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CVENG324:
PRINCIPLES OF STEEL DESIGN
INSTRUCTOR:
ENGR. JOSHUA FERDINAND B. VILLAFUERTE
MODULE 1:
PROPERTIES OF SECTION
PART II
SHAPE
STRUCTURAL
SHAPES
Structural steels are available of many
shapes. The dimension and weight must
be added to the designation to uniquely
identify the shape.
Example:
W 40 x 436
DESIGNATION
Wide Flange Beam
W
American Standard Beam
S
Bearing Piles
HP
Miscellaneous (those that
cannot be classified as W, S, or
HP)
M
Channel
C
Angle
L
Structural Tee (cut from W or S
or M)
Structural Tubing
WT or ST
TS
W-Shape
Pipe
Pipe
Depth = 40 inches (100 mm)
Plate
PL
Weight = 436 lb/ft (640 kg/m)
Bar
Bar
STRUCTURAL STEEL SHAPES
WIDE FLANGE SECTIONS
Designation W (Nominal Depth x Mass per unit length)
W 44 X 290
44 – Nominal depth = 44 inches
290 – Mass per unit length = 290 lb/ft
STRUCTURAL STEEL SHAPES
AMERICAN STANDARD SECTIONS
Designation S (Nominal Depth x Mass per unit length)
S 44 X 290
44 – Nominal depth = 44 inches
290 – Mass per unit length = 290 lb/ft
STRUCTURAL STEEL SHAPES
BEARING PILES
Designation HP (Nominal Depth x Mass per unit length)
HP 44 X 290
44 – Nominal depth = 44 inches
290 – Mass per unit length = 290 lb/ft
STRUCTURAL STEEL SHAPES
MISCELLANEOUS
(those that cannot be classified as W, S, or HP)
Designation M (Nominal Depth x Mass per unit length)
M 44 X 290
44 – Nominal depth = 44 inches
290 – Mass per unit length = 290 lb/ft
STRUCTURAL STEEL SHAPES
CHANNEL SECTIONS
Designation C (Nominal Depth x Mass per unit length)
C 44 X 290
44 – Nominal depth = 44 inches
290 – Mass per unit length = 290 lb/ft
STRUCTURAL STEEL SHAPES
ANGLE SECTIONS
Designation L (Depth x Base x Thickness)
𝟏
πŸ–
L8x8x1
8 – Depth
8 – Base
1
1 - Thickness
8
STRUCTURAL STEEL SHAPES
DOUBLE ANGLE SECTIONS
Designation L (Deepth x Base x Thickness)
L8x8x1
𝟏
πŸ–
8 – Depth
8 – Base
1
8
1 - Thickness
STRUCTURAL STEEL SHAPES
DOUBLE ANGLE SECTIONS
Designation L (Depth x Base x Thickness)
L8x8x1
𝟏
πŸ–
8 – Depth
8 – Base
1
8
1 - Thickness
STRUCTURAL STEEL SHAPES
DOUBLE ANGLE SECTIONS
Designation L (Depth x Base x Thickness)
L8x8x1
𝟏
πŸ–
8 – Depth
8 – Base
1
8
1 - Thickness
STRUCTURAL STEEL SHAPES
STRUCTURAL TEE SECTIONS
(cut from W shapes)
Designation WT (Nominal Depth x Mass per unit length)
WT 44 X 290
44 – Nominal depth = 44 inches
290 – Mass per unit length = 290 lb/ft
STRUCTURAL STEEL SHAPES
STRUCTURAL TEE SECTIONS
(cut from M shapes)
Designation MT (Nominal Depth x Mass per unit length)
WT 44 X 290
44 – Nominal depth = 44 inches
290 – Mass per unit length = 290 lb/ft
STRUCTURAL STEEL SHAPES
STRUCTURAL TEE SECTIONS
(cut from S shapes)
Designation ST (Nominal Depth x Mass per unit length)
ST 44 X 290
44 – Nominal depth = 44 inches
290 – Mass per unit length = 290 lb/ft
STRUCTURAL STEEL SHAPES
COMBINATION SECTIONS
W SHAPES AND CHANNELS
STRUCTURAL STEEL SHAPES
COMBINATION SECTIONS
S SHAPES AND CHANNELS
STRUCTURAL STEEL SHAPES
COMBINATION SECTIONS
TWO CHANNELS
STRUCTURAL STEEL SHAPES
COMBINATION SECTIONS
CHANNELS AND ANGLES
(Long leg of angle turned out)
STRUCTURAL STEEL SHAPES
COMBINATION SECTIONS
CHANNELS AND ANGLES
(Short leg of angle turned out)
STRUCTURAL STEEL SHAPES
STRUCTURAL STEEL SHAPES
SAMPLE PROBLEM # 4:
MAY 2014 CE BOARD EXAM PROBLEM
A built-up steel beam composed of an W shape (W 21 x 83) and a channel (C 15 x 50) bolted together as
shown is subjected to a moving concentrated load P. The beam carries a 100-mm-thick concrete slab having an
effective width of 1.50 m. Determine the properties of the composite section.
