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Numerical study of high temperature non-equilibrium effects of double-wedge in hypervelocity flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 124, 页码: 17
Authors:
Dai, Chunliang
;
Sun, Bo
;
Zhuo, Changfei
;
Zhou, Shengbing
;
Zhou, Changsheng
;
Yue LJ(岳连捷)
Adobe PDF(6822Kb)
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View/Download:198/35
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Submit date:2022/07/18
Hypervelocity double-wedge flow
High temperature non-equilibrium effects
Laminar and turbulence flow
Shock wave interaction
Shock wave
boundary layer interaction
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
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View/Download:301/73
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Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
斜爆轰波系在受限空间内的演变及其临界条件的数值研究
期刊论文
推进技术, 2021, 卷号: 42, 期号: 04, 页码: 738-744
Authors:
彭俊
;
马嘉文
;
杨鹏飞
;
胡宗民
Adobe PDF(4986Kb)
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View/Download:371/91
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Submit date:2021/04/19
斜爆轰发动机
波系结构
临界条件
受限空间
激波反射
Formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3599Kb)
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View/Download:382/94
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Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation
Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel
期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(1471Kb)
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View/Download:264/61
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Submit date:2020/07/06
Experimental and Numerical Study on Hypersonic Flow over Double-Wedge Configuration
期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 9, 页码: 3227-3230
Authors:
Meng BQ(孟宝清)
;
Han GL(韩桂来)
;
Yuan CK(苑朝凯)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(207Kb)
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View/Download:510/115
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Submit date:2018/01/04
超高速流动模拟及热化学反应模型对比研究
期刊论文
北京航空航天大学学报, 2017, 卷号: 43, 期号: 06, 页码: 1173-1181
Authors:
周凯
;
李旭东
;
胡宗民
;
姜宗林
Adobe PDF(652Kb)
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View/Download:404/81
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Submit date:2017/12/22
超高速
膨胀管
数值模拟
热化学反应模型
适用范围
High-Pressure Capturing Wing Configurations
期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
Authors:
Cui K(崔凯)
;
Li GL
;
Xiao Y(肖尧)
;
Xu YZ
;
Cui,K(reprint author), Chinese Acad Sci, Inst Mech
Adobe PDF(671Kb)
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View/Download:660/189
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Submit date:2017/07/24
On the numerical technique for the simulation of hypervelocity test flows
期刊论文
Computers & Fluids, 2015, 卷号: 106, 页码: 12-18
Authors:
Hu ZM(胡宗民)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
;
Khoo BC
;
Hu ZM(胡宗民)
Adobe PDF(1617Kb)
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View/Download:1603/929
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Submit date:2014/11/27
Hypervelocity Test Flow
Dcd Scheme
Flux-splitting
Spurious Oscillation
Numerical investigation on three-dimensional shock wave reflection over two perpendicularly intersecting wedges
期刊论文
SHOCK WAVES, 2012, 卷号: 22, 期号: 2, 页码: 151-159
Authors:
Yang Y(杨旸)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Takayama K
;
Yang, Y
;
Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2013/01/18
Shock Wave Reflection
Three-dimensional Mach Stem
Perpendicularly Intersecting Wedges
Numerical Simulation
Mach-reflection
Steady Flows
Transition
Reconsideration