01.11.2021 Views

Timothy A. Philpot - Mechanics of materials _ an integrated learning system-John Wiley (2017)

You also want an ePaper? Increase the reach of your titles

YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.

283

C

M = Pe

F

+ =

bENdINg duE TO AN

ECCENTRIC AxIAL LOAd

Internal

axial force

and bending

moment

Uniform

stress due

to axial

force

Stress caused

by bending

moment

FIGURE 8.14 Normal stresses caused by an eccentric axial load.

Complete

stress

distribution

Neutral-Axis Location

Whenever an internal axial force F acts simultaneously with an internal bending moment M,

the neutral axis is no longer located at the centroid of the cross section. In fact, depending

upon the magnitude of the force F, there may be no neutral axis at all. All normal stresses

on the cross section may be either tension stresses or compression stresses. The location of

the neutral axis can be determined by setting σ x = 0 in Equation (8.19) and solving for the

distance y measured from the centroid of the cross section.

Limitations

The stresses determined by this approach assume that the internal bending moment in the

flexural member can be accurately calculated from the original undeformed dimensions. In

other words, the deflections caused by the internal bending moment must be relatively

small. If the flexural member is relatively long and slender, the lateral deflections caused by

the eccentric axial load may significantly increase the eccentricity e, thereby amplifying

the bending moment.

The use of Equations (8.19) and (8.20) should be consistent with Saint-Venant’s

principle. In practice, this condition means that stresses cannot be accurately calculated

near points H and K in Figure 8.13a.

ExAmpLE 8.8

A structural member with a rectangular cross section 10 in. wide by 6 in. deep supports

a 30 kip concentrated load as shown. Determine the distribution of normal

stresses on section a–a of the member.

y

13 in.

30 kips

Plan the Solution

The internal forces acting on section a–a must be determined at the outset. The

principle of equivalent force systems will be used to determine a force and a moment

acting at the section of interest that together are equivalent to the single 30 kip

concentrated load acting on the top of the structural member. Once the equivalent

force and moment have been determined, the stresses produced at section a–a can

be computed.

a

10 in.

a

SolutioN

Equivalent Force and Moment

The cross section of the structural member is rectangular; therefore, by symmetry,

the centroid must be located 5 in. from the left side of the structural

member. The 30 kip concentrated load is located 13 in. from the left side of

z

x

Hooray! Your file is uploaded and ready to be published.

Saved successfully!

Ooh no, something went wrong!