The area of the cross section of an airplane wing has the
Chapter 10, Problem 10-82(choose chapter or problem)
The area of the cross section of an airplane wing has the following properties about the x and y axes passing through the centroid \(C: \bar{I}_x = 450\ in^4\), \(\bar{I}_y = 1730\ in^4\), \(\bar{I}_{xy} = 138\ in^4\). Determine the orientation of the principal axes and the principal moments of inertia.
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