×
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 ... [3]
Creator
He GY [1]
LNM, Insti... [1]
Liu YM [1]
Qi DW [1]
Wang Q [1]
Zhang SG [1]
More...
Document Type
Conference... [2]
Journal ar... [1]
Date Issued
2012 [3]
Language
英语 [3]
Source Publication
50TH AIAA ... [1]
Acta Mecha... [1]
The 23rd I... [1]
Indexed By
EI [2]
CSCD [1]
SCI [1]
Funding Project
Funding Organization
The projec... [1]
Thesis Advisor
×
Knowledge Map
IMECH-IR
Start a Submission
Submissions
Unclaimed
Claimed
Attach Fulltext
Bookmarks
QQ
Weibo
Feedback
Browse/Search Results:
1-3 of 3
Help
Filters
Date Issued:2012
Community:非线性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
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 analysis on transitions and symmetry-breaking in the wake of a flapping foil
期刊论文
Acta Mechanica Sinica, 2012, 卷号: 28, 期号: 6, 页码: 1551-1556
Authors:
He GY
;
Wang Q
;
Zhang X(张星)
;
Zhang SG
;
Zhang X(张星)
;
LNM, Institute of Mechanics,Chinese Academy of Sciences,100190 Beijing, China
Adobe PDF(8088Kb)
  |  
Favorite
  |  
View/Download:981/240
  |  
Submit date:2013/01/31
Flapping Motion
Immersed Boundary Method
Wake
Symmetry-breaking
Lattice Boltzmann Simulations of a pitch-up and pitch-down maneuver of a span-wise flexible wing in a free stream flow Read More: http://arc.aiaa.org/doi/abs/10.2514/6.2012-300
会议论文
50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Nashville, TN, United states, JAN 09-12, 2012
Authors:
Qi DW
;
He GW(何国威)
;
Liu YM
Adobe PDF(738Kb)
  |  
Favorite
  |  
View/Download:862/170
  |  
Submit date:2013/02/26
Aerospace Engineering
Deformation
Exhibitions
Flexible Wings
Reynolds Number
Rigidity
Vortex Flow
Aerodynamic Forces
Chord-based Reynolds Number
Flexural Rigidities
Free Stream
Free-stream Flow
Lattice Boltzmann
Leading-edge Vortices
Lift Coefficient
Lift Force
Particle Methods
Pitch Rate
Power Efficiency
Reduced Frequency
Three Dimensional Space
Time-periods
Tip Edge
Trailing Edges
Trailing Vortex
Intrinsic lengths govern failure mode transition in metallic glasses
会议论文
ICTAM, 北京, 2012-8
Authors:
Dai LH(戴兰宏)
;
Chen Y(陈艳)
Adobe PDF(691Kb)
  |  
Favorite
  |  
View/Download:1813/1236
  |  
Submit date:2013/03/01