Abstract
A semi-unstructured grid generation method especially taylored for the meshing of turbomachinery blade passages and their associated cavities is presented. The method is based on a smart combination of quasi-3D methods, an ad-hoc block decomposition of the domain and a grid-based reconstruction of the computational domain.
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References
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Burgos, M.A., Corral, R., Fernández-Castañeda, J., López, C. (2006). Rapid Meshing of Turbomachinery Rows Using Semi-Unstructured Conformal Grids. In: Pébay, P.P. (eds) Proceedings of the 15th International Meshing Roundtable. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-34958-7_6
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DOI: https://doi.org/10.1007/978-3-540-34958-7_6
Publisher Name: Springer, Berlin, Heidelberg
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Online ISBN: 978-3-540-34958-7
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