×
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 ... [3]
State Key ... [2]
Creator
姚卫 [3]
范学军 [3]
Liu CY [1]
reprint au... [1]
xfan@imech... [1]
张健 [1]
More...
Document Type
Conference... [5]
Date Issued
2017 [5]
Language
英语 [5]
Source Publication
21st AIAA ... [3]
10th U.S. ... [1]
POWDER TEC... [1]
Indexed By
EI [5]
CPCI-S [1]
Funding Project
Funding Organization
This work ... [1]
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-5 of 5
Help
Filters
Indexed By:EI
Date Issued:2017
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
Issue Date Ascending
Issue Date Descending
Submit date Ascending
Submit date Descending
Journal Impact Factor Ascending
Journal Impact Factor Descending
WOS Cited Times Ascending
WOS Cited Times Descending
Title Ascending
Title Descending
Author Ascending
Author Descending
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:478/232
  |  
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
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:285/99
  |  
Submit date:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
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:309/94
  |  
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
Detailed transitional process of the flames in hot and diluted environments from lifted flames to MILD combustion
会议论文
10th U.S. National Combustion Meeting, College Park, MD, United states, April 23, 2017 - April 26, 2017
Authors:
Liu CY
;
Zhang J(张健)
View
  |  
Adobe PDF(414Kb)
  |  
Favorite
  |  
View/Download:245/90
  |  
Submit date:2018/11/08
Oxygen
Diluted environments
Monotonic trend
Partial premixing
Stabilization mechanisms
Transition process
Transitional flames
Transitional process
Turbulent combustion
Large-eddy simulation of turbulent preferential concentration and collision of bidisperse heavy particles in isotropic turbulence
会议论文
1st International Workshop on Computational Particle Technology, Suzhou, PEOPLES R CHINA, MAR, 2016
Authors:
Chen JC(陈进财)
;
Jin GD(晋国栋)
;
Jin, GD (reprint author), Chinese Acad Sci, Inst Mech, LNM, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(962Kb)
  |  
Favorite
  |  
View/Download:409/115
  |  
Submit date:2018/01/16
Direct Numerical Simulations
Space-time Correlations
Inertial Particles
Approximate Deconvolution
Cloud Droplets
Fluidized-bed
Flow
Model
Motion
Particle-laden Turbulence
Large-eddy Simulation
Subgrid Scale Motion
Bidisperse Particles
Preferential Concentration
Collision Rate Attenuation