×
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 ... [7]
Creator
汪球 [7]
赵伟 [7]
李进平 [5]
姜宗林 [3]
栗继伟 [2]
Einhoff J [1]
More...
Document Type
Journal ar... [6]
Conference... [1]
Date Issued
2024 [1]
2021 [1]
2019 [1]
2018 [1]
2017 [1]
2016 [1]
More...
Language
英语 [7]
Source Publication
21st AIAA ... [1]
AIAA JOURN... [1]
EXPERIMENT... [1]
JOURNAL OF... [1]
SCIENCE CH... [1]
SHOCK WAVE... [1]
More...
Indexed By
EI [5]
SCI [5]
CSCD [2]
Funding Project
National N... [2]
National N... [2]
China Scho... [1]
Key-Area R... [1]
Key-Area R... [1]
National N... [1]
More...
Funding Organization
National N... [3]
China Scho... [2]
Key-Area R... [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
(Note: the search results are based on claimed items)
Browse/Search Results:
1-7 of 7
Help
Filters
Author:赵伟
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
Author Ascending
Author Descending
WOS Cited Times Ascending
WOS Cited Times Descending
Title Ascending
Title Descending
Issue Date Ascending
Issue Date Descending
Submit date Ascending
Submit date Descending
Journal Impact Factor Ascending
Journal Impact Factor Descending
Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities
期刊论文
AIAA JOURNAL, 2024, 页码: 8
Authors:
Wang WT(王文韬)
;
Wang Q(汪球)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Gao, Liangjie
;
Liu, Zhongchen
;
Qian, Zhansen
Favorite
  |  
View/Download:31/0
  |  
Submit date:2024/02/26
Finite Element Method
Hypersonic
Shock Tube/Tunnel
Diaphragm
Burst Pressure
Evolution of heat transfer at the stagnation point during the detached bow shock establishment
期刊论文
SHOCK WAVES, 2021, 页码: 8
Authors:
Wang Q(汪球)
;
Li JP(李进平)
;
Luo K(罗凯)
;
Li JW(栗继伟)
;
Zhao W(赵伟)
Adobe PDF(1158Kb)
  |  
Favorite
  |  
View/Download:228/45
  |  
Submit date:2021/05/17
Hypersonic
Aerodynamic heating
Detached bow shock
Shock tube
expansion tube
Influence of test model material on the accuracy of transient heat transfer measurements in impulse facilities
期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2019, 卷号: 104, 页码: 59-66
Authors:
Wang Q(汪球)
;
Olivier H
;
Einhoff J
;
Li JP(李进平)
;
Zhao W(赵伟)
View
  |  
Adobe PDF(1085Kb)
  |  
Favorite
  |  
View/Download:404/97
  |  
Submit date:2019/05/29
Heat transfer measurement
Lateral heat conduction
Shock tunnel
Thermocouple
Hypersonic
Performance of Copper Calorimeter for Heat Transfer Measurement in High Enthalpy Shock Tunnel
期刊论文
JOURNAL OF THERMAL SCIENCE, 2018, 卷号: 27, 期号: 4, 页码: 373-381
Authors:
Wang Q(汪球)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
View
  |  
Adobe PDF(1208Kb)
  |  
Favorite
  |  
View/Download:611/129
  |  
Submit date:2018/10/30
copper calorimeter
high enthalpy shock tunnel
heat transfer
hypersonic
Performance of a detonation driven shock tunnel
会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:
Li JW
;
Wang Q(汪球)
;
Zhao W(赵伟)
;
Lu P
;
Tan YX
View
  |  
Adobe PDF(468Kb)
  |  
Favorite
  |  
View/Download:286/80
  |  
Submit date:2018/01/16
Detonation
Gas Dynamics
Hypersonic Flow
Shock Tubes
Supersonic Aerodynamics
Comparative study on aerodynamic heating under perfect and nonequilibrium hypersonic flows
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2016, 卷号: 59, 期号: 2, 页码: 624701
Authors:
Wang Q(汪球)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Jiang ZL(姜宗林)
;
Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(763Kb)
  |  
Favorite
  |  
View/Download:522/226
  |  
Submit date:2016/03/21
Aerodynamic Heating
Hypersonic
Shock Tunnel
Stanton Number
Sharp Cone
高超声速电离绕流中电子密度的静电探针测量方法研究
期刊论文
实验流体力学, 2013, 卷号: 27, 期号: 6, 页码: 64-69+85
Authors:
汪球
;
赵伟
;
余西龙
;
姜宗林
Adobe PDF(487Kb)
  |  
Favorite
  |  
View/Download:883/228
  |  
Submit date:2014/01/24
静电探针
电子密度
高超声速
高焓激波风洞
Electrostatic Probe
Electron Density
Hypersonic
High Enthalpy Shock Tunnel