Y
π‘¨πŸ
π‘¨πŸ
𝐻 = 𝑑(π‘€π‘ β„Žπ‘Žπ‘π‘’) + 𝑑𝑀(π‘β„Žπ‘Žπ‘›π‘›π‘’π‘™)
𝐻 = 544.30 π‘šπ‘š + 18.20 π‘šπ‘š
𝑯 = πŸ“πŸ”πŸ. πŸ“πŸŽ π’Žπ’Ž
π΄π‘β„Žπ‘Žπ‘›π‘›π‘’π‘™ = 9,484 π‘šπ‘š2
π‘¦π‘β„Žπ‘Žπ‘›π‘›π‘’π‘™ = 20.27 π‘šπ‘š
𝐴𝑀𝑓 = 15,677.00 π‘šπ‘š2
π‘‘π‘€π‘ β„Žπ‘Žπ‘π‘’ = 544.30 π‘šπ‘š
X
π΄π‘‘π‘œπ‘‘π‘Žπ‘™ = π΄π‘β„Žπ‘Žπ‘›π‘›π‘’π‘™ + 𝐴𝑀𝑖𝑑𝑒 π‘“π‘™π‘Žπ‘›π‘”π‘’
π΄π‘‘π‘œπ‘‘π‘Žπ‘™ = 9,484 π‘šπ‘š2 + 15,677.00 π‘šπ‘š2
𝑨𝒕𝒐𝒕𝒂𝒍 = πŸπŸ“, πŸπŸ”πŸ π’Žπ’ŽπŸ
Centroid from the Y-axis:
𝑿𝒄 = ?
π΄π‘‘π‘œπ‘‘π‘Žπ‘™ 𝑋𝑐 = σ(𝐴 π‘₯ 𝑋)
π΄π‘‘π‘œπ‘‘π‘Žπ‘™ 𝑋𝑐 = π΄π‘β„Žπ‘Žπ‘›π‘›π‘’π‘™ π‘‹π‘β„Žπ‘Žπ‘›π‘›π‘’π‘™ + 𝐴𝑀𝑖𝑑𝑒 π‘“π‘™π‘Žπ‘›π‘”π‘’ 𝑋𝑀𝑖𝑑𝑒 π‘“π‘™π‘Žπ‘›π‘”π‘’
𝑿𝒄 = 𝟎
Centroid from the X-axis:
𝒀𝒄 = ?
