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Ti17模拟叶片在空气中的阻尼试验
引用本文:王梅,陆山,古远兴.Ti17模拟叶片在空气中的阻尼试验[J].航空动力学报,2009,24(10):2291-2295.
作者姓名:王梅  陆山  古远兴
作者单位: 
摘    要:通过Ti17平板模拟叶片在空气中测阻尼试验研究,用自由振动衰减法测取到各阶振型衰减系数,得出其各阶振型阻尼比,推导出比例阻尼系数,为叶片响应计算时的阻尼系数取值提供了参考.研究还发现振型阻尼比与材料硬度、叶片固有频率及振型密切相关,并给出了定性分析.

关 键 词:阻尼  试验  模拟叶片  振型阻尼比  阻尼系数
收稿时间:2008/10/27 0:00:00
修稿时间:2008/12/22 0:00:00

Analysis of damp trial result of Ti17 simulation blade in air
WANG Mei,LU Shan and Gu Yuan-xing.Analysis of damp trial result of Ti17 simulation blade in air[J].Journal of Aerospace Power,2009,24(10):2291-2295.
Authors:WANG Mei  LU Shan and Gu Yuan-xing
Institution:School of Power and Energy, Northwest Polytechnical University, Xi'an 710072, China;Gas Turbine Establishment of China, Aviation Industry Corporation of China, Chengdu 610500, China;School of Power and Energy, Northwest Polytechnical University, Xi'an 710072, China;Gas Turbine Establishment of China, Aviation Industry Corporation of China, Chengdu 610500, China
Abstract:Through simulation blade's damp trial in air,various order vibration model attenuation coefficients have been achieved by the method of free vibration attenuation,then various order vibration model damp ratios were obtained,and the ratio damp coefficients were deduced.These could offer reference for analysis of the relationship between the blade's damp and vibration model in nature and deciding the damp coefficient when calculating the response.
Keywords:damp  trial  simulation blade  vibration mode damp ratio  damp coefficient
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