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

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(a) the normal stress in each material at point H, which is located

a distance a = 1.75 in. above the z centroidal axis.

(b) the normal strain in each material at point H.

(c) the maximum bending stress in each material.

p8.39 A composite

y

beam consists of a bronze

[E = 105 GPa] bar (2) attached

rigidly to an alu-

z

d

(2)

minum alloy [E = 70 GPa]

bar (1) as shown in Figure

(1)

P8.39. The dimensions of

b

the cross section are b 1 =

2 b 1

60 mm, b 2 = 25 mm, and FIGURE p8.39

d = 40 mm. The allowable

stress of the aluminum alloy is 165 MPa, and the allowable stress of

the bronze is 210 MPa. What is the magnitude of the allowable bending

moment M z that may be applied to the composite cross section?

p8.40 Two aluminum alloy

plates (2) are attached to the

b2

b2

sides of a wooden beam (1) as a

shown in Figure P8.40. The dimensions

of the composite cross

y

section are b 1 = 80 mm, d 1 = d 2 z

240 mm, b 2 = 10 mm, d 2 =

120 mm, and a = 60 mm. Determine

(2)

(2)

the maximum bending a

(1)

stresses produced in both the

wooden beam and the aluminum

b 1

plates if a bending moment FIGURE p8.40

M z = +6,000 N ⋅ m is applied

about the z axis. Assume that E 1 = 12.5 GPa and E 2 = 70 GPa.

p8.41 A wooden beam (1) is reinforced

with steel plates (2) rigidly attached to its

top and bottom surfaces, as shown in Figure

P8.40. The dimensions of the cross section

are b 1 = 6 in., d 1 = 12 in., b 2 = 4 in., and d 2 =

0.5 in. The elastic moduli of the wood and

steel are E 1 = 1,250 ksi and E 2 = 30,000 ksi,

respectively. The allowable bending

stresses of the wood and steel are 1,200 psi

and 20,000 psi, respectively. Determine the

largest concentrated vertical load that can

be applied at midspan if a simply supported

beam with this cross section spans 18 ft.

p8.42 A bronze [E = 15,200 ksi] bar is rigidly attached to a

stainless steel [E = 27,500 ksi] bar to form a composite beam.

The composite beam is subjected to a bending moment

M = 6,400 lb ⋅ ft about the z axis (Figure P8.42a/43a). The dimensions

of the beam cross section are b = 4.5 in., d B = 2.25 in., and

d S = 1.00 in. (Figure P8.42b/8.43b). Determine

(a) the maximum bending stresses in the bronze and stainless

steel bars.

(b) the normal stress in each bar at the surface where they contact

each other.

(1)

z

(2)

b 1

y

(2)

b 2

FIGURE p8.41

d 2

d 1

d 2

d 1

M

Bronze

Stainless

steel

FIGURE p8.42a/43a

FIGURE p8.42b/43b

p8.43 A bronze [E = 100 GPa] bar is rigidly attached to a stainless

steel [E = 190 GPa] bar to form a composite beam. The allowable

bending stresses for the bronze and stainless steel bars are

180 MPa and 225 MPa, respectively. Determine the allowable

bending moment M (Figure P8.42a/43a) that can be applied to the

composite beam if the dimensions of the beam cross section are

b = 150 mm, d B = 85 mm, and d S = 40 mm (Figure P8.42b/8.43b).

p8.44 A wooden beam (1) is

reinforced on its lower surface by

a steel plate (2) as shown in Figure

P8.44. The dimensions of the cross

section are b 1 = 220 mm, d =

380 mm, b 2 = 160 mm, and t =

20 mm. The elastic moduli of the

wood and steel are E 1 = 12.5 GPa

and E 2 = 200 GPa, respectively.

The allowable bending stresses of

the wood and steel are 7.5 MPa and

150 MPa, respectively. This cross

z

y

section is used for a simply supported beam that spans 9 m. What is

the largest uniformly distributed load that can be applied to the beam?

p8.45 A composite beam consists of a concrete slab (1) that is

rigidly attached to the top flange of a W16 × 40 standard steel shape

(2). The cross section of the beam is shown in Figure P8.45. The

slab has a width b = 48 in., a thickness t = 4 in., and an elastic

modulus of 3,500 ksi. The elastic modulus of the steel shape is

30,000 ksi, and the cross-sectional dimensions are presented in

Appendix B. For a bending moment of M z = +150 kip ⋅ ft, determine

(a) the location of the centroid for the transformed section,

measured upward from point K.

(b) the normal stress at H in the concrete slab.

(c) the normal stress at K in the steel shape.

H

Concrete slab (1)

z

Steel shape (2)

FIGURE p8.45

K

y

b

M

x

Bronze

z

y

Stainless steel

Steel

plate (2)

b

Cross section

Wooden

beam (1)

z

FIGURE p8.44

d

b 1

y

b 2

t

d B

d S

d

t

281

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