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A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels 会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
作者:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1121Kb)  |  收藏  |  浏览/下载:151/42  |  提交时间:2022/07/04
Flow Modulation and Mixing Enhancement of Highly Underexpanded Jet by Vortex Excitation 期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2462-2474
作者:  Wang Y(汪也);  Wu K(吴坤);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(6305Kb)  |  收藏  |  浏览/下载:331/87  |  提交时间:2020/07/06
Modeling Analysis of an Actively Cooled Scramjet Combustor Under Different Kerosene/Air Ratios 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 4, 页码: 975-991
作者:  Yao W(姚卫);  Lu Y(陆阳);  Wu K(吴坤);  Wang J(王晶);  Fan XJ(范学军)
浏览  |  Adobe PDF(2427Kb)  |  收藏  |  浏览/下载:355/106  |  提交时间:2018/10/19
Numerical Investigation on Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 期刊论文
COMBUSTION SCIENCE AND TECHNOLOGY, 2017, 卷号: 189, 期号: 12, 页码: 2154-2179
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, P (reprint author), Hong Kong Polytech Univ, Dept Mech Engn, Hong Kong 999077, Hong Kong, Peoples R China.
浏览  |  Adobe PDF(2993Kb)  |  收藏  |  浏览/下载:357/168  |  提交时间:2017/12/18
Detailed Hydrogen Oxidation Mechanism  Dlr  Flame Stabilization  Sensitivity Analysis  Supersonic Combustion  
Three-dimensional numerical study of the acoustic properities of a highly underexpanded jet 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Wu K(吴坤);  Li XP(李晓鹏);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(590Kb)  |  收藏  |  浏览/下载:364/92  |  提交时间:2017/05/05
Frequency Spectrum Analysis  High Temporal Resolution  Instantaneous Flow  Noise Generation Mechanisms  Theoretical Modeling  Three  Dimensional Numerical Studies  Transport Mechanism  Under  Expanded Jets