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基于二阶抛物线方法的短舱外涵道声传播

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,文章对目前短舱外涵道管道声传播的计算方法开展研究与分析。在抛物方程法理论基础上,推导了二阶抛物方程法的控制方程,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,与传统抛物方程法相比,二阶抛物方程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°,且计算效率与传统抛物线方法基本一致。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 is studied. Based on the theory of parabolic approximation, theoretical equation of second-order order parabolic equation method is developed. The accuracy of standard parabolic equation and second-order order parabolic equation method is analyzed and compared, and then followed with validation cases for parabolic equation prediction result and analytical solution. Validation case result indicates that compared with the traditional parabolic equation method, the second-order parabolic equation method can effectively improve the accuracy of high-order modes and large angle sound propagation, increasing the sound propagation angle limit from 20 ° to 43 °. The calculation efficiency of the second-order parabolic equation method is almost the same as that of the traditional parabolic equation method. From 0° to 43° of sound propagation angle, the error between second-order parabolic equation prediction and analytical solution is less than 5%.

     

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