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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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High-order simulation solving Navier-Stokes equations with Spalart–Allmaras turbulence model
会议论文
4th International Conference on Fluid Mechanics and Industrial Applications, FMIA 2020,, Asian Union of Information Technology, June 27, 2020 - June 28, 2020
Authors:
Yang L
;
岳连捷
;
张启帆
;
张新宇
Adobe PDF(1289Kb)
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View/Download:221/55
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Submit date:2021/01/12
Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model
会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
Authors:
Yao W(姚卫)
;
Chen L(陈留)
Adobe PDF(2272Kb)
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View/Download:279/149
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Submit date:2021/06/11
Multiple structure in oxy-hydrogen detonation propagation in rectangular tubes with an improved CE/SE scheme
会议论文
The 2nd International Symposium on Application of Materials Science and Energy Materials, Shanghai, China., December 17-18, 2018
Authors:
ShenY
;
Chen P
;
Zhang DL(张德良)
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Submit date:2019/05/30
AERODYNAMIC DRAG MEASUREMENT IN A HIGH-ENTHALPY SHOCK TUNNEL
会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
;
Teng HH(滕宏辉)
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View/Download:292/62
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Submit date:2019/04/19
Numerical study of oblique detonation initiations with chain-branching kinetics
会议论文
AIAA SciTech Forum - 55th AIAA Aerospace Sciences Meeting, Grapevine, Texas, 9-13 January 2017
Authors:
Teng HH(滕宏辉)
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
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Submit date:2018/01/16
Detailed transitional process of the flames in hot and diluted environments from lifted flames to MILD combustion
会议论文
10th U.S. National Combustion Meeting, College Park, MD, United states, April 23, 2017 - April 26, 2017
Authors:
Liu CY
;
Zhang J(张健)
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Submit date:2018/11/08
Oxygen
Diluted environments
Monotonic trend
Partial premixing
Stabilization mechanisms
Transition process
Transitional flames
Transitional process
Turbulent combustion
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Wang Q(汪球)
;
Li JW
;
Lu P
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
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  |  
Adobe PDF(679Kb)
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Submit date:2018/01/16
Calibration
Detonation
Heat Transfer
Nozzles
Spacecraft
Supersonic Aerodynamics
Thermodynamics
Uncertainty Analysis
Performance of a detonation driven shock tunnel
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Li JW
;
Wang Q(汪球)
;
Zhao W(赵伟)
;
Lu P
;
Tan YX
Adobe PDF(468Kb)
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Submit date:2018/01/16
Detonation
Gas Dynamics
Hypersonic Flow
Shock Tubes
Supersonic Aerodynamics
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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Submit date:2016/06/28
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)
Adobe PDF(6592Kb)
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View/Download:315/79
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Submit date:2017/05/05
Aerodynamic Forces
Chinese Academy Of Sciences
Different Structure
Digital Filtering
Large
Scale Modeling
Low
Frequency Vibration
Strain Gauge Balances
Strain Gauge Sensors