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北京航空航天大学 [8]
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会议论文 [16]
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Flutter analysis of very large flexible wing based on structural rom and finite-state inflow aerodynamics
会议论文
AIAA Scitech Forum, 2019, San Diego, CA, United states, 2019-01-07
作者:
Chao, An
;
Changchuan, Xie
;
Chao, Yang
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2019/12/30
Flutter study on high speed train external windshield by a tight coupling method
会议论文
San Francisco, CA, United states, July 28, 2019 - August 1, 2019
作者:
Jiang Q(姜倩)
;
Zheng GN(郑冠男)
;
Zhao GL(赵桂林)
收藏
  |  
浏览/下载:7/0
  |  
提交时间:2020/11/20
Flutter
High speed train external windshield
Tight coupling method
Vibration
Substructure-based flutter analysis for a wing-aileron system with freeplay
会议论文
AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2018, 2018-01-08
作者:
Xiangyu, W.
;
Zhigang, W.
;
Chao, Y.
;
Xufei, H.
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  |  
浏览/下载:7/0
  |  
提交时间:2019/12/30
Aeroelasticity
Ailerons
Aviation
Control nonlinearities
Elastic waves
Finite element method
Flutter (aerodynamics)
Frequency domain analysis
Hopf bifurcation
Nonlinear analysis
Stiffness
Structural analysis
Structural dynamics
Vibration analysis
Aeroelastic system
Bending stiffness
Effective approaches
Ground vibration tests
Nonlinear aeroelasticity
Nonlinear flutters
Structural non-linearities
Wing aileron system
Time domain analysis
Flutter boundary prediction for a flying-wing model exhibiting body freedom flutter
会议论文
58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2017, Grapevine, TX, United states, 2017-01-09
作者:
Huang, Chao
;
Wu, Zhigang
;
Yang, Chao
;
Dai, Yuting
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
Design, manufacture and frequency experiment of a novel flutter model for AGARD WING 445.6 with structure-similarity
会议论文
30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016, 2016-09-25
作者:
Qian W.
;
Bai Y.
;
Wang D.
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  |  
浏览/下载:3/0
  |  
提交时间:2019/12/09
Time marching simulation of aeroelasticity based on a coupled numerical method
会议论文
2014 International Conference on Applied Mechanics, Mechatronics and Intelligent System, AMMIS 2014, April 18, 2014 - April 20, 2014, Changsha, China
Xi R.
;
Ji Z. L.
;
Jia H. G.
;
Xiao Q. J.
收藏
  |  
浏览/下载:21/0
  |  
提交时间:2015/04/27
Numerical simulation and wind tunnel testing of flutter about an all- Movable horizontal tail at transonic speeds
会议论文
29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014, St. Petersburg, Russia, September 7, 2014 - September 12, 2014
作者:
Qian W
;
Yang GW(杨国伟)
;
Zheng GN(郑冠男)
;
Zhang GJ
收藏
  |  
浏览/下载:14/0
  |  
提交时间:2017/05/27
All-movable horizontal tail
Flutter boundaries
Overload factors
Structure dynamics
Transonic flutter
Transonic speed
Wind tunnel tests
Wind-tunnel testing
Flutter Analysis and Active Suppression for High Aspect Ratio Wing
会议论文
The 14th International Conference on Dynamics Vibration and Control
作者:
Zhou WY(周文雅)
;
Wu ZG(吴志刚)
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  |  
浏览/下载:1/0
  |  
提交时间:2019/12/11
Aeroelastic Analysis of High Aspect Ratio Wing in Subsonic Flow
会议论文
2013 10TH INTERNATIONAL BHURBAN CONFERENCE ON APPLIED SCIENCES AND TECHNOLOGY (IBCAST), 2013-01-01
作者:
Ahmad, Kamran
;
Wuzhigang
;
Rahman, Hammad
收藏
  |  
浏览/下载:3/0
  |  
提交时间:2020/01/06
aeroelasticity
bending mode
torsion mode
modal analysis
high aspect ratio
flutter velocity
Continuum Aeroelastic Model and Flutter Analysis for a Variable-span Morphing Wing
会议论文
2nd International Conference on Mechatronics and Applied Mechanics (ICMAM2012), Taipei, PEOPLES R CHINA, 2013-01-01
作者:
Huang, Ren
;
Qiu, Zhiping
;
Wang, Xiaojun
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2020/01/06
Morphing aircraft
Variable-span wing
Flutter
Stepped beam
Unsteady vortex lattice
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