×
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
Key Labora... [7]
Creator
杨国伟 [7]
Prapamonth... [3]
郑冠男 [3]
银波 [3]
宋鑫 [2]
Kong FB [1]
More...
Document Type
Journal ar... [4]
Conference... [3]
Date Issued
2019 [7]
Language
英语 [5]
中文 [2]
Source Publication
ASME-JSME-... [2]
北京航空航天大学学报 [2]
ASME 2019 ... [1]
CASE STUDI... [1]
PHYSICS OF... [1]
Indexed By
EI [7]
CPCI-S [2]
CSCD [2]
SCI [2]
Funding Project
National K... [1]
National N... [1]
Funding Organization
King Mongk... [1]
National K... [1]
National K... [1]
National N... [1]
National N... [1]
国家自然基金面上项目... [1]
More...
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:杨国伟
First author
Date Issued:2019
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
Issue Date Ascending
Issue Date Descending
Submit date Ascending
Submit date Descending
Title Ascending
Title Descending
Author Ascending
Author Descending
WOS Cited Times Ascending
WOS Cited Times Descending
变时滞间隙非线性机翼颤振主动控制方法
期刊论文
北京航空航天大学学报, 2019, 卷号: 46, 期号: 10, 页码: 1899-1906
Authors:
聂雪媛
;
郑冠男
;
杨国伟
Adobe PDF(1255Kb)
  |  
Favorite
  |  
View/Download:287/59
  |  
Submit date:2020/11/18
颤振抑制
间隙非线性
时滞控制系统
状态观测
时变时延
Understanding of temperature and cooling effectiveness sensitivity of a film-cooled vane under coolant inlet temperature effect: A case study
期刊论文
CASE STUDIES IN THERMAL ENGINEERING, 2019, 卷号: 14, 页码: UNSP 100505
Authors:
Prapamonthon P
;
Yin B(银波)
;
Yang GW(杨国伟)
;
Zhang MH
View
  |  
Adobe PDF(3342Kb)
  |  
Favorite
  |  
View/Download:280/86
  |  
Submit date:2020/03/21
TURBINE BLADE
HEAT-TRANSFER
Finite obstacle effect on the aerodynamic performance of a hovering wing
期刊论文
PHYSICS OF FLUIDS, 2019, 卷号: 31, 期号: 10, 页码: 12
Authors:
Yin B(银波)
;
Yang GW(杨国伟)
;
Prapamonthon P
View
  |  
Adobe PDF(5326Kb)
  |  
Favorite
  |  
View/Download:274/99
  |  
Submit date:2020/03/11
几何不确定性区间分析及鲁棒气动优化设计
期刊论文
北京航空航天大学学报, 2019, 页码: 15
Authors:
宋鑫
;
郑冠男
;
杨国伟
;
姜倩
View
  |  
Adobe PDF(914Kb)
  |  
Favorite
  |  
View/Download:310/78
  |  
Submit date:2019/12/16
几何不确定性
非线性区间分析
DFFD(直接操作自由变形)
气动优化设计
鲁棒优化设计
自适应多目标粒子群算法
Kriging代理模型
A robust aerodynamic optimization design for airfoil based on interval uncertainty analysis method
会议论文
ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019, San Francisco, CA, United states, July 28, 2019 - August 1, 2019
Authors:
Song X(宋鑫)
;
Zheng GN(郑冠男)
;
Yang GW(杨国伟)
Favorite
  |  
View/Download:141/0
  |  
Submit date:2020/11/20
Adaptive MOPSO
DFFD
Geometric uncertainty
Interval analysis
Kriging model
Robust design optimization
Numerical study on unsteady wake characteristics of an urban maglev train
会议论文
ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference, AJKFluids 2019, San Francisco, CA, United states, July 28, 2019 - August 1, 2019
Authors:
Sun ZX(孙振旭)
;
Kong FB
;
Yao YF(姚永芳)
;
Yang GW(杨国伟)
Adobe PDF(2054Kb)
  |  
Favorite
  |  
View/Download:163/57
  |  
Submit date:2020/11/20
Numerical prediction of cooling performance sensitivity of 1st stage nozzle guide vane under aerothermal conditions
会议论文
ASME 2019 Gas Turbine India Conference, GTINDIA 2019, Chennai, Tamil Nadu, India, December 5, 2019 - December 6, 2019
Authors:
Prapamonthon P
;
Yin B(银波)
;
Yang GW(杨国伟)
;
Zhang MH(张莫晗)
Adobe PDF(2782Kb)
  |  
Favorite
  |  
View/Download:214/75
  |  
Submit date:2020/11/20
Aerothermal condition
Cooling effectiveness
Cooling performance
Thermal sensitivity
Turbine vane