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Finite element simulation study on influence of spacecraft stiffener structure on elastic wave propagation

机译:有限元仿真研究对航天器加强筋结构对弹性波传播的影响

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Aiming at the propagation process of elastic wave in spacecraft stiffener structure. In this paper, the phase and energy changes of elastic waves propagating in the wall structure of stiffeners at different frequencies are analyzed by using finite element method and laser Doppler vibrometer (LDVS). Meanwhile, the relationship between the parameters of stiffeners and the diffusion of acoustic wave energy and the phase change of elastic waves respectively is obtained. The results show that in the range of parameters involved in this paper, the stiffener has a significant effect on elastic waves propagation. When wavelength λ > 10mm, most of the elastic waves are reflected by the stiffener, while when λ < 6mm, elastic waves propagate more easily across the stiffener, and the proportion of those propagated by the stiffener increases. Moreover, the functional expression of the relationship between the height of the stiffener and the frequency of the elastic wave which can easily propagate through the stiffener is obtained.
机译:针对航天器加强筋结构弹性波的传播过程。在本文中,通过使用有限元方法和激光多普勒振动计(LDVS)分析在不同频率下在不同频率的加强件壁结构中传播的弹性波的相位和能量变化。同时,获得了加强筋参数与声波能量的扩散之间的关系及分别的弹性波的相变。结果表明,在本文涉及的参数范围内,加强筋对弹性波传播具有显着影响。当波长λ> 10mm时,大部分弹性波被加强件反射,而当λ<6mm时,弹性波在加强件上更容易传播,并且由加强件传播的那些比例增加。此外,获得了加强筋的高度与可以容易地通过加强件传播的弹性波的频率之间的关系的功能表达。

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