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Starting Process in a Large-Scale Shock Tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:  Wang YP;  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林);  Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Force measurement in a shock tunnel with 100 milliseconds test duration 会议论文
34th AIAA Applied Aerodynamics Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
Authors:  Wang YP(汪运鹏);  Liu YF(刘云峰);  Luo ZT(罗长童);  Jiang ZL(姜宗林)
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Aerodynamic Forces  Chinese Academy Of Sciences  Different Structure  Digital Filtering  Large  Scale Modeling  Low  Frequency Vibration  Strain Gauge Balances  Strain Gauge Sensors  
Plasma Assisted Low Temperature Combustion 会议论文
22nd International Symposium on Plasma Chemistry (ISPC 22), Antwerp, BELGIUM, JUL 05-10, 2015
Authors:  Ju YG;  Lefkowitz JK;  Reuter CB;  Won SH;  Yang XL;  Yang S;  Sun WT;  Jiang ZL(姜宗林);  Chen Q;  Ju, YG (reprint author), Princeton Univ, Dept Mech & Aerosp Engn, Princeton, NJ 08544 USA.
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Plasma Assisted Combustion  Low Temperature Chemistry  Kinetics  Cool Flames  S-curve Transition  Nonequilibrium Plasma  Saturated-hydrocarbons  Diffusion Flames  Pulsed Discharge  Ignition  Mixtures  Oxidation  Kinetics  Enhancement  
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
Authors:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle 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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Flux Splitting  Hybrid Upwind Method  Ausm Scheme  K-cusp Scheme  
Development of the advanced high-enthalpy test facility for hypersonic vehicles 会议论文
The 29th International Symposium on Rarefied Gas Dynamics, 中国陕西西安, 2014-07-13
Authors:  Jiang ZL(姜宗林);  Yu HR(俞鸿儒)
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Enthalpy  Facility  Challenging  Capable  Aerospace  Promoting  Detonation  Viewing  Facilities  Tunnel  
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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Shock-expansion Tube  Computation  Spurious Oscillation  Flus Splliting  
The applicability of Mach number independence principle in case of hypersonic thermo-chemical nonequilibrium flow 会议论文
First International Conference on High Temperature Gas Dynamics, Beijing, 2012
Authors:  Li K(李康);  Li JP(李进平);  Jiang ZL(姜宗林)
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Keywords: Mach Number Independence  Oswatitsch  Nonequilibrium Flow  Real-gas Effect  Expansion Effect  
Vortex generation arising from the interaction of shock wave and fuel bubble 会议论文
The Sixth Across-strait Workshop on Shock/Vortex Interaction, Guiyang, 2012-07
Authors:  Hu ZM(胡宗民);  Jiang ZL(姜宗林);  Dou HS
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CFD for chemically reacting flow and its applications 会议论文
International Conference on Advanced Aircraft Technologies 2012, South Korea, 2012-5
Authors:  Hu ZM(胡宗民);  Sun XF;  Jiang ZL(姜宗林)
Adobe PDF(1482Kb)  |  Favorite  |  View/Download：619/152  |  Submit date：2013/03/16