×
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... [34]
宽域飞行工程科学与应... [3]
力学所知识产出(19... [1]
Laboratory... [1]
Creator
崔凯 [34]
李广利 [17]
胡守超 [16]
杨国伟 [12]
肖尧 [10]
王秀平 [9]
More...
Document Type
Conferenc... [17]
Journal a... [17]
Date Issued
2023 [2]
2022 [1]
2021 [3]
2018 [1]
2017 [5]
2014 [1]
More...
Language
中文 [22]
英语 [12]
Source Publication
高温气体动力学研究进... [6]
力学学报 [4]
21st AIAA ... [3]
RECENT PRO... [2]
航空学报 [2]
16th AIAA/... [1]
More...
Indexed By
EI [14]
CSCD [11]
SCI [6]
CPCI [2]
Funding Project
National N... [1]
Funding Organization
中国科学院基础前沿科... [3]
国家自然科学基金(1... [2]
11572333) [1]
National N... [1]
National N... [1]
National N... [1]
More...
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-10 of 34
Help
Filters
Creator:崔凯
First author
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
翼反角对高压捕获翼构型高超气动特性的影响
期刊论文
航空学报, 2023, 卷号: 44, 期号: 08, 页码: 45-58
Authors:
常思源
;
肖尧
;
李广利
;
田中伟
;
张凯凯
;
崔凯
Adobe PDF(3584Kb)
  |  
Favorite
  |  
View/Download:208/44
  |  
Submit date:2022/10/17
高压捕获翼
高超声速
数值模拟
上/下反角
稳定性
机体尾缘形状对高压捕获翼构型亚声速特性影响
期刊论文
航空学报, 2023, 卷号: 44, 期号: 06, 页码: 10.7527/S1000-6893.2022.27215
Authors:
王浩祥
;
肖尧
;
张凯凯
;
李广利
;
常思源
;
田中伟
;
崔凯
Adobe PDF(2111Kb)
  |  
Favorite
  |  
View/Download:198/55
  |  
Submit date:2022/10/17
高压捕获翼
亚声速
流动特性
流动分离
数值模拟
翼反角对高压捕获翼构型亚声速气动特性影响分析研究
期刊论文
力学学报, 2022, 卷号: 54, 期号: 10, 页码: 2760-2772
Authors:
常思源
;
肖尧
;
李广利
;
田中伟
;
崔凯
Adobe PDF(1833Kb)
  |  
Favorite
  |  
View/Download:287/82
  |  
Submit date:2022/11/07
高压捕获翼构型亚跨超流动特性数值研究
期刊论文
力学学报, 2021, 卷号: 53, 期号: 11, 页码: 3056-3070
Authors:
王浩祥
;
李广利
;
杨靖
;
肖尧
;
王小永
;
徐应洲
;
许先贵
;
崔凯
Adobe PDF(2607Kb)
  |  
Favorite
  |  
View/Download:308/81
  |  
Submit date:2022/03/16
高压捕获翼
计算流体力学
宽速域
流动分离
气动干扰
Numerical study on aerodynamic performance of waverider with a new bluntness method
期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 卷号: 235, 期号: 10, 页码: 1225-1233
Authors:
Qu ZP
;
Xiao HD
;
Lv MY
;
Li GL(李广利)
;
Cui K(崔凯)
Adobe PDF(1179Kb)
  |  
Favorite
  |  
View/Download:262/109
  |  
Submit date:2021/06/11
bluntness method
computational fluid dynamics
hypersonic
volume
Waverider
高压捕获翼构型的跨流域气动特性
期刊论文
空气动力学学报, 2021, 卷号: 39, 期号: 03, 页码: 11-20
Authors:
田鹏
;
李广利
;
崔凯
;
李志辉
;
张俊
Adobe PDF(1652Kb)
  |  
Favorite
  |  
View/Download:350/81
  |  
Submit date:2021/08/25
高压捕获翼
跨流域
稀薄气体效应
DSMC
气动性能
Hypersonic I-shaped aerodynamic configurations
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2018, 卷号: 61, 期号: 2, 页码: 24722
Authors:
Cui K(崔凯)
;
Xiao Y(肖尧)
;
Xu YZ
;
Li GL
View
  |  
Adobe PDF(665Kb)
  |  
Favorite
  |  
View/Download:452/138
  |  
Submit date:2018/10/30
High-Pressure Capturing Wing Configurations
期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
Authors:
Cui K(崔凯)
;
Li GL
;
Xiao Y(肖尧)
;
Xu YZ
;
Cui,K(reprint author), Chinese Acad Sci, Inst Mech
View
  |  
Adobe PDF(671Kb)
  |  
Favorite
  |  
View/Download:660/189
  |  
Submit date:2017/07/24
乘波体压缩面变化对其气动性能影响分析
期刊论文
力学学报, 2017, 卷号: 49, 期号: 01, 页码: 75-83
Authors:
崔凯
;
徐应洲
;
肖尧
;
李广利
Adobe PDF(5584Kb)
  |  
Favorite
  |  
View/Download:383/97
  |  
Submit date:2017/12/22
乘波体
优化设计
增量参数化方法
微分演化算法
计算流体力学
Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Li GL(李广利)
;
Cui K(崔凯)
;
Xiao Y(肖尧)
;
Xu YZ(徐应洲)
Adobe PDF(664Kb)
  |  
Favorite
  |  
View/Download:412/102
  |  
Submit date:2018/01/16
Aerodynamics
Angle Of Attack
Angle Of Attack Indicators
Boundary Layers
Drag
Drag Coefficient
High Pressure Effects
Hypersonic Aerodynamics
Hypersonic Flow
Spacecraft