This paper presents a new finite volume cell-centered scheme for solving the two-dimensional Euler equations. The technique for computing the advective derivatives is based on a high-order Gauss quadrature and an original quadratic reconstruction of the conservative variables for each control volume. A very sensitive detector identifying discontinuity regions switches the scheme to a TVD scheme, and ensures the monotonicity of the solution. The code uses unstructured meshes whose cells are polygons with any number of edges. A mesh adaptation based on cell division is performed in order to increase the resolution of shocks. The accuracy, insensitivity to grid distortions, and shock capturing properties of the scheme are demonstrated for different cascade flow computations.
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April 1997
Research Papers
Finite Volume Scheme With Quadratic Reconstruction on Unstructured Adaptive Meshes Applied to Turbomachinery Flows
M. Delanaye,
M. Delanaye
Aerodynamics Group, Institute of Mechanics and Aeronautics, The University of Lie`ge, Lie`ge, Belgium
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J. A. Essers
J. A. Essers
Aerodynamics Group, Institute of Mechanics and Aeronautics, The University of Lie`ge, Lie`ge, Belgium
Search for other works by this author on:
M. Delanaye
Aerodynamics Group, Institute of Mechanics and Aeronautics, The University of Lie`ge, Lie`ge, Belgium
J. A. Essers
Aerodynamics Group, Institute of Mechanics and Aeronautics, The University of Lie`ge, Lie`ge, Belgium
J. Turbomach. Apr 1997, 119(2): 263-269 (7 pages)
Published Online: April 1, 1997
Article history
Received:
March 2, 1995
Online:
January 29, 2008
Citation
Delanaye, M., and Essers, J. A. (April 1, 1997). "Finite Volume Scheme With Quadratic Reconstruction on Unstructured Adaptive Meshes Applied to Turbomachinery Flows." ASME. J. Turbomach. April 1997; 119(2): 263–269. https://doi.org/10.1115/1.2841109
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