A Parametric Design Study for a Swashplateless Helicopter Rotor with Trailing-Edge Flaps

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.49, Iss.1, 2004-01, pp. : 43-53

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

Experimental/Numerical Evaluation of Integral Trailing Edge Flaps for Helicopter Rotor Applications

By Hassan Ahmed A. Straub Friedrich K. Noonan Kevin W.

Journal of the American Helicopter Society, Vol. 50, Iss. 1, 2005-01 ,pp. : 3-17

AHS International

Access to resources Recommend Favorite

Integrated Trailing-Edge Flaps and Servotabs for Helicopter Primary Control

By Falls Jaye Datta Anubhav Chopra Inderjit

Journal of the American Helicopter Society, Vol. 55, Iss. 3, 2010-07 ,pp. : 32005-0

AHS International

Access to resources Recommend Favorite

Trailing-Edge Flaps for Rotor Performance Enhancement and Vibration Reduction

By Ravichandran Kumar Chopra Inderjit Wake Brian E. Hein Benjamin

Journal of the American Helicopter Society, Vol. 58, Iss. 2, 2013-04 ,pp. : 1-13

AHS International

Access to resources Recommend Favorite

Closed-Loop Test of a Rotor with Individually Controlled Trailing-Edge Flaps for Vibration Reduction

By Roget Beatrice Chopra Inderjit

Journal of the American Helicopter Society, Vol. 55, Iss. 1, 2010-01 ,pp. : 12009-0

AHS International

Access to resources Recommend Favorite

Aeroelastic Stability of Trailing-Edge Flap Helicopter Rotors

By Shen Jinwei Chopra Inderjit

Journal of the American Helicopter Society, Vol. 48, Iss. 4, 2003-10 ,pp. : 236-243

AHS International

Access to resources Recommend Favorite