Wind Tunnel Tests of Helicopter Blade Designs Optimized for Minimum Vibration

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.34, Iss.3, 1989-07, pp. : 40-50

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

Helicopter Blade Vibration and Flutter

By Miller R. H. Ellis C. W.

Journal of the American Helicopter Society, Vol. 1, Iss. 3, 1956-07 ,pp. : 19-38

AHS International

Access to resources Recommend Favorite

Blade Design for Reduced Helicopter Vibration

By Blackwell R. H.

Journal of the American Helicopter Society, Vol. 28, Iss. 3, 1983-07 ,pp. : 33-41

AHS International

Access to resources Recommend Favorite

Helicopter Vibration Reduction with Higher Harmonic Blade Pitch

By McHugh Frank J. Shaw John

Journal of the American Helicopter Society, Vol. 23, Iss. 4, 1978-10 ,pp. : 26-35

AHS International

Access to resources Recommend Favorite

Full Scale Wind Tunnel Investigation of Helicopter Drag

By Moser Herbert H.

Journal of the American Helicopter Society, Vol. 6, Iss. 1, 1961-01 ,pp. : 27-33

AHS International

Access to resources Recommend Favorite

Helicopter Vibration Suppression Using Simple Pendulum Absorbers on the Rotor Blade

By Hamouda M-Nabil H. Pierce G. Alvin

Journal of the American Helicopter Society, Vol. 29, Iss. 3, 1984-07 ,pp. : 19-29

AHS International

Access to resources Recommend Favorite