×
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(19... [4]
Creator
岳连捷 [4]
张新宇 [3]
王世芬 [2]
肖雅彬 [2]
龚鹏 [2]
Gong P [1]
More...
Document Type
Journal ar... [3]
Conference... [1]
Date Issued
2008 [4]
Language
中文 [3]
英语 [1]
Source Publication
实验流体力学 [2]
15th AIAA ... [1]
燃气轮机技术 [1]
Indexed By
CSCD [2]
EI [1]
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:
1-4 of 4
Help
Filters
Creator:岳连捷
First author
Date Issued:2008
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
可变几何轴对称进气道初步设计
期刊论文
燃气轮机技术, 2008, 期号: 3, 页码: 21-24+28
Authors:
张辉
;
伊卫林
;
岳连捷
;
季路成
Adobe PDF(606Kb)
  |  
Favorite
  |  
View/Download:648/202
  |  
Submit date:2010/05/03
轴对称进气道
变几何结构
超声速段
吸气
一维优化设计
三面压缩式高超声速进气道流动结构研究
期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 2, 页码: 64-67
Authors:
肖雅彬
;
岳连捷
;
龚鹏
;
王世芬
;
陈立红
;
张新宇
Adobe PDF(413Kb)
  |  
Favorite
  |  
View/Download:881/184
  |  
Submit date:2010/05/03
超声速进气道
流动结构
油滴显示
数值模拟
带中心支板侧压进气道流场特性研究
期刊论文
实验流体力学, 2008, 卷号: 22, 期号: 1, 页码: 31-35
Authors:
龚鹏
;
岳连捷
;
肖雅斌
;
王世芬
;
张新宇
Adobe PDF(621Kb)
  |  
Favorite
  |  
View/Download:493/123
  |  
Submit date:2010/05/03
超燃冲压发动机
高超声速进气道
侧压式进气道
支板
Investigation on a truncated streamline-traced hypersonic Busemann inlet
会议论文
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008
Authors:
Xiao YB(肖雅彬)
;
Yue LJ(岳连捷)
;
Gong P
;
Chang XY(张新宇)
View
  |  
Adobe PDF(3472Kb)
  |  
Favorite
  |  
View/Download:228/87
  |  
Submit date:2017/06/01
Boundary Layer Corrections
Busemann Inlet
Core Flow
Correction Method
Design Points
Finite Differential Methods
Internal Contraction Ratio
Internal Flows
Mass Flow