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Calculation of sound fields in small enclosures using a meshless model

机译:使用无网格模型计算小型机壳中的声场

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The details are provided for the derivation and implementation of a meshless model based on the Element-free Galerkin Method for calculating sound fields. The model is applicable to three-dimensional small enclosures with arbitrary shape. In the model, the system equation for calculating the sound pressure of nodes is derived using the Galerkin weighted residual method. The shape functions are constructed using the moving least squares method, and the methods for calculating the integrals are described in detail. The frequency response function of a rectangular enclosure and a cylindrical enclosure are calculated using the model, and the results are compared with the results obtained using a theoretical method. Boundary Element Method (BEM), and with experimental results, respectively. Next, the factors that influence the performance of the method, which include the distribution and number of nodes, the number of integration points, the types of basis, and the weight functions, are discussed. The suitable support domain radius for the calculation of sound fields in small enclosures is also obtained through use of numerical experiments. Finally, the meshless model with suitable parameters is used to calculate the sound field of an airplane cabin. Comparison of the calculated sound pressure levels with the measured results has validated the model's accuracy and applicability to enclosures with complicated structures.
机译:为基于计算声场的无元素Galerkin方法推导和实现无网格模型提供了详细信息。该模型适用于任意形状的三维小空间。在该模型中,使用Galerkin加权残差法推导了计算节点声压的系统方程。使用移动最小二乘法构造形状函数,并详细描述用于计算积分的方法。使用该模型计算矩形外壳和圆柱外壳的频率响应函数,并将结果与​​使用理论方法获得的结果进行比较。边界元法(BEM)和实验结果。接下来,讨论影响该方法性能的因素,包括节点的分布和数量,积分点的数量,基础的类型以及权重函数。还可以通过使用数值实验来获得用于计算小型机壳中声场的合适支撑域半径。最后,使用具有合适参数的无网格模型来计算飞机机舱的声场。将计算出的声压级与测量结果进行比较,验证了该模型的准确性和适用于结构复杂的外壳的适用性。

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