×
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
MOST Discipline Catalogue
Study Hall
Image search
Paste the image URL
Home
Collections
Authors
DocType
Subjects
K-Map
News
Search in the results
Collection
State Key... [22]
力学所知识产出(19... [7]
Authors
岳连捷 [28]
肖雅彬 [26]
Zhang Xin... [24]
Chen LiHo... [16]
卢洪波 [5]
卢鑫 [3]
More...
Document Type
Conferenc... [17]
Journal ar... [8]
Patent [3]
Thesis [1]
Date Issued
2019 [1]
2017 [1]
2016 [1]
2015 [2]
2014 [2]
2013 [1]
More...
Language
中文 [22]
英语 [7]
Source Publication
高温气体动力学研究进... [5]
实验流体力学 [2]
推进技术 [2]
第四届高超声速科技学... [2]
15th AIAA ... [1]
16th AIAA/... [1]
More...
Indexed By
EI [8]
CSCD [6]
SCI [2]
Funding Project
Funding Organization
中国力学学会、中国科... [2]
American I... [1]
National N... [1]
The author... [1]
国家自然科学基金(9... [1]
国家自然科学基金(9... [1]
More...
Thesis Advisor
岳连捷 [1]
张新宇 [1]
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-10 of 29
Help
Show only claimed items
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
Journal Impact Factor Ascending
Journal Impact Factor Descending
WOS Cited Times Ascending
WOS Cited Times Descending
Author Ascending
Author Descending
Title Ascending
Title Descending
Submit date Ascending
Submit date Descending
全流量捕获的高超声速变截面内转式进气道快速设计方法
专利
发明专利. 全流量捕获的高超声速变截面内转式进气道快速设计方法, 专利号: ZL201810269911.2, 申请日期: 2018-03-29,
Inventors:
肖鸿文
;
岳连捷
;
肖雅彬
View
  |  
Adobe PDF(404Kb)
  |  
Favorite
  |  
View/Download:40/4
  |  
Submit date:2020/02/10
隔离段抽吸引起的激波迟滞现象研究
期刊论文
推进技术, 2017, 卷号: 38, 期号: 04, 页码: 732-739
Authors:
马生虎
;
岳连捷
;
贾轶楠
;
肖雅彬
;
张新宇
View
  |  
Adobe PDF(1677Kb)
  |  
Favorite
  |  
View/Download:101/24
  |  
Submit date:2017/12/22
超燃冲压发动机
隔离段
激波反射迟滞
边界层分离迟滞
Design methodology for shape transition inlets based on constant contraction of discrete streamtubes
期刊论文
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2016, 卷号: 230, 期号: 8, 页码: 1496-1506
Authors:
Xiao YB(肖雅斌)
;
Yue LJ(岳连捷)
;
Ma SH
;
Zhang XY(张新宇)
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, 15 Beisihuanxi Rd, Beijing 100864, Peoples R China.
View
  |  
Adobe PDF(1353Kb)
  |  
Favorite
  |  
View/Download:138/39
  |  
Submit date:2016/09/14
Hypersonic Inlet
Shape Transition
Inward Turning
Scramjet
Design Method
高超声速进气道快速破膜开启的流动特性
期刊论文
航空学报, 2015, 卷号: 36, 期号: 6, 页码: 1795-1804
Authors:
徐骁
;
岳连捷
;
卢洪波
;
肖雅彬
;
张新宇
View
  |  
Adobe PDF(711Kb)
  |  
Favorite
  |  
View/Download:100/33
  |  
Submit date:2015/12/25
高超声速进气道
破膜开启
非定常效应
激波边界层相互作用
分离流
带有边界层流动控制的内转式进气道
会议论文
第八届全国高超声速科技学术会议, 中国黑龙江哈尔滨, 2015-12-28
Authors:
肖雅彬
;
岳连捷
;
张新宇
View
  |  
Adobe PDF(624Kb)
  |  
Favorite
  |  
View/Download:116/35
  |  
Submit date:2016/08/16
流场品质
隔离段
边界层流动
流向涡
斜激波
横向流动
唇口
压力梯度
收缩段
边界层控制
局部收缩比一致的变截面高超声速内转式进气道
专利
发明专利. 局部收缩比一致的变截面高超声速内转式进气道, 专利号: ZL201210157992.X, 申请日期: 2012-05-21, 授权日期: 2014-06-13
Inventors:
肖雅彬
;
岳连捷
;
卢洪波
;
陈立红
;
张新宇
View
  |  
Adobe PDF(457Kb)
  |  
Favorite
  |  
View/Download:580/124
  |  
Submit date:2014/06/13
基于激波风洞的高超声速进气道自起动测试装置
专利
发明专利. 基于激波风洞的高超声速进气道自起动测试装置, 专利号: ZL2011103420788, 申请日期: 2011-11-03, 授权日期: 2014-01-24
Inventors:
岳连捷
;
肖雅彬
;
彭辉
;
陈立红
;
张新宇
Adobe PDF(269Kb)
  |  
Favorite
  |  
View/Download:499/121
  |  
Submit date:2014/01/24
Interaction of isentropic compression waves with a bow shock
期刊论文
AIAA JOURNAL, 2013, 卷号: 51, 期号: 10, 页码: 2474-2484
Authors:
Lu HB(卢洪波)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
;
Zhang XY(张新宇)
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(764Kb)
  |  
Favorite
  |  
View/Download:579/208
  |  
Submit date:2014/01/17
局部收缩比处处一致的变截面高超声速内转式进气道设计方法
会议论文
LHD2012夏季学术研讨会, 吉林延吉, 2012
Authors:
肖雅彬
;
岳连捷
;
高占彪
;
陈立红
;
张新宇
Adobe PDF(2046Kb)
  |  
Favorite
  |  
View/Download:399/169
  |  
Submit date:2014/01/23
Iso-contraction-ratio methodology for the design of hypersonic inward turning inlets with shape transition
会议论文
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference 2012, Tours, France, SEP 24-28, 2012
Authors:
Xiao YB(肖雅彬)
;
Yue LJ(岳连捷)
;
Chen LH(陈立红)
;
Zhang XY(张新宇)
;
Xiao YB(肖雅彬)
View
  |  
Adobe PDF(1674Kb)
  |  
Favorite
  |  
View/Download:315/72
  |  
Submit date:2014/02/24