×
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 ... [5]
Creator
姜宗林 [5]
王春 [5]
项高翔 [3]
reprint au... [2]
Li XD [1]
刘云峰 [1]
More...
Document Type
Journal ar... [5]
Date Issued
2023 [1]
2021 [1]
2018 [1]
2016 [2]
Language
英语 [5]
Source Publication
CHINESE JO... [2]
AIAA JOURN... [1]
Journal of... [1]
SCIENCE CH... [1]
Indexed By
EI [5]
SCI [5]
CSCD [3]
Funding Project
National N... [1]
Funding Organization
Fundamenta... [1]
National N... [1]
The projec... [1]
This work ... [1]
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:
1-5 of 5
Help
Filters
Indexed By:EI
Creator:王春
First author
Author:姜宗林
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
Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle
期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(5479Kb)
  |  
Favorite
  |  
View/Download:431/82
  |  
Submit date:2022/08/24
Multistage Launch Vehicle
Aerodynamic Characteristics
Shock Wave Interaction
Angle of Attack
Waverider
Boundary Layer Flow
Total Variation Diminishing
Adverse Pressure Gradient
Hypersonic Flows
Hypersonic Wind Tunnels
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
Adobe PDF(1806Kb)
  |  
Favorite
  |  
View/Download:294/64
  |  
Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Shock/shock interactions between bodies and wings
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2018, 卷号: 31, 期号: 2, 页码: 255-261
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(腾宏辉)
;
Jiang ZL(姜宗林)
View
  |  
Adobe PDF(1161Kb)
  |  
Favorite
  |  
View/Download:326/78
  |  
Submit date:2018/10/30
Body And Wing
Flow Field
Hypersonic Flow
Shock/shock Interaction
Wave Configurations
Investigations of Three-Dimensional Shock/Shock Interactions over Symmetrical Intersecting Wedges
期刊论文
AIAA JOURNAL, 2016, 卷号: 54, 期号: 5, 页码: 1472-1481
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(578Kb)
  |  
Favorite
  |  
View/Download:510/172
  |  
Submit date:2016/09/14
Ceramics
Thermal Shock
Size Effect
Theoretical solutions to three-dimensional asymmetrical shock/shock interaction
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2016, 卷号: 59, 期号: 8, 页码: 1208-1216
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Hu ZM(胡宗民)
;
Li XD
;
Jiang ZL(姜宗林)
;
Wang, C (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(995Kb)
  |  
Favorite
  |  
View/Download:512/125
  |  
Submit date:2016/12/08
3d Asymmetrical Shock/shock Interaction
Spatial-dimension Reduction
Mach Reflection
Flow Field
Theoretical Analysis