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

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z

D

(3)

A

y

(1)

L1,

L3

N B

B

L 2

(a) Determine the temporary installation torque T′ B that must be

applied at B to align the bolt holes at A.

(b) Determine the maximum shear stress τ initial in the pipe after

the bolts are connected and the temporary installation torque

at B is removed.

(c) Determine the magnitude of the maximum shear stress in

segments (1) and (2) if an external torque T B = 150 kip ⋅ in. is

applied at B after the bolts are connected.

(2)

T C

FIGURE p6.47

N E

E

x'

C

x

y

L 1

L 2

p6.48 The aluminum alloy [G = 4,000 ksi] pipe shown in Figure

P6.48 is fixed to the wall support at C. The bolt holes in the flange at

A were supposed to align with mating holes in the wall support; however,

an angular misalignment of 4° was found to exist. To connect

the pipe to its supports, a temporary installation torque T′ B must be

applied at B to align flange A with the mating holes in the wall

support. The outside diameter of the pipe is 5.5625 in. and its wall

thickness is 0.258 in. The segment lengths are L 1 = 16 ft and L 2 = 24 ft.

z

A

FIGURE p6.48

(1)

T B

B

(2)

C

x

6.10 Stress concentrations in circular Shafts

Under Torsional Loadings

In Section 5.7, it was shown that the introduction of a circular hole or other geometric discontinuity

into an axially loaded member causes a significant increase in the magnitude of

the stress in the immediate vicinity of the discontinuity. This phenomenon, called stress

concentration, also occurs for circular shafts under torsional forms of loading.

Previously in this chapter, the maximum shear stress in a circular shaft of uniform

cross section and made of a linearly elastic material was given by Equation (6.5):

τ max =

In the context of stress concentrations in circular shafts, this stress is considered a nominal

stress, meaning that it gives the shear stress in regions of the shaft that are sufficiently

removed from discontinuities. Shear stresses become much more intense near abrupt

changes in shaft diameter, and Equation (6.5) does not predict the maximum stresses near

discontinuities such as grooves or fillets. The maximum shear stress at discontinuities is

expressed in terms of a stress-concentration factor

K

τ

Tc

J

max

= (6.21)

τ nom

In this equation, τ nom is the stress given by Tc/J for the minimum diameter of the shaft

(termed the minor diameter) at the discontinuity.

183

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