Engineering, 08.12.2020 16:50 mismhan01
For a cantilevered wing with uniform torsion stiffness GJ , chord c, aerodynamic center offset a distance e ahead of the elastic axis, and span L, calculate the divergence speed using the Rayleigh-Ritz method (single mode approximation with the assumed mode sin πx 2L ). Compare this to the exact solution derived in class for the uniform elastic wing
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For a cantilevered wing with uniform torsion stiffness GJ , chord c, aerodynamic center offset a dis...
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