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(Solved): This question is from Advanced Mechanics of Materials. Please solve it in MATLAB or handwritten. T ...


Q5. A rectangular airplane wing spar is loaded so that the panel is in a state of plane strain \( \left(\epsilon_{z z}=\epsil

This question is from Advanced Mechanics of Materials. Please solve it in MATLAB or handwritten. Thank you.

Q5. A rectangular airplane wing spar is loaded so that the panel is in a state of plane strain . Given the deformation shown, determine a. The state of strain at point ; b. The state of strain at point B;


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