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TsAGI Science Journal
BEAM STIFFNESSES OF A COMPOSITE WING WITH ANISOTROPIC SKIN
E. I. Kryuchkov
Central Aerohydrodynamic Institute (TsAGI), 1, Zhukovsky Str., Zhukovsky, Moscow Region, 140180, Russian Federation
Equations for the definition of beam stiffnesses, positions of neutral axes, and rotation centers at bending and torsion, stresses, and deformations of a composite wing with an anisotropic skin are obtained based on the classical beam theory. A comparison of the results obtained from the analytical solutions and the results obtained from the finite-element computations is performed.
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