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Qian W [1]
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Source Publication：29th Congress of the International Council of the Aeronautical Sciences, ICAS 2014
Date Issued：2014
Language：英语
Document Type：会议论文
Community：高温气体动力学国家重点实验室
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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
Authors:
Qian W
;
Yang GW(杨国伟)
;
Zheng GN(郑冠男)
;
Zhang GJ
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Submit date：2017/05/27
All-movable Horizontal Tail
Flutter Boundaries
Overload Factors
Structure Dynamics
Transonic Flutter
Transonic Speed
Wind Tunnel Tests
Wind-tunnel Testing
