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所属单位：航空学院
发表刊物：Int. J. Aerosp. Eng.
摘要：In this paper, an analytical method is proposed to directly obtain the aeroelastic time domain response of the elastic boundary panel. Based on a modified Fourier series method (MFSM), the vibration analysis of elastic boundary panels is carried out, after the dynamics equation of the panel is obtained. Then, the vibrational functions are combined with the supersonic piston theory to establish the aeroelastic equation. The aeroelastic time domain response of the panel is obtained to analyze the flutter speed of the panel more intuitively. Finally, the flutter speeds of panels with different length-width ratios, thicknesses, and elastic boundary conditions are discussed in detail. Copyright © 2019 Xiyue Zhou et al.
ISSN号：1687-5966
是否译文：否
发表时间：2019-01-01
合写作者：Zhou, Xiyue,Jiang, Jingnong,F70206580
通讯作者：王立峰