RESEARCH OF AERODYNAMIC CHARACTERISTICS OF THE MODEL OF MANEUVERABLE AIRCRAFT WITH MECHANIZED LEADING EDGE USING SOFTWARE ANSYS FLUENT
Abstract
The calculations of the aerodynamic characteristics of the aircraft model having mechanized leading edge are conducted, and then comparing the results with experimental data. It is shown that the use of computational methods for the determination of the aerodynamic characteristics allows to deepen the results of experimental modeling in air tunnels.
About the Authors
A. V. Golovnev
ВУНЦ ВВС ВВА (г. Воронеж)
Russian Federation
Russian Federation
A. L. Tarasov
ВУНЦ ВВС ВВА (г. Воронеж)
Russian Federation
Russian Federation
References
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Review
For citations:
Golovnev A.V., Tarasov A.L. RESEARCH OF AERODYNAMIC CHARACTERISTICS OF THE MODEL OF MANEUVERABLE AIRCRAFT WITH MECHANIZED LEADING EDGE USING SOFTWARE ANSYS FLUENT. Civil Aviation High Technologies. 2015;(218):42-49. (In Russ.)
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