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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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reprint a... [13]
姜宗林 [13]
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Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel
期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:
Liu YF(刘云峰)
;
Wang YP(汪运鹏)
;
Yuan CK(苑朝凯)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
;
Liu, YF (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:2017/08/22
Aerodynamic Force And Moment Measurement
10° Half-angle Cone Model
Jf12
Real-gas Effects
Shock Tunnel
Theories and technologies for duplicating hypersonic flight conditions for ground testing
期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
Authors:
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.
;
Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
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Submit date:2017/11/29
Study on Mach stems induced by interaction of planar shock waves on two intersecting wedges
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 3, 页码: 362-368
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(滕宏辉)
;
Yang Y
;
Jiang ZL(姜宗林)
;
Wang, C (reprint author), Chinese Acad Sci, Inst Mech, 15 Beisihuan Xi Rd, Beijing 100190, Peoples R China.
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Submit date:2016/09/14
3d Shock/shock Interaction
Mach Interaction
Spatial Dimension Reduction
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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Submit date:2017/05/04
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
Wave system fitting: A new method for force measurements in shock tunnels with long test duration
期刊论文
MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2015, 卷号: 62-63, 页码: 2841-2848
Authors:
Luo CT(罗长童)
;
Wang YP(汪云鹏)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
;
Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:372/105
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Submit date:2016/01/07
Aerodynamic Force Measurements
Strain Gauge Balance
Inertia Compensation
Signal Decomposition
Accelerometer-free
Shock Tunnels
Numerical study of oblique detonation wave initiation in a stoichiometric hydrogen-air mixture
期刊论文
PHYSICS OF FLUIDS, 2015, 卷号: 27, 期号: 9, 页码: 96101
Authors:
Wang T
;
Zhang YN
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Ng HD
;
Wang, T (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:2016/01/08
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
Approximate analytic solution of heat conduction in hollow semi-spheres flying at hypersonic speed
期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2013, 卷号: 43, 页码: 46-52
Authors:
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
;
Han, GL (reprint author), Chinese Acad Sci, Stake Key Lab High Temp Gas Dynam LHD, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2013/05/31
Heat Conduction
Theoretical Investigation
Approximate Solution
Hypersonic
Concept of non-ablative thermal protection system for hypersonic vehicles
期刊论文
AIAA Journal, 2013, 卷号: 51, 期号: 3, 页码: 584-590
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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View/Download:1415/508
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Submit date:2013/04/07
Flow Fields
Flow Visualization
Hypersonic Aerodynamics
Hypersonic Vehicles
Mach Number
Shock Waves
Thermal Insulating Materials
Engineering Applications
Experimental Datum
Hypersonic Wind Tunnels
Numerical Results
Stagnation Points
Thermal Protection
Thermal Protection System
Working Pressures
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