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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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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
作者:
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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浏览/下载:363/69
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提交时间: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
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
作者:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2434Kb)
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浏览/下载:305/81
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提交时间: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
The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:
Jia YN(贾轶南)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
;
Jia, Yinan(yuelj@imech.ac.cn)
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Adobe PDF(566Kb)
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浏览/下载:325/70
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提交时间:2018/01/16
Boundary Layer Flow
Boundary Layers
Spacecraft
Wind Tunnels
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
作者:
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.
Adobe PDF(5046Kb)
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浏览/下载:1380/493
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提交时间: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
Experimental and computational investigation of a full aircraft flutter at transonic speeds
会议论文
International Forum on Aeroelasticity and Structural Dynamics, IFASD 2013, Bristol, United kingdom, June 24, 2013 - June 27, 2013
作者:
Qian W
;
Yang GW(杨国伟)
;
Luo JG
;
Yang R
;
Zhang GJ
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浏览/下载:152/0
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提交时间:2018/11/08
Aeroelasticity
Aircraft manufacture
Airframes
Computational fluid dynamics
Elastic waves
Flutter (aerodynamics)
Structural dynamics
Supersonic aircraft
Transonic aerodynamics
Viscous flow
Wind stress
Wind tunnels
Aircraft structure
CFD simulations
CFD/CSD
Computational investigation
Flutter boundary predictions
Transonic flutter
Unsteady aerodynamics
Wind tunnel tests
Aerodynamic design on China new high-speed trains
会议论文
1st International Workshop on High-Speed and Intercity Railways, IWHIR 2011, Shenzhen, Hong Kong, China, JULY 19-22, 2011
作者:
Yang GW(杨国伟)
;
Yang GW(杨国伟)
Adobe PDF(553Kb)
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浏览/下载:730/231
  |  
提交时间:2013/02/06
Railroad Cars
Railroad Transportation
Railroad Tunnels
Railroads
Wind Effects
Aerodynamic Designs
Aerodynamic Noise
Aerodynamic Performance
Cross-wind Effects
High Speed Trains
Pressure Waves
Running Conditions
Running Tests
Running-in
Wind Tunnel Experiment