32th Congress of the International Council of the Aeronautical Sciences

03.2 - Experimental Aerodynamics

EXPERIMENTAL INVESTIGATION OF DAMAGE WING IMPACT ON THE AIRLINER AERODYNAMIC CHARACTERISTICS

A. Krzysiak, Lukasiewicz Research Network – Institute of Aviation, Poland; A. Olejnik¹, L. Kiszkowiak¹; ¹Faculty of Mechatronics, Armament & Aerospace; Military Universi, Poland

The wind tunnel tests of the Tu-154M aircraft model in a few configurations of the left wing damage are presented. The investigation made it possible to determine the impact of the wing damage on the aircraft aerodynamic characteristics. The tests were performed in the Institute of Aviation low speed wind tunnel at the V=40m/s.


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