×
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]
Key Labora... [3]
State Key ... [1]
Creator
reprint a... [11]
杨国伟 [3]
李新亮 [2]
赵瑞 [2]
阎超 [2]
Kong WX [1]
More...
Document Type
Journal a... [11]
Date Issued
2013 [11]
Language
英语 [11]
Source Publication
SCIENCE CH... [3]
Acta Mecha... [2]
AIAA JOURN... [1]
AIAA Journ... [1]
CHINESE JO... [1]
JOURNAL OF... [1]
More...
Indexed By
SCI [11]
EI [10]
CSCD [3]
Funding Project
Funding Organization
11232011 [1]
11302238 [1]
11372331) [1]
National B... [1]
National B... [1]
National B... [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 11
Help
Filters
Creator:reprint author
First author
Date Issued:2013
Document Type:期刊论文
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
Journal Impact Factor Ascending
Journal Impact Factor Descending
Submit date Ascending
Submit date Descending
Title Ascending
Title Descending
WOS Cited Times Ascending
WOS Cited Times Descending
Issue Date Ascending
Issue Date Descending
Author Ascending
Author Descending
Numerical study on wake characteristics of high-speed trains
期刊论文
Acta Mechanica Sinica, 2013, 卷号: 29, 期号: 6, 页码: 811-822
Authors:
Yao SB(姚拴宝)
;
Sun ZX(孙振旭)
;
Guo DL(郭迪龙)
;
Chen DW(陈大伟)
;
Yang GW(杨国伟)
;
Guo, DL (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
Adobe PDF(6677Kb)
  |  
Favorite
  |  
View/Download:784/287
  |  
Submit date:2014/01/17
Wake Flow Structures
Urans
Des
High Speed Trains
Interaction of isentropic compression waves with a bow shock
期刊论文
AIAA JOURNAL, 2013, 卷号: 51, 期号: 10, 页码: 2474-2484
Authors:
Lu HB(卢洪波)
;
Yue LJ(岳连捷)
;
Xiao YB(肖雅彬)
;
Zhang XY(张新宇)
;
Yue, LJ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temperature Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(764Kb)
  |  
Favorite
  |  
View/Download:771/289
  |  
Submit date:2014/01/17
Towards an entropy-based detached-eddy simulation
期刊论文
SCIENCE CHINA-PHYSICS MECHANICS & ASTRONOMY, 2013, 卷号: 56, 期号: 10, 页码: 1970-1980
Authors:
Zhao R(赵瑞)
;
Yan C(阎超)
;
Li XL(李新亮)
;
Kong WX
;
Zhao, R (reprint author), Beijing Univ Aeronaut & Astronaut, Natl Lab Computat Fluid Dynam, Beijing 100191, Peoples R China.
Adobe PDF(1098Kb)
  |  
Favorite
  |  
View/Download:1170/255
  |  
Submit date:2013/10/23
Hybrid Rans/les
Detached-eddy Simulation
Turbulence
Compressible Flows
Entropy
A lift formula applied to low-Reynolds-number unsteady flows
期刊论文
PHYSICS OF FLUIDS, 2013, 卷号: 25, 期号: 9, 页码: 093605/1-093605/22
Authors:
Wang SZ(王士召)
;
Zhang X(张星)
;
He GW(何国威)
;
Liu TS
;
He, GW (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab Nonlinear Mech, Beijing 100190, Peoples R China.
Adobe PDF(2214Kb)
  |  
Favorite
  |  
View/Download:892/378
  |  
Submit date:2013/11/18
Reynolds Number
Acceleration Terms
Control Volumes
Flapping Wing
Inertial Effect
Lamb Vectors
Low Reynolds Number
Separated Flows
Unsteady Lift
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
Authors:
Cui K(崔凯)
;
Hu SC(胡守超)
;
Li GL(李广利)
;
Qu ZP(屈志朋)
;
Situ M
;
Cui, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1426Kb)
  |  
Favorite
  |  
View/Download:902/296
  |  
Submit date:2013/09/27
Hypersonic
Flanking Air Inlet
Waverider
Computational Fluid Dynamics(Cfd)
A diffusive information preservation method for small Knudsen number flows
期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2013, 卷号: 243, 页码: 179-193
Authors:
Fei F(费飞)
;
Fan J(樊菁)
;
Fan, J (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(1093Kb)
  |  
Favorite
  |  
View/Download:984/354
  |  
Submit date:2013/06/27
Dsmc
Ip
Molecular Diffusion
Time Step
Cell Size
Improvement of Baldwin-Lomax turbulence model for supersonic complex flows
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2013, 卷号: 26, 期号: 3, 页码: 529–534
Authors:
Zhao R(赵瑞)
;
Yan C(阎超)
;
Yu J(于剑)
;
Li XL(李新亮)
;
Yan, C (reprint author), Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China.
Adobe PDF(1609Kb)
  |  
Favorite
  |  
View/Download:899/298
  |  
Submit date:2013/09/21
Baldwin-lomax Model
Boundary Layers
Computational Aerodynamics
Entropy
Supersonic Flows
Turbulence Models
Train model acceleration and deceleration
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 3, 页码: 642-647
Authors:
Yang QS(杨乾锁)
;
Song JH(宋军浩)
;
Li D(李多)
;
Zhang J(张杰)
;
Yang GW(杨国伟)
;
Yang, QS (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(605Kb)
  |  
Favorite
  |  
View/Download:960/257
  |  
Submit date:2013/03/25
Moving Train Model
Acceleration
Deceleration
Magnetic Braking
Air Gun
Compressed Air
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:1410/505
  |  
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
Flutter analyses of complete aircraft based on hybrid grids and parallel computing
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 2, 页码: 398-404
Authors:
Zheng GN(郑冠男)
;
Yang GW(杨国伟)
;
Qian W
;
Yang, GW (reprint author), Chinese Acad Sci, Inst Mech, Key Lab Mech Fluid Solid Coupling Syst, Beijing 100190, Peoples R China.
Adobe PDF(4121Kb)
  |  
Favorite
  |  
View/Download:989/219
  |  
Submit date:2013/03/25
Cfd
Csd
Aeroelasticity
Coupled Method
Flutter
Mpi