π΄π‘‘π‘œπ‘‘π‘Žπ‘™ π‘Œπ‘ = σ(𝐴 π‘₯ π‘Œ)
π΄π‘‘π‘œπ‘‘π‘Žπ‘™ π‘Œπ‘ = π΄π‘β„Žπ‘Žπ‘›π‘›π‘’π‘™ π‘Œπ‘β„Žπ‘Žπ‘›π‘›π‘’π‘™ + 𝐴𝑀𝑖𝑑𝑒 π‘“π‘™π‘Žπ‘›π‘”π‘’ π‘Œπ‘€π‘–π‘‘π‘’ π‘“π‘™π‘Žπ‘›π‘”π‘’
(25,161 π‘šπ‘š2 )(π‘Œπ‘ ) = 9,484 π‘šπ‘š2 (20.27 π‘šπ‘š)
544.30
+ 15,677.00 π‘šπ‘š2 ( 2 π‘šπ‘š + 18.20 π‘šπ‘š)
𝒀𝒄 = πŸπŸ–πŸ–. πŸ“πŸ“ π’Žπ’Ž
Y
π‘¨πŸ
Distance of the Centroid of Area 1 and Area 2 from the
Geometric Center:
π‘Œπ‘β„Žπ‘Žπ‘›π‘›π‘’π‘™
𝒀𝒄
π‘‘π‘€π‘ β„Žπ‘Žπ‘π‘’
2
NA of Channel
π’…πŸ
X
π’…πŸ
π‘¨πŸ
NA of W shape
π‘‘π‘€π‘ β„Žπ‘Žπ‘π‘’
π’…π’šπŸ = π‘Œπ‘ − π‘Œπ‘β„Žπ‘Žπ‘›π‘›π‘’π‘™
π’…π’šπŸ =
𝑑𝑦1 = 188.55 π‘šπ‘š − 20.27 π‘šπ‘š
𝑑𝑦2 =
π’…π’šπŸ = πŸπŸ”πŸ–. πŸπŸ– π’Žπ’Ž
π’…π’šπŸ = 𝟏𝟎𝟏. πŸ–πŸŽ π’Žπ’Ž
2
544.30
2
+ 𝑑𝑀 − π‘Œπ‘
π‘šπ‘š + 18.20 − 188.55π‘šπ‘š
Moment of Inertia with respect to X-axis:
𝐼π‘₯ = ෍(𝐼𝑔π‘₯ + 𝐴𝑑 2 )
𝐼π‘₯ = 𝐼𝐢𝑔𝑦 + 𝐴𝐢 (𝑑1 )2 + (πΌπ‘Šπ‘”π‘₯ + π΄π‘Š (𝑑2 )2 )
𝒀𝒄 = πŸπŸ–πŸ–. πŸ“πŸ“ π’Žπ’Ž
𝑨𝒕𝒐𝒕𝒂𝒍 = πŸπŸ“, πŸπŸ”πŸ π’Žπ’ŽπŸ
𝑿𝒄 = 𝟎
𝒀𝒄 = πŸπŸ–πŸ–. πŸ“πŸ“ π’Žπ’Ž
𝐼π‘₯ = [4.579π‘₯106 π‘šπ‘š4 + 9,484 π‘šπ‘š2 168.28 π‘šπ‘š 2 ]
+[761.704π‘₯106 π‘šπ‘š4 + 15,677 π‘šπ‘š2 101.80 π‘šπ‘š 2 ]
𝑰𝒙 = 𝟏, πŸπŸ—πŸ•. πŸ‘πŸπ’™πŸπŸŽπŸ” π’Žπ’ŽπŸ’
Moment of Inertia with respect to Y-axis:
𝐼𝑦 = ෍(𝐼𝑔𝑦 + 𝐴𝑑 2 )
𝐼𝑦 = 𝐼𝐢𝑔π‘₯ + 𝐴𝐢 (𝑑π‘₯1 )2 + (πΌπ‘Šπ‘”π‘¦ + π΄π‘Š (𝑑π‘₯2 )2 )
𝐼𝑦 = 168.157π‘₯106 π‘šπ‘š4 + 0 + 33.881π‘₯106 π‘šπ‘š4 + 0
π‘°π’š = 𝟐𝟎𝟐. πŸŽπŸ‘πŸ–π’™πŸπŸŽπŸ” π’Žπ’ŽπŸ’
Y
