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An approximate method for determining the maximum amplitude of higher-order duct modes

机译:确定高阶管道模式最大振幅的一种近似方法

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Previous investigations have used Hankel transforms to establish the amplitudes of the wave fields resulting from arbitrary angle impingement on a circular orifice in a baffle. Investigations have also been undertaken on the effects of model coupling between the higher modes in the orifice. In particular, these studies concentrated on establishing the contributions at the cut-on wave number for a particular mode. This work is extended to introduce a method of simply approximating the complex amplitude of the forward and backward waves in the duct at the cut-on wave number, based only on the modal wave number. The interest focuses on the cut-on wave number because the forcing functions for the various fields will be at a maximum at cut-on. This technique is established by observing the relationships between the peak values of the driving functions and the modal wave number. If simple approximations are established for the in-duct field, it is also possible to approximate the maximum amplitude of the scattered field.
机译:先前的研究已经使用汉克尔变换来建立由折流板中的圆形孔口上任意角度撞击产生的波场的幅度。还对孔中较高模式之间的模型耦合效果进行了研究。尤其是,这些研究集中于确定特定模式下切入波数的贡献。这项工作被扩展为引入一种仅基于模态波数简单地以切合波数近似估算管道中向前和向后波的复振幅的方法。兴趣集中在切入波数上,因为在切入时各个字段的作用力将最大。通过观察驱动功能的峰值与模态波数之间的关系来建立该技术。如果为感应场建立简单的近似,则也可以近似散射场的最大幅度。

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