Abstract
In the field of compressible high Mach number flow, the availability of robust and versatile solvers capable of handling both severe flow conditions and general geometries, and including local mesh refinement, is of crucial importance in Aerospace Engineering studies.
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© 1992 Springer Science+Business Media New York
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Dervieux, A. et al. (1992). Unstructured-Grid Algorithms for High-Speed CFD Analysis. In: Bertin, J.J., Periaux, J., Ballmann, J. (eds) Advances in Hypersonics. Birkhäuser, Boston, MA. https://doi.org/10.1007/978-1-4612-0375-9_3
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DOI: https://doi.org/10.1007/978-1-4612-0375-9_3
Publisher Name: Birkhäuser, Boston, MA
Print ISBN: 978-1-4612-6732-4
Online ISBN: 978-1-4612-0375-9
eBook Packages: Springer Book Archive