×
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 ... [2]
Creator
姜宗林 [2]
王春 [2]
腾宏辉 [2]
项高翔 [2]
Document Type
Journal ar... [2]
Date Issued
2018 [2]
Language
英语 [2]
Source Publication
CHINESE JO... [1]
SHOCK WAVE... [1]
Indexed By
SCI [2]
CSCD [1]
EI [1]
Funding Project
Funding Organization
Fundamenta... [1]
National N... [1]
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-2 of 2
Help
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
WOS Cited Times Ascending
WOS Cited Times Descending
Submit date Ascending
Submit date Descending
Author Ascending
Author Descending
Journal Impact Factor Ascending
Journal Impact Factor Descending
Issue Date Ascending
Issue Date Descending
Title Ascending
Title Descending
Three-dimensional shock wave configurations induced by two asymmetrical intersecting wedges in supersonic flow
期刊论文
SHOCK WAVES, 2018, 卷号: 28, 期号: 2, 页码: 311-319
Authors:
Xiang GX(项高翔)
;
Wang C(王春)
;
Teng HH(腾宏辉)
;
Jiang ZL(姜宗林)
View
  |  
Adobe PDF(1333Kb)
  |  
Favorite
  |  
View/Download:644/185
  |  
Submit date:2018/10/30
Supersonic Flow
3d Shock/shock Interaction
3d Asymmetrical Wave Configurations
Spatial Dimension Reduction
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:393/86
  |  
Submit date:2018/10/30
Body And Wing
Flow Field
Hypersonic Flow
Shock/shock Interaction
Wave Configurations