoni (2009). 29 Fig. 34: Normalized load-deflection curve for all 11 specimens (deflection w was measured between center of column and reaction points at perimeter), Guandalini, Burdet and Muttoni (2009). 30 Fig. 35: Results of 99 punching tests analyzed by Guandalini, Burdet and Muttoni (2009) and 88 tests taken from the literature compared with the failure criterion of the critical shear crack theory: (b) 99 tests with identification of the reinforcement ratio; and (c) 99 tests with identification of effective depth. 2.5. Influence of support and loading conditions According to ASCE-ACI committee 426 (1974), long-term loading did not have a negative effect on the shear strength. Rapid loading resulted in an increase in strength. Elstner and Hognestad (1956) tested slabs with different support conditions. They reported that a two-edge support as compared to a four-edge support decreased Pflex, increased φo and decreased the estimated maximum load. 2.6. Influence of the side length of the loaded area Fig. 36 shows the results for the ultimate shear strength for tests with different side length to effective depth (c/d) ratios as compared by ASCE-ACI committee 426 (1974). The data show a decrease in the shear strength for increasing c/d ratios. 31 Fig. 36: Effect of large c/d values on shear strength, ASCE-ACI committee 426 (1974). r Moe (1961) assumed a linear expression (1 − 0.075 ) where r is the side length of d the loaded area and d is the effective depth of the slab. In the case of a continuous slab supported on a wall, r/d becomes infinite and the shearing strength approaches the shearing strength of a beam (Fig. 37). Fig. 37: Beam and slab effect as function of r/d, Moe (1961). 32 Sherif, Emara, Ibrahim and Magd (2005) studied the influence of the bo/d ratio (with bo the perimeter of the critical section) on the punching capacity. From a theoretic point of view they stated that the punching shear strength decreased with an increase in the bo/d ratio, because confinement was reduced. This effect can also be seen in the data gathered in Fig. 38. The critical section was taken at a distance d/2 from the face of the loaded area. Fig. 38: Effect of the ratio bo/d on the punching shear strength of slab-column connections, from Sherif, Emara, Ibrahim and Magd (2005). 2.7. Size effect Elstner and Hognestad (1956) questioned the extrapolation of observations on thick footing slabs to flat plate floors from a theoretical point of view, since lower thickness-tospan ratios and higher moment-to-shear ratios are more associated with floor slabs than with footings. 33 According to ASCE-ACI committee 426 however, there was no effect of scale on shear strength, provided that deformed bars are approximately scaled, concrete mixes are scaled, and measurements of compressive strength are made on scaled cylinders. Collins and Kuchma (1999) investigated the importance of the size effect on beams, slabs and footings and concluded that the size effect has to be taken into account and that high-strength concrete members display a more significant size effect. They pointed out that the shear stress at failure decreases, both as the member depth increases and as the maximum aggregate size decreases. According to Collins and Kuchma (1999), the size effect had to be studied especially in slabs and footings, as these members can be both very thick and very lightly reinforced. Mitchell, Cook and Dilger (2005) stated that it is difficult to gather experimental data solely on the size effect, as many reported experiments varied other parameters together with the thickness. For example, the reinforcement ratio was changed together with the slab thickness to keep the ratio of flexural capacity to shear capacity constant. Mitchell, Cook and Dilger (2005) gathered information of tests where only the size was varied. It is clear from the data in Fig. 39 that there is a size effect for slabs thicker than about 200 mm (8 in). The data in Fig. 40 also show a size effect, even for slabs with a thickness smaller than 200 mm (8 in). Fig. 41 also shows the size effect. Tests with varying maximum aggregate size are not included. As can be seen in Fig. 39, Fig. 40 and Fig. 41, the shear stress at punching failure decreases as the effective depth increases. According to Mitchell, Cook and Dilger (2005) the size effect is significant, but the available data are scarce. Fig. 39: Normalized punching shear stress ( v / f c' ) vs. average effective depth for tests reported by Li (2000), Mitchell, Cook and Dilger (2005). 34 Fig. 40: Normalized punching shear stress ( v / f c' ) vs. average effective depth for tests reported by Nylander and Sundquist (1972), from Mitchell, Cook and Dilger (2005). Fig. 41: Normalized punching shear stress ( v / f c' ) vs. average effective depth for tests reported by Regan (1986) and Birkle (2004), from Mitchell, Cook and Dilger (2005). Birkle and Dilger (2008) state that the size effect has to be taken into account for slabs with an effective depth larger than 220 mm (9 in), as can be estimated from Fig. 42. 35 Fig. 42: Influence of slab thickness on failure stress in slabs without shear reinforcement, Birkle and Dilger (2008). According to Sundquist (2005), no good analysis method has been presented to date that can really explain the size effect. A model developed by Hallgren (1996) was cited, based on fracture mechanics that incorporated the aggregate size. This led to the formula: 3.6 G F 0 1.4 x (SI units) 90 G F 0 889 x (US customary units) ε cTu = ε cTu = Eq. 14 where ε cTu = the ultimate tangential strain, x = the depth of the compression zone in mm (SI units) or in (US customary units), GF0 = the fracture energy equal to 0.025, 0.030, 0.038 for aggregate size da = 8 mm (0.31 in), 16 mm (0.62 in), 32 mm (1.26 in), respectively. With the ultimate tangential strain, the stress distribution in a section at a given location in the critical zone can be calculated. Then the forces are found and the maximum punching force is calculated. The expression in Eq. 14 could be optimized by including information on the concrete properties. Hallgren and Bjerke (2002), however, stated that the influence of tensile strength and fracture energy has been found significant for the size effect in earlier research, but in their research based on non-linear finite element analysis of footings, no significant influence was found. 36 2.8. Influence of restraints Hewitt and Batchelor (1975) stated that restraining forces at the slab boundaries can result from compressive membrane (arch) action as well as from “fixed boundary action” (Fig. 43). The compressive membrane action gives a net in-plane force at the slab boundaries, while fixed boundary action is due to moment restraint with no net in-plane force at the slab boundary. Compressive membrane forces can be induced in a cracked concrete slab but, unlike fixed boundary moments, cannot occur in a slab that is uncracked or made from a material having the same stress-strain relationships in compression and tension. Thus, compressive membrane action can occur in a cracked unreinforced concrete slab, whereas fixed boundary action in a cracked slab requires the provision of tension reinforcement at the boundary. A restrained reinforced slab loaded to its punching load goes through the following stages: fixed boundary action, cracking, compressive membrane action superimposed on fixed boundary action, and finally punching shear failure. Fig. 43: Idealized restrained slabs: forces and stress distributions, Hewitt and Batchelor (1975). The area of the slab beyond the line of contraflexure and external frames enhances the capacity of slabs due to the action of in-plane compression forces. The portion of the slab beyond the line of contraflexure acts as a tension ring which reacts against compressive 37 forces induced in the inner portion of the slab. Hewitt and Batchelor (1975) wrote that the first model which took fixed boundary action into account, was the model developed by Kinnunen and Nylander (1960). Tests carried out by Csagoly (1979) for the Ontaria Ministry of Transportation and Communications also indicated the increase in punching resistance due to membrane action. Very high factors of safety against punching of slabs designed by conventional methods were found. While Hewitt and Batchelor (1975) made a clear distinction between the compressive membrane action and the fixed boundary action, Bakker (2008) and Wei (2008) name the existence of any restraining force “compressive membrane action”. Bakker (2008) studied the influence of the compressive membrane action on the decks of plate-girder bridges. The influence of the compressive membrane action on the punching shear strength is presented in the model shown in Fig. 44. In Fig. 44, the following symbols are used: nr = the dimensionless radial membrane force working on the surface of the failure cone, na = the dimensionless membrane force in the mid-depth of the slab, d1 = the outer diameter of the punched cone, a = the radius of the slab, r(x) = a function of the failure surface over the height, d0 = the length over which the concentrated load is spread, α = the angle between yield surface and displacement rate vector, β = a factor between 0 and 0.5. Fig. 44: Punching shear failure model, taking compressive membrane action into account, Bakker (2008). 