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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 [11]
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Author:姜宗林
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Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle
期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(5479Kb)
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Submit date:2022/08/24
Multistage Launch Vehicle
Aerodynamic Characteristics
Shock Wave Interaction
Angle of Attack
Waverider
Boundary Layer Flow
Total Variation Diminishing
Adverse Pressure Gradient
Hypersonic Flows
Hypersonic Wind Tunnels
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)
Adobe PDF(1090Kb)
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities
Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework
期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40
Authors:
Zhang ZJ(张子健)
;
Wen CY
;
Liu YF(刘云峰)
;
Zhang DL(张德良)
;
Jiang ZL(姜宗林)
Adobe PDF(4374Kb)
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View/Download:415/142
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Submit date:2019/09/09
Two-phase detonation
CE/SE
Eulerian-Lagrangian
MPI
Aluminum-air detonation
Experimental investigation of liquid film cooling in hypersonic flow
期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 4, 页码: 10
Authors:
Yuan CK(苑朝凯)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
Adobe PDF(4383Kb)
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Submit date:2019/06/10
Spectral measurements of hypervelocity flow in an expansion tunnel
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Liu YF(刘云峰)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
Adobe PDF(1468Kb)
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Submit date:2019/04/11
Spectral measurement
Hypervelocity flow
Radiation
Expansion tunnel
Performance of Copper Calorimeter for Heat Transfer Measurement in High Enthalpy Shock Tunnel
期刊论文
JOURNAL OF THERMAL SCIENCE, 2018, 卷号: 27, 期号: 4, 页码: 373-381
Authors:
Wang Q(汪球)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
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Submit date:2018/10/30
copper calorimeter
high enthalpy shock tunnel
heat transfer
hypersonic
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
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
Numerical Study on the Performance of Nozzle Flow for Supersonic Chemical Oxygen-Iodine Lasers
期刊论文
ACTA MECHANICA SINICA, 2008, 卷号: 24, 期号: 2, 页码: 133-142
Authors:
Hu ZM(胡宗民)
;
Lv JM(吕俊明)
;
Jiang ZL(姜宗林)
;
Myong RS
;
Cho TH
;
Jiang, ZL (reprint author), CAS, Inst Mech, LHD, Beijing 100080, Peoples R China.
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Submit date:2016/01/11
Chemical Oxygen-iodine Laser (Coil)
Numerical Simulation
Small Signal Gains
Unsteady Structures
NUMERICAL ANALYSIS OF THE FLOWFIELD IN A SUPERSONIC COIL WITH AN INTERLEAVED JET CONFIGURATION AND ITS EFFECT ON THE GAIN DISTRIBUTION
期刊论文
Engineering Applications of Computational Fluid Mechanics, 2007, 卷号: 1, 期号: 3, 页码: 207-215
Authors:
Hu ZM(胡宗民)
;
Myong RS
;
Nguyen AT
;
Singh VP
;
Jiang ZL(姜宗林)
;
Cho TH
;
Myong, RS (reprint author), Gyeongsang Natl Univ, Res Ctr Aircraft Parts Technol, Jinju 660701, South Korea.
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Submit date:2009/08/03
Coil Without Buffer
Interleaved Jet
Flowfield
Small Signal Gain