×
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
力学所知识产出(1... [12]
State Key... [12]
Key Labora... [5]
微重力重点实验室 [3]
State Key ... [3]
Creator
姚卫 [7]
reprint au... [6]
范学军 [6]
何国威 [5]
Lee YC [2]
姜宗林 [2]
More...
Document Type
Conferenc... [35]
Date Issued
2020 [1]
2019 [3]
2017 [8]
2014 [1]
2013 [2]
2012 [4]
More...
Language
英语 [34]
中文 [1]
Source Publication
21st AIAA ... [5]
New Trends... [2]
12th Asia-... [1]
2005 NSTI ... [1]
2006 1st I... [1]
28TH INTER... [1]
More...
Indexed By
EI [18]
CPCI-S [11]
CPCI [2]
CPCI(ISTP) [2]
CPCI(ISTP) [1]
Funding Project
Funding Organization
National N... [1]
This work ... [1]
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-10 of 35
Help
Filters
Document Type:会议论文
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
Author Ascending
Author Descending
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
Impact of water on methane adsorption in nanopores: A hybrid GCMC-MD simulation study
会议论文
ICCS 2020 Conference, Amsterdam, The Netherlands, 3-5 June, 2020
Authors:
Zhou J(周羁)
;
Jiang WB(江文滨)
;
Lin M(林缅)
;
Ji LL(姬莉莉)
;
Cao GH(曹高辉)
Adobe PDF(3451Kb)
  |  
Favorite
  |  
View/Download:150/42
  |  
Submit date:2021/01/28
Shale gas Adsorption GCMC MD Water saturation
Application of dynamic zone flamelet model to a GH2/GO2 rocket combustor
会议论文
AIAA Propulsion and Energy Forum and Exposition, 2019, Indianapolis, IN, United states, August 19, 2019 - August 22, 2019
Authors:
Yao W(姚卫)
;
Li B(李波)
Adobe PDF(1665Kb)
  |  
Favorite
  |  
View/Download:129/42
  |  
Submit date:2020/11/20
Dynamic zone flamelet model
GH2/GO2
Large Eddy Simulation (LES)
Rocket combustor
Turbulence-chemistry interaction
A molecular dynamics simulation on the oxidation of core-shell aluminum nanoparticles in oxygen and water environments
会议论文
12th Asia-Pacific Conference on Combustion, ASPACC 2019, Fukuoka, Japan, July 1, 2019 - July 5, 2019
Authors:
Chu QZ
;
Liao LJ(廖丽涓)
;
Shi BL
;
Luo KH
;
Wang NF
View
  |  
Adobe PDF(850Kb)
  |  
Favorite
  |  
View/Download:170/31
  |  
Submit date:2019/11/20
Aluminum nanoparticles
Concentration distributions
Heat and mass transfer process
Heat transfer efficiency
Molecular dynamics simulations
Oxidation mechanisms
Particle temperature
Structure evolution
Numerical study on unsteady wake characteristics of an urban maglev train
会议论文
ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019, San Francisco, CA, United states, July 28, 2019 - August 1, 2019
Authors:
Sun ZX(孙振旭)
;
Kong FB
;
Yao YF(姚永芳)
;
Yang GW(杨国伟)
Adobe PDF(2054Kb)
  |  
Favorite
  |  
View/Download:119/46
  |  
Submit date:2020/11/20
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:269/110
  |  
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:425/210
  |  
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:412/102
  |  
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
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)
View
  |  
Adobe PDF(623Kb)
  |  
Favorite
  |  
View/Download:242/79
  |  
Submit date:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
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:470/88
  |  
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
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)
View
  |  
Adobe PDF(832Kb)
  |  
Favorite
  |  
View/Download:262/78
  |  
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