Sherer Scott E
Air Vehicles Directorate, Air Force Research Laboratory, Wright-Patterson AFB, Ohio 45433-7521, USA.
J Acoust Soc Am. 2004 Feb;115(2):488-96. doi: 10.1121/1.1641790.
A general analytic method for calculating the scattering of sound by multiple rigid circular cylinders arranged in an arbitrary parallel configuration is presented. The sound scattered by this collection of cylinders is generated by a time-periodic, spatially distributed, axisymmetric source located within the domain of interest. A Hankel transform method is used to calculate the incident field, while separation of variables is used to obtain the scattered fields from each cylinder in the collection. The unknown scattering coefficients are determined through the use of general addition theorems that allows the various fields to be readily transformed between coordinate systems. The method is validated using various two-, three-, and four-cylinder configurations, and the number of coefficients that must be retained in the truncated series is examined. Benchmark configurations consisting of two- and three-cylinder systems with cylinders of varying radii are also presented. These solutions have been used to validate computational aeroacoustic solvers developed for complex geometries.
提出了一种用于计算任意平行排列的多个刚性圆柱散射声的通用解析方法。由该圆柱集合散射的声是由位于感兴趣区域内的时谐、空间分布的轴对称源产生的。使用汉克尔变换方法计算入射场,而用变量分离法从集合中的每个圆柱获得散射场。未知散射系数通过使用通用加法定理来确定,该定理允许各种场在坐标系之间轻松转换。使用各种双圆柱、三圆柱和四圆柱配置对该方法进行了验证,并研究了截断级数中必须保留的系数数量。还给出了由不同半径圆柱组成的双圆柱和三圆柱系统的基准配置。这些解已用于验证为复杂几何形状开发的计算气动声学求解器。