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

Author： Patt Dan   Liu Li   Friedmann Peretz P.  

Publisher： AHS International

ISSN： 2161-6027

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

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Simultaneous Vibration and Noise Reduction in Rotorcraft Using Aeroelastic Simulation

By Patt Dan   Liu Li   Friedmann Peretz P.  

Journal of the American Helicopter Society, Vol. 51, Iss. 2, 2006-04 ,pp. : 127-140

AHS International

Access to resources Recommend Favorite

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

By Padthe Ashwani K.   Friedmann Peretz P.  

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

AHS International

Access to resources Recommend Favorite

A Nonlinear Response Analysis and Solution Method for Rotorcraft Vibration

By Kunz Donald L.  

Journal of the American Helicopter Society, Vol. 28, Iss. 1, 1983-01 ,pp. : 56-62

AHS International

Access to resources Recommend Favorite

Prediction of Aeroelastic Response of a Model X-Wing Rotor

By Sopher Robert   Duh James E.  

Journal of the American Helicopter Society, Vol. 32, Iss. 4, 1987-10 ,pp. : 54-62

AHS International

Access to resources Recommend Favorite

Rotorcraft Gross Weight and Center of Gravity Prediction Using Regime Recognition

By Moon Suresh   Phan Nam  

Journal of the American Helicopter Society, Vol. 60, Iss. 4, 2015-10 ,pp. : 1-8

AHS International

Access to resources Recommend Favorite