Uniform Downwash with Rotors Having a Finite Number of Blades

Author： Harris Franklin D.   McVeigh Michael A.  

Publisher： AHS International

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.21, Iss.1, 1976-01, pp. : 9-20

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

Free Wake Model of Hovering Rotors Having Straight or Curved Blades

By Rosen Aviv   Graber Avinoam  

Journal of the American Helicopter Society, Vol. 33, Iss. 3, 1988-07 ,pp. : 11-19

AHS International

Access to resources Recommend Favorite

Response, Loads and Stability of Rotors With Interconnected Blades

By Suresh J. K.   Nagabhushanam J.  

Journal of the American Helicopter Society, Vol. 41, Iss. 4, 1996-10 ,pp. : 283-290

AHS International

Access to resources Recommend Favorite

Optimum number of blades for maximum efficiency of centrifugal blowers

By REDDY Y.R.   KONNUR M.S.  

Aircraft Engineering, Vol. 43, Iss. 8, 1993-12 ,pp. : 16-17

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Noise Radiation from Helicopter Rotors Operating at High Tip Mach Number

By Arndt Roger E. A.   Borgman Dean C.  

Journal of the American Helicopter Society, Vol. 16, Iss. 1, 1971-01 ,pp. : 36-45

AHS International

Access to resources Recommend Favorite

Hover Performance of a Micro Air Vehicle: Rotors at Low Reynolds Number

By Hein Benjamin R.   Chopra Inderjit  

Journal of the American Helicopter Society, Vol. 52, Iss. 3, 2007-07 ,pp. : 254-262

AHS International

Access to resources Recommend Favorite