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Parametric Study on Lateral–Directional Stability of Hypersonic Waverider 期刊论文
AIAA Journal, 2021, 卷号: 59, 期号: 8, 页码: 3025-3042
作者:  刘文;  张陈安;  Wang Xiao-Peng;  Li Jin-Jie;  王发民
Adobe PDF(7528Kb)  |  收藏  |  浏览/下载:321/49  |  提交时间:2021/08/30
On the application of tabulated dynamic adaptive chemistry in ethylene-fueled supersonic combustion 期刊论文
COMBUSTION AND FLAME, 2018, 卷号: 197, 页码: 265-275
作者:  Wu K(吴坤);  Contino F;  Yao W(姚卫);  Fan XJ(范学军)
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Tabulated dynamic adaptive chemistry  Skeletal mechanism  Supersonic combustion  Ethylene  Large Eddy Simulation  
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)
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超声速燃烧室火焰稳定模式与化学反应机理简化研究 学位论文
博士论文,北京: 中国科学院大学, 2018
作者:  吴坤
Adobe PDF(18227Kb)  |  收藏  |  浏览/下载:718/24  |  提交时间:2018/05/22
超声速燃烧  支板稳焰  凹腔稳焰  简化机理  动态自适应化学  
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
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Comment on "Mechanics of Combustion Mode Transition in a Direct-Connect Ramjet-Scramjet Experiment" 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 2, 页码: 550-551
作者:  Chen KT(陈科挺);  Yue LJ(岳连捷);  Chang XY(张新宇)
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Effect of cowl shock on restart characteristics of simple ramp type hypersonic inlets with thin boundary layers 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 卷号: 74, 页码: 72-80
作者:  Yue LJ(岳连捷);  Jia YN(贾轶南);  Xu X;  Zhang XY(张新宇);  Zhang P(张鹏)
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Inlet restart  Cowl shock  Shock wave boundary layer interactions  
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
作者:  Yao W(姚卫);  Yuan YM(袁越明);  Li XP(李晓鹏);  Wang J(王晶);  Wu K(吴坤);  Fan XJ(范学军)
浏览  |  Adobe PDF(805Kb)  |  收藏  |  浏览/下载:386/143  |  提交时间:2018/06/06