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A Data-Correlation Model of Aerodynamic Heating Based on Globally Optimal Learning Method
会议论文
16th International Conference on Natural Computation, Fuzzy Systems and Knowledge Discovery (ICNC-FSKD 2020), 西安,中国, 19-21 December 2020
作者:
Chen Z(陈阵)
;
Li S(李森)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
Adobe PDF(1545Kb)
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浏览/下载:145/39
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提交时间:2021/02/01
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
作者:
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)
浏览
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Adobe PDF(805Kb)
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浏览/下载:392/146
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提交时间:2018/06/06
INFLUENCE OF TYPICAL SUBGRADE STRUCTURES ON AERODYNAMIC CHARACTERISTICS OF HIGH SPEED TRAINS IN CROSS WIND CONDITIONS
会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
作者:
Sun ZX(孙振旭)
;
Yang GW(杨国伟)
Adobe PDF(1819Kb)
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浏览/下载:232/40
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提交时间:2019/04/19
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:
Yao W(姚卫)
;
Yuan YM(袁越明)
;
Li XP(李晓鹏)
;
Wang J(王晶)
;
Fan XJ(范学军)
;
Fan, Xuejun(xfan@imech.ac.cn)
Adobe PDF(1173Kb)
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浏览/下载:440/216
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提交时间:2018/01/16
Adiabatic Flame Temperature
Aerodynamics
Boundary Layer Flow
Boundary Layers
Chemical Analysis
Combustion
Computational Chemistry
Directed Graphs
Flow Separation
Mach Number
Principal Component Analysis
Regression Analysis
Sensitivity Analysis
Spacecraft
Supersonic Aerodynamics
Supersonic Aircraft
Transients
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
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(623Kb)
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浏览/下载:259/88
  |  
提交时间:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
Downstream pressure variation induced hysteresis in the scramjet isolator
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH
;
Jia YN(贾轶南)
;
Zhang XY(张新宇)
;
Yue, Lianjie(yuelj@imech.ac.cn)
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Adobe PDF(704Kb)
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浏览/下载:259/90
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提交时间:2018/01/16
Spacecraft
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
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
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Adobe PDF(832Kb)
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浏览/下载:274/81
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提交时间: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
Starting Process in a Large-Scale Shock Tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
作者:
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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Adobe PDF(764Kb)
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浏览/下载:351/98
  |  
提交时间: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
作者:
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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浏览/下载:257/88
  |  
提交时间: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
作者:
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)
浏览
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Adobe PDF(2131Kb)
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浏览/下载:322/123
  |  
提交时间:2017/05/05
Equivalence Ratios
Heat Flux Distributions
Heat Transfer Characteristics
Scramjet
Supercritical Kerosenes
Supersonic Combustion
Supersonic Combustors
Total Temperatures