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

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at intervals of s along each side of the built-up shape. The cross section

of the built-up shape is shown in Figure P9.32b, and the crosssectional

properties for a single hat shape are shown in Figure P9.32c.

For an applied load P = 6,800 N, determine the maximum spacing

interval s that can be used if each rivet has a shear strength of 1,700 N.

z

y

FIGURE p9.32a Riveted beam.

y

s

Rivets

y

P

x

p9.33 A steel wide-flange beam in an existing structure is to be

strengthened by adding a cover plate to its lower flange, as shown

in Figure P9.33. The wide-flange shape has dimensions b f = 7.50 in.,

t f = 0.57 in., d = 18.0 in., and t w = 0.355 in. The cover plate has a

width b = 15 in. and t = 1.0 in. The cover plate is attached to the

lower flange by pairs of 0.875 in. diameter bolts spaced at intervals

s along the beam span. Bending occurs about the z centroidal axis.

(a) If the allowable bolt shear stress is 14 ksi, determine the maximum

bolt spacing interval s required to support an internal

shear force in the beam of V = 55 kips.

(b) If the allowable bending stress is 24 ksi, determine the

allowable bending moment for the existing wide-flange shape,

the allowable bending moment for the wide-flange shape with

the added cover plate, and the percentage increase in moment

capacity that is gained by adding the cover plate.

t f

Rivet

z

FIGURE p9.32b

Cross section.

V

Rivet

z'

60 mm

A = 2,400 mm 2

Iz' = 3.76 × 10 6 mm 4

FIGURE p9.32c Crosssectional

properties for a

single hat shape.

Cover

plate

t w

z

b f

y

b

d

t

FIGURE p9.33

9.9 Shear Stress and Shear Flow in

Thin-Walled members

In the preceding discussion of built-up beams, the internal shear force F H required for

horizontal equilibrium of a specific portion and length of a flexural member was expressed

by Equation (9.11):

F

H

VQ

= Dx

I

As shown in Figure 9.14c, the force F H acts parallel to the bending stresses (i.e., in the

x direction). The shear flow q was derived in Equation (9.12),

FH

VQ

q

D x

= = I

to express the shear force per unit length of beam span required to satisfy horizontal equilibrium

for a specific portion of the cross section. In this section, these ideas will be applied

to the analysis of average shear stress and shear flow in thin-walled members such as the

flanges of wide-flange beam sections.

Shear Stress in Thin-Walled Sections

Consider the segment of length dx of the wide-flange beam shown in Figure 9.16a. The bending

moments M and M + dM produce compressive bending stresses in the upper flange of the

z

z

356

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