38 In this model, the following assumptions are made: the failure mechanism consists of a solid cone-like plug, the compressive membrane force has a constant value, the behavior is rigidly plastic, and the energy in hoop expansion outside the plug is neglected. An upper-bound solution is found by using virtual work theory. The value for na is derived by using the flow theory. The method is suitable for the use with a calculation sheet. Details of the method and an example Maple sheet can be found in Bakker (2008). This method is compared with test results as shown in Table 3. The “analytical” solution is the solution obtained by using the Dutch code NEN 6720. The NEN 6720 takes the critical perimeter at d/2 from the face of the loaded area and calculates the maximum shearing stress. Table 3: Test values with the analytical (Pa), experimental (Pe) and predicted (Pp) solutions, Bakker (2008). Wei (2008) developed a model which considers boundary restraint based on Hallgren’s punching shear model. The dowel effect is ignored in Wei’s model. In Fig. 45, the following symbols are used: T = the inclined compressive force in the compressed conical shell, ∆φ = the central angle, RcT = the horizontal force in the concrete crossing the shear crack, RsT = the horizontal force in the reinforcement crossing the shear crack, RsR = the horizontal force in the reinforcement at right angles to the radial cracks, P = the external load, Fb = the total boundary restraint force, Mb = the boundary restraint moment, B = the diameter of the loading area, xm = the neutral axis depth at mid-span or plastic hinges, c = the diameter of the slab area with negative radial bending moment, xb = the neutral axis depth at the boundary. 39 Fig. 45: Modified Hallgren model considering boundary restraint, Wei (2008). This model led to a set of three kinematic equations, eight constitutive equations in St (lateral stiffness of surrounding structures) and Sφ (rotation stiffness depending on the boundary restraint), and six equilibrium equations. The lateral and rotational stiffness can be found by 40 using the elasticity theory. Results obtained by using this method are compared with test results in Table 4. Table 4: List of test results and calculated results, Wei (2008). 2.9. Influence of the shape of the loaded area According to ASCE-ACI committee 426 (1974), slabs supporting circular columns have greater punching shear resistance than the same slabs supporting square columns. The tire contact area is typically rectangular. Fig. 46 shows slab-column test results for the ultimate shear strength as a function of the column rectangularity. The data suggest a decrease in ultimate shear strength for an increase in rectangularity. Fig. 46: Effect of column rectangularity on shear strength, ASCE-ACI committee 426 (1974). Mitchell, Cook and Dilger (2005) also stated that the normalized shear stress decreases as the column rectangularity increases. Fig. 47 shows the decrease in normalized shear stress for increasing column rectangularity. 41 Fig. 47: Influence of rectangularity of column on shear strength from tests by Hawkins et al. (1971), Leong and Teng (2000) and Oliveira et al. (2004), figure by Mitchell, Cook and Dilger (2005). Sherif, Emara, Ibrahim and Magd (2005) remarked that slab-column specimen test results from the literature indicate an increasingly high concentration of concrete strains towards the corners of the loaded area with an increased column aspect ratio (c1/c2). The results from the literature also indicated that the effect of c1/c2 diminishes for ratios greater than 3. 2.10. Discussion of shear stress theory Alexander and Simmonds (1986) pointed out that the shear stress theory assumes that the vertical load is carried by shear stress on some critical section. The critical section is a vertically oriented surface at some distance from the face of the column or loaded area. The description of a punching failure suggests that it is unlikely that vertical load on a slabcolumn connection is controlled by shear stress on some vertical plane. Shear stress on a vertical plane creates diagonal principal tension and compression stresses which may be regarded as a diagonal tension field. However, diagonal cracking at a relatively early load stage should preclude the tension field. The area of concrete available to participate in the tension field ought to be confined to the uncracked region in the compression zone of the slab at the face of the loaded area. In spite of this, most critical sections are placed at some distance from the column or loaded area and the area of the critical section is based on the depth of the reinforcement rather than the thickness of the compression zone. 42 Another weakness of the shear stress model, as pointed out by Alexander and Simmonds (1986), is the way it accounts for the flexural reinforcement. Some simplified design techniques neglect the flexural reinforcement, and those methods which do not usually assume a smooth distribution of reinforcement. There are three main drawbacks for this idealization. The first reason is that the slab reinforcement is discrete. At collapse, a bar either crosses a failure surface or not. Secondly, reinforcement is often irregularly spaced, making smooth distributions difficult to define. Finally, with design moments and shears based on smoothly distributed reinforcement, there is no clear indication as to where a particular bar is best placed. A last critique on the shear stress theory, as stated by Alexander and Simmonds (1986) is the assumption of a critical section. The shape of the failure surface changes with the ratio of moment to shear. It was suggested to remedy this problem by making the critical section a variable of the model. It is also not clear how to account for slab discontinuities, such as reinforcing bars, which are located at or very near the assumed section. Using a distributed reinforcing ratio is the usual solution to these discontinuities, but this amounts into covering up one inaccuracy with another. Regardless of these three points of critique, the shear stress theory is still the most commonly used method and serves as a basis for the code provisions. The shear stress theory offers an easy way to design structures for shear, but it does not explain the mechanics of the punching shear problem and is, therefore, unable to precisely assess the ultimate strength of existing structures. 43 3. Plate Theory and Finite Elements According to Alexander and Simmonds (1986), plate theory and finite element methods range from simple elastic plate models to sophisticated nonlinear models which account for cracking and plastic behavior. Most models assume that the reinforcement can be described by a thin membrane rather than by discrete bars. 3.1. Material modeling Bakker (2008) used finite element modeling to calculate the ultimate punching strength by using the software DIANA. The cracking model used is the total strain rotating crack model. The total strain crack model describes the tensile and compressive behavior of a material with one stress-strain relationship, and the rotating model calculates the direction of the crack in each load step. Both the brittle and Hordijk tension softening models are used to describe the behavior of concrete in tension (Fig. 48). The ideal plastic model as shown in Fig. 49 is used to describe the concrete in compression. The reinforcement steel is modeled as ideal plastic. Fig. 48: Models for behavior of concrete in tension: brittle and Hordijk tension softening, Bakker (2008). Fig. 49: Ideal plastic model used for concrete in compression, Bakker (2008). 