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During a static test of an airplane wing, the strain gage readings from a 45 0 rosette see figure are as follows gage

During a static test of an airplane wing, the strain gage readings from a 45 0 rosette (see figure) are as follows: gage A, 520 x 10- 6 ; gage B, 360 x 10- 6 , and gage C, -80 x 10- 6 . Determine the principal strains and maximum shear strains.

 

Jun 28 2020 View more View Less

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