Effects of boundary-layers bleeding on unstart/restart characteristics of hypersonic inlets

被引:44
作者
Chang, J. [1 ]
Yu, D. [1 ]
Bao, W. [1 ]
Fan, Y. [1 ]
Shen, Y. [1 ]
机构
[1] Harbin Inst Technol, Harbin, Heilongjiang, Peoples R China
关键词
UNSTART; MACH-6; FLOW;
D O I
10.1017/S0001924000002992
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A series of mixed-compression hypersonic inlets at different bleeding rates were simulated at different freestream conditions in this paper. The unstart/restart characteristics of hypersonic inlets were analysed and the reasons why the unstart/restart phenomenon is in existence is presented. The unstart/restart characteristics of hypersonic inlets at different bleeding rates were given. The effects of boundary-layer bleeding on the performance parameter (mass-captured coefficient, total-pressure recovery coefficient), starting and restarting Mach number of hypersonic inlets were discussed. In conclusion, boundary-layer bleeding can improve the performance parameter of hypersonic inlets, and can reduce the starting and restarting Mach number, and can broad the operation range of the hypersonic inlet.
引用
收藏
页码:319 / 327
页数:9
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