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Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载：254/85  |  提交时间：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Jia YN(贾轶南);  Yue LJ(岳连捷);  Zhang XY(张新宇);  Jia, Yinan(yuelj@imech.ac.cn)
浏览  |  Adobe PDF(566Kb)  |  收藏  |  浏览/下载：321/68  |  提交时间：2018/01/16
Boundary Layer Flow  Boundary Layers  Spacecraft  Wind Tunnels  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载：268/80  |  提交时间：2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion  
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