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

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• When θ p is positive, the element is rotated in a counterclockwise sense from the

reference x axis. When θ p is negative, the rotation is clockwise.

• Note that the angle calculated from Equation (13.9) does not necessarily give the orientation

of the ε p1 direction. Either ε p1 or ε p2 may act in the θ p direction given by that equation.

The principal strain oriented at θ p can be determined from the following two-part rule:

• If ε x − ε y is positive, then θ p indicates the orientation of ε p1 .

• If ε x − ε y is negative, then θ p indicates the orientation of ε p2 .

• Elongate or contract the element into a rectangle according to the principal strains acting

in the two orthogonal directions. If a principal strain is positive, then the element is

elongated in that direction. The element is contracted if the principal strain is negative.

• Add either tension or compression arrows, labeled with the corresponding strain

magnitudes, to each edge of the element.

• To show the distortion caused by the shear strain, draw a diamond shape inside of the

rectangular principal strain element. The corners of the diamond should be located at

the midpoint of each edge of the rectangle.

• The maximum in-plane shear strain calculated from Equation (13.11) or Equation

(13.12) will be a positive value. Since a positive shear strain causes the angle between

two axes to decrease, label one of the acute angles with the value π/2 − γ max .

ExAmpLE 13.2

The strain components at a point in a body subjected to plane strain are ε x =

−680 µε, ε y = 320 µε, and γ xy = −980 m µrad. The deflected shape of an element

that is subjected to these strains is shown. Determine the principal strains, the

maximum in-plane shear strain, and the absolute maximum shear strain at point O.

Show the principal strain deformations and the maximum in-plane shear strain

distortion in a sketch.

ε y dy

dy

y

π

– γ xy

2

SolutioN

From Equation (13.10), the in-plane principal strains are

ε

p1, p2

2 2

εx + εy ⎛εx − εy⎞

γ xy

= ± ⎜ ⎟ + ⎛ 2 ⎝ 2 ⎠ ⎝ ⎜

2 ⎠

O

dx

ε x dx

x

680 320

= − + ±

2

=− 180 ± 700

2 2

⎛−680 − 320 ⎞ 980

⎜ ⎟ + ⎛−

⎜ ⎟

⎝ 2 ⎠ ⎝ 2 ⎠

= 520 µε, − 880 µε Ans.

and from Equation (13.11), the maximum in-plane shear strain is

2 2

γ max ⎛ εx − εy⎞

γ xy

2 ⎝

2 ⎠

⎟ + ⎛ ⎝ ⎜ ⎞

2 ⎠

2 2

⎛ −680 − 320⎞

980

2 ⎠

⎟ + ⎛ − ⎞

2 ⎠

= 700 µ rad

∴ γ = 1, 400 µ rad

Ans.

max

549

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