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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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力学所知识产出(19... [2]
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姜宗林 [10]
胡宗民 [10]
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基于第二粘性的Navier-Stokes方程组求解正激波结构
期刊论文
计算物理, 2020, 卷号: 37, 期号: 5, 页码: 505-513
Authors:
李馨东
;
赵英奎
;
胡宗民
;
姜宗林
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Submit date:2019/12/16
Navier-Stokes方程
Stokes假设
第二粘性
体积粘性,正激波结构
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
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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Submit date:2019/09/09
Shock reflection
Vibration excitation
Mach reflection
Transition criterion
Hypersonic flow
Shock relations in gases of heterogeneous thermodynamic properties
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:
Hu ZM(胡宗民)
;
Zhou K(周凯)
;
Peng J(彭俊)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
;
Li, JP (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:2017/10/25
Shock Wave
Imperfect Gas
Heterogeneous
Theoretical Solution
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
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Hu ZM(胡宗民)
;
Li XD
;
Jiang ZL(姜宗林)
;
Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
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Submit date:2016/12/08
3d Asymmetrical Shock/shock Interaction
Spatial-dimension Reduction
Mach Reflection
Flow Field
Theoretical Analysis
Adaptive space transformation: An invariant based method for predicting aerodynamic coefficients of hypersonic vehicles
期刊论文
Engineering Applications of Artificial Intelligence, 2015, 卷号: 46, 页码: 93-103
Authors:
Luo CT(罗长童)
;
Hu ZM(胡宗民)
;
Zhang SL
;
Jiang ZL(姜宗林)
;
Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/01/07
Aerodynamic Coefficient
Data Correlation
Scaling Parameter
Genetic Programming
Invariant
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 study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows
期刊论文
SHOCK WAVES, 2008, 卷号: 18, 期号: 1, 页码: 41-51
Authors:
Hu ZM(胡宗民)
;
Myong R S
;
Wang C(王春)
;
Cho T H
;
Jiang ZL(姜宗林)
Adobe PDF(954Kb)
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Submit date:2020/08/26
Shock
Shock Interaction
Oscillation
Hypersonic
Double-wedge
Numerical Study
Numerical Investigation On Detonation Cell Evolution In A Channel With Area-Changing Cross Section
期刊论文
Science In China Series G-Physics Mechanics & Astronomy, 2007, 页码: 797-808
Authors:
Deng B(邓博)
;
Hu ZM(胡宗民)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Deng, B (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temperature Gas Dynam, Beijing 100080, Peoples R China.
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Submit date:2009/08/03
Detonation Cells
Transverse Waves
Detailed Chemical Reaction Model
Numerical Simulation
Shock