3.2. 3D solids model First a slab (Fig. 50) was modeled using 3D solid elements. The CHX60 element was used (Fig. 51). The slab was modeled using two symmetry lines, resulting in a model of a fourth of the slab using 108 elements with the load applied on 9 elements (Fig. 52). The size of the elements is smaller on the loaded area and larger towards the outer corners. The 44 smallest used element was 2.77mm x 2.77mm x 50mm (0.11in x 0.11in x 1.97in), and the largest element was 75mm x 75mm x 50mm (2.95in x 2.95in x 1.97in). Fig. 50: Dimensions of the 3D solids model. All the edges are clamped and horizontally restrained. Dimensions are in mm, Bakker (2008). Fig. 51: 3D solid element of DIANA software, Bakker (2008). Fig. 52: Model of a slab using 3D solid elements. The load is applied to the red zone. Figure by Bakker, personal communication 07-15-2009 The predicted solution in Fig. 53 is based on the method described in Bakker (2008) and briefly introduced in section 2.8. Model (a) was simply supported and did not take compressive membrane action into account, while model (b) was clamped and laterally 45 restrained and hence took compressive membrane action fully into account. The results of the 3D solids model seemed not to correspond very well to the expected values. Fig. 53: The load-displacement graphs of the 3D solids model, Bakker (2008). 3.3. Axi-symmetric model Another way punching shear strength was studied by Bakker (2008), was by using an axi-symmetric model (Fig. 54). In the axi-symmetric model, CQ16A elements were used (Fig. 55). Note that Fig. 54 shows how the model was built up; the number of elements used in the finite element calculation of the 2D slice was about 500, because the axi-symmetric model does not have a long calculation time. This model was evaluated for the same four cases as the 3D solids model (Fig. 56). The axi-symmetric model with brittle material behavior gave the best results. It also led to a realistic crack pattern (Fig. 57). 46 Fig. 54: Axi-symmetric model, Bakker (2008). Fig. 55: CQ16A element from DIANA (2008), used in the axi-symmetric model by Bakker (2008). 47 Fig. 56: Load-displacement graphs for 4 different models of the axi-symmetric model, Bakker (2008). Fig. 57: Crack pattern just before (loadstep 16) and after (loadstep 17) failure, Bakker (2008). The results of measurements on bridge decks reported by Taylor, Rankin, Cleland and Kirckpatrick (2007) were compared with the deflection results obtained through the finite element modeling. Bakker (2008) reported that the results for the deflections (Table 5) did not match at all with the experimentally found values. Further improvement of the model is needed. 48 Table 5: Comparison of test results reported by Taylor, Ranking, Cleland and Kirckpatrick (2007) and finite element modeling, Bakker (2008). Polak (2005) used layered shell finite elements for punching shear analysis. This finite element type allows for the use of 3D constitutive models. Special attention was given to the formulation of the concrete cracked shear modulus, the calculation of the cracking load and tension stiffening formulations and modeling the dowel action. 3.4. Discussion of plate theory and finite elements solutions Finite element solutions require a very good understanding of the material behavior and the software. The correct material property models have to be selected and implemented. The user needs to be aware of the limitations of the material models, element types and calculation techniques he is using. Even though in previous sections good approximations for the ultimate load were found, none of the consulted literature reported a finite elements model which succeeded to realistically display the behavior from first loading until the ultimate punching shear loading. 49 4. Beam Analogy 4.1. Currently used beam analogy The beam analogy method is described by Park and Gamble (1999). The slab segments adjacent to the loaded area are considered to act as beams running in two directions at right angles as shown in Fig. 58. The slab strips making up the beams are subjected to bending moment, torsional moment and shear force; and redistribution of these actions is able to occur between the beams. Each beam is assumed to be able to develop its ultimate bending moment, torsional moment, and shear force, and interaction effects can be taken into account. The total strength is the sum of the contributions of the strength of the beams. Failure occurs when at least three beams reach their ultimate strength. A detailed description of the method can be found in Park and Gamble (1999). This beam analogy predicts up to eight possible limiting strength combinations of bending, torsion and shear (Fig. 58). The large number of possible limiting strength combinations makes the application relatively difficult. Fig. 58: Limiting strength combinations for beam analogy, Park and Gamble (1999). In a simplified beam analogy model the ultimate strength is obtained as the sum of the flexural, torsional and shear strength of all the beams. Sufficient ductility in bending, torsion and shear to allow the simultaneous development of the ultimate capacities is assumed. Other beam analogies of semi-empirical nature exist. According to Alexander and Simmonds (1986), the differences between the several beam analogies lie largely in the method by which shear and torsional strengths are calculated and in the degree of redistribution allowed between beam elements. 4.2. Design based on the equivalent width of a beam strip Elstner and Hognestad (1956) indicated that the shearing stress 50 v= V bjd Eq. 15 can also be calculated with b the “equivalent width”, the width of a fictitious beam strip of slab across which a concentrated load should be considered as distributed to produce calculated shearing stresses equal to the maximum stress that actually occurs in the slab. To evaluate this procedure, eight beam specimens representing center strips of slabs were tested. They observed that six of the eight beams representing the slabs failed in flexure while the corresponding fully tested slabs failed in shear. This observation led to the conclusion that the behavior of beam strip specimens does not reflect the behavior and mode of failure of a corresponding slab and that beam strips are unsuitable to evaluate the shearing strength of slabs even though they are successfully used to model the flexural behavior of slabs. 4.3. Discussion of beam analogy methods The beam analogy methods lead to an approximate ultimate punching shear load which can be used for design purposes. However, the beam analogy methods are not based upon the mechanics of the punching shear problem and, therefore, are not suitable for the analysis of existing structures. Alexander and Simmonds (1986) pointed out that beam analogy methods, just like the shear stress methods discussed in section 2.10, assume that the vertical load is carried by shear stress on some vertically inclined critical section. Also, the beam analogy methods do not account correctly for the influence of the flexural reinforcement and use the assumption of a critical section, which is the geometry of the beams for the beam analogy. 51 5. Strut and Tie models 5.1. Strut and tie model A more plausible source of shear strength than explained through the shear stress theory and beam analogy, is an inclined compression field in the concrete. Together with steel tension ties, this approach is often referred to as a truss model. Not only does this mechanism provide a load path for shear forces in the presence of diagonal cracking, it explains the role that flexural reinforcement plays in determining shear strength. The variables used in the strut and tie model developed by Alexander and Simmonds (1986) are: the overall geometry of the connection, the concrete strength, the strength of the flexural reinforcement, and the placement of the flexural reinforcement. The strut and tie model, as developed by Alexander and Simmonds (1986), consisted of two types of compression struts: in-plane or anchoring struts (parallel to the slab) and outof plane or shear struts (at some angle (α) to the plane of the slab). The anchoring, in-plane struts are presented in Fig. 59, showing a plane parallel to the plane of the slab. Four anchoring struts are shown. Each is equilibrated by two mutually perpendicular reinforcing bars: one passing through the loaded zone and the other at some distance from the loaded zone. This mechanism gives an explanation for the influence of the flexural reinforcement on the shearing strength: bars at some distance from the loaded zone are able to exert flexural moment. Fig. 59: In-plane or anchoring struts, Alexander and Simmonds (1986). 