Thermally Induced Twist in Composite Tubes and Their Applications to Helicopter Rotor Blades with Controllable Twist

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.39, Iss.1, 1994-01, pp. : 41-49

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

Modeling of Flexible Rotor Blades for Helicopter Flight Dynamics Applications

By Turnour Stephen R. Celi Roberto

Journal of the American Helicopter Society, Vol. 41, Iss. 1, 1996-01 ,pp. : 52-66

AHS International

Access to resources Recommend Favorite

Modeling of Flexible Rotor Blades for Helicopter Flight Dynamics Applications

By Turnour Stephen R. Celi Roberto

Journal of the American Helicopter Society, Vol. 41, Iss. 3, 1996-07 ,pp. : 191-193

AHS International

Access to resources Recommend Favorite

Structural Optimization for Vibratory Loads Reduction of Composite Helicopter Rotor Blades with Advanced Geometry Tips

By Yuan Kuo-An Friedmann Peretz P.

Journal of the American Helicopter Society, Vol. 43, Iss. 3, 1998-07 ,pp. : 246-256

AHS International

Access to resources Recommend Favorite

Acoustic Aspects of Active-Twist Rotor Control

By Booth Earl R. Wilbur Matthew L.

Journal of the American Helicopter Society, Vol. 49, Iss. 1, 2004-01 ,pp. : 3-10

AHS International

Access to resources Recommend Favorite