THE INVESTIGATION OF ROTOR’S INFLOW AND MAIN ROTOR’S INDUCED VELOCITY AT HOVER AND AT STEEP DESCENTS
Abstract
– an angle of attack of the main rotor). The vortex ring state has been considered also.
About the Authors
V. S. Krimskiy
ЦАГИ им. проф. Н.Е. Жуковского
Russian Federation
Russian Federation
V. M. Shcheglova
ЦАГИ им. проф. Н.Е. Жуковского
Russian Federation
Russian Federation
References
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2. E. Berton, D. Favier, C. Maresca, M. Nsi Mba and E.S. Vozhdayev, V.A. Golovkin, N.N. Tarasov, A.A. Maslennikov. Experimental and Numerical Obtained at LAMB and TsAGI. 29th European Rotorkraft Forum, 16 – 18 September 2003, Friedrichshafen, Germany.
3. У. Джонсон. Теория вертолета: в 2-х т. - М.: Мир, 1983.
4. Chang Chen, J.V.R. Pracad. Ring Vortex Model for Descent Flight. American Helicopter Society 61st Annual Forum, Grapevine, Texas, June 1 – 3, 2005.
Review
For citations:
Krimskiy V.S., Shcheglova V.M. THE INVESTIGATION OF ROTOR’S INFLOW AND MAIN ROTOR’S INDUCED VELOCITY AT HOVER AND AT STEEP DESCENTS. Civil Aviation High Technologies. 2014;(200):86-90. (In Russ.)
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