SIMULATION AND OPTIMIZATION OF ULTRALIGHT HELICOPTER AERODYNAMIC CHARACTERISTICS
Abstract
The simulation and optimization of the ultralight helicopter aerodynamic characteristics at the design stages and phases which permit to determine optimal values of the engine power and speed are performed.
About the Authors
Viktor P. Zharov
Don State Technical University
Russian Federation
Russian Federation
Sergey P. Lisin
“Rostvertol” JSC.
Russian Federation
Russian Federation
References
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4. Mil` M.L. Vertolyoty`. Raschyot i proektirovanie. Ch. 1. Ae`rodinamika / M.L. Mil`, A.V. Ne-krasov, A.S. Bravermann, L.N. Grodko, M.A. Lejkand. – M.: Mashinostroenie, 1966. – 455 s. – In Russian.
Review
For citations:
Zharov V.P., Lisin S.P. SIMULATION AND OPTIMIZATION OF ULTRALIGHT HELICOPTER AERODYNAMIC CHARACTERISTICS. Vestnik of Don State Technical University. 2012;12(4):35-37. (In Russ.)
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