Application of a New Compressible Time Domain Aerodynamic Model to Vibration Reduction in Helicopters Using an Actively Controlled Flap

Author： Myrtle Timothy F. Friedmann Peretz P.

Publisher： AHS International

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.46, Iss.1, 2001-01, pp. : 32-43

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