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Model study of conditions,when the reverse jet ingests into the engine input located behind the wing
Authors:G F Mingaleev  S G Margulis  A V Kosterin
Institution:1.Tupolev Kazan National Research Technical University,Tatarstan,Russia;2.OAO Ural Works of Civil Aviation,Ekaterinburg,Russia
Abstract:This paper presents the results of the model studies of the reverse jet distribution limits in the air cross-flow, performed in the wind tunnel, as well as the conditions of the jet’s ingestion into the engine air intake in the context of aircraft configuration, when the engines are the input of engines.
Keywords:
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