MECHANICS OF MATERIALS
MECHANICS OF MATERIALS
11th Edition
ISBN: 9780137605521
Author: HIBBELER
Publisher: RENT PEARS
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Chapter 13, Problem 1RP

The wood column has a thickness of 4 in. and a width of 6 in. Using the NFPA equations of Sec.13.6 and Eq.13-30, determine the maximum allowable eccentric load P that can be applied. Assume that the column is pinned at both its top and bottom.

Chapter 13, Problem 1RP, The wood column has a thickness of 4 in. and a width of 6 in. Using the NFPA equations of Sec.13.6

R13−1

Expert Solution & Answer
Check Mark
To determine
The value of maximum allowable eccentric load on the column.

Answer to Problem 1RP

The maximum allowable eccentric load on the column is 5.76kip_.

Explanation of Solution

Given information:

The load applied on the wooden column is P.

The column is pinned at both the ends.

The width of cross-sectional area of the column is b=6in.

The depth of cross-sectional area of the column is d=4in.

The length of the column is L=10ft.

Show the expression ofNFPA Equation of Sec 13.6 as follows:

(σa)allow=[540(KLd)2]ksi,26<KLr<50

Here, (σa)allow is the allowable stress and (KLd) is the slenderness ratio.

Show the expression for Equation 13-30 as follows:

σmax=PA+McI

Here, σmax is the maximum compressive stress, P is the load, A is the cross-sectional area, M is the moment, c is the distance between the centroid of member and outer fiber, and I is the moment of inertia.

Calculation:

Calculate the cross-sectional area (A) of the rectangular column using the relation:

A=bd (1)

Substitute 3in. for b and 6in. for d in Equation (1):

A=4×6=24in.2

Calculate the moment of inertia using the relation:

I=bd312 (2)

Substitute 6in. for b and 4in. for d in Equation (2):

I=6×4312=32in.4

The ends of the column are pinned. Thus, the value of K=1.

Calculate the value of (KLd) as follows:

Substitute 1 for K and 3in. for d.

(KLd)=(1×10ft×12in1ft4in.)=(120in.4in.)=30

The value of (KLd) lies between 26 and 50.

Show the expression of NFPA Equation of Sec 13.6 as follows:

(σa)allow=[540(KLd)2]ksi,26<KLd<50 (3)

Here, (σa)allow is the allowable stress and (KLr) is the slenderness ratio.

Substitute 30 for (KLd) in Equation (3).

(σa)allow=[540(30)2]ksi=[540900]ksi=0.6ksi

Show the expression for Equation 13-30 as follows:

σmax=PA+McIσmax=PA+(Pe)cI (4)

Here, σmax is the maximum compressive stress, P is the load, A is the area, M is the moment, c is the distance between the centroid of member and outer fiber, and I is the moment of inertia.

The eccentricity (e) of the load is 1in.

Calculate the value of c using the relation:

c=d2

Substitute 4in. for d.

c=42=2in.

Substitute 0.6ksi for (σa)allow, 24in.2 for A,1in. for e, 2in. for c, 32in.4 for I in Equation (4).

σallow=σmax0.6=P24+P×1×232=32P+24×P×1×224×32=32P+48P24×32

0.6=80P768=0.1041PP=0.60.1041=5.76kip

Thus, the maximum allowable eccentric load on the column is 5.76kip_.

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Chapter 13 Solutions

MECHANICS OF MATERIALS

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