Given:
Span=20 ft
D.L=8 kips, L.L=24 kips, self weight=not given
(a)
Step 1:
Pu=1.2(8)+1.6(24)
Pu=48 kips
M=48x20/4
M=240 ft-kips
Step 2:
Calculate the section modulus required
Zx=M/(0.9Fy)
Zx=240x12/(0.9x50)
Zx=64 in3
As the self weight is neglected take any flange which will have section modulus greater than 64 in3 and for self weight assume a slightly higher W section
Step 3:
Consider a W18X35 section Zx=66.5 in3
Now verify it for self weight
D.L=35/1000=0.035 kip/ft
Pu=1.2(8.035)+1.6(24)=48.042 ft-kips
M=48.042x20/4=240.21 ft-kips
Zx=240.21x12/(0.9x50)
Zx=64.056 in3 is required section modulus W18X35is safe
(b)
L.L deflection permissilbe=L/360=20x12/360=0.66 in
L.L actual=WL3/48EI
=24x(20x12)3/(48x29000x510)
=0.47 in
Actual is less than permssible so W18X35 satisfies it
(c)
Actual deflection=0.47 in
Permissible=24x12/1000=0.29 in, modify this by selecting a W section having greater moment of inertia
Assume permissilbe=actual and find MOI
L.L deflection=WL3/48EI
0.29=24x(240)3/48x29000xIx
Ix=827 in4
Provide W21X44 section having Ix=843 in4
(d)
Assumptions: Fy=50 ksifor beam, Fy=36 ksi for plate fc=4ksi, 21X44 section
Pu=1.2(0.044+8)+1.6(24)=48.0576
Ru=Pu/2
Ru=24.0288 kips
For web yielding
Rn=(2.5k+N)Fytw
24.0288=(2.5(0.95)+N)x50x0.35
N=negative value, negative value is not possible in dimensions
Provide N=6 in (Assume)
For web crippling
We get same negative value for N
So provide N=4 in
From AISC equation
(0.85fcA)=Ru
0.6x0.85x4xA=24.0288
A=11.77
A=BN
11.7=B(4)
B=3.92 in, provide 4 in, but as the flange width of W21x44 section is 6.5 in, provide 8in, B=8 in
n=B-2k/2
n=8-2(0.95)/2
n=3.05
t=(2.2Run2/BNfy)0.5
t=0.65 in, provide 1 in
Use PL1x4x8
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