×
验证码:
换一张
Forgotten Password?
Stay signed in
China Science and Technology Network Pass Registration
×
China Science and Technology Network Pass Registration
Log In
Chinese
|
English
中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
Log In
Register
ALL
ORCID
Title
Creator
Thesis Advisor
Keyword
Document Type
Source Publication
Publisher
Date Issued
Date Accessioned
Indexed By
Funding Project
DOI
Study Hall
Image search
Paste the image URL
Home
Collections
Authors
DocType
Subjects
K-Map
News
Search in the results
Collection
State Key... [14]
力学所知识产出(19... [3]
Creator
范学军 [17]
姚卫 [9]
俞刚 [4]
李建国 [4]
李晓鹏 [4]
陆阳 [4]
More...
Document Type
Conferenc... [17]
Date Issued
2021 [1]
2020 [1]
2018 [1]
2017 [4]
2016 [1]
2015 [3]
More...
Language
英语 [17]
Source Publication
21st AIAA ... [3]
49th AIAA/... [2]
20th AIAA ... [1]
40th AIAA/... [1]
41st AIAA/... [1]
AIAA Propu... [1]
More...
Indexed By
EI [14]
CPCI-S [2]
Funding Project
Funding Organization
Aerojet Ro... [2]
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
(Note: the search results are based on claimed items)
Browse/Search Results:
1-10 of 17
Help
Filters
Language:英语
Document Type:会议论文
Author:范学军
First author
Selected(
0
)
Clear
Items/Page:
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
Sort:
Select
WOS Cited Times Ascending
WOS Cited Times Descending
Title Ascending
Title Descending
Issue Date Ascending
Issue Date Descending
Submit date Ascending
Submit date Descending
Journal Impact Factor Ascending
Journal Impact Factor Descending
Author Ascending
Author Descending
A one-dimensional transient calculation method for flow instability of supercritical hydrocarbon in cooling channels
会议论文
AIAA Propulsion and Energy Forum, VIRTUAL EVENT, 2021年8月9-11日
Authors:
Jin YC(靳一超)
;
Wu K(吴坤)
;
Lu Y(陆阳)
;
Fan XJ(范学军)
Adobe PDF(1121Kb)
  |  
Favorite
  |  
View/Download:193/51
  |  
Submit date:2022/07/04
Evaluation of the influence of radiation on a GH2/GO2 rocket combustor
会议论文
AIAA Propulsion & Energy Forum, VIRTUAL EVENT, 2020-08-17
Authors:
Li B(李波)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(1358Kb)
  |  
Favorite
  |  
View/Download:179/60
  |  
Submit date:2021/02/01
Influence of Chemical Mechanisms on Supersonic Combustion Characteristics Fueled by Kerosene
会议论文
2018 Joint Propulsion Conference, Cincinnati, Ohio, July 9-11, 2018
Authors:
Yao W(姚卫)
;
Wu K(吴坤)
;
Lee YC(李亚超)
;
Fan XJ(范学军)
Adobe PDF(1156Kb)
  |  
Favorite
  |  
View/Download:470/0
  |  
Submit date:2018/12/26
A low-dissipation solver based on OpenFOAM designed for large eddy simulation in compressible flows
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Lee YC(李亚超)
;
Yao W(姚卫)
;
Fan XJ(范学军)
View
  |  
Adobe PDF(1377Kb)
  |  
Favorite
  |  
View/Download:318/122
  |  
Submit date:2020/08/26
Low-dissipation compressible Solver, Skew-symmetric Form, Benchmark Flow Problems
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
Authors:
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)
View
  |  
Adobe PDF(1173Kb)
  |  
Favorite
  |  
View/Download:487/235
  |  
Submit date: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
A low-dissipation scheme based on OpenFoam designed for large eddy simulation in compressible flow
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Lee YC
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Yao, Wei(weiyao@imech.ac.cn)
View
  |  
Adobe PDF(1358Kb)
  |  
Favorite
  |  
View/Download:462/118
  |  
Submit date:2018/01/16
Computational Fluid Dynamics
Computer Software
Digital Storage
Kinetic Energy
Kinetics
Open Source Software
Open Systems
Runge Kutta Methods
Shock Tubes
Shock Waves
Spacecraft
Turbulence
Two Phase Flow
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
Authors:
Lee YC
;
Yao W(姚卫)
;
Fan XJ(范学军)
View
  |  
Adobe PDF(1377Kb)
  |  
Favorite
  |  
View/Download:531/112
  |  
Submit date: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
Visualization of flow separation inside cut kerf during laser cutting of thick sections
会议论文
34th International Congress on Applications of Lasers and Electro-Optics (ICALEO), Atlanta, GA, OCT 18-22, 2015
Authors:
Zhang C
;
Wen P
;
Yao ZH
;
Yuan YM(袁越明)
;
Fan XJ(范学军)
;
Wen, P (reprint author), Tsinghua Univ, State Key Lab Tribol, Beijing 100084, Peoples R China.
View
  |  
Adobe PDF(1350Kb)
  |  
Favorite
  |  
View/Download:350/121
  |  
Submit date:2016/06/28
Development and Preliminary Validation of A Thermal Analysis Method for Hydrocarbon Regenerative-cooled Supersonic Combustor
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015
Authors:
Lu Y(陆阳)
;
Wang XZ(王新竹)
;
Li L(李龙)
;
Cheng D(程迪)
;
Yuan T(袁涛)
;
Yao W(姚卫)
;
Fan XJ(范学军)
Adobe PDF(445Kb)
  |  
Favorite
  |  
View/Download:505/103
  |  
Submit date:2016/01/08
Hydrocarbons
Combustors
Cooling
Heat Transfer
Full-scale Detached Eddy Simulation of kerosene fueled scramjet combustor based on skeletal mechanism
会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:
Yao W(姚卫)
;
Wang J(王晶)
;
Lu Y(陆阳)
;
Li XP(李晓鹏)
;
Fan XJ(范学军)
Adobe PDF(1195Kb)
  |  
Favorite
  |  
View/Download:522/192
  |  
Submit date:2016/07/01
Adiabatic Flame Temperature
Combustion
Directed Graphs
Flow Separation
Heat Flux
Kerosene
Large Eddy Simulation
Musculoskeletal System
Real Time Systems
Sensitivity Analysis
Spacecraft
Transients