Summary
A recently developed algorithm to adapt computational grids [1] is applied to aerodynamic problems. The algorithm is briefly described and the main features are discussed. Applications to both inviscid and viscous flows around two-dimensional airfoils show that the algorithm is robust and almost fully automatic, and that shocks, expansion zones, boundary layers and shear layers are well resolved by the adapted grid.
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© 1993 Friedr. Vieweg & Sohn Verlagsgesellschaft mbH, Braunschweig/Wiesbaden
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Hagmeijer, R., de Cock, K.M.J. (1993). Grid Adaption in Computational Aerodynamics. In: Weatherill, N.P., Marchant, M.J., King, D.A. (eds) Multiblock Grid Generation. Notes on Numerical Fluid Mechanics (NNFM), vol 44. Vieweg+Teubner Verlag. https://doi.org/10.1007/978-3-322-87881-6_17
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DOI: https://doi.org/10.1007/978-3-322-87881-6_17
Publisher Name: Vieweg+Teubner Verlag
Print ISBN: 978-3-528-07644-3
Online ISBN: 978-3-322-87881-6
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