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A parallel three-dimensional computational aeroacoustics method using nonlinear disturbance equations

机译:使用非线性扰动方程的并行三维计算航空声学方法

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This paper describes the application of a three-dimensional com- putational aeroacoustics (CAA) methodology to the prediction of jet noise. The technique has been implemented using parallel com- puters. In this approach the nonlinear disturbance equations are solved in a conservative form using a finite-difference based tech- nique. A fourth-order optimized dispersion relation preserving scheme is used for spatial discretization and a fourth-order classical Runge-Kutta scheme is employed for temporal discretization. The Three-dimensional CAA code has been parallelized using a domain Decomposition strategy in the streamwise direction.
机译:本文介绍了三维计算航空声学(CAA)方法在喷射噪声预测中的应用。该技术已使用并行计算机实现。在这种方法中,非线性扰动方程采用基于有限差分的技术以保守的形式求解。将四阶优化色散关系保留方案用于空间离散化,并将四阶经典Runge-Kutta方案用于时间离散化。三维CAA代码已使用域分解策略在流方向上进行了并行化。

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