×
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 ... [1]
Creator
Ji, Feng [1]
Lu, Hongbo [1]
吴坤 [1]
敖彧 [1]
范学军 [1]
Document Type
Journal ar... [1]
Date Issued
2023 [1]
Language
英语 [1]
Source Publication
ACTA ASTRO... [1]
Indexed By
EI [1]
SCI [1]
Funding Project
Funding Organization
High-level... [1]
National K... [1]
Strategic ... [1]
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-1 of 1
Help
Filters
Source Publication：ACTA ASTRONAUTICA
Funding Organization：High-level Innovation Research Institute Program of Guangdong Province [2020B0909010003]
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
Combustion dynamics of high Mach number scramjet under different inflow thermal nonequilibrium conditions
期刊论文
ACTA ASTRONAUTICA, 2023, 卷号: 208, 页码: 281-295
Authors:
Ao Y(敖彧)
;
Wu K(吴坤)
;
Lu, Hongbo
;
Ji, Feng
;
Fan XJ(范学军)
Adobe PDF(11339Kb)
|
Favorite
|
View/Download：96/5
|
Submit date：2023/06/15
Hypervelocity combustion
Thermal nonequilibrium
Two-temperature model
Numerical simulation
