STEEL DESIGN (LOOSELEAF)
STEEL DESIGN (LOOSELEAF)
6th Edition
ISBN: 9781337400329
Author: Segui
Publisher: CENGAGE L
Question
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Chapter 4, Problem 4.7.3P
To determine

(a)

If the compression member is adequate to support the loads using LRFD.

Expert Solution
Check Mark

Answer to Problem 4.7.3P

W12×79 is adequate

Explanation of Solution

Given information:

Dead load,DL=180kips

Live load,LL=320kips

Length of the column,L=28ft

W12×79Kx=1.0Ky=1.0bf=12.1intf=0.735inh/tw=20.7

Steel type=A572

Yield stress=60ksi

Concept used:

Slenderness ratio=KLr

Fe=π2E(KL/r)2

ϕcPn=ϕc×Fcr×Ag

Pu=1.2(DL)+1.6(LL)

KEffective length factorrRadius of gyrationFeBuckling stressFcrCritical stress

EModulus of elasticityPnNominal compressive strengthAgGross areaϕcResistance factor=0.90ΩcSafety factor=1.67

Calculation:

From AISC manual, the radius of gyration for the given material is 5.34 in. and 3.05 in.

KxLrx=1.0×28ft×12in1ft5.34=62.92

KyLry=1.0×16ft×12in1ft3.05=62.95

Taking the higher value of slenderness ratio is 62.95.

Fe=π2E(KL/r)2=π2×29,000(62.95)2=72.23ksi

Check:

4.71EFy=4.7129,00060=103.55

KyLry<4.71EFy62.95<103.55

Use AISC equation 3-2.

Fcr=0.658(Fy/Fe)Fy=0.658(60/72.23)×60=42.38ksi

From AISC manual, the gross area for the given material is 23.2in2.

ϕcPn=ϕc×Fcr×Ag=0.9×42.38×23.2=884.89kips

Check for slender:

λ=bf2tf=12.12×0.735=8.23

λr=0.56EFy=0.5629,00060=12.31

λ<λr8.23<12.31

The flange is non-slender.

λ=htw=20.7

λr=1.49EFy=1.4929,00060=32.76

λ<λr20.7<32.76

The web is non-slender.

Pu=1.2(DL)+1.6(LL)=1.2(180)+1.6(320)=728kips

ϕcPn>Pu884.89kips>728kips

Hence, the section is safe.

Conclusion:

The section W12×79 is adequate.

To determine

(b)

The compression member is adequate to support the loads using ASD.

Expert Solution
Check Mark

Answer to Problem 4.7.3P

W12×79 is adequate

Explanation of Solution

Given information:

Dead load,DL=180kips

Live load,LL=320kips

Length of the column,L=28ft

W12×79Kx=1.0Ky=1.0bf=12.1intf=0.735inh/tw=20.7

Steel type=A572

Yield stress=60ksi

Concept used:

Slenderness ratio=KLr

Fe=π2E(KL/r)2

PnΩc=Fcr×AgΩc

Pa=DL+LL

KEffective length factorrRadius of gyrationFeBuckling stressFcrCritical stress

EModulus of elasticityPnNominal compressive strengthAgGross areaϕcResistance factor=0.90ΩcSafety factor=1.67

Calculation:

From AISC manual, the radius of gyration for the given material is 5.34 in. and 3.05 in.

KxLrx=1.0×28ft×12in1ft5.34=62.92

KyLry=1.0×16ft×12in1ft3.05=62.95

Taking the higher value of slenderness ratio is 62.95.

Fe=π2E(KL/r)2=π2×29,000(62.95)2=72.23ksi

Check:

4.71EFy=4.7129,00060=103.55

KyLry<4.71EFy62.95<103.55

Use AISC equation 3-2.

Fcr=0.658(Fy/Fe)Fy=0.658(60/72.23)×60=42.38ksi

From AISC manual, the gross area for the given material is 23.2in2.

PnΩc=Fcr×AgΩc=42.38×23.21.67=588.75kips

Check for slender

λ=bf2tf=12.12×0.735=8.23

λr=0.56EFy=0.5629,00060=12.31

λ<λr8.23<12.31

The flange is non-slender.

λ=htw=20.7

λr=1.49EFy=1.4929,00060=32.76

λ<λr20.7<32.76

The web is non-slender.

Pa=DL+LL=180+320=500kips

ϕcPn>Pu500kips>588.75kips

Hence, the section is safe.

Conclusion:

The section W12×79 is adequate.

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