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姜宗林 [6]
胡宗民 [6]
吴波 [2]
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Creator:姜宗林
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On theory and methods for advanced detonation-driven hypervelocity shock tunnels
期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:
Jiang ZL(姜宗林)
;
Li JP(李进平)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Yu HR(俞鸿儒)
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities
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
Development of the detonation-driven expansion tube for orbital speed experiments
期刊论文
Science China-Technological Sciences, 2015, 卷号: 58, 期号: 4, 页码: 695-700
Authors:
Jiang ZL(姜宗林)
;
Wu B(吴波)
;
Gao YL
;
Zhao W(赵伟)
;
Hu ZM(胡宗民)
;
Jiang, ZL (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:2015/04/28
Detonation Driver
Shock-expansion Tube
High-enthalpy Flow
Test Flow
A New Flux Splitting Scheme for Euler Equations of Gas Dynamics
会议论文
International Conference on Numerical Analysis and Applied Mathematics, Rhodes GREECE, SEP 22-28 2014
Authors:
Li XD(李馨东)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
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Submit date:2015/09/29
Flux Splitting
Hybrid Upwind Method
Ausm Scheme
K-cusp Scheme
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
Analysis of the test condition of a shock-expansion tube: JF-16
会议论文
First International Conference on High Temperature Gas Dynamics, Beijing, 2012-10
Authors:
Hu ZM(胡宗民)
;
Wu B(吴波)
;
Jiang ZL(姜宗林)
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Submit date:2013/03/16
Shock-expansion Tube
Computation
Spurious Oscillation
Flus Splliting