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�������պ����ѧѧ�� 2006, Vol. 32 Issue (02) :163-166    DOI:
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����, ���¹�, л����, �*
�������պ����ѧ ���տ�ѧ�빤��ѧԺ, ���� 100083
Optimization designing method of wing flutter model for low-speed wind tunnel test
Lü Bin, Liu Deguang, Xie Changchuan, Yang Chao*
School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

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Abstract�� To solve the multidisciplinary problem of flutter wing model designing for low-speed wind tunnel test, which there is lots of difficulty in and expended abundant time conventionally, a design method named genetic/sensitivity-based hybrid algorithm was applied, which has very well global and local search capabilities and optimization efficiency. The theory, process and applicability of genetic/sensitivity-based hybrid algorithm were presented. The math model, based on real physical one, was modeled according the essential theory and design course of the flutter wing model designing. With the method using in design, not only the time of model designing is reduced to a great extent, but also the design precision is assured, for the error comparing result and target of model design can reach below 5% relatively. An optimization method of flutterwing model was developed and was used in many aspects of model designing, providing an efficient design method in engineering.
Keywords�� aeroelastic   flutter   genetic algorithms   sensitivity algorithms   natural vibration   wind testing     
Received 2005-01-06;


About author: �� ��(1980-), ��, ������ˮ��, ��ʿ��, lvbin12@163.com.
����, ���¹�, л����, �.������ٷ綴�������ģ���Ż���Ʒ���[J]  �������պ����ѧѧ��, 2006,V32(02): 163-166
L�� Bin, Liu Deguang, Xie Changchuan, Yang Chao.Optimization designing method of wing flutter model for low-speed wind tunnel test[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2006,V32(02): 163-166
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