×
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
reprint au... [7]
刘云峰 [7]
姜宗林 [7]
汪运鹏 [3]
罗长童 [2]
Wang YP [1]
More...
Document Type
Journal ar... [5]
Conference... [2]
Date Issued
2017 [1]
2016 [4]
2013 [2]
Language
英语 [7]
Source Publication
AIAA JOURN... [2]
AIAA Journ... [1]
Chinese Jo... [1]
INTERNATIO... [1]
REVIEW OF ... [1]
SHOCK WAVE... [1]
More...
Indexed By
EI [6]
SCI [5]
CPCI-S [2]
CSCD [1]
Funding Project
Funding Organization
National N... [1]
The force ... [1]
This work ... [1]
Y210061021 [1]
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-7 of 7
Help
Filters
Creator:reprint author
First author
Creator:刘云峰
Creator:姜宗林
Language:英语
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
Aerodynamic force and moment measurement of 10° half-angle cone in JF12 shock tunnel
期刊论文
Chinese Journal of Aeronautics, 2017, 卷号: 30, 期号: 3, 页码: 983-987
Authors:
Liu YF(刘云峰)
;
Wang YP(汪运鹏)
;
Yuan CK(苑朝凯)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
;
Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(1080Kb)
  |  
Favorite
  |  
View/Download:532/133
  |  
Submit date:2017/08/22
Aerodynamic Force And Moment Measurement
10° Half-angle Cone Model
Jf12
Real-gas Effects
Shock Tunnel
Force measurement using strain-gauge balance in a shock tunnel with long test duration
期刊论文
REVIEW OF SCIENTIFIC INSTRUMENTS, 2016, 卷号: 87, 期号: 5, 页码: 55108
Authors:
Wang YP(汪运鹏)
;
Liu YF(刘云峰)
;
Luo ZT(罗长童)
;
Jiang ZL(姜宗林)
;
Wang, YP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(6592Kb)
  |  
Favorite
  |  
View/Download:382/98
  |  
Submit date:2016/09/14
Design of a pulse-type strain gauge balance for a long-test-duration hypersonic shock tunnel
期刊论文
SHOCK WAVES, 2016, 卷号: 26, 期号: 6, 页码: 835-844
Authors:
Wang YP(汪运鹏)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Wang, Y (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(2538Kb)
  |  
Favorite
  |  
View/Download:454/94
  |  
Submit date:2016/12/08
Hypersonic Shock Tunnel
Force Measurement
Strain Gauge Balance
Starting Process in a Large-Scale Shock Tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:
Wang YP
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(764Kb)
  |  
Favorite
  |  
View/Download:380/108
  |  
Submit date:2016/06/28
Relationship between ignition delay time and cell size of H-2-Air detonation
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2016, 卷号: 41, 期号: 28, 页码: 11900-11908
Authors:
Liu YF(刘云峰)
;
Zhang W
;
Jiang ZL(姜宗林)
;
Liu, YF (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(2332Kb)
  |  
Favorite
  |  
View/Download:279/103
  |  
Submit date:2016/12/08
H-2-air Detonation
Chemical Reaction Kinetics
Ignition Delay Time
Triple-shock Point
Concept of non-ablative thermal protection system for hypersonic vehicles
期刊论文
AIAA Journal, 2013, 卷号: 51, 期号: 3, 页码: 584-590
Authors:
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(5046Kb)
  |  
Favorite
  |  
View/Download:1416/509
  |  
Submit date:2013/04/07
Flow Fields
Flow Visualization
Hypersonic Aerodynamics
Hypersonic Vehicles
Mach Number
Shock Waves
Thermal Insulating Materials
Engineering Applications
Experimental Datum
Hypersonic Wind Tunnels
Numerical Results
Stagnation Points
Thermal Protection
Thermal Protection System
Working Pressures
Concept of non-ablative thermal protection system for hypersonic vehicles
会议论文
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, CA, APR 11-14, 2011
Authors:
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(5046Kb)
  |  
Favorite
  |  
View/Download:533/165
  |  
Submit date:2013/12/12