π‘¨πŸ
X
Polar Moment of Inertia with respect to X and Y axes, JO :
𝑱𝑢 = 𝑰 𝑿 + 𝑰 𝒀
𝐽𝑂 = 1,197.32 π‘₯ 106 +𝟐𝟎𝟐.πŸŽπŸ‘πŸ– π‘₯ 106
π‘¨πŸ
𝑱𝑢 = πŸπŸ‘πŸ—πŸ—. πŸ‘πŸ“πŸ– 𝒙 πŸπŸŽπŸ” π¦π¦πŸ’
Radius of Gyration, 𝒓𝒙 𝐚𝐧𝐝 π’“π’š
𝑨𝒕𝒐𝒕𝒂𝒍 = πŸπŸ“, πŸπŸ”πŸ π’Žπ’ŽπŸ
𝑿𝒄 = 𝟎
𝒀𝒄 = πŸπŸ–πŸ–. πŸ“πŸ“ π’Žπ’Ž
𝑰𝒙 = 𝟏, πŸπŸ—πŸ•. πŸ‘πŸπ’™πŸπŸŽπŸ” π’Žπ’ŽπŸ’
π‘°π’š = 𝟐𝟎𝟐. πŸŽπŸ‘πŸ–π’™πŸπŸŽπŸ” π’Žπ’ŽπŸ’
𝒓𝒙 =
𝑰𝒙
𝑨
π‘Ÿπ‘₯ =
1,197.32π‘₯106 π‘šπ‘š4
25,161 π‘šπ‘š2
𝒓𝒙 = πŸπŸπŸ–. πŸπŸ’ 𝐦𝐦
π’“π’š =
π‘°π’š
𝑨
π‘Ÿπ‘¦ =
202.038π‘₯106 π‘šπ‘š4
25,161 π‘šπ‘š2
π’“π’š = πŸ–πŸ—. πŸ”πŸ 𝐦𝐦
Y
π‘¨πŸ
𝑯 = πŸ“πŸ”πŸ. πŸ“πŸŽ π’Žπ’Ž
π‘¨πŸ
X
Section Modulus, 𝑺𝒙 𝐚𝐧𝐝 π‘Ίπ’š
𝐼π‘₯
𝑆π‘₯ =
𝑐
1,197.32π‘₯106 π‘šπ‘š4
𝑆π‘₯ =
562.50 π‘šπ‘š − 188.55 π‘šπ‘š
𝑺𝒙 = πŸ‘. πŸπŸŽπŸπŸ– 𝐱 πŸπŸŽπŸ” π¦π¦πŸ‘
𝑨𝒕𝒐𝒕𝒂𝒍 = πŸπŸ“, πŸπŸ”πŸ π’Žπ’ŽπŸ
𝑿𝒄 = 𝟎
𝒀𝒄 = πŸπŸ–πŸ–. πŸ“πŸ“ π’Žπ’Ž
𝑰𝒙 = 𝟏, πŸπŸ—πŸ•. πŸ‘πŸπ’™πŸπŸŽπŸ” π’Žπ’ŽπŸ’
π‘°π’š = 𝟐𝟎𝟐. πŸŽπŸ‘πŸ–π’™πŸπŸŽπŸ” π’Žπ’ŽπŸ’
𝑆𝑦 =
𝐼𝑦
𝑐
202.038π‘₯106 π‘šπ‘š4
𝑆𝑦 =
381
π‘šπ‘š
2
π‘Ίπ’š = 𝟏. πŸŽπŸ”πŸπ’™πŸπŸŽπŸ” π¦π¦πŸ‘
SAMPLE PROBLEM # 5:
Determine the properties of the double angle shown in the figure. The section is
made of 2L150 x 90 x 12 with long legs back-to-back and spacing s = 6mm.
B = 90 mm
B = 90 mm
X = 21.16 mm
X = 21.16 mm
π΄π‘‘π‘œπ‘‘π‘Žπ‘™ = 𝐴1 + 𝐴2
π΄π‘‘π‘œπ‘‘π‘Žπ‘™ = 2 π‘₯ (2,751.45 π‘šπ‘š2 )
𝑨𝒕𝒐𝒕𝒂𝒍 = πŸ“, πŸ“πŸŽπŸ. πŸ—πŸŽ π’Žπ’ŽπŸ
Y = 50.82 mm
H = 150 mm
𝐈𝐱 = ?
