×
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 ... [3]
Creator
姜宗林 [3]
汪运鹏 [2]
王粤 [2]
周凯 [1]
汪球 [1]
王春 [1]
More...
Document Type
Journal ar... [3]
Date Issued
2023 [2]
2016 [1]
Language
中文 [3]
Source Publication
航空学报 [3]
Indexed By
CSCD [3]
EI [3]
Funding Project
Funding Organization
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
(Note: the search results are based on claimed items)
Browse/Search Results:
1-3 of 3
Help
Filters
Source Publication:航空学报
Document Type:期刊论文
Author:姜宗林
First 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
Issue Date Ascending
Issue Date Descending
Submit date Ascending
Submit date Descending
Title Ascending
Title Descending
Author Ascending
Author Descending
WOS Cited Times Ascending
WOS Cited Times Descending
激波风洞两级入轨飞行器纵向级间分离试验技术
期刊论文
航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126
Authors:
王粤
;
汪运鹏
;
姜宗林
Adobe PDF(6797Kb)
  |  
Favorite
  |  
View/Download:426/44
  |  
Submit date:2022/12/01
两级入轨
轨迹捕获
激波风洞
多体分离
动态试验
试验技术
一种并联两级入轨飞行器纵向分离方案的数值研究
期刊论文
航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634
Authors:
王粤
;
汪运鹏
;
王春
;
姜宗林
Adobe PDF(4901Kb)
  |  
Favorite
  |  
View/Download:632/99
  |  
Submit date:2022/07/11
两级入轨
高超声速
纵向分离
气动干扰
非定常流动
爆轰驱动膨胀管性能研究
期刊论文
航空学报, 2016, 卷号: 37, 期号: 3, 页码: 810-816
Authors:
周凯
;
汪球
;
胡宗民
;
姜宗林
View
  |  
Adobe PDF(481Kb)
  |  
Favorite
  |  
View/Download:422/96
  |  
Submit date:2016/12/16
Hypervelocity
Detonation-driven
Expansion Tube
Performance Study
Experimental Tests
Numerical Simulation