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ASD (Steel Beam and Composite Slab)
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Architecture 324
Structures II
Composite Sections and Steel Beam Design
Steel Beam Selection - ASD Composite Sections Analysis Method
University of Michigan, TCAUP Structures II Slide 2/21
Standard section shapes: W wide flange S american standard beam C american standard channel L angle WT or ST structural T Pipe Structural Tubing
Steel W-sections for beams and columns
University of Michigan, TCAUP Structures II Slide 3/21
Source: University of Michigan, Department of Architecture
Columns: Closer to square Thicker web & flange
Beams: Deeper sections Flange thicker than web
Steel W-sections for beams and columns
University of Michigan, TCAUP Structures II Slide 4/21
Source: University of Michigan, Department of Architecture
Source: University of Michigan, Department of Architecture
Columns: Closer to square Thicker web & flange
Beams: Deeper sections Flange thicker than web
Steel W-sections for beams and columns
University of Michigan, TCAUP Structures II Slide 5/21
CC:BY-SA Gregor_y (flickr) http://creativecommons.org/licenses/by-sa/2.0/
Steel Beams by ASD
Yield Stress Values A36 Carbon Steel Fy = 36 ksi A992 High Strength Fy = 50 ksi
Allowable Flexure Stress Fb = 0.66 Fy = Lc
Compact Section
Braced against LTB (l Lu)
Allowable Shear Stress Fv = 0.40 Fy
fv=V/(twd) University of Michigan, TCAUP Structures II Slide 6/21
Source: AISC, Manual of Steel Construction Allowable Stress Design, 9th ed. 1989
Section Modulus Table
Calculate Required Moment Assume Allowable Stress
Fb = 0.66Fy = 24 ksi (A36) Fb = 0.60Fy = 21.6 ksi (A36)
Using the flexure equation, set fb=Fb and solve for S
Choose a section based on S from the table (D-35 and D-36)
Bold faced sections are lighter Fy is the stress up to which the
section is compact ( is ok for all grades of Fy)
University of Michigan, TCAUP Structures II Slide 7/21
Source: Structural Principles, I. Engel 1984
1. Find the Section Modulus for the given section from the tables (D-35 and D-36).
2. Determine the maximum moment equation.
Example Load Analysis of Steel Beam
FindLoadwinKLF
University of Michigan, TCAUP Structures II Slide 8/21
Source: University of Michigan, Department of Architecture
3. Using the flexure equation, fb=Fb, solve for the moment, M.
5. Using the maximum moment equation, solve for the distributed loading, w.
Example Load Analysis cont. W30x116
w=1.28KLF
University of Michigan, TCAUP Structures II Slide 9/21
Source: University of Michigan, Department of Architecture
1. Use the maximum moment equation, and solve for the moment, M.
2. Use the flexure equation to solve for Sx.
Design of Steel Beam Example
University of Michigan, TCAUP Structures II Slide 10/21
Source: University of Michigan, Department of Architecture
3. Choose a section based on Sx from the table (D35 and D36).
4. Most economical section is: W16 x 40 Sx = 64.7 in3
Design of Steel Beam Example
University of Michigan, TCAUP Structures II Slide 11/21
Source: I. Engel, Structural Principles, 1984
5. Add member self load to M and recheck Fb (we skip this step here)
7. Check shear stress: Allowable Stress Fv = 0.40 Fy
Actual Stress fv=V/(twd)
fv Fv
Design of Steel Beam Example
University of Michigan, TCAUP Structures II Slide 12/21
6. Check Deflections calculate actual deflection
compare to code limits
if the actual deflection exceeds the code limit
a stiffer section is needed
Design of Steel Beam Example
University of Michigan, TCAUP Structures II Slide 1335
Source: Standard Building Code, 1991
Composite Design
Steel W section with concrete slab attached by shear studs.
The slab acts as a wider and thicker compression flange.
University of Michigan, TCAUP Structures II Slide 14/21
Source: University of Michigan, Department of Architecture Source: University of Michigan, Department of Architecture
Effective Flange Width Slab on both sides: (Least of the three) Total width: of the beam span Overhang: 8 x slab thickness Overhang: the clear distance to next
beam (i.e. the web on center spacing)
Slab on one side: (Least of the three) Total width: 1/12 of the beam span Overhang: 6 x slab thickness Overhang: the clear distance to next
beam
University of Michigan, TCAUP Structures II Slide 15/21
Source: University of Michigan, Department of Architecture
Source: University of Michigan, Department of Architecture
Analysis Procedure
1. Define effective flange width 2. Calculate n = Ec/Es 3. Transform Concrete width = n bc 4. Calculate Transformed Itr
do NOT include concrete in tension
5. If load is known, calculate stress
or
6. If finding maximum load use allowable stresses. The lesser M will determine which material controls the section.
University of Michigan, TCAUP Structures II Slide 16/21
Given: DLslab = 62.5 psf DLbeam = 135 plf n = 1/9 fsteel = 24 ksi ( Fy = 36 ) fconc = 1.35 ksi
For this example the floor capacity is found for two different floor systems:
1. Find capacity of steel section independent from slab
2. Find capacity of steel and slab as a composite
Non-composite vs. Composite Sections
University of Michigan, TCAUP Structures II Slide 17/21
Source: University of Michigan, Department of Architecture
Find section modulus, Sx in chart.
Assume an allowable stress, Fb. Determine the total moment
capacity of the section, M.
Subtract the DL moment to find the remaining LL moment.
Calculate LL capacity in PSF.
Part 1 Non-composite Analysis
University of Michigan, TCAUP Structures II Slide 18/21
Source: University of Michigan, Department of Architecture
1. Determine effective width of slab. (using 90y92)
2. Find n=Ec/Es (1/9)
3. Draw transformed section (transform the concrete)
4. Calculate Transformed Ix:
Locate neutral axis.
Part 2 - Composite Analysis
University of Michigan, TCAUP Structures II Slide 19/21
Source: University of Michigan, Department of Architecture
Source: University of Michigan, Department of Architecture
4. Calculate Transformed Ix: Use parallel axis theorem.
Ia=Ig+Ad2
Composite Analysis cont.
University of Michigan, TCAUP Structures II Slide 20/21
Source: University of Michigan, Department of Architecture
5. Calculate moment capacity for steel and concrete each assuming full allowable stress level.
6. Choose the smaller moment. It will control capacity.
Composite Analysis cont.
University of Michigan, TCAUP Structures II Slide 21/21
Source: University of Michigan, Department of Architecture
7. Subtract the DL moment to find the remaining LL moment.
8. Calculate the LL in PSF based on the MLL.
Composite Analysis cont.
University of Michigan, TCAUP Structures II Slide 22/21
Source: University of Michigan, Department of Architecture
Source: University of Michigan, Department of Architecture