𝐼π‘₯ = 2 π‘₯ (6.273π‘₯106 π‘šπ‘š4 )
𝑰𝒙 = 𝟏𝟐. πŸ“πŸ’πŸ”π’™πŸπŸŽπŸ” π’Žπ’ŽπŸ’
𝐼𝑦 = ෍(𝐼𝑔𝑦 + 𝐴𝑑 2 )
𝐼𝑦 = 2 π‘₯ (𝐼𝑔𝑦 + 𝐴(𝑑)2 )
𝐼𝑦 = 2 π‘₯ (1,708,656.95 π‘šπ‘š4 + (2,751.45 π‘šπ‘š2 )(21.16π‘šπ‘š + 3π‘šπ‘š)2 )
s = 6mm
π‘°π’š = πŸ”, πŸ”πŸπŸ—, πŸ‘πŸ–πŸ• π’Žπ’ŽπŸ’
π΄π‘‘π‘œπ‘‘π‘Žπ‘™ = 5,502.90 π‘šπ‘š2
𝐼π‘₯ = 12.546π‘₯106 π‘šπ‘š4
𝐼𝑦 = 6.629π‘₯106 π‘šπ‘š4
Polar Moment of Inertia
with respect to X and Y axes, JO :
B = 90 mm
B = 90 mm
X = 21.16 mm
𝑱𝑢 = 𝑰𝑿 + 𝑰𝒀
X = 21.16 mm
π½π‘œ = 12.546π‘₯106 π‘šπ‘š4 + 6.629π‘₯106 π‘šπ‘š4
𝑱𝑢 = πŸπŸ—. πŸπŸ•πŸ“π±πŸπŸŽπŸ” π¦π¦πŸ’
Section Modulus, 𝑺𝒙 𝐚𝐧𝐝 π‘Ίπ’š
12.546π‘₯106 π‘šπ‘š4
𝐼π‘₯
=
𝑆π‘₯ =
150 π‘šπ‘š − 50.82 π‘šπ‘š
𝑐
Y = 50.82 mm
H = 150 mm
𝐼𝑦
𝑆𝑦 =
𝑐
6.629π‘₯106 π‘šπ‘š4
=
90 π‘šπ‘š + 3π‘šπ‘š
= πŸπŸπŸ”, πŸ’πŸ—πŸ• π¦π¦πŸ‘
= πŸ•πŸ, πŸπŸ–πŸŽ π¦π¦πŸ‘
Radius of Gyration, 𝒓𝒙 𝐚𝐧𝐝 π’“π’š
𝒓𝒙 =
s = 6mm
π’“π’š =
𝑰𝒙
𝑨
π‘°π’š
𝑨
=
12.546π‘₯106 π‘šπ‘š4
5,502.90 π‘šπ‘š2
= πŸ’πŸ•. πŸ•πŸ’πŸ– 𝐦𝐦
=
6.629π‘₯106 π‘šπ‘š4
5,502.90 π‘šπ‘š2
= πŸ‘πŸ’. πŸ•πŸŽπŸ— 𝐦𝐦
SEATWORK # 1:
Y
X
NOVEMBER 2013 CE BOARD EXAM QUESTION:
The deck of a bridge consist of ribbed metal deck with 100
mm concrete slab on top. The superstructure supporting the
deck is made of wide flange steel beams strengthened by
cover plate 16 mm x 260 mm one at a top and one at the
bottom.
Properties of W 850 x 185:
A = 23,750 π‘šπ‘š2
d = 850 mm
π‘π‘“π‘™π‘Žπ‘›π‘”π‘’ = 290 π‘šπ‘š
π‘‘π‘“π‘™π‘Žπ‘›π‘”π‘’ = 20 π‘šπ‘š
𝑑𝑀𝑒𝑏 = 15 mm
𝐼π‘₯ = 2,662 π‘₯ 106 π‘šπ‘š4
𝐼𝑦 = 81.52 π‘₯ 106 π‘šπ‘š4
Determine the following:
a. Moment of Inertia along X and Y axes.
b. Polar Moment of Inertia with respect to X and Y axes.
c. Section Modulus, 𝑆π‘₯ and 𝑆𝑦
d. Radius of Gyration, π‘Ÿπ‘₯ and π‘Ÿπ‘¦
SEATWORK # 1:
Y
MAY 2015 CE BOARD EXAM QUESTION:
The column shown in the figure is made from four 300 mm x
16 mm A36 Steel.
Determine the following:
a. Moment of Inertia along X and Y axes.
b. Polar Moment of Inertia with respect to X and Y axes.
c. Section Modulus, 𝑆π‘₯ and 𝑆𝑦
d. Radius of Gyration, π‘Ÿπ‘₯ and π‘Ÿπ‘¦
X
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