×
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]
俞鸿儒 [1]
李进平 [1]
王春 [1]
腾宏辉 [1]
苑朝凯 [1]
More...
Document Type
Journal ar... [2]
Date Issued
2018 [2]
Language
中文 [1]
英语 [1]
Source Publication
CHINESE JO... [1]
中国科学. 技术科学 [1]
Indexed By
CSCD [2]
EI [2]
SCI [1]
Funding Project
Funding Organization
Fundamenta... [1]
国家自然科学基金 [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
Filters
Indexed By：CSCD
Creator：姜宗林
First author
Date Issued：2018
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
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
高超声速条件下溢流液膜厚度测量方法
期刊论文
中国科学. 技术科学, 2018, 卷号: 48, 期号: 6, 页码: 629-638
Authors:
苑朝凯
;
李进平
;
陈宏
;
姜宗林
;
俞鸿儒
View
|
Adobe PDF(4824Kb)
|
Favorite
|
View/Download：558/103
|
Submit date：2018/10/24
高超声速热防护
主动冷却
液膜厚度
电导法
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：330/79
|
Submit date：2018/10/30
Body And Wing
Flow Field
Hypersonic Flow
Shock/shock Interaction
Wave Configurations
