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- W2352626313 abstract "Design and study of a two-dimensional hypersonic inlet based on dual-mode combustion was conducted.The duct was divided into a supersonic duct and a subsonic combustion duct by a splitter plate.The influence of the geometry parameters on the inlet performance was mainly studied by using numerical method.The geometry parameters included the profile of the shoulder,the height and position of splitter plate,the turning position and expansion angle of transition duct,the height of subsonic combustion duct and the shape of the head of splitter plate.Results indicate that the profile of the shoulder,the height and position of splitter plate,the turning position of transition duct have great effects on the total pressure recovery coefficient,while the height of splitter plate,the shape of the head of splitter plate,the expansion angle of transition duct and the height of subsonic combustion duct have great effects on characteristics of back pressure." @default.
- W2352626313 created "2016-06-24" @default.
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- W2352626313 date "2012-01-01" @default.
- W2352626313 modified "2023-09-24" @default.
- W2352626313 title "Research on two-dimensional hypersonic inlet based on dual-mode combustion" @default.
- W2352626313 hasPublicationYear "2012" @default.
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