STEEL DESIGN (LOOSELEAF)
STEEL DESIGN (LOOSELEAF)
6th Edition
ISBN: 9781337400329
Author: Segui
Publisher: CENGAGE L
Question
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Chapter 5, Problem 5.5.15P
To determine

(a)

Whether a W24×104 of A992 steel for the given beam by using LRFD

Expert Solution
Check Mark

Answer to Problem 5.5.15P

Inadequate

Explanation of Solution

Given:

A992 steel

STEEL DESIGN (LOOSELEAF), Chapter 5, Problem 5.5.15P , additional homework tip  1

Formula used:

Mn=Cb[Mp(Mp0.7FySx)(LbLpLrLp)]Mp

Mn is nominal moment strength

Mp is plastic moment capacity

Sx is Elastic section modulus about X -axis

Lp is unbraced length in an inelastic behavior

Lr is unbraced length in an elastic behavior

Cb=12.5Mmax2.5Mmax+3MA+4MB+3MC

Cb is factor to account for non- uniform bending within the unbraced length

Mmax is absolute value of the maximum moment within the unbraced length

MA is absolute value of the moment at the quarter point of the unbraced length

MB is absolute value of the moment at the midpoint of the unbraced length

MC is absolute value of the moment at the three- quarter point of the unbraced length

Calculation:

Determine the nominal flexural strength:

From the Zx table,

Lp=10.3ftLr=29.2ft

For Lb=20ft, Lp<Lb<Lr

This shape is compact because there is no footnote in the dimensions and properties tables to indicate otherwise.

Since Lp<Lb<Lr,

Mn=Cb[Mp(Mp0.7FySx)(LbLpLrLp)]Mp (Inelastic Lateral torsional buckling)

Mp=FyZx=50(289)=14450inkips=1204.167ftkips

Mn=Cb[14450(144500.7(50)(258))(2010.329.210.3)]=Cb(9815.56)

Determine the factored point loads:

Pu=1.2PD+1.6PL

D is dead point load and L is live point load

Pu=1.2(12)+1.6(36)=72kips

Determine the factored distributed loads:

wu=1.2wD+1.6wL

wD is uniformly distributed dead load and wL is uniformly distributed live load

wu=1.2(1+.104)+1.6(3)=6.125kips/ft

Determine the beam reactions:

RA+RB=72+6.125×30=255.75kMA=0RB×3072×106.125×30×15=0RB=115.875kRA=255.75k115.875k=139.875k

STEEL DESIGN (LOOSELEAF), Chapter 5, Problem 5.5.15P , additional homework tip  2

STEEL DESIGN (LOOSELEAF), Chapter 5, Problem 5.5.15P , additional homework tip  3

Mu=139.875(11.08)72(11.0810)6.125(11.0822)=1096.08ftkips

Compute Cb :

Mmax=Mu=1096.08ftkipsMA=139.875(15)6.125(1522)72(1510)=1049.06ftkipsMB=139.875(20)6.125(2022)72(2010)=852.5ftkipsMC=139.875(25)6.125(2522)72(2510)=502.81ftkipsCb=12.5Mmax2.5Mmax+3MA+4MB+3MC=12.5(1096.08)2.5(1096.08)+3(1049.06)+4(852.5)+3(502.81)=1.268Mn=Cb(9815.56)=1.268(9815.56)=12446.13inkips<Mp=14450inkipsϕbMn=0.9(12446.13)=11201.517inkips=933.46ftkips

Since Mu=1096.08ftkips>ϕbMn=933.46ftkips, W24×104 is not adequate.

Conclusion:

W24×104 of A992 steel for the given beam is not adequate.

To determine

(b)

Whether a W24×104 of A992 steel for the given beam by using ASD

Expert Solution
Check Mark

Answer to Problem 5.5.15P

Inadequate

Explanation of Solution

Given:

A992 steel

STEEL DESIGN (LOOSELEAF), Chapter 5, Problem 5.5.15P , additional homework tip  4

Formula used:

Mn=Cb[Mp(Mp0.7FySx)(LbLpLrLp)]Mp

Mn is nominal moment strength

Mp is plastic moment capacity

Sx is Elastic section modulus about X -axis

Lp is unbraced length in an inelastic behavior

Lr is unbraced length in an elastic behavior

Cb=12.5Mmax2.5Mmax+3MA+4MB+3MC

Cb is factor to account for non- uniform bending within the unbraced length

Mmax is absolute value of the maximum moment within the unbraced length

MA is absolute value of the moment at the quarter point of the unbraced length

MB is absolute value of the moment at the midpoint of the unbraced length

MC is absolute value of the moment at the three- quarter point of the unbraced length

Calculation:

Determine the nominal flexural strength:

From the Zxtable,

Lp=10.3ftLr=29.2ft

For Lb=20ft, Lp<Lb<Lr

This shape is compact because there is no footnote in the dimensions and properties tables to indicate otherwise.

Since Lp<Lb<Lr,

Mn=Cb[Mp(Mp0.7FySx)(LbLpLrLp)]Mp (Inelastic Lateral torsional buckling)

Mp=FyZx=50(289)=14450inkips=1204.167ftkips

Mn=Cb[14450(144500.7(50)(258))(2010.329.210.3)]=Cb(9815.56)

Determine the factored point loads:

Pa=PD+PL

PD is dead point load and PL is live point load

Pu=12+36=48kips

Determine the factored distributed loads:

wu=wD+wL

wD is uniformly distributed dead load and wL is uniformly distributed live load

wa=(1+.104)+3=4.104kips/ft

Determine the beam reactions:

RA+RB=48+4.104×30=171.12kMA=0RB×3048×104.104×30×15=0RB=77.56kRA=171.12k77.56k=93.56k

STEEL DESIGN (LOOSELEAF), Chapter 5, Problem 5.5.15P , additional homework tip  5

STEEL DESIGN (LOOSELEAF), Chapter 5, Problem 5.5.15P , additional homework tip  6

Mu=93.56(11.101)48(11.10110)4.104(11.10122)=732.89ftkips

Compute Cb :

Mmax=Mu=732.89ftkipsMA=93.56(15)48(1510)4.104(1522)=701.7ftkipsMB=93.56(20)48(2010)4.104(2022)=570.4ftkipsMC=93.56(25)48(2510)4.104(2522)=336.5ftkipsCb=12.5Mmax2.5Mmax+3MA+4MB+3MC=12.5(732.89)2.5(732.89)+3(701.7)+4(570.4)+3(336.5)=1.267Mn=Cb(9815.56)=1.267(9815.56)=12439.995inkips<Mp=14450inkipsMnΩb=12439.9951.67=7449.0988inkips=620.76ftkips

Since Mu=732.89ftkips>ϕbMn=620.76ftkips, W24×104 is not adequate.

Conclusion:

W24×104 of A992 steel for the given beam is not adequate.

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STEEL DESIGN (LOOSELEAF)

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