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pro vyhledávání: '"LD5655.V856 1987.S874"'
Autor:
Strganac, Thomas W.
A method for predicting unsteady, subsonic aeroelastic responses has been developed. The technique accounts for aerodynamic nonlinearities associated with angles of attack, vortex-dominated flow, static deformations, and unsteady behavior. The angle
Externí odkaz:
http://hdl.handle.net/10919/74775
