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[American Institute of Aeronautics and Astronautics 28th Structures, Structural Dynamics and Materials Conference - Monterey,CA,U.S.A. (06 April 1987 - 08 April 1987)] 28th Structures, Structural Dynamics and Materials Conference - Use of an implicit formulation based on quasilinearization for the aeroelastic response and stability of rotor blades in forward flight

✍ Scribed by CELI, R.; FRIEDMANN, P.

Book ID: 121033901
Publisher: American Institute of Aeronautics and Astronautics
Year: 1987
Weight: 791 KB
Category: Article
DOI: 10.2514/6.1987-921

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