基于多孔材料的圆柱空腔声学覆盖层优化设计方法研究

Research on Optimization Design Method of Acoustic Cover Layer Based on Porous Materials for Cylindrical Cavity

  • 摘要: 运载火箭在发射及飞行过程中外部环境产生的声学和振动激励易对其内部有效载荷产生威胁,多孔材料作为一种轻质吸声材料被广泛运用于运载火箭整流罩的降噪减振相关研究中。本文结合多孔材料物理模型以及阻抗管实验,采用粒子群优化算法开展了多孔材料参数拟合以及声学性能优化研究,得到一种多层多孔材料优化设计方法,并通过实验与仿真验证其吸声性能;基于整流罩圆柱段圆柱空腔实验平台验证多层多孔材料声学覆盖层的降噪减振性能,并对多孔材料敷设位置以及敷设率的影响开展仿真分析,能对多孔材料的应用提供设计指导。

     

    Abstract: During the launch and flight of carrier rockets, the acoustic and vibration excitations generated by the external environment may pose threats to the internal payloads. Porous materials, as lightweight sound-absorbing materials, have been widely used in research related to noise reduction and vibration damping of fairing structures. This paper combines the physical model of porous materials and impedance tube experiments, and employs particle swarm optimization algorithm to conduct parameter fitting and acoustic performance optimization of porous materials. A multilayer porous material optimization design method is proposed, and its sound absorption performance is validated through experiments and simulations. Based on the scaled model experiment platform of the fairing cylindrical section, the noise reduction and vibration damping performance of the multilayer porous material acoustic cover layer are verified, and the influence of porous material laying position and laying rate is analyzed through simulation, providing design guidance for the application of porous materials.

     

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