52 An out-of-plane or shear strut can be compared to the familiar force diagram used in corbel design (Fig. 60). However, there are two differences between the shear struts for slabs and the struts in corbel design. First, the point of load application does not coincide with the junction of the tensile and compressive force, and as a result the angle of inclination of the shear strut, α, is not pre-set. The second difference is that the vertical component of the compression strut is no longer equilibrated at the junction by the applied load. There exists a force component out of the plane of the slab which must be balanced by some form of tension field within the concrete, resulting in a three-dimensional truss. Fig. 60: Comparison of corbel with out-of-plane or shear strut, Alexander and Simmonds (1986). In a slab, the amount of steel participating in the tension ties (called “shear steel”) is not clearly defined. Alexander and Simmonds (1986) assumed that all steel aligned through the loaded zone participates in the tension tie, plus some fraction of the steel within a distance ds (the effective depth) of the face of the loaded zone. This fraction decreases linearly from 1 at the face of the loaded zone to 0 at a distance ds from the face of the loaded zone. Three conditions can lead to failure in the strut and tie model of Alexander and Simmonds (1986): failure of the tension tie, failure of the compression strut, and failure when the out-of-plane component of the compression strut exceeds the confining strength of the slab. 53 The primary assumption in the strut and tie model of Alexander and Simmonds (1986) is that the shear steel will always reach yield, and, therefore, a compression failure never governs. This statement is false for heavily reinforced slabs. The justification for this assumption is that test data have shown that the shear steel yields before failure and that predicting a compression failure requires many assumptions, while a compression failure is not ductile. Therefore a compressive failure mode is precluded rather than described. The ultimate capacity of an in-plane bar-strut unit is limited by the yield of the reinforcing bars. To define the ultimate capacity, the bar force at yield and the angle of the compression strut (α) need to reach a critical value. The parameters which are likely to affect α are assembled in a non-dimensional, empirically determined, term. From geometric considerations, tan(α) equals the ratio of the out-of-plane component (defined by the ability of the slab to confine the bar, function of tributary width of each bar (s), cover (d’) and concrete strength) to the in-plane component (yield force in steel). These observations led to the expression: tan α = K= Pfailure K top ASV fy s eff .d ' . f c' Abar . f y .(c / d s ) 0.25 Eq. 16 where Pfailure = the failure load, ASVtop = the top mat shear steel, fy = the yield strength of the steel, seff = the maximum of s or 3d’, d’ = the cover of the reinforcement measured to the near side of the slab, ds = the cover of the reinforcement measured to the far side of the slab, c = the column dimension perpendicular to the bar being considered, fc’ = the concrete strength, and Abar = the area of a single reinforcing bar. Based on these theoretical considerations, a design equation for α was determined from test results. The data from Fig. 61 led to a design equation: tan α = 1.0 − e −0.85 K (US customary units) tan α = 1.0 − e −2.25 K (SI units) Eq. 17 54 Fig. 61: Calibration of α, Alexander and Simmonds (1986). Alexander and Simmonds (1986) compared this model to test results from the literature. The accuracy of the predicted results depended upon the density of the reinforcement. As can be seen in Fig. 62, for reinforcement ratios of the top shear steel between 1 to 2.5%, an excellent prediction was obtained. In lightly reinforced specimens, strain hardening led to an underestimation of the capacity. In heavily reinforced specimens, the assumption of yielding bars was not always met, and some specimens had a compression failure. In this strut and tie model, f c' is used determine α. A better result could be attained by using the split cylinder tensile strength. The main reason why the split cylinder tensile strength is not used, is the absence of the value of the tensile strength in the tests from the literature that Alexander and Simmonds (1986) used to calibrate the factor α. 55 Fig. 62: Effect of the reinforcement density, Alexander and Simmonds (1986). Alexander and Simmonds (1986) also stated that the truss model is applicable to a wide range of boundary conditions and in-plane forces can be taken into account. The ACI 318-08 and EN 1992-1-1:2004 based the provisions for torsion on the use of a thin-walled tube, space-truss analogy (Fig. 63). The background to the ACI code provisions using a three dimensional truss model is discussed in MacGregor and Ghoneim (1995). Fig. 63: Space truss analogy for torsion, MacGregor and Ghoneim (1995). 56 5.2. Bond model Alexander and Simmonds (1992) developed a bond model in which radial arching action and the concept of a critical shear stress on a critical section are combined. The bond strength of the reinforcement is the significant factor. With the bond model, a simple lower bound estimate of the ultimate punching strength was derived. The bond model is the result of experiments carried out by Alexander and Simmonds after the development of the truss model discussed in the previous section. The tests showed that the radial compression struts are actually curved and parallel to the reinforcement in plan, which changed the mechanics of the truss model. The revised model could be called a “force gradient model for punching shear”. The bond model combines features of the truss model with the concept of a limiting shear stress, thereby explaining why code procedures give good results. The basis of the method is the following expression of the shear force: V= d (Tjd ) d (T ) d ( jd ) = jd + T dx dx dx Eq. 18 in which the first part is carried by beam action (requiring strong bond forces) and the second part by arching action (requiring only remote anchorage of the reinforcement). In Eq. 18 the following parameters are used: T = the steel tension force, jd = the effective moment arm. The geometry of the curved arch (which replaced the compression strut) is not governed by conditions at the intersection of the arch and the reinforcement tying the arch, but rather by the interaction between the arch and the adjacent quadrants of the two-way plate. The radial strips (Fig. 64) extend from the loaded zone, up to a “remote end”, which is a position of zero shear. The shear carried in the radial compression arch varies from a maximum near the loaded zone where the slope of the arch is large, to a minimum at the intersection of the arch and the reinforcing bar, where the slope is small. The shear carried by a radial strip needs to be dissipated some distance away from the loaded area, depending on the curvature of the arch. 57 Fig. 64: Layout of radial strips, Alexander and Simmonds (1992). Fig. 65 describes the radial strip as a cantilever beam. The length l is called the loaded area, and w the uniformly distributed load. For four radial strips extending from the loaded area, a lower bound of the shear capacity is expressed as: P = 8 M sw Eq. 19 Fig. 65: Equilibrium of radial strip, Alexander and Simmonds (1992). The flexural capacity of the strip Ms and the loading term w are consequently defined to meet two conditions: the equilibrium of the strip has to be satisfied and both the flexural capacity and shear capacity of the strip may not be exceeded at any point in the strip. The flexural capacity depends upon the amount of reinforcement that effectively acts within the strip and is composed of the negative and positive moment capacity. 