Progress on the development and the application of an accurate and efficient flow solver for steady turbomachinery flows is reported. The code uses unstructured tetrahedral grids, its space-discretization is based on a fluctuation splitting scheme and an implicit strategy is used for the time integration. Results include the three-dimensional analysis of the flow field of a compressor stator and thorough comparisons with experimental data and numerical results obtained with other codes.

Computing Three-Dimensional Turbomachinery Flows with an Implicit Fluctuation Splitting Scheme

BONFIGLIOLI, Aldo;
2006-01-01

Abstract

Progress on the development and the application of an accurate and efficient flow solver for steady turbomachinery flows is reported. The code uses unstructured tetrahedral grids, its space-discretization is based on a fluctuation splitting scheme and an implicit strategy is used for the time integration. Results include the three-dimensional analysis of the flow field of a compressor stator and thorough comparisons with experimental data and numerical results obtained with other codes.
2006
9789634208723
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11563/10134
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