Helicopter Rotor Periodic Differential Pressures and Structural Response Measured in Transient and Steady-State Maneuvers

Author： Ward John F.  

Publisher： AHS International

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.16, Iss.1, 1971-01, pp. : 16-25

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

Periodic Response of Thin-Walled Composite Helicopter Rotor Blades

By Rand Omri  

Journal of the American Helicopter Society, Vol. 36, Iss. 4, 1991-10 ,pp. : 3-11

AHS International

Access to resources Recommend Favorite

Calculated and Measured Blade Structural Response on a Full-Scale Rotor

By Esculier Jacques   Bousman William G.  

Journal of the American Helicopter Society, Vol. 33, Iss. 1, 1988-01 ,pp. : 3-16

AHS International

Access to resources Recommend Favorite

A nonlinear inverse simulation technique applied to coaxial rotor helicopter maneuvers

By Su Yuan   Cao Yihua  

Aircraft Engineering, Vol. 74, Iss. 6, 2002-11 ,pp. : 525-533

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Theoretical and Experimental Study of the Flap Droop Stop Impact Transient Aero-Elastic Response of a Helicopter Rotor Blade

By Leone Peter F.  

Journal of the American Helicopter Society, Vol. 9, Iss. 1, 1964-01 ,pp. : 32-37

AHS International

Access to resources Recommend Favorite

Structural Dynamics of a Helicopter Rotor Blade System

By Srinivasan A. V.   Cutts D. G.   Shu H. T.   Sharpe D. L.   Bauchau O. A.  

Journal of the American Helicopter Society, Vol. 35, Iss. 1, 1990-01 ,pp. : 75-85

AHS International

Access to resources Recommend Favorite