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作 者:Hualong Du Limei Xu Hongping Hu Yuantai Hu Xuedong Chen Hui Fan Jiashi Yang
机构地区:[1]Institute of Astronautics and Aeronautics, University of Electronic Science and Technology, Chengdu 610054, China [2]Shool of Civil Engineering and Mechanics, Huazhong University of Science and Technology, Wuhan 430074, China [3]National NC System Engineering Research Center, Huazhong University of Science and Technology, Wuhan 430074, China [4]School of Mechanical and Aerospace Engineering, Nanyang Technological University, 639798 Singapore [5]Department of Engineering Mechanics, University of Nebraska, Lincoln, NE 68588-0526, USA
出 处:《Acta Mechanica Solida Sinica》2008年第6期564-572,共9页固体力学学报(英文版)
基 金:supported by the National Natural Science Foundation of China(Nos.60302001 and 10872074);Major State Basic Research Development Program of China(973 Program)(No.2009CB724205).
摘 要:Coupled extensional and flexural cylindrical vibrations of a corrugated cylindrical piezoelectric shell consisting of multiple pieces of circular cylindrical surfaces smoothly connected along their generatrix are studied. To validate the results for the case of relatively thick shells or equivalently high-frequency modes with short wavelengths, existing analysis is extended by considering shear deformation and rotatory inertia. An analytical solution is obtained. Based on the solution, resonant frequencies and mode shapes are calculated.Coupled extensional and flexural cylindrical vibrations of a corrugated cylindrical piezoelectric shell consisting of multiple pieces of circular cylindrical surfaces smoothly connected along their generatrix are studied. To validate the results for the case of relatively thick shells or equivalently high-frequency modes with short wavelengths, existing analysis is extended by considering shear deformation and rotatory inertia. An analytical solution is obtained. Based on the solution, resonant frequencies and mode shapes are calculated.
关 键 词:corrugated shell piezoelectric transducer multi-piece structure shear deformation rotatory inertia
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