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TsAGI Science Journal

ISSN 印刷: 1948-2590
ISSN オンライン: 1948-2604

TsAGI Science Journal

DOI: 10.1615/TsAGISciJ.2017022802
pages 251-260

COMPUTATIONAL INVESTIGATION OF THE INFLUENCE OF A COMPLEX SPATIAL CONFIGURATION INLET ON THE PERFORMANCE CHARACTERISTICS OF AN AVIATION GAS-TURBINE ENGINE WITH A HIGH BYPASS RATIO

S. E. Krasnov
Central Institute of Aviation Motors, 2 Aviamotornaya Str., Moscow, 111116, Russian Federation
Oleg Petrovich Minin
Tupolev Design Bureau, 17 Academician Tupolev Embankment, Moscow, 105005, Russian Federation
Dmitrii Aleksandrovich Olishevskii
Tupolev Design Bureau, 17 Academician Tupolev Embankment, Moscow, 105005, Russian Federation
Sergei Grigorievich Shevel'kov
Tupolev Design Bureau, 17 Academician Tupolev Embankment, Moscow, 105005, Russian Federation

要約

The propulsion in a curvilinear inlet integrated into a flying wing airframe is considered. Numerical investigations are conducted of the influence of the flow in the curvilinear channel of the inlet on the performance characteristics of the engine.