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State Key... [19]
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姜宗林 [19]
reprint au... [6]
汪运鹏 [5]
王粤 [5]
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刘云峰 [3]
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Creator:姜宗林
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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
Unsteady interaction mechanism of transverse stage separation in hypersonic flow for a two-stage-to-orbit vehicle
期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 5, 页码: 056120
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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Submit date:2023/05/26
Two-stage-to-orbit
Hypersonic
Numerical simulation
Stage separation
Aerodynamic interaction
Unsteady flow
Center of gravity
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)
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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)
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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
Shock relations in gases of heterogeneous thermodynamic properties
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:
Hu ZM(胡宗民)
;
Zhou K(周凯)
;
Peng J(彭俊)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
;
Li, JP (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:2017/10/25
Shock Wave
Imperfect Gas
Heterogeneous
Theoretical Solution
Influence of Thermal Sensor Installation on Measuring Accuracy at Stagnation Points
期刊论文
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2017, 卷号: 31, 期号: 2, 页码: 318-323
Authors:
Wang Q(汪球)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
;
Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
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Submit date:2017/10/27
高超声速电离绕流中电子密度的静电探针测量方法研究
期刊论文
实验流体力学, 2013, 卷号: 27, 期号: 6, 页码: 64-69+85
Authors:
汪球
;
赵伟
;
余西龙
;
姜宗林
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Submit date:2014/01/24
静电探针
电子密度
高超声速
高焓激波风洞
Electrostatic Probe
Electron Density
Hypersonic
High Enthalpy Shock Tunnel
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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View/Download:1110/331
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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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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