Abstract
AbstractStrictly stable high order finite difference operators have been applied to the compressible Navier‐Stokes equations in perturbation form for low Mach number computational aeroacoustics. Aeolian tones generated by vortex shedding from a circular cylinder have been simulated. (© 2005 WILEY‐VCH Verlag GmbH & Co. KGaA, Weinheim)
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