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.
RESEARCH OF AERODYNAMIC CHARACTERISTICS OF THE MODEL OF MANEUVERABLE AIRCRAFT WITH MECHANIZED LEADING EDGE USING SOFTWARE ANSYS FLUENT
2016
Aufsatz (Zeitschrift)
Elektronische Ressource
Unbekannt
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