Home / Questions / During a static test of an airplane wing, the strain gage readings from a 45 0 rosette see...
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.
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