Abstract
The method of space-time conservation element solution element (STCS) is originally designed for Euler equations or Navier-Stokes equations in CFD. The scheme is found to possess very low dispersion error and handles both continuous and discontinuous waves. In addition, the non-reflecting boundary condition is strikingly simple. It is then tested in several benchmark computational aeroacoustics (CAA) problems from weak linear acoustic waves to strongly non-linear or even discontinuous waves to demonstrate its robustness.
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© 1997 Springer-Verlag
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Chang, S.C., Loh, C.Y., Yu, S.T. (1997). Computational aeroacoustics via a new global conservation scheme. In: Kutler, P., Flores, J., Chattot, JJ. (eds) Fifteenth International Conference on Numerical Methods in Fluid Dynamics. Lecture Notes in Physics, vol 490. Springer, Berlin, Heidelberg. https://doi.org/10.1007/BFb0107095
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DOI: https://doi.org/10.1007/BFb0107095
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