Rotorcraft Vibration Reduction and Noise Prediction Using a Unified Aeroelastic Response Simulation

By Patt Dan   Liu Li   Friedmann Peretz P.  

Journal of the American Helicopter Society, Vol. 50, Iss. 1, 2005-01 ,pp. : 95-106

AHS International

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Simultaneous Blade–Vortex Interaction Noise and Vibration Reduction in Rotorcraft Using Microflaps, Including the Effect of Actuator Saturation

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Journal of the American Helicopter Society, Vol. 60, Iss. 4, 2015-10 ,pp. : 1-16

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Notes Regarding Fundamental Understandings of Rotorcraft Aeroelastic Instability

By Bielawa Richard L.  

Journal of the American Helicopter Society, Vol. 32, Iss. 4, 1987-10 ,pp. : 4-15

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Rotorcraft Aeroelastic Testing in the Langley Transonic Dynamics Tunnel

By Yeager William T.   Mirick Paul H.   Hamouda M-Nabil H.   Wilbur Matthew L.   Singleton Jeffrey D.   Wilkie W. Keats  

Journal of the American Helicopter Society, Vol. 38, Iss. 3, 1993-07 ,pp. : 73-82

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A Study of Rotorcraft Structure-Borne Noise Isolation Using Empirical Component Coupling

By Unruh James F.   Fox Douglas J.  

Journal of the American Helicopter Society, Vol. 44, Iss. 3, 1999-07 ,pp. : 172-178

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