58 M neg = ρ neg f y jd 2 c Eq. 20 M pos = k r ρ neg f y jd 2 c Eq. 21 In these equations, the following symbols are used: ρ neg = AsT bd = the negative effective reinforcing ratio, ρ pos = AsB bd = the positive effective reinforcing ratio, AsT = the total cross-sectional area of top steel within the radial strip plus one-half the area of the first top bar on either side of the strip, AsB = the total cross-sectional area of bottom steel within the radial strip plus one- half the area of the first top bar on either side of the strip, b = the total distance between the first reinforcing bars on either side of the radial strip, d = the effective depth, jd = the internal moment arm, c = the width of the radial strip, fy = the yield stress of the reinforcement, kr = a factor which accounts for the proportion of the bottom steel that can be developed by the rotational restraint at the remote end of the strip. This is zero if the remote end is simply supported. The loading term w represents a lower bound estimate of the maximum shear load that may be delivered to one side of a radial strip by the adjacent quadrant of the two-way plate. Fig. 66 shows any load applied directly to the strip (q) and the internal shears and moments. The near side face of the half-strip is loaded in shear (v), torsion (mt) and bending (mn). Two approximations are made: the direct load (q) and the torsional shear are neglected. The maximum value of the loading term w is based on the maximum value of beam action shear w ACI = 0.166d f c' (SI units) Eq. 22 w ACI = 2d f c' (US customary units) 59 Fig. 66: Free-body diagram of one-half radial strip, Alexander and Simmonds (1992). Fig. 67 shows the predicted failure load compared to 115 test results reported in the literature. The mean value is 1.29. This value is reasonably close to unity, which suggests that the mechanics of the bond model are not unrealistic. The effect of the reinforcement is taken into account by estimating the flexural capacity Ms of the radial strip and, thus, can be combined with an estimate of the one-way shear strength which does not take the reinforcement ratio into account. Fig. 67: Bond model results using ACI one-way shear, Alexander and Simmonds (1992). The bond model also explains how load may be carried in the presence of diagonal cracking. Test results have shown that diagonal cracking occurs at 50 to 70% of the ultimate load. The bond model is limited to plates with a value c/d larger than 0.66. Most practical slabs have a value of c/d larger than 1.5, and, thus, this requirement is not considered as a serious limitation of the bond model. 60 5.3. Discussion of strut and tie models The strut and tie model as developed by Alexander and Simmonds (1986) does not have the weak points which were pointed out in the discussion of the shear stress theory and the beam analogy models. Strut and tie models are successfully used to calculate forces in various types of reinforced concrete structures. Three dimensional strut and tie models are currently used to evaluate torsion and seem to answer several questions regarding the basic mechanics of the punching shear problem. Testing of the strut and tie model developed by Alexander and Simmonds (1986), showed that the compression strut is actually curved. This experimental observation led to the development of the bond model as described by Alexander and Simmonds (1992). The bond model combined elements of the shear stress theory and the truss model, and gave an explanation why code provisions, based on shear stress theory, give results which safely match experimental data. Further research on the bond model could lead to a powerful method to analyze existing structures. 61 6. Code Provisions A good overview of different code provisions is written by Gardner (2005). 6.1. ACI 318-08 The nominal shear strength Vc shall be taken as the smallest of (ACI 318-08 §11.11.2.1, in US customary units): 4 Vc = 2 + λ f c' bo d β Eq. 23 α d Vc = s + 2 λ f c' bo d b0 Eq. 24 Vc = 4λ f c' bo d Eq. 25 in which: f c' = the specified concrete cylinder strength, psi, β = the ratio of the long side to the short side of the column, concentrated load or reaction area, λ = the factor to account for concrete density (1.0 for normal density concrete), bo = the perimeter of the critical section for shear, αs = 40 for interior columns, 30 for edge columns, 20 for corner columns, d = the distance from the extreme compression fiber to the centroid of tensile reinforcement. The critical section is taken at a distance of d/2 away from the periphery of the loaded area. 6.2. EN 1992-1-1: 2004 The critical section is taken at 2d from the loaded area (Fig. 68). Around rectangular loaded areas, rounded corners are used (Fig. 69). 62 Fig. 68: Verification model for punching shear at the ultimate limit state, figure 6.12 from EN 1992-1-1:2004. Fig. 69: Typical basic control perimeters around loaded areas, Figure 6.13 from EN 1992-11: 2004. 63 The design punching shear capacity is calculated as follows (equation 6.47 in the EN 1992-11:2004, in SI units): v Rd ,c = C Rd ,c k (100 ρ l f ck ) 1/ 3 + k1σ cp ≥ (v min + k 1σ cp ) Eq. 26 with fck = the characteristic concrete strength in MPa, 200 ≤ 2,0 d k = 1+ d = the effective depth in mm, ρ l = ρ ly .ρ lz ≤ 0,02 ρly, ρlz relate to the bonded tension steel y- and z-directions respectively. The values ρly and ρlz should be calculated as mean values taking into account a slab width equal to the column width plus 3d each side. σ cp = (σ cy + σ cz ) / 2 σcy, σcz = the normal concrete stresses in the critical section in y- and z-directions (MPa, positive if compression) σ cy = NEd,y, NEd,z N Ed , y Acy and σ cz = N Ed , z Acz = the longitudinal forces across the full bay for internal columns and the longitudinal force across the control section for edge columns. The force may be from a load or prestressing action. Ac = the area of concrete according to the definition of NEd. The values of the next parameters depend on the National Annex. The recommended values are: CRd,c = 0.18/γc with γc=1.5, v min = 0.035k 3 / 2 f ck1 / 2 , k1 = 0.1. 6.3. Comparison of code provisions 6.3.1. Comparison of ACI 318 and EN 1992-1-1 Gardner (2005) compared experimental data with the provisions of ACI 318-05, Fig. 70 and Fig. 71, and EN 1992-1-1:2003, Fig. 72. According to Gardner, comparison of the code provisions with experimental results is not straightforward because the code expressions were developed to be conservative and use specified or characteristic concrete strengths, 64 depending on the code and not the mean concrete strength reported for experimental studies. The code punching shear predictions were calculated using the reported mean concrete cylinder strengths. A second note to the data is that the median thickness of the tested slabs was 140 mm (5.51 in), with a maximum of 320 mm (12.6 in), which is smaller than slabs used in practice. The data (Fig. 70, Fig. 71 and Fig. 72) show that only ACI 318-05 with a rounded shear perimeter meets the criterion of a 5% fractile value greater than one. The results obtained by using EN 1992-1-1:2003 seemed to be unconservative, but the coefficient of variation was smaller than for the results obtained by using ACI 318-05. Fig. 70: Comparison of test/predicted using ACI 318-05 with rounded corners shear perimeter, by Gardner (2005). 65 Fig. 71: Comparison of test/predicted using ACI 318-05 with assumption of square shear perimeter, by Gardner (2005). Fig. 72: Comparison of test/predicted using CEB-FIP MC90 and EN 1992-1-1:2003, by Gardner (2005). Albrecht (2002) remarked that the different code provisions have been derived from tests which take into account the reinforcement practices common in the respective countries. It should be emphasized that design and construction form an integral whole. As an example, Albrecht (2002) points out that the comparatively high punching shear resistance provided by the ACI code should be seen together with the required integrity reinforcement. Integrity reinforcement is continuous reinforcement required in bridge decks to prevent progressive 66 collapse. EN 1992-1-1:2004 §9.10.1 requires that structures, which are not designed to withstand accidental actions should have a suitable tying system to prevent progressive collapse. In practice, this requirement could also result in continuous reinforcement. 