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Computational fluid dynamics applied to the aerodynamic design of a land-based supersonic vehicle

B.J Evans, O Hassan, J.W Jones, K Morgan, L Remaki, Kenneth Morgan Orcid Logo, Oubay Hassan Orcid Logo, Jason Jones Orcid Logo, Ben Evans Orcid Logo

Numerical Methods for Partial Differential Equations, Volume: 27, Issue: 1, Pages: 141 - 159

Swansea University Authors: Kenneth Morgan Orcid Logo, Oubay Hassan Orcid Logo, Jason Jones Orcid Logo, Ben Evans Orcid Logo

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DOI (Published version): 10.1002/num.20644

Published in: Numerical Methods for Partial Differential Equations
ISSN: 0749-159X
Published: 2011
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URI: https://cronfa.swan.ac.uk/Record/cronfa6255
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Item Description: This paper presents the work to adapt the FLITE CFD code for it to be applied to the particularly challenging flow conditions experienced by the BLOODHOUND SSC i.e. high Mach number, complex geometry and boundary conditions, including supersonic rotating surfaces. The stabilisation of the finite volume scheme using a consistent HLLC flux function and the resulting algorithm performance discussed along with its impact on the aerodynamic design of BLOODHOUND SSC.
College: Faculty of Science and Engineering
Issue: 1
Start Page: 141
End Page: 159