×
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 ... [4]
力学所知识产出(19... [1]
State Key ... [1]
Creator
姚卫 [4]
范学军 [3]
Gong J [1]
Guo B [1]
guobin@mai... [1]
xfan@imech... [1]
More...
Document Type
Conference... [6]
Date Issued
2019 [1]
2017 [2]
2016 [1]
2012 [1]
1999 [1]
Language
英语 [6]
Source Publication
21st AIAA ... [2]
32nd AIAA ... [1]
AIAA Propu... [1]
Proceeding... [1]
The 23rd I... [1]
Indexed By
EI [4]
Funding Project
Funding Organization
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-6 of 6
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
Journal Impact Factor Ascending
Journal Impact Factor Descending
Submit date Ascending
Submit date Descending
Title Ascending
Title Descending
WOS Cited Times Ascending
WOS Cited Times Descending
Issue Date Ascending
Issue Date Descending
Author Ascending
Author Descending
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:169/51
  |  
Submit date:2020/11/20
Dynamic zone flamelet model
GH2/GO2
Large Eddy Simulation (LES)
Rocket combustor
Turbulence-chemistry interaction
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:283/99
  |  
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)
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
Measurement of heat flux distribution of supercritical kerosene fueled supersonic combustor
会议论文
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2016, Washington, DC, United states, June 13, 2016 - June 17, 2016
Authors:
Cheng D(程迪)
;
Wang J(王晶)
;
Gong J
;
Lu Y(陆阳)
;
Yao W(姚卫)
;
Li L(李龙)
;
Fan XJ(范学军)
;
Fan, Xuejun (xfan@imech.ac.cn)
Adobe PDF(2131Kb)
  |  
Favorite
  |  
View/Download:346/125
  |  
Submit date:2017/05/05
Equivalence Ratios
Heat Flux Distributions
Heat Transfer Characteristics
Scramjet
Supercritical Kerosenes
Supersonic Combustion
Supersonic Combustors
Total Temperatures
Intrinsic lengths govern failure mode transition in metallic glasses
会议论文
ICTAM, 北京, 2012-8
Authors:
Dai LH(戴兰宏)
;
Chen Y(陈艳)
Adobe PDF(691Kb)
  |  
Favorite
  |  
View/Download:1821/1239
  |  
Submit date:2013/03/01
Short geomagnetic event recorded in chinese loess-soil sequences
会议论文
IUGG 99, Birmingham, UK, 1999
Authors:
Guo B
;
Lin M(林缅)
;
guobin@mail.c-geos.ac.cn
Adobe PDF(12184Kb)
  |  
Favorite
  |  
View/Download:569/163
  |  
Submit date:2013/03/11