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| Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
作者: Huang TL(黄庭隆); Yue LJ(岳连捷) ; Ma SH(马生虎); Zhang QF(张启帆); Zhang, Peng; Zhang XY(张新宇)
 Adobe PDF(3937Kb) |  收藏 | 浏览/下载：187/44 | 提交时间：2021/03/30
Adverse pressure gradient Back pressure Hysteresis effects Non-uniform flow Shock train |
| Numerical investigation of flow structures resulting from the interaction between an oblique detonation wave and an upper expansion corner 期刊论文
JOURNAL OF FLUID MECHANICS, 2020, 卷号: 903, 页码: 17
作者: Wang KL(王宽亮); Teng HH(滕宏辉); Yang PF(杨鹏飞); Ng HD
Adobe PDF(1764Kb) | 收藏 | 浏览/下载：245/67 | 提交时间：2020/11/30
detonation waves |
| 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：253/69 | 提交时间：2020/12/28
PROJECTILE MECHANISM SYSTEMS |
| Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
作者: Zhang ZJ(张子健); Ma KF(马凯夫); Zhang WS(张文硕); Han X(韩鑫); Liu YF(刘云峰); Jiang ZL(姜宗林)
Adobe PDF(2608Kb) | 收藏 | 浏览/下载：265/110 | 提交时间：2020/11/30
Oblique detonation engine Pre-injection Detonative combustion Mixing Hydrogen |
| 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：253/103 | 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 |
| 过热流动和闪急沸腾雾化过程的数值模拟研究 学位论文
博士论文，北京: 中国科学院大学, 2020
作者: 李亚超
 Adobe PDF(22044Kb) | 收藏 | 浏览/下载：478/7 | 提交时间：2020/08/27
过热流动，闪急沸腾雾化， 气泡生长模型，过热液滴破碎模型， 过热相变模型 |
| 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 |
