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Analysis: V-n Diagram. Analysis: Wing Loading. Loads on the wing due to Lift and Drag forces, Shear forces, and Moments. Loading is necessary to design for bending stresses, buckling, and divergence. Forces found using a mixture of analytical and empirical formulas. Analysis: Wing Loading.
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Analysis: Wing Loading • Loads on the wing due to Lift and Drag forces, Shear forces, and Moments. • Loading is necessary to design for bending stresses, buckling, and divergence. • Forces found using a mixture of analytical and empirical formulas.