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Abstract
A high-lift configuration of the civil aircraft including body, wing in high-lift configuration, nacelle with pylon and empennage is considered in the present work. Numerical simulations of the flow have been carried out in the framework of Reynolds averaged Navier-Stokes (RANS) equations for low subsonic Mach number. The active flow control method, which is capable to improve maximal lift of the aircraft, has been considered. The influence of jet blowing near wing-body junction on aerodynamic characteristics has been investigated.
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Details
1 Central Aerohydrodynamic Institute, Zhukovsky, Moscow region, Russia