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ch01-03 stress & strain & properties

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<strong>03</strong> Solutions 46060 5/7/10 8:45 AM Page 8<br />

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exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher.<br />

3–11. The <strong>stress</strong>–<strong>strain</strong> diagram for a steel alloy having an<br />

original diameter of 0.5 in. and a gauge length of 2 in. is<br />

given in the figure. If the specimen is loaded until it is<br />

<strong>stress</strong>ed to 90 ksi, determine the approximate amount of<br />

elastic recovery and the increase in the gauge length after it<br />

is unloaded.<br />

s (ksi)<br />

105<br />

90<br />

75<br />

60<br />

45<br />

30<br />

15<br />

0 P (in./in.)<br />

0 0.05 0.10 0.15 0.20 0.25 0.30 0.35<br />

0 0.001 0.002 0.0<strong>03</strong> 0.004 0.005 0.006 0.007<br />

From the <strong>stress</strong>–<strong>strain</strong> diagram Fig. a, the modulus of elasticity for the steel alloy is<br />

E<br />

1<br />

=<br />

60 ksi - 0<br />

0.002 - 0 ; E = 30.0(1<strong>03</strong> ) ksi<br />

when the specimen is unloaded, its normal <strong>strain</strong> recovered along line AB, Fig.a,<br />

which has a gradient of E. Thus<br />

Elastic Recovery = 90<br />

E =<br />

Thus, the permanent set is<br />

90 ksi<br />

30.0(10 3 ) ksi<br />

= 0.0<strong>03</strong> in>in<br />

Ans.<br />

Then, the increase in gauge length is<br />

P P = 0.05 - 0.0<strong>03</strong> = 0.047 in>in<br />

¢L =P P L = 0.047(2) = 0.094 in<br />

Ans.<br />

8

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