Abstract
An approach for the treatment of CFD simulations on configurations consisting of more than one discretized components is described. The approach interfaces the dual meshes of the different blocks through cutting with an interface common for the blocks and is named the Dual Mesh Connect (DMC) approach. This approach is spatially conservative and capable of treating blocks with intersecting geometries in a natural manner. A description of the current implementation is given and the application of the method a wing geometry is shown.
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© 2013 Springer-Verlag Berlin Heidelberg
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Sørensen, K.A. (2013). Multi-component Modeling with the Dual Mesh Connect Approach. In: Kroll, N., Radespiel, R., Burg, J., Sørensen, K. (eds) Computational Flight Testing. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 123. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-38877-4_18
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DOI: https://doi.org/10.1007/978-3-642-38877-4_18
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-642-38876-7
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