×
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... [69]
Laboratory... [1]
Creator
岳连捷 [69]
张新宇 [63]
陈立红 [20]
肖雅彬 [18]
张启帆 [10]
卢洪波 [8]
More...
Document Type
Conferenc... [38]
Journal a... [28]
Patent [3]
Date Issued
2023 [2]
2022 [2]
2021 [3]
2020 [5]
2019 [8]
2018 [1]
More...
Language
中文 [45]
英语 [24]
Source Publication
推进技术 [6]
高温气体动力学研究进... [6]
AEROSPACE ... [4]
第三届高超声速科技学... [4]
CHINESE JO... [3]
第八届全国高超声速科... [3]
More...
Indexed By
EI [30]
SCI [18]
CSCD [14]
CPCI-S [1]
Funding Project
National N... [6]
National N... [5]
National N... [2]
Central Re... [1]
Central Re... [1]
China Post... [1]
More...
Funding Organization
National N... [8]
中国力学学会、中国科... [3]
National N... [2]
"Open Fund... [1]
11472279 [1]
11672309) [1]
More...
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
(Note: the search results are based on claimed items)
Browse/Search Results:
1-10 of 69
Help
Filters
Author:岳连捷
First author
Community:高温气体动力学国家重点实验室
First author affiliation
The first author
Corresponding Author
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
Thermochemical non-equilibrium flow characteristics of high Mach number inlet in a wide operation range
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 12, 页码: 164-184
Authors:
Dai, Chunliang
;
Sun, Bo
;
Yue LJ(岳连捷)
;
Zhou, Shengbing
;
Zhuo, Changfei
;
Zhou, Changsheng
;
Yu, Jianyi
Adobe PDF(5674Kb)
  |  
Favorite
  |  
View/Download:67/10
  |  
Submit date:2024/02/19
Scramjet inlet
Starting ability
Thermochemical
Work performance
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor
期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
Authors:
Wu ZJ(吴振杰)
;
Zhang QF(张启帆)
;
Yu FY(于方游)
;
Luo WH(罗苇航)
;
Gao ZB(高占彪)
;
Yue LJ(岳连捷)
Adobe PDF(582Kb)
  |  
Favorite
  |  
View/Download:57/8
  |  
Submit date:2023/06/15
Scramjet Engines
Combustor Design
flame stabilization mode
transition
path dependence
Numerical study on wave configuration of wedge-induced oblique detonation wave: Reactive boundary layer effect
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 11, 页码: 11
Authors:
Yang L(杨理)
;
Yue LJ(岳连捷)
;
Yu, Dehai
;
Chen, Zheng
Adobe PDF(4548Kb)
  |  
Favorite
  |  
View/Download:184/50
  |  
Submit date:2022/12/29
Lagrange Optimization of Shock Waves for Two-Dimensional Hypersonic Inlet with Geometric Constraints
期刊论文
AEROSPACE, 2022, 卷号: 9, 期号: 10, 页码: 15
Authors:
Li YL(李育凌)
;
Yue LJ(岳连捷)
;
He CM(何成明)
;
Wu WN(邬婉楠)
;
Chen H(陈昊)
Adobe PDF(3520Kb)
  |  
Favorite
  |  
View/Download:268/82
  |  
Submit date:2022/11/14
scramjet inlet
Lagrange optimization method
shock configuration
Parameters for evaluating the efficiency of inlet compression
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:
Chen KT(陈科挺)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(511Kb)
  |  
Favorite
  |  
View/Download:233/52
  |  
Submit date:2022/01/12
Airbreathing engine
Compression efficiency
Compression quality
Inlet
Self-consistency
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:
Zhou GX(周功喜)
;
Zhang X(张旭)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Zhang SZ(张仕忠)
;
Lin X(林鑫)
;
Li F(李飞)
;
Chen H(陈宏)
;
Yue LJ(岳连捷)
;
Yu XL(余西龙)
Adobe PDF(4108Kb)
  |  
Favorite
  |  
View/Download:344/53
  |  
Submit date:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
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:413/75
  |  
Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow
高速进气道低马赫数不起动特性及马赫数影响规律
期刊论文
推进技术, 2020, 卷号: 42, 期号: 10, 页码: 2207-2217
Authors:
贺理浩
;
张启帆
;
岳连捷
;
张新宇
;
王卫星
;
谭慧俊
Adobe PDF(9600Kb)
  |  
Favorite
  |  
View/Download:271/41
  |  
Submit date:2021/11/12
高速进气道
低马赫数不起动
非定常
气动力
自起动
Numerical investigation on flow nonuniformity-induced hysteresis in scramjet isolator
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3176-3188
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Ma SH(马生虎)
;
Zhang QF(张启帆)
;
Zhang, Peng
;
Zhang XY(张新宇)
Adobe PDF(3937Kb)
  |  
Favorite
  |  
View/Download:218/56
  |  
Submit date:2021/03/30
Adverse pressure gradient
Back pressure
Hysteresis effects
Non-uniform flow
Shock train
Numerical study on the shock/combustion interaction of oblique detonation waves
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 104, 页码: 13
Authors:
Yang L
;
Yue LJ(岳连捷)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
Adobe PDF(5176Kb)
  |  
Favorite
  |  
View/Download:286/113
  |  
Submit date:2020/11/30
Oblique detonation wave
Shock/combustion interaction
Shock polar analysis
High-resolution simulation