×
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
Key Labora... [1]
State Key ... [1]
Creator
Gao X [1]
Li YW [1]
Qiu ZP [1]
Wang XJ [1]
Zhang HG [1]
Zhu JJ [1]
More...
Document Type
Journal ar... [2]
Date Issued
2022 [1]
2019 [1]
Language
英语 [2]
Source Publication
AIAA JOURN... [1]
CHINESE JO... [1]
Indexed By
EI [2]
SCI [2]
CSCD [1]
Funding Project
Defence In... [1]
Defence In... [1]
Defence In... [1]
National K... [1]
National N... [1]
National N... [1]
More...
Funding Organization
National N... [2]
Defence In... [1]
National K... [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
Funding Organization:National Nature Science Foundation of China
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
Issue Date Ascending
Issue Date Descending
Author Ascending
Author Descending
Submit date Ascending
Submit date Descending
Title Ascending
Title Descending
Journal Impact Factor Ascending
Journal Impact Factor Descending
Jet-Driven Unstart Process of a Hypersonic Inlet with Ramp Mass Injection
期刊论文
AIAA JOURNAL, 2022, 页码: 5
Authors:
Li JJ(李江江)
;
Chen H(陈昊)
;
Tong XT(仝晓通)
;
Gao X
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
Adobe PDF(1812Kb)
  |  
Favorite
  |  
View/Download:217/46
  |  
Submit date:2022/05/17
Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
Authors:
Zhu JJ
;
Wang XJ
;
Zhang HG
;
Li YW
;
Wang RX(王睿星)
;
Qiu ZP
View
  |  
Adobe PDF(2082Kb)
  |  
Favorite
  |  
View/Download:434/192
  |  
Submit date:2020/03/21
Hypersonic vehicle
Six sigma robust optimization
Successive response surface
Thermal protection system
Uncertainty