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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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姜宗林 [12]
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Indexed By:EI
Creator:姜宗林
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Document Type:会议论文
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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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Submit date:2019/04/19
THE MECHANISM OF THREE-DIMENSION STEADY SHOCK WAVE INTERACTION
会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
Authors:
Wang C(王春)
;
Yang RX(杨瑞欣)
;
Jiang ZL(姜宗林)
Adobe PDF(3021Kb)
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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)
Adobe PDF(464Kb)
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Submit date:2018/01/16
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)
Adobe PDF(679Kb)
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Submit date:2018/01/16
Calibration
Detonation
Heat Transfer
Nozzles
Spacecraft
Supersonic Aerodynamics
Thermodynamics
Uncertainty Analysis
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.
Adobe PDF(764Kb)
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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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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
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)
Adobe PDF(5104Kb)
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Submit date:2017/05/05
Inviscid Flows
Numerical Investigations
Outlet Diameters
Reflected Shock Waves
Simulated Results
Starting Process
Transmitted Shock
Unsteady Nozzle Flow
Concept of non-ablative thermal protection system for hypersonic vehicles
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, APR 11-14, 2011
Authors:
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2013/12/12
Conceptual Study on Non-ablative TPS for Hypersonic Vehicles
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, United states, APR 11-14, 2011
Authors:
Jiang ZL(姜宗林)
;
Liu YF(刘云峰)
;
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
Adobe PDF(1058Kb)
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Submit date:2014/02/24
An Integrated Evolutionary Algorithm for Expensive Global Optimization
会议论文
2010 Sixth International Conference on Natural Computation (ICNC 2010), 烟台, 2010-08-10~2010-08-12
Authors:
Luo CT(罗长童)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
;
Zhang SL
;
Luo ZT(罗长童)
Adobe PDF(121Kb)
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Submit date:2010/08/20
Expensive Global Optimization
Evolutionary Computation
Low Dimensional Simplex Evolution
Radial Basis Function
Response Surface
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