Multiblock residual-based compact schemes for the computation of complex turbomachinery flows
by B. Michel, P. Cinnella, A. Lerat
International Journal of Engineering Systems Modelling and Simulation (IJESMS), Vol. 3, No. 1/2, 2011

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.

Online publication date: Sat, 21-Mar-2015

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