中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
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CAS IR Grid
机构
力学研究所 [6]
采集方式
OAI收割 [6]
内容类型
会议论文 [6]
发表日期
2017 [4]
2013 [1]
2003 [1]
学科主题
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Development of zone flamelet model for scramjet combustor modeling
会议论文
OAI收割
Xiamen, China, 6-9 March 2017
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
会议论文
OAI收割
Xiamen, China, 6-9 March 2017
作者:
Wu K(吴坤)
;
Zhang P(张鹏)
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
收藏
  |  
浏览/下载:29/0
  |  
提交时间:2018/01/16
Combustion
Diesel Engines
Hydrogen
Large Eddy Simulation
Spacecraft
Stabilization
Supersonic Aircraft
Temperature Measurement
Wall Flow
Development of zone flamelet modelfor scramjet combustor modeling
会议论文
OAI收割
Xiamen, China, March 6, 2017 - March 9, 2017
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
  |  
收藏
  |  
浏览/下载:36/0
  |  
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
A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation
会议论文
OAI收割
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)
收藏
  |  
浏览/下载:37/0
  |  
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
Experimental and computational investigation of a full aircraft flutter at transonic speeds
会议论文
OAI收割
Bristol, United kingdom, June 24, 2013 - June 27, 2013
作者:
Qian W
;
Yang GW(杨国伟)
;
Luo JG
;
Yang R
;
Zhang GJ
  |  
收藏
  |  
浏览/下载:21/0
  |  
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
Numerical analyses of discrete gust response for a flexible aircraft
会议论文
OAI收割
21st AIAA Applied Aerodynamics Conference 2003, Orlando, FL, United states, June 23, 2003 - June 26, 2003
作者:
Yang GW(杨国伟)
;
Obayashi S
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2017/06/01
Direct-coupling method
Dynamic equations of motion
Flexible aircraft
Flexible airplane
Freedom of motion
One-minus-cosine gust
Quasi-steady model
Supersonic transport