The Effects of Control System Stiffness Models on the Dynamic Stall Behavior of a Helicopter

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.45, Iss.4, 2000-10, pp. : 263-269

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

Dynamic Stall of Helicopter Blades

By Ericsson Lars E. Reding J. Peter

Journal of the American Helicopter Society, Vol. 17, Iss. 1, 1972-01 ,pp. : 11-19

AHS International

Access to resources Recommend Favorite

Dynamic Stall Considerations in Helicopter Rotors

By Ham Norman D. Garelick Melvin S.

Journal of the American Helicopter Society, Vol. 13, Iss. 2, 1968-04 ,pp. : 49-55

AHS International

Access to resources Recommend Favorite

On the effect of mass and stiffness unbalance on helicopter tail rotor system behavior

By Singh Hemant K. Pawar Prashant M. Ganguli Ranjan Jung Sung Nam

Aircraft Engineering, Vol. 80, Iss. 2, 2008-03 ,pp. : 129-138

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Stall Flutter of Helicopter Rotor Blades: A Special Case of the Dynamic Stall Phenomenon

By Ham Norman D.

Journal of the American Helicopter Society, Vol. 12, Iss. 4, 1967-10 ,pp. : 19-21

AHS International

Access to resources Recommend Favorite

Testing of a Stall Flutter Suppression System for Helicopter Rotors Using Individual-Blade-Control

By Quackenbush Todd R.

Journal of the American Helicopter Society, Vol. 29, Iss. 3, 1984-07 ,pp. : 38-44

AHS International

Access to resources Recommend Favorite