6.3.2. Size effect Mitchell, Cook and Dilger (2005) investigated the influence of the size effect. As can be seen in Fig. 73, the code predictions match the test data up to an average effective depth of 300 mm (11.8 in). ACI 318-05 does not have a size factor and overestimates the punching capacity of thicker slabs. The capacity of the 500 mm (19.7 in) thick slab is overestimated by 40%. EN 1992-1-1:2003 has a size factor, but overestimates the capacity of the 500 mm (19.7 in) thick slab by about 20%. Fig. 73: Comparison of code expressions with results reported by Li (2000) from Mitchell, Cook and Dilger (2005). Muttoni (2008) claimed that a failure criterion based on the critical shear crack theory predicts the size effect better than ACI 318, which becomes unconservative for large values of ψd d g0 + d g , as can be seen in Fig. 74. According to Muttoni (2008), there are two explanations for the difference between the test data and the value obtained by using ACI for slabs with a value of ψd d g0 + d g larger than 0.1. When the ACI formula was developed in the 1960s, only tests with relatively small effective depths were available in which the size effect was not apparent. Tests in which punching occurred as a second failure after reaching the flexural capacity are considered in the comparison (empty squares in Fig. 74). 67 Fig. 74: Failure criterion: punching shear strength as function of width of critical shear crack compared with 99 experimental results and ACI 318-05 design equation, Muttoni (2008). 6.3.3. Influence of concrete strength Mitchell, Cook and Dilger (2005) investigated the influence of the concrete strength and compared test results to the code equations. Note that ACI 318 uses a square root of the concrete strength and EN 1992-1-1:2004 a cube root. The authors concluded from Fig. 75 that the EN 1992-1-1 prediction seems to be more conservative than the ACI 318 prediction. This conclusion is only valid for high strength concrete. As seen in section 6.3.1. experimental data indicate that EN 1992-1-1 leads to less conservative results than ACI 318. 68 Fig. 75: Comparison of code expressions with test results reported by Ghannoum (1998) and McHarg et al. (2000), figure by Mitchell, Cook and Dilger (2005). 6.3.4. Influence of reinforcement ratio The ACI 318 code does not take the reinforcement ratio into account, while EN 19921-1 does. Dilger, Birkle and Mitchell (2005) concluded that the reinforcement ratio should be used in the ACI 318 code equations, as gathering test data (Fig. 28, Fig. 29, Fig. 30, Fig. 31 and Fig. 32) showed a distinct decrease in punching shear resistance with decreasing reinforcement ratio. The reinforcement ratio should be calculated in the region where the punching cone occurs. The authors noted that a definition of the extent of this region needs to be developed. Alexander and Hawkins (2005) on the other hand advised not to include the flexural reinforcement ratio in code equations. They pointed out that ACI 318 works as well as any detailed analytical model available for design purposes, with a fraction of the computational effort, provided that the slab has been correctly designed for flexure. The reason is that ACI 318 is based on the work of Moe (1961) (see section 2.1) in which the goal is to prevent punching shear failures prior to developing full flexural strength. As can be seen from Eq. 7 and Eq. 8, the ACI 318 code equation actually comes from an analytical equation that does account for the flexural reinforcement. Alexander and Hawkins (2005) concluded that the scatter of the ACI 318 code equation which is criticized by several authors is, in fact, statistically invalid (Fig. 76). The code equation is intended to handle the case where the 69 flexural and shear strengths match. Specimens designed for higher or lower loads are from other populations. The code equation was never meant to handle these cases; the goal of the code has never been to predict slab-column test results. Fig. 76: Effect of analysis on perceived scatter, Alexander and Hawkins (2005). 70 7. Discussion While the mechanics at the basis of the punching shear problem are still not very well understood, engineers need tools to design and analyze slabs. Several methods have been developed over the years. These methods are typically compared to the results of slabcolumn tests. The behavior of the samples used in these tests is not fully comparable with the behavior of slabs in real buildings or bridge decks. However, due to the high cost of largescale tests, slab-column tests are used to study the effect of several variables on the shear strength of slabs. To design slabs, code provisions have been developed. There are significant differences between the code provisions. Comparing and judging these code equations is hard, as there is not a generally accepted mechanical model representing the behavior of a slab in shear to compare with these code equations. The ACI 318 code provisions for shear in slabs appear to be easier to use for practicing engineers than the EN 1992-1-1 provisions. The influence of several effects has been discussed in the previous sections. The work of Guandalini, Burdet and Muttoni (2009) indicates that ACI 318 might not be conservative for slabs with low reinforcement ratios (ρ < 0.5%), and the work of Muttoni (2008) indicates that ACI 318 might not be conservative for slabs thicker than 300 mm (11.81 in). As Alexander and Hewitt (2005) argued, it might not be needed to add the reinforcement ratio to the code expression because the code expression assures that the slab fails in flexure before punching. To decide whether the punching shear strength needs to be calculated using the square or the cube root of the concrete compressive strength, a better understanding of the behavior of concrete in tension and under splitting is needed. In spite of these drawbacks, the code provisions generally appear to lead to safe designs. To analyze the strength of slabs in existing structures, a good mechanical model is needed. Test results, such as those by Taylor, Rankin, Cleland and Kirckpatrick (2007) and Csagoly (1979) indicate that the shear strength of bridge deck slabs is significantly higher than calculated by the code provisions. This observation is typically contributed to the influence of compressive membrane forces and fixed boundary action. Among the methods that calculate the shear strength using the shear stress on a critical perimeter, recent developments include the critical shear crack theory, which accounts for the size effect, and models which take the fixed boundary action and compressive membrane action into account. All of these models use empirical formulations, and none of them fully explains the mechanics of the punching shear problem. 71 The combination of plate theory and finite element models could give a more realistic assessment of the real punching capacity. In these models, the material behavior can be selected to approach the real material behavior. Results up to now found a good approximation of the ultimate loading as compared to test results. A good model should however reproduce the full behavior of a specimen (such as the load-deflection curves) up to punching failure. Current models do not meet this criterion yet. Beam analogy methods are widely used in the design of slabs in flexure. By combining the effects of flexure, shear and torsion, beam analogy methods can be used to find the ultimate punching strength. However, beam analogy methods do not give a realistic mechanical model of shear in slabs. The truss analogy (strut and tie) method is a different concept and seems to answer some of the fundamental problems of the shear stress and beam analogy methods. Test results indicated that the compression struts have a curved shape, which led to the bond model. The bond model unites the apparently conflicting methods of the truss model and the shear stress method. It might be an interesting method for the analysis of existing structures. Further research on the bond model is needed to verify its applicability. It can be concluded that, even though a large number of methods exist which describe the punching shear problem, none of these methods explains the mechanics at the basis of the punching shear problem. Therefore, semi-experimental formulas have been developed which lead to safe designs for commonly used structures. However, there is a need for an understanding of the mechanics at the basis of the punching shear problem to find the real shear capacity of existing structures. 