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Direct numerical simulation of acoustic waves interacting with a shock wave in a quasi-1D convergent-divergent nozzle using an unstructured finite volume algorithm

机译:利用非结构有限体积算法直接数值模拟准1D收敛 - 扩散喷管中声波与冲击波相互作用

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Numerical simulation of a very small amplitude acoustic wave interacting with a shock wave in a quasi-1D convergent-divergent nozzle is performed using an unstructured finite volume algorithm with a piece-wise linear, least square reconstruction, Roe flux difference splitting, and second-order MacCormack time marching. First, the spatial accuracy of the algorithm is evaluated for steady flows with and without the normal shock by running the simulation with a sequence of successively finer meshes. Then the accuracy of the Roe flux difference splitting near the sonic transition point is examined for different reconstruction schemes. Finally, the unsteady numerical solutions with the acoustic perturbation are presented and compared with linear theory results.

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