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State Key... [12]
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姜宗林 [12]
汪运鹏 [5]
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刘云峰 [4]
王粤 [4]
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Indexed By:SCI
Creator:姜宗林
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Language:英语
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Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration
期刊论文
Physics of Fluids, 2024, 卷号: 36, 页码: 016116
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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Submit date:2024/01/15
Two-stage-to-orbit
Wind tunnel test
Numerical simulation
Stage separation
Hypersonic
Shock waves
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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View/Download:434/83
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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
Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System
期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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Submit date:2022/11/14
Two-stage to orbit
Numerical simulation
Stage separation
Hypersonic flow
Aerodynamic interference
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel
期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2434Kb)
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Submit date:2022/08/23
Aerodynamic Coefficients
Two Stage to Orbit
Aerodynamic Performance
Hypersonic Flight
Hypersonic Wind Tunnels
Solenoid Valves
Oblique Shock
Pneumatic Actuator
Hypersonic Flows
Computer Aided Engineering
Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel
期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(1471Kb)
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Submit date:2020/07/06
Numerical simulation of the interaction of two shear layers in double backward-facing steps
期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 5, 页码: 15
Authors:
Deng F(邓放)
;
Han GL(韩桂来)
;
Liu MK(刘美宽)
;
Ding, J
;
Weng, PF
;
Jiang ZL(姜宗林)
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Submit date:2019/10/21
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)
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Submit date:2019/04/11
Spectral measurement
Hypervelocity flow
Radiation
Expansion tunnel
Three-dimensional shock wave configurations induced by two asymmetrical intersecting wedges in supersonic flow
期刊论文
SHOCK WAVES, 2018, 卷号: 28, 期号: 2, 页码: 311-319
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(腾宏辉)
;
Jiang ZL(姜宗林)
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Submit date:2018/10/30
Supersonic Flow
3d Shock/shock Interaction
3d Asymmetrical Wave Configurations
Spatial Dimension Reduction
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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View/Download:532/133
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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
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