A flexible multiblock implementation of second and third-order accurate Residual-Based Compact (RBC) schemes is proposed and validated for turbomachinery flows of increasing complexity. 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.

Multiblock Residual-Based Compact Schemes for the Computation of Complex Turbomachinery Flows

CINNELLA, Paola;
2011-01-01

Abstract

A flexible multiblock implementation of second and third-order accurate Residual-Based Compact (RBC) schemes is proposed and validated for turbomachinery flows of increasing complexity. 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.
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11587/342497
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