Abstract
The unsteady transonic aerodynamic and aeroelastic behavior of a rectangular wing with a NACA 64A010 profile and a swept-back wing with a supercritical MBB-A3 profile is investigated analytically, applying 2D analysis of viscous effects to the 3D case. The results are presented in graphs and tables and discussed. It is found that the inclusion of viscous effects increases the flutter speed of the wings.
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