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

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484

STRESS TRANSFORMATIONS

such as the normal stresses produced by axial loads or bending moments, or the shear

stresses produced by torsion or transverse shear in beams. Before proceeding to the methods

used for stress transformations, it is helpful to consider how the analyst determines the

stresses that appear on a stress element. This section focuses on solid components in which

several internal loads or moments act simultaneously on a member’s cross section. The

method of superposition will be used to combine the various stresses acting at a particular

point, and the results will be summarized on a stress element.

The analysis of the stresses produced by multiple internal loads or moments that act

simultaneously on a member’s cross section is usually referred to as combined loadings.

In Chapter 15, combined loadings will be examined more completely. For instance, structures

with multiple external loads will be considered, along with solid components that

have three-dimensional geometry and loadings. Stress transformations will also be incorporated

into the analysis in that discussion. The intent of this section is simply to introduce

the reader to the process of evaluating the state of stress at a specific point. The process of

putting together the stress element is demonstrated with the use of geometrically simple

components and basic loadings.

ExAmpLE 12.1

A vertical pipe column with an outside diameter D = 114 mm and an

inside diameter d = 102 mm supports the loads shown. Determine the

normal and shear stresses acting at point H, and show these stresses on

a stress element.

Column cross-sectional

dimensions.

Plan the Solution

The cross-sectional properties will be

computed for the pipe column. Each

of the applied loads will be considered

in turn. The normal and/or shear

stresses created by each at point H will

be computed. Both the magnitude and

direction of the stress must be evaluated

and shown on the proper face of a

stress element. By the principle of superposition,

the stresses will be combined

appropriately so that the state of

stress at point H is summarized succinctly

by the stress element.

SolutioN

Section Properties

The outside diameter of the pipe is D = 114 mm, and the inside diameter is d = 102 mm.

The area, the moment of inertia, and the polar moment of inertia for the cross section

are, respectively, as follows:

π

A D d

4 [ 2 2 ] π

2 2 2

= − = [(114 mm) − (102 mm) ] = 2,035.752 mm

4

π

I D d

64 [ ] π

= − = [(114 mm)

64

− (102 mm) ] = 2,977,287 mm

π

J D d

32 [ ] π

= − = [(114 mm)

32

− (102 mm) ] = 5,954,575 mm

4 4 4 4 4

4 4 4 4 4

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