俄罗斯空气动力研究所中心学报
每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
AERODYNAMIC EXPERIMENTAL PLANTS FOR AIR-JET ENGINES
卷 43,
册 2, 2012,
pp. 193-209
DOI: 10.1615/TsAGISciJ.2012005496
摘要
The peculiarities of simulating the flight conditions necessary to fulfill the ground tests of air-jet engines at fuel combustion, as well as the possible tests and their constraints, are considered. Ways to design the gasdynamic channels of plants with two-stage diffusers in engine testing is discussed.
键词: wind tunnel, parallel-flow air-jet engine for high flight speeds, fuel combustion in the supersonic flow, simulation of the flight conditions, experimental investigations in aerodynamics
对本文的引用
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Sladkova L. A., Krylov V. V., Kuznetsov F. A., Installation of physical simulation of wind load on crane structures, Proceedings of Irkutsk State Technical University, 24, 6, 2021. Crossref
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