Experimental Downwash Velocity, Static Pressure, and Temperature Distributions in Ground Effect for a 75-Foot Jet Driven Rotor

Author： Bolanovich Mirko   Marks Marvin D.  

Publisher： AHS International

ISSN： 2161-6027

Source： Journal of the American Helicopter Society, Vol.4, Iss.2, 1959-04, pp. : 22-36

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

Insight into the effects of rotor downwash on engine jet

By Cao Yihua   Su Yuan  

Aircraft Engineering, Vol. 75, Iss. 4, 2003-04 ,pp. : 345-349

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

A new method for predicting rotor wake geometries and downwash velocity field

By Cao Yihua  

Aircraft Engineering, Vol. 71, Iss. 2, 1999-02 ,pp. : 129-135

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Modelling Rotor Wakes in Ground Effect

By Brown Richard E.   Whitehouse Glen R.  

Journal of the American Helicopter Society, Vol. 49, Iss. 3, 2004-07 ,pp. : 238-249

AHS International

Access to resources Recommend Favorite

Jet Flow and Its Effects on Aircraft: An Analysis of Experimental Data on Velocity and Temperature Distribution with a Discussion of the Effects of Jets on Drag and Stability

By M.A. H.B. Squire  

Aircraft Engineering, Vol. 22, Iss. 3, 1993-12 ,pp. : 62-67

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

The Effect of Helicopter Pitching Velocity on Rotor Lift Capability

By Brown E. L.   Schmidt P. S.  

Journal of the American Helicopter Society, Vol. 8, Iss. 4, 1963-10 ,pp. : 1-6

AHS International

Access to resources Recommend Favorite