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Investigation on Sound Source in Cascades by Computational Aero-Acoustics

机译:计算航空声学级联声源调查

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The wake/stator interaction has been predicted using an N-S solver, in order to obtain unsteady pressure fluctuations on blade surface and the variety of unsteady vortex. So the noise can be computed. The equations are solved using a finite volume time-integration Ni scheme. For improving the ability to simulate the turbulent flow , K-ε turbulence models are utilized for the turbulent closure. Then the numerical calculations on a turbine and an axial compressor cascades are carried out in this paper.
机译:使用N-S求解器预测了唤醒/定子相互作用,以便在叶片表面和各种不稳定涡流上获得不稳定的压力波动。所以可以计算噪声。使用有限音量时间积分Ni方案来解决方程。为了改善模拟湍流的能力,k-ε湍流模型用于湍流封闭。然后在本文中进行涡轮机和轴向压缩机级联的数值计算。

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