72 8. Conclusions In previous sections, four methods to find the ultimate punching shear strength in reinforced concrete slabs and punching shear code provisions were discussed. None of the methods is fully theoretical, and test results from slab-column specimens are widely used to determine semi-empirical formulations. The methods based on the shear strength on a critical section are most commonly used in practice. The shear stress on a critical section at a certain distance from the face of the loaded area is compared to a maximum shear stress. The basis for the most commonly used method was provided by Moe (1961). The distance from the face of the loaded area was determined through a statistical analysis of test results and determined to be d/2. Then, a criterion was developed to ensure that slabs would fail in a ductile flexural manner rather than in a usually brittle punching shear manner. Most of the methods based on the shear stress take the concrete strength and/or the flexural reinforcement into account. Other factors, such as the shape of the column or loaded area, size of the loaded area, boundary conditions, load duration, size effect and influence of restraints can be taken into account, but are generally considered of less importance. Muttoni (2008) however argued that the size effect should be taken into account because the ACI code provisions are not conservative for slabs of thickness larger than 300 mm (11.81 in). The critical shear crack theory takes the size effect into account and correctly predicts the ultimate punching shear loading of slab-column specimens with a large thickness. Methods based on plate theory and non-linear finite elements are currently being developed. The difficulty here is to select the appropriate material behavior when modeling a specimen. Methods based on beam analogies are not often used. Accounting for redistribution of forces and interaction between shear, flexure and torsion can approach the behavior of a test specimen, but it does not provide a mechanical model of the shear force in slabs. The strut and tie, truss model uses steel ties and concrete struts and gives a different approach to the shear problem. Additional testing led to the bond model, in which the concrete compression strut is curved and a load gradient is carried along the strut up to a certain point where the internal loading reaches zero. The external loading is calculated on strips extending from the faces of the loaded area. The maximum loading on these strips is taken as the maximum loading per area for a beam given in the ACI code. 73 The provisions of ACI 318 and EN 1992-1-1 appear very different at first sight. These code provisions are, however, based on the same theory, namely the shear stress on a critical perimeter. An obvious difference is the place of the critical perimeter. While ACI 318 takes this critical perimeter at d/2 away from the face of the loaded area and straight around rectangular areas, EN 1992-1-1 takes it at 2d away from the loaded area and uses rounded corners for the perimeters. Another apparent difference is the use of the square root of the concrete strength in ACI 318 and the cube root in EN 1992-1-1. There is no consensus up to now as to which of these is better. While EN 1992-1-1 takes the flexural reinforcement into account, ACI 318 does not use reinforcement ratio in its provisions. Using the flexural reinforcement seems to match the experimental data better, but is not guaranteed to make the code a better design tool. In general, there is a significant distinction between the design practice which needs a good tool to guarantee a safe design on one hand and the analysis practice which needs a model which accurately describes the mechanical behavior of a slab under shear. The first need seems to be satisfied with code provisions that work well in practice. The second need is not fulfilled, as none of the above mentioned models fully explain the behavior of slabs in shear. 74 9. 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Polak, M.A., American Concrete Institute, Farmington Hills, MI, pp. 175-192. Sundquist, H., 2005, “Punching Research at the Royal Institute of Technology (KTH) in Stockholm,” SP-232, Ed. Polak, M.A., American Concrete Institute, Farmington Hills, MI, pp. 229-256. Taylor, S.E., Rankin, B., Cleland, D.J., Kirckpatrick, J., 2007, “Serviceability of bridge deck slabs with arching action,” ACI Structural Journal, V. 104, No. 1, pp. 39-48. Theodorakopoulos, D. D., Swamy, R.N., 2002, “Ultimate punching shear strength analysis of slab-column connections,” Cement & Concrete Composites, V. 24, No. 6, pp. 509-521. Wei, X., 2008, Assessment of Real Loading Capacity of Concrete Slabs, MSc Thesis, Delft University of Technology, Delft, The Netherlands, 112 pp. 77 Appendix A: Notations A.1. List of notations by symbol a radius of the slab (Bakker, 2008) A coefficient, =1 for normal density concrete (Theodorakopoulos and Swamy, 2002) A constant, determined by statistical analysis (Moe, 1961) Abar area of a single reinforcing bar (Alexander and Simmonds, 1986) Ac area of concrete AsB total cross-sectional area of bottom steel within the radial strip plus one-half the area of the first top bar on either side of the strip (Alexander and Simmonds, 1992) AsT total cross-sectional area of top steel within the radial strip plus one-half the area of the first top bar on either side of the strip (Alexander and Simmonds, 1992) ASVtop top mat shear steel (Alexander and Simmonds, 1986) b width of critical section in shear (Moe, 1961) b total distance between the first reinforcing bars on either side of the radial strip (Alexander and Simmonds, 1992) b0 control perimeter at d/2 from the edge of the column (Guandalini, Burdet and Muttoni, 2009) bo perimeter of the critical section at d/2 form the edge of the loaded area B constant, determined by statistical analysis (Moe, 1961) B diameter of the loading area (Wei, 2008) c length of side of loaded area c diameter of the slab area with negative radial bending moment (Wei, 2008) c column dimension perpendicular to the bar being considered (Alexander and Simmonds, 1986) c width of the radial strip (Alexander and Simmonds, 1992) C constant, determined by statistical analysis (Moe, 1961) C1 compressive force above inclined crack (ASCE-ACI Committee 426, 1974) d effective depth of the slab 78 d’ cover of the reinforcement measured to the near side of the slab (Alexander and Simmonds, 1986) d0 length over which the concentrated load is spread (Bakker, 2008) d1 outer diameter of the punched cone (Bakker, 2008) dg maximum size of the aggregate (Guandalini, Burdet and Muttoni, 2009) dg0 reference aggregate size equal to 16mm = 0.63 in (Guandalini, Burdet and Muttoni, 2009) ds cover of the reinforcement measured to the far side of the slab (Alexander and Simmonds, 1986) f2 lateral compressive stresses (Moe, 1961) f3 vertical compressive stresses (Moe, 1961) fc direct compressive stresses (Moe, 1961) fc compressive strength of the concrete (Guandalini, Burdet and Muttoni, 2009) fc’ ultimate concrete strength, cylinder stength fck characteristic concrete strength fcu ultimate concrete strength fs steel stresses in tension (Theodorakopoulos and Swamy, 2002) fs’ steel stresses in compression (Theodorakopoulos and Swamy, 2002) fy yield strength of the steel Fb total boundary restraint force (Wei, 2008) GF0 fracture energy equal to 0.025, 0.030, 0.038 for aggregate size da = 8mm, 16mm, 32 mm respectively (Sundquist, 2005) h thickness of the slab jd moment arm between centre of compression zone and tensile reinforcement k size factor (EN 1992-1-1) kr a factor which accounts for the proportion of the bottom steel that can be developed by the rotational restraint at the remote end of the strip (Alexander and Simmonds, 1992) K constant (Alexander and Simmonds, 1986) mn bending (Alexander and Simmonds, 1992) mt torsion (Alexander and Simmonds, 1992) Mb boundary restraint moment (Wei, 2008) Mneg negative moment capacity 79 Mr radial moment (ASCE-ACI Committee 426, 1974) Mpos positive moment capacity Ms flexural capacity of the strip (Alexander and Simmonds, 1992) Mθ tangential moment (ASCE-ACI Committee 426, 1974) na dimensionless membrane force in the mid depth of the slab (Bakker, 2008) nr dimensionless radial membrane force working on the surface of the failure cone (Bakker, 2008) NEd,y longitudinal force across the full bay for internal columns and the longitudinal force across the control section for edge columns (EN 1992-1-1) NEd,z longitudinal force across the full bay for