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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
A Multi-space Interrelation Theory for Correlating Aerodynamic Data from Hypersonic Ground Testing
会议论文
31st International Symposium on Shock Waves, Nagoya, Japan, 2017-07-9~14
Authors:
Jiang ZL(姜宗林)
;
Luo ZT(罗长童)
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Submit date:2020/01/06
Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Wu K(吴坤)
;
Fan XJ(范学军)
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View/Download:411/153
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Submit date:2018/06/06
Development of zone flamelet model for scramjet combustor modeling
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Yao W(姚卫)
;
Fan XJ(范学军)
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Submit date:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
Force Test in a Large-Scale Shock Tunnel
会议论文
55th AIAA Aerospace Sciences Meeting , Grapevine, Texas, 9-13 January 2017
Authors:
Wang YP(汪运鹏)
;
Liu YF(刘云峰)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
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Submit date:2018/01/16
Development of zone flamelet modelfor scramjet combustor modeling
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors:
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(832Kb)
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View/Download:294/88
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Submit date:2018/11/08
Combustion
Cost benefit analysis
Costs
Mixtures
Ramjet engines
Supersonic aircraft
Computational costs
Equivalence ratios
Local flow conditions
Scramjet combustors
Statistics approaches
Supersonic combustion
Supersonic combustors
Turbulent combustion
Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Xiao Y(肖尧)
;
Cui K(崔凯)
;
Li GL(李广利)
;
Xu YZ(徐应洲)
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Adobe PDF(639Kb)
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View/Download:287/90
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Submit date:2018/01/16
Aerodynamics
Air Engines
Aspect Ratio
Computational Fluid Dynamics
Drag
Engines
Hypersonic Aerodynamics
Lift
Lift Drag Ratio
Propulsion
Spacecraft
Vehicles
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)
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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
A conceptual design of next generation hypersonic air-breathing airplanes with dual waveriders forebody
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Cui K(崔凯)
;
Hu SC(胡守超)
;
Li GL
;
Xiao Y(肖尧)
;
Situ M
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Adobe PDF(872Kb)
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View/Download:367/157
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Submit date:2017/05/05
Aero
Dynamic Performance
Aerodynamic Performance Predictions
Design Methodology
Flight Altitudes
Numerical Results
Propulsion System
Turbulent Models
Wing Body Aircraft
Research on compressible flow around cylinder and truncated cone with LES method
会议论文
4th International Conference on Structures and Building Materials, ICSBM 2014, Guangzhou, China, March 15, 2014 - March 16, 2014
Authors:
Zhao M
;
Mao J
;
Yang GW(杨国伟)
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Submit date:2017/05/27
Flow Around Circular Cylinder
Flow Around Cylinder
Flow Filed
High Reynolds Number
Les
Pressure Coefficients
Sub-grid Scale Models
Vortex Street