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Performance of a detonation driven shock tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Li JW;  Wang Q(汪球);  Zhao W(赵伟);  Lu P;  Tan YX
浏览  |  Adobe PDF(468Kb)  |  收藏  |  浏览/下载:292/81  |  提交时间:2018/01/16
Detonation  Gas Dynamics  Hypersonic Flow  Shock Tubes  Supersonic Aerodynamics