internal columns and the longitudinal force across the control section for edge columns (EN 1992-1-1) P lower bound for punching shear capacity (Alexander and Simmonds, 1992) P external load (Wei, 2008) Pshear ultimate shear capacity (Elstner and Hognestad, 1956) Pfailure failure load (Alexander and Simmonds (1986) Pflex ultimate flexural capacity of the slab computed by the yield-line theory without regard to a shear failure (Elstner and Hognestad, 1956) q direct load on strip (Alexander and Simmonds, 1992) r side length of loaded area r(x) a function of the failure surface over the height (Bakker, 2008) rs radius of the slab (Guandalini, Burdet and Muttoni, 2009) RcT horizontal force in the concrete crossing the shear crack (Wei, 2008) RsR horizontal force in the reinforcement at right angles to the radial cracks (Wei, 2008) RsT horizontal force in the reinforcement crossing the shear crack (Wei, 2008) s spacing of bars T inclined compressive force in the compressed conical shell (Wei, 2008) T steel force (Alexander and Simmonds 1992) vo vertical shearing stresses (Moe, 1961) v nominal shear stress (Moe, 1961) v2 shearing stress at face of loaded area (Elstner and Hognestad, 1956) vadj adjusted shear strength (Dilger, Birkle and Mitchell, 2005) vtest tested shear strength (Dilger, Birkle and Mitchell, 2005) 80 V shear force (Moe, 1961) Ve shear force at which failure in the compression zone above the inclined cracks occurs (Moe, 1961) Vflex shear force at the ultimate flexural strength (Moe, 1961) Vi shear force at which inclined cracks form (Moe, 1961) Vo fictitious shear strength if bending could be eliminated (Moe, 1961) VR shear strength (Guandalini, Burdet and Muttoni, 2009) wc width of critical shear crack (Guandalini, Burdet and Muttoni, 2009) w loading x depth of the compression zone (Sundquist, 2005) xb neutral axis depth at the boundary (Wei, 2008) xm neutral axis depth at mid-span or plastic hinges (Wei, 2008) Xf depth of critical section for straight flexural crack (Theodorakopoulos and Swamy, 2002) Xs depth of critical section for inclined shear crack (Theodorakopoulos and Swamy, 2002) α punching crack inclination (Menétry, 2002) α angle between yield surface and displacement rate vector (Bakker, 2008) α angle of the compression strut (Alexander and Simmonds, 1986) αs factor, 40 for interior columns, 30 for edge columns, 20 for corner columns (ACI 318) β factor between 0 and 0,5 (Bakker, 2008) β ratio of the long side to the short side of the column, concentrated load or reaction area (ACI 318) ∆φ central angle (Wei, 2008) ε cTu ultimate tangential strain (Sundquist, 2005) εcu ultimate concrete strain (Theodorakopoulos and Swamy, 2002) εo concrete strain at the level of the end of the rectangular stress block (Theodorakopoulos and Swamy, 2002) φo ratio of ultimate shear capacity to ultimate flexural capacity (Moe, 1961) λ factor to account for concrete density (ACI 318) ψ rotation of slab (Guandalini, Burdet and Muttoni, 2009) ρ reinforcement ratio of tensile steel 81 ρ’ reinforcement ratio of compression steel (Theodorakopoulos and Swamy, 2002) ρly bonded tension steel in y-direction (EN 1992-1-1) ρlz bonded tension steel in z-direction (EN 1992-1-1) ρneg negative effective reinforcing ratio ρpos positive effective reinforcing ratio σcy normal concrete stress in the critical section in y-direction σcz normal concrete stress in the critical section in y-direction A.2. Table of notations by parameter Table 6: Overview of the notations by parameter Parameter ACI 318 EN 1992-1-1 Other authors Adjusted shear strength vadj (Dilger, Birkle and Mitchell, 2005) Angle between yield surface and α (Bakker, 2008) displacement rate vector Angle of the compression strut α (Alexander and Simmonds, 1986) Area of concrete Ac Ac Area of single reinforcing bar Abar Bending mn (Alexander and Simmonds, 1992) Bonded tension steel in y-direction ρly Bonded tension steel in z-direction ρlz Boundary restraint moment Mb (Wei, 2008) Central angle ∆φ (Wei, 2008) Characteristic/Nominal compressive fck strength Compressive force above inclined crack C1 (ASCE-ACI 426, 1974) Compressive strength fc (Guandalini, Burdet and Muttoni, 2009) Considered steel in bond model AsB, AsT (Alexander and Simmonds, 1992) Crack width wk wc (Guandalini, Burdet and Muttoni, 2009) Critical perimeter bo u1 b0 Depth of compression reinforcement d’ d’ from extreme compression fibre 82 Depth of compression zone Depth of critical section for inclined shear crack Depth of critical section for straight flexural crack Depth of tensile reinforcement from extreme tension fibre Diameter of critical perimeter c x ds h-d b1, b2 by, bz Diameter of slab with negative radial bending moment Dimensionless membrane force Dimensionless radial membrane force Direct compressive stress Direct load on strip (bond model) Distance between reinforcing bars s w Effective depth External shear force d d Factor to account for concrete density Failure surface over height Fictitious shear strength if bending could be eliminated Flexural capacity of strip (bond model) λ Fracture energy Horizontal force in the concrete crossing the shear crack Horizontal force in the reinforcement at right angles to the radial cracks Horizontal force in the reinforcement crossing the shear crack Inclined compressive force in the compressed conical shell Lateral compressive stress Load Longitudinal force Maximum size of aggregate Moment arm between centre of compression zone and tensile reinforcement Negative effective reinforcing ratio Negative moment capacity Neutral axis depth at boundary Neutral axis depth at mid-span x (Sundquist, 2005) Xs (Theodorakopoulos and Swamy, 2002) Xf (Theodorakopoulos and Swamy, 2002) d1 (Bakker, 2008), B (Wei, 2008) c (Wei, 2008) na (Bakker, 2008) nr (Bakker, 2008) fc (Moe, 1961) q (Alexander and Simmonds, 1992) b (Alexander and Simmonds, 1992) P (Wei, 2008), V (Moe, 1961) r(x) (Bakker, 2008) Vo (Moe, 1961) MS (Alexander and Simmonds, 1992) GF0 (Wei, 2008) RcT (Wei, 2008) RsR (Wei, 2008) RsT (Wei, 2008) T (Wei, 2008) f2 (Moe, 1961) w P jd w NEd,y, NEd,z dg z ρneg Mneg xb (Wei, 2008) xm (Wei, 2008) 83 Nominal shear stress Normal concrete stress in the critical section in y-direction Normal concrete stress in the critical section in y-direction Positive effective reinforcing ratio Positive moment capacity Proportion of bottom steel which can be developed at the end of a strip (bond model) Punching crack inclination Punching shear capacity vn vEd σcy σcz ρpos Mpos kr (Alexander and Simmonds, 1992) Vc θ VEd Radius of the slab r r Ratio of the long side to the short side of the column, concentrated load or reaction area Ratio of ultimate shear capacity to ultimate flexural capacity Reference aggregate size Reinforcement ratio of compression steel Reinforcement ratio of tensile steel Rotation of slab β Radial moment Shear force at the ultimate flexural strength Shear force at which failure in the compression zone above the inclined cracks occurs Shear force at which inclined cracks form Shear steel (truss model) v (Moe, 1961) v2 (Elstner and Hognestad, 1956) α (Menétry, 2002) P (Alexander and Simmonds, 1992), Pshear (Elstner and Hognestad, 1956), Pfailure (Alexander and Simmonds, 1986), VR (Guandalini, Burdet and Muttoni, 2009) Mr (ASCE-ACI 426, 1974) a (Bakker, 2008) rs (Guandalini, Burdet and Muttoni, 2009) φo (Moe, 1961) dg0 ρ’ ρ ρl’ ρl ψ (Guandalini, Burdet and Muttoni, 2009) Vflex (Moe, 1961) Ve (Moe, 1961) Vi (Moe, 1961) Asvtop, ASVbottom (Alexander and Simmonds, 1992) 84 Side length of loaded area (column) c1, c2 Size factor Steel force Steel stress in compression Steel stress in tension Tangential moment c k T (Alexander and Simmonds, 1992) fs’ fs fs2 fs1 Mθ (ASCE-ACI 426, 1974) vtest (Dilger, Birkle and Mitchell, 2005) Tested shear strength Thickness of slab Torsion Total boundary restraint force Ultimate compressive strength Ultimate concrete strain d0 (Bakker, 2008) r h h mt (Alexander and Simmonds, 1992) Fb (Wei, 2008) fc’ fcu εcu2, εcu3 Ultimate flexural capacity calculated with yield line theory Ultimate tangential strain Vertical compressive stress Vertical shearing stress Width of critical section Width of radial strip (bond model) vc b vRd,c ui Yield strength of steel fy fy εcu (Theodorakopoulos and Swamy, 2002) Pflex (Elstner and Hognestad, 1956) ε cTu (Sundquist, 2005) f3 (Moe, 1961) vo (Moe, 1961) b (Moe, 1961) c (Alexander and Simmonds, 1992) 85 View publication stats