During a test of an airplane wing, the strain gage readings from a 45o rosette (see figure)

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During a test of an airplane wing, the strain gage readings from a 45o rosette (see figure) are as follows: gage A, 520 ( 10-6; gage B, 360 ( 10-6; and gage C,- 80 ( 10-6 .
Determine the principal strains and maximum shear strains, and show them on sketches of properly oriented elements?
During a test of an airplane wing, the strain gage

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Mechanics of Materials

ISBN: 978-0495438076

7th edition

Authors: James M. Gere, Barry J. Goodno

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