×
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 ... [9]
Creator
reprint au... [9]
姜宗林 [4]
张德良 [2]
Chen P [1]
Jiang Y [1]
Liu KX [1]
More...
Document Type
Journal ar... [9]
Date Issued
2017 [2]
2016 [3]
2015 [1]
2014 [1]
2011 [2]
Language
英语 [9]
Source Publication
Chinese Ph... [2]
ACTA MECHA... [1]
APPLIED MA... [1]
CHINESE PH... [1]
CHINESE PH... [1]
Chinese Jo... [1]
More...
Indexed By
CSCD [9]
SCI [9]
EI [8]
Funding Project
Funding Organization
National N... [1]
National N... [1]
National N... [1]
Project su... [1]
Project su... [1]
Supported ... [1]
More...
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-9 of 9
Help
Filters
Indexed By:CSCD
Creator:reprint author
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
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
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.
Adobe PDF(1080Kb)
  |  
Favorite
  |  
View/Download:524/129
  |  
Submit date:2017/08/22
Aerodynamic Force And Moment Measurement
10° Half-angle Cone Model
Jf12
Real-gas Effects
Shock Tunnel
Theories and technologies for duplicating hypersonic flight conditions for ground testing
期刊论文
NATIONAL SCIENCE REVIEW, 2017, 卷号: 4, 期号: 3, 页码: 290-U461
Authors:
Jiang ZL(姜宗林)
;
Yu HR(俞鸿儒)
;
Jiang, ZL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing, Peoples R China.
;
Jiang, ZL (reprint author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing, Peoples R China.
Adobe PDF(1315Kb)
  |  
Favorite
  |  
View/Download:349/133
  |  
Submit date:2017/11/29
Theoretical approach to one-dimensional detonation instability
期刊论文
APPLIED MATHEMATICS AND MECHANICS-ENGLISH EDITION, 2016, 卷号: 37, 期号: 9, 页码: 1231-1238
Authors:
Wang C(王春)
;
Xiang GX(项高翔)
;
Jiang ZL(姜宗林)
;
Wang, C (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(514Kb)
  |  
Favorite
  |  
View/Download:449/91
  |  
Submit date:2016/12/08
Detonation Wave
Detonation Instability
Shock Wave
Chemical Reaction
Three-dimensional detonation cellular structures in rectangular ducts using an improved CESE scheme
期刊论文
CHINESE PHYSICS B, 2016, 卷号: 25, 期号: 11, 页码: 114702
Authors:
Shen Y
;
Shen H
;
Liu KX
;
Chen P
;
Zhang DL(张德良)
;
Zhang, DL (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(7986Kb)
  |  
Favorite
  |  
View/Download:268/77
  |  
Submit date:2017/02/24
Ce/se Scheme
Three-dimensional Gaseous Detonation
Cellular Pattern
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(1162Kb)
  |  
Favorite
  |  
View/Download:340/87
  |  
Submit date:2016/09/14
Dual-mode Scramjet
Engine Performance
Thrust
Optimization
Heat Release Distribution
Simulated Annealing Algorithm
High-Power Continuous-Wave Nd:GdVO4 Solid-State Laser Dual-End-Pumped at 880nm
期刊论文
CHINESE PHYSICS LETTERS, 2015, 卷号: 32, 期号: 9, 页码: 94201
Authors:
Mao YF
;
Zhang HL
;
Sang SH
;
Zhang X
;
Yu XL(余西龙)
;
Xing JC
;
Xin JG
;
Jiang Y
;
Zhang, HL (reprint author), Beijing Inst Technol, Sch Optoelect, Beijing 100081, Peoples R China.
View
  |  
Adobe PDF(723Kb)
  |  
Favorite
  |  
View/Download:285/88
  |  
Submit date:2016/01/08
Nonlinear saturation amplitude of cylindrical Rayleigh-Taylor instability
期刊论文
Chinese Physics B, 2014, 卷号: 23, 期号: 9, 页码: 94502
Authors:
Liu WH
;
Yu CP(于长平)
;
Ye WH
;
Wang LF
;
Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam LHD, Beijing 100190, Peoples R China.
View
  |  
Adobe PDF(338Kb)
  |  
Favorite
  |  
View/Download:519/146
  |  
Submit date:2014/11/27
Nonlinear Saturation Amplitude
Rayleigh-taylor Instability
Cylindrical Interface
Three-Dimensional Simulation of Detonation Propagation in a Rectangular Duct by an Improved CE/SE Scheme
期刊论文
Chinese Physics Letters, 2011, 卷号: 28, 期号: 12, 页码: 124705
Authors:
Shen H(申华)
;
Liu KX(刘凯欣)
;
Zhang DL(张德良)
;
Liu, KX (reprint author), Peking Univ, LTCS, Beijing 100871, Peoples R China
Adobe PDF(3217Kb)
  |  
Favorite
  |  
View/Download:689/160
  |  
Submit date:2012/04/01
Time Conservation Element
Numerical-simulation
Diagonal Structures
Flows
Instability Criterion of One-Dimensional Detonation Wave with Three-Step Chain Branching Reaction Model
期刊论文
Chinese Physics Letters, 2011, 卷号: 28, 期号: 8, 页码: 84704
Authors:
Teng HH(滕宏辉)
;
Jiang ZL(姜宗林)
;
Teng, HH (reprint author), Chinese Acad Sci, Inst Mech, Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
Adobe PDF(424Kb)
  |  
Favorite
  |  
View/Download:1865/651
  |  
Submit date:2012/04/01
Plane Detonation
Stability
Limit