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基于二阶抛物线方法的短舱外涵道声传播研究

Sound Propagation in a Nacelle Bypass Duct Based on the Second Order Parabolic Equation Method

  • 摘要: 为提升外涵道声传播计算和声衬优化效率,本文针对目前短舱外涵道管道声传播的计算方法开展计算方法研究与分析。在抛物线方法理论基础上,推导了二阶抛物线方法的控制方程,对比分析该方法的声传播角度适用范围和计算精度,并结合解析解对该方法进行验证。研究结果表明,相比于传统抛物线方法,二阶抛物线方法可以有效改善高阶模态及大角度声传播的精度,将声传播角度限制由20°提升到43°,且计算效率基本与传统抛物线方法一致。在0~43°传播角度范围内,二阶抛物线方法与解析解的计算误差小于5%。

     

    Abstract: To improve the efficiency of bypass duct sound propagation and liner optimization, a technique for calculating the effect of aft fan sound propagation was studied. Based on the theory of parabolic approximation, theoretical equation of 2nd order parabolic equation is developed. The accuracy of standard parabolic equation and 2nd order parabolic equation was analyzed and compared, and then followed with validation cases for parabolic equation prediction result and analytical solution. Validation case result indicates that standard parabolic equation can estimate propagation angle from 0 degree to 20 degree, and 2nd parabolic equation removes phase inaccuracy of 20 degree to 43 degree. Parabolic equation solution is much cheaper than solving the elliptic equation both in memory and running time. Meanwhile, calculation efficiency of standard parabolic equation and 2nd parabolic equation are almost the same. From 0 degree to 43 degree of sound propagation angle, the error between 2nd order parabolic equation prediction and analytical solution is less than 5%.

     

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