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姜宗林 [7]
胡宗民 [7]
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Creator:姜宗林
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Creator:胡宗民
Document Type:期刊论文
Community:高温气体动力学国家重点实验室
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Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors:
Peng J(彭俊)
;
Zhang ZJ(张子健)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
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View/Download:424/99
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Submit date:2019/09/09
Shock reflection
Vibration excitation
Mach reflection
Transition criterion
Hypersonic flow
Spectral measurements of hypervelocity flow in an expansion tunnel
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Liu YF(刘云峰)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
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View/Download:361/108
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Submit date:2019/04/11
Spectral measurement
Hypervelocity flow
Radiation
Expansion tunnel
Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263
Authors:
Fang YS(方宜申)
;
Hu ZM(胡宗民)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Ng HD
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Submit date:2018/02/08
Oblique Detonation
Equivalence Ratio
Mixture Inhomogeneity
Detailed Chemistry
Continuum perspective of bulk viscosity in compressible fluids
期刊论文
JOURNAL OF FLUID MECHANICS, 2017, 卷号: 812, 页码: 966-990
Authors:
Li XD
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
;
Hu, ZM (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2017/04/26
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)
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View/Download:1602/928
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Submit date:2014/11/27
Hypervelocity Test Flow
Dcd Scheme
Flux-splitting
Spurious Oscillation
Numerical simulation of deflagration to detonation transition in a straight duct: Effects of energy release and detonation stability
期刊论文
Advances in Applied Mathematics and Mechanics, 2014, 卷号: 6, 期号: 6, 页码: 718-731
Authors:
Dou HS
;
Hu ZM(胡宗民)
;
Khoo BC
;
Jiang ZL(姜宗林)
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Submit date:2014/11/27
Numerical Simulation
Detonation
Ddt
Energy Release
Duct