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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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Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model
会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
Authors:
Yao W(姚卫)
;
Chen L(陈留)
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Submit date:2021/06/11
Numerical Study of Heat Transfer on Confined Under-Expanded Impinging Jet from Slot into a Plenum
会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(714Kb)
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View/Download:36/17
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Submit date:2023/03/17
Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon
会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
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Submit date:2020/01/06
Experimental Studies of Film Cooling in Supersonic Combustors
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Fan C(樊川)
;
Wang J(王晶)
;
Fan XJ(范学军)
Adobe PDF(735Kb)
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Submit date:2018/01/16
Combustion
Combustors
Coolants
Kerosene
Spacecraft
Supersonic Aerodynamics
Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Li GL(李广利)
;
Cui K(崔凯)
;
Xiao Y(肖尧)
;
Xu YZ(徐应洲)
Adobe PDF(664Kb)
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Submit date:2018/01/16
Aerodynamics
Angle Of Attack
Angle Of Attack Indicators
Boundary Layers
Drag
Drag Coefficient
High Pressure Effects
Hypersonic Aerodynamics
Hypersonic Flow
Spacecraft
Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Wang Q(汪球)
;
Li JW
;
Lu P
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
Adobe PDF(679Kb)
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Submit date:2018/01/16
Calibration
Detonation
Heat Transfer
Nozzles
Spacecraft
Supersonic Aerodynamics
Thermodynamics
Uncertainty Analysis
Performance of a detonation driven shock tunnel
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Li JW
;
Wang Q(汪球)
;
Zhao W(赵伟)
;
Lu P
;
Tan YX
Adobe PDF(468Kb)
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Submit date:2018/01/16
Detonation
Gas Dynamics
Hypersonic Flow
Shock Tubes
Supersonic Aerodynamics
Starting Process in a Large-Scale Shock Tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:
Wang YP
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/06/28
Role of wall temperature on shock train in a rectangular isolator
会议论文
52nd AIAA/SAE/ASEE Joint Propulsion Conference, 2016, Salt Lake City, UT, United states, July 25, 2016 - July 27, 2016
Authors:
Lu HB
;
Wang D
;
Chen X
;
Yue LJ(岳连捷)
;
Ji, Feng (yuelj@imech.ac.cn)
Adobe PDF(560Kb)
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Submit date:2017/05/05
Aero
Heating
Dual Mechanisms
On Flow
Shock Train
Specific Heat Ratio
Total Pressure
Total Temperatures
Wall Temperatures
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor
会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
Authors:
Cheng D(程迪)
;
Wang J(王晶)
;
Gong J
;
Lu Y(陆阳)
;
Yao W(姚卫)
;
Li L(李龙)
;
Fan XJ(范学军)
;
Fan, Xuejun (xfan@imech.ac.cn)
Adobe PDF(2131Kb)
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Submit date:2017/05/05
Equivalence Ratios
Heat Flux Distributions
Heat Transfer Characteristics
Scramjet
Supercritical Kerosenes
Supersonic Combustion
Supersonic Combustors
Total Temperatures