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Reverse jet parameters study on aerodynamic thermal uncertainty of a blunt body 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 107, 页码: 106260
作者:  Zhang W;  Wang S;  Wang Q;  Ju SJ(鞠胜军);  Yan C
Adobe PDF(2859Kb)  |  收藏  |  浏览/下载:253/98  |  提交时间:2021/02/09
Aerodynamic thermal  Opposing jets  Parametric sensitivity analysis  Uncertainty quantification  Analysis of Variance  Non-Intrusive Polynomial Chaos  
Unsteady combustion mode with a super-high frequency induced by a curved shock 期刊论文
PHYSICS OF FLUIDS, 2020, 卷号: 32, 期号: 11, 页码: 116101
作者:  Teng HH(滕宏辉);  Liu S;  Zhang ZJ(张子健)
Adobe PDF(5194Kb)  |  收藏  |  浏览/下载:254/69  |  提交时间:2020/12/28
PROJECTILE  MECHANISM  SYSTEMS  
Development and application of ANN model for property prediction of supercritical kerosene 期刊论文
Computers and Fluids, 2020, 卷号: 209, 期号: 2020, 页码: 1-18
作者:  Li B(李波);  Lee YC(李亚超);  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(10546Kb)  |  收藏  |  浏览/下载:333/120  |  提交时间:2020/08/27
Artificial Neural Network (Ann)  Principle Of Extended Corresponding State (Ecs)  Rp-3 Kerosene  Superitical Pressure  Openfoam  
Numerical study on the shock/combustion interaction of oblique detonation waves 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
作者:  Yang L;  Yue LJ(岳连捷);  Zhang QF(张启帆);  Zhang XY(张新宇)
Adobe PDF(5176Kb)  |  收藏  |  浏览/下载:254/103  |  提交时间:2020/11/30
Oblique detonation wave  Shock/combustion interaction  Shock polar analysis  High-resolution simulation  
Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
作者:  Xue R;  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3912Kb)  |  收藏  |  浏览/下载:331/226  |  提交时间:2020/08/26
Compressible boundary layer combustion  Skin-friction reduction  Boundary layer transition  Transition k-kl-w model  Hydrogen combustion  
On the application of dynamic zone flamelet model to large eddy simulation of supersonic hydrogen flame 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 41, 页码: 21940-21955
作者:  Yao W(姚卫)
Adobe PDF(3791Kb)  |  收藏  |  浏览/下载:260/131  |  提交时间:2020/09/27
Dynamic zone flamelet model  Supersonic hydrogen jet  Large eddy simulation  Supersonic combustion  Turbulent combustion model  
Evaluation of the influence of radiation on a GH2/GO2 rocket combustor 会议论文
AIAA Propulsion & Energy Forum, VIRTUAL EVENT, 2020-08-17
作者:  Li B(李波);  Yao W(姚卫);  Fan XJ(范学军)
Adobe PDF(1358Kb)  |  收藏  |  浏览/下载:150/45  |  提交时间:2021/02/01
PaSR和CMC模型在超声速燃烧模拟中的应用研究 学位论文
硕士论文,北京: 中国科学院大学, 2020
作者:  陈刘
Adobe PDF(5929Kb)  |  收藏  |  浏览/下载:845/11  |  提交时间:2020/09/28
超声速燃烧,湍流燃烧模型,部分搅拌反应器模型(pasr),条件矩封闭模型(cmc),可压缩性修正,大涡模拟(les)  
Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8
作者:  Ma KF(马凯夫);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(1657Kb)  |  收藏  |  浏览/下载:266/91  |  提交时间:2020/08/26
Scramjet engines  Shock-induced combustion ramjet engines  Supersonic combustion  Chapman-Jouguet detonation  
Study of shock train/flame interaction and skin-friction reduction by hydrogen combustion in compressible boundary layer 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2020, 卷号: 45, 期号: 31, 页码: 15683-15696
作者:  Xue R(薛瑞);  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3251Kb)  |  收藏  |  浏览/下载:339/111  |  提交时间:2020/07/06
Compressible boundary layer combustion  Skin-friction reduction  Shock train/flame interaction