This paper describes the development and application of CFD codes, based on time-marching finite-volume formulations to the flow analysis in blade cascades, blade rows and stages of modern turbomachines. Special attention is paid to the reduction of the numerical dissipation of finite-volume discretization schemes, the numerical simulation of shock waves and to viscous effects. Furthermore, the application of solution-adaptive structured and unstructured computational grids is investigated. Finally, the ability of time-marching finite-volume methods to simulate three-dimensional flow effects in turbomachinery bladings is demonstrated.
Use of Advanced CFD Codes in the Turbomachinery Design Process
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Novak, O, Schäfer, O, Schönung, B, & Pätzold, H. "Use of Advanced CFD Codes in the Turbomachinery Design Process." Proceedings of the ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition. Volume 1: Turbomachinery. Cologne, Germany. June 1–4, 1992. V001T01A117. ASME. https://doi.org/10.1115/92-GT-324
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