×
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 ... [6]
Key Labora... [1]
Creator
岳连捷 [3]
姚卫 [2]
姜宗林 [2]
张新宇 [2]
胡宗民 [2]
Chen XJ [1]
More...
Document Type
Journal ar... [7]
Date Issued
2021 [2]
2019 [2]
2017 [3]
Language
英语 [7]
Source Publication
AEROSPACE ... [7]
Indexed By
EI [7]
SCI [7]
Funding Project
National N... [2]
National N... [2]
National K... [1]
National N... [1]
National N... [1]
National N... [1]
More...
Funding Organization
National N... [3]
111 Projec... [1]
11372333) [1]
11572024) [1]
China Post... [1]
Defense In... [1]
More...
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-7 of 7
Help
Filters
Source Publication:AEROSPACE SCIENCE AND TECHNOLOGY
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
Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors:
Yao W(姚卫)
;
Liu H(刘杭)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
Adobe PDF(2954Kb)
  |  
Favorite
  |  
View/Download:297/71
  |  
Submit date:2021/11/15
Hypersonic combustion
Hydrogen
Improved Delayed Detached Eddy
Simulation (IDDES)
Dynamic zone flamelet model
Scramjet
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(8067Kb)
  |  
Favorite
  |  
View/Download:410/75
  |  
Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
Numerical study of a fully confined supersonic slot impinging jet from bleed system
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Chang XY(张新宇)
View
  |  
Adobe PDF(3918Kb)
  |  
Favorite
  |  
View/Download:545/176
  |  
Submit date:2019/09/09
Fully confined supersonic jet
Inclined impingement
Heat transfer
Boundary layer bleed
Numerical simulation
A theoretical and computational study of the vibration excitation on the transition criteria of shock wave reflections
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 89, 页码: 299-306
Authors:
Peng J(彭俊)
;
Zhang ZJ(张子健)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
View
  |  
Adobe PDF(2165Kb)
  |  
Favorite
  |  
View/Download:420/98
  |  
Submit date:2019/09/09
Shock reflection
Vibration excitation
Mach reflection
Transition criterion
Hypersonic flow
Numerical study of inflow equivalence ratio inhomogeneity on oblique detonation formation in hydrogen-air mixtures
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 256-263
Authors:
Fang YS(方宜申)
;
Hu ZM(胡宗民)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Ng HD
View
  |  
Adobe PDF(2663Kb)
  |  
Favorite
  |  
View/Download:395/100
  |  
Submit date:2018/02/08
Oblique Detonation
Equivalence Ratio
Mixture Inhomogeneity
Detailed Chemistry
Uncertain reduced-order modeling for unsteady aerodynamics with interval parameters and its application on robust flutter boundary prediction
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 71, 页码: 214-230
Authors:
Chen XJ
;
Qiu ZP
;
Wang XJ
;
Li YL
;
Wang RX(王睿星)
View
  |  
Adobe PDF(4860Kb)
  |  
Favorite
  |  
View/Download:413/93
  |  
Submit date:2018/02/08
Uncertain Reduced-order Modeling
Robust Flutter Analysis
Interval Perturbation Method
Uncertain Aeroelastic System
Numerical investigation of characteristic frequency excited highly underexpanded jets
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 卷号: 63, 页码: 304-316
Authors:
Li XP
;
Fan E
;
Yao W(姚卫)
;
Fan XJ(范学军)
;
Fan, XJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
;
Fan, XJ (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
View
  |  
Adobe PDF(3588Kb)
  |  
Favorite
  |  
View/Download:474/151
  |  
Submit date:2017/07/24
Fuel Jets
Underexpanded Jets
Jet Mixing Control
Excited Jets
Large Eddy Simulation