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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


Sergey P. Lisin
“Rostvertol” JSC.
Russian Federation


References

1. Aloyan O.M. Ae`rodinamika i dinamika polyota vertolyota / O.M. Aloyan, V.F. Romasevich, V.S. Sovgirenko. – M.: Voennoe izd-vo MO SSSR, 1973. – 466 s. – In Russian.

2. Bramvell A.R.S. Dinamika vertolyotov / A.R.S. Bramvell. – M.: Mashinostroenie, 1982. – 368 s. – In Russian.

3. D`yakonov V. P. MATLAB 6/6.1/6.5+. Simulink 4/5 v matematike i modelirovanii. Polnoe rukovodstvo pol`zovatelya / V.P. D`yakonov. – M.: SOLON-Press, 2003. – 576 s. – In Russian.

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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ISSN 2687-1653 (Online)