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Part of the book series: Notes on Numerical Fluid Mechanics (NNFM) ((NNFM,volume 43))

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Abstract

To solve the ID Euler equations for compressible low Mach number flow, we investigated two flux-vector splittings. Both splittings are applied to a quasi one-dimensional nozzle flow, using the explicit as well as a semi-implicit Euler scheme with a finite volume upwind formulation. Results at low and very low Mach numbers are compared with calculations using the Roe scheme. À von Neumann stability analysis was carried out for the more promising scheme based on a convection-pressure splitting.

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Andrea Donato Francesco Oliveri

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© 1993 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden

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Sesterhenn, J., Müller, B., Thomann, H. (1993). Flux — Vector Splitting for Compressible Low Mach Number Flow. In: Donato, A., Oliveri, F. (eds) Nonlinear Hyperbolic Problems: Theoretical, Applied, and Computational Aspects. Notes on Numerical Fluid Mechanics (NNFM), vol 43. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-87871-7_64

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  • DOI: https://doi.org/10.1007/978-3-322-87871-7_64

  • Publisher Name: Vieweg+Teubner Verlag

  • Print ISBN: 978-3-528-07643-6

  • Online ISBN: 978-3-322-87871-7

  • eBook Packages: Springer Book Archive

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