×
验证码:
换一张
忘记密码?
记住我
切换中国科技网通行证登录
×
切换中国科技网通行证登录
登录
中文版
|
English
中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
登录
注册
ALL
ORCID
题名
作者
导师
关键词
文献类型
出处
出版者
发表日期
存缴日期
收录类别
资助项目
DOI
学习讨论厅
图片搜索
粘贴图片网址
首页
研究单元&专题
作者
文献类型
学科分类
知识图谱
新闻&公告
在结果中检索
研究单元&专题
高温气体动力学国家重... [9]
作者
范学军 [5]
姚卫 [4]
张新宇 [2]
王晶 [2]
Chen LZ [1]
Lee YC [1]
更多...
文献类型
会议论文 [9]
发表日期
2017 [9]
语种
英语 [9]
出处
21st AIAA ... [9]
收录类别
EI [9]
资助项目
资助机构
导师
×
知识图谱
IMECH-IR
开始提交
已提交作品
待认领作品
已认领作品
未提交全文
收藏管理
QQ客服
官方微博
反馈留言
浏览/检索结果:
共9条,第1-9条
帮助
限定条件
出处:21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
已选(
0
)
清除
条数/页:
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
排序方式:
请选择
题名升序
题名降序
期刊影响因子升序
期刊影响因子降序
发表日期升序
发表日期降序
WOS被引频次升序
WOS被引频次降序
作者升序
作者降序
提交时间升序
提交时间降序
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)
浏览
  |  
Adobe PDF(1173Kb)
  |  
收藏
  |  
浏览/下载:434/214
  |  
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 Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:
Cheng LW(程柳维)
;
Zhong FQ(仲峰泉)
;
Wang ZP(王知溥)
;
Gu HB(顾洪斌)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
浏览
  |  
Adobe PDF(517Kb)
  |  
收藏
  |  
浏览/下载:307/99
  |  
提交时间:2018/01/16
Combustors
Cracks
Diesel Engines
Efficiency
Ethylene
Fighter Aircraft
Fuels
High Speed Cameras
Ignition
Kerosene
Luminance
Spacecraft
Stabilization
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, 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)
浏览
  |  
Adobe PDF(1249Kb)
  |  
收藏
  |  
浏览/下载:294/87
  |  
提交时间:2018/01/16
Combustion
Diesel Engines
Hydrogen
Large Eddy Simulation
Spacecraft
Stabilization
Supersonic Aircraft
Temperature Measurement
Wall Flow
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)
浏览
  |  
Adobe PDF(704Kb)
  |  
收藏
  |  
浏览/下载:254/86
  |  
提交时间:2018/01/16
Spacecraft
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
作者:
Fan C(樊川)
;
Wang J(王晶)
;
Fan XJ(范学军)
浏览
  |  
Adobe PDF(735Kb)
  |  
收藏
  |  
浏览/下载:305/99
  |  
提交时间:2018/01/16
Combustion
Combustors
Coolants
Kerosene
Spacecraft
Supersonic Aerodynamics
A low-dissipation solver based on openFOAM designed for large eddy simulation in compressible flow
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:
Lee YC
;
Yao W(姚卫)
;
Fan XJ(范学军)
浏览
  |  
Adobe PDF(1377Kb)
  |  
收藏
  |  
浏览/下载:476/90
  |  
提交时间:2018/11/08
Computational Fluid Dynamics
Digital Storage
Kinetic Energy
Kinetics
Open Source Software
Open Systems
Ramjet Engines
Runge Kutta Methods
Shock Tubes
Turbulence
Two Phase Flow
Bench
Mark Problems
Central
Upwind Scheme
Computational Fluid Dynamics Software
Skew
Symmetric Forms
Temporal Discretization
Turbulence Structures
Unstructured Meshes
Wall Bounded Turbulence
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)
浏览
  |  
Adobe PDF(832Kb)
  |  
收藏
  |  
浏览/下载:267/80
  |  
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
Multispecies Absorption Measurement in an Ammonium Dinitramide based Thruster
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:
Zeng W(曾徽)
;
Lin X(林鑫)
;
Zhen RP
;
Chen LZ
;
Li F(李飞)
;
Yu XL(余西龙)
;
Li, Fei(lifei@imech.ac.cn)
浏览
  |  
Adobe PDF(897Kb)
  |  
收藏
  |  
浏览/下载:445/94
  |  
提交时间:2018/01/16
Combustion
Gas Absorption
Infrared Devices
Monopropellants
Optical Parametric Oscillators
Spacecraft
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
作者:
Xiao Y(肖尧)
;
Cui K(崔凯)
;
Li GL(李广利)
;
Xu YZ(徐应洲)
浏览
  |  
Adobe PDF(639Kb)
  |  
收藏
  |  
浏览/下载:274/88
  |  
提交时间:2018/01/16
Aerodynamics
Air Engines
Aspect Ratio
Computational Fluid Dynamics
Drag
Engines
Hypersonic Aerodynamics
Lift
Lift Drag Ratio
Propulsion
Spacecraft
Vehicles