Abstract
A robust implementation of residual-based compact schemes of second- and third-order accuracy on structured multiblock grids of industrial use is proposed. Applications to complex transonic unsteady flows in turbomachinery show the advantages of using such schemes in terms of increased accuracy and better insight into the flow physics. © 2011 Springer-Verlag Berlin Heidelberg.
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CITATION STYLE
Michel, B., Cinnella, P., & Lerat, A. (2011). Multiblock computations of complex turbomachinery flows using residual-based compact schemes. In Computational Fluid Dynamics 2010 - Proceedings of the 6th International Conference on Computational Fluid Dynamics, ICCFD 2010 (pp. 509–514). Kluwer Academic Publishers. https://doi.org/10.1007/978-3-642-17884-9_64
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