Research carried out at the MAI in the field of separated and jet flows around aircraft and their parts


Аuthors

Artamonova L. G., Radtsig A. N., Ryzhov Y. A., Semenchikov N. V.*, N. , N. , Yakovlevsky O. V.

Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: semenchikovnv@rambler.ru

Abstract

Results of theoretical and experimental investigations are discussed for a broad class of three-dimensional separated flows around aircraft bodies and wings as well as around a whole vehicle configuration for transcritical and supercritical angle of attack areas. The experimental investigations are carried out in the MAI wind tunnels for Reynolds number values from the 0.26106-3.4106 м-1 region. Some general regularities are revealed for generation and transformation of separated flows and vortex systems. Relationships are found between a flow structure and shape of aircraft parts together with flow conditions for large angle of attack values. A possibility is discovered to use interaction of vortex structures in wing systems and vehicle configurations to enhance their lifting properties for large angle of attack values. It is demonstrated that a blowing of jets is an effective means to control a flow and aerodynamic characteristics of a vehicle for nonseparated or separated flows.

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