2017
DOI: 10.1016/j.compfluid.2017.01.002
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Assessment of high-order finite volume methods on unstructured meshes for RANS solutions of aeronautical configurations

Abstract: This version is available at https://strathprints.strath.ac.uk/59947/ Strathprints is designed to allow users to access the research output of the University of Strathclyde. Unless otherwise explicitly stated on the manuscript, Copyright © and Moral Rights for the papers on this site are retained by the individual authors and/or other copyright owners. Please check the manuscript for details of any other licences that may have been applied. You may not engage in further distribution of the material for any pro… Show more

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Cited by 42 publications
(15 citation statements)
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References 79 publications
(115 reference statements)
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“…The interface fluxes are computed based on the boundary extrapolated reconstructed values, which are obtained by a polynomial reconstruction from element-averaged data. The spatial discretisation is based on the approach of [8,9] and lies in the the k-exact least square reconstruction, which is suitable for unstructured meshes with various types of element shapes in 2D and 3D, and it has been previously used successfully for laminar, transitional and turbulent flows [13,[46][47][48][49][50][51][52][53] and all the schemes are implemented in the UCNS3D CFD code as detailed in [52]. Therefore, only the key characteristics of this approach are going to be described in this paper.…”
Section: General Formulationmentioning
confidence: 99%
“…The interface fluxes are computed based on the boundary extrapolated reconstructed values, which are obtained by a polynomial reconstruction from element-averaged data. The spatial discretisation is based on the approach of [8,9] and lies in the the k-exact least square reconstruction, which is suitable for unstructured meshes with various types of element shapes in 2D and 3D, and it has been previously used successfully for laminar, transitional and turbulent flows [13,[46][47][48][49][50][51][52][53] and all the schemes are implemented in the UCNS3D CFD code as detailed in [52]. Therefore, only the key characteristics of this approach are going to be described in this paper.…”
Section: General Formulationmentioning
confidence: 99%
“…High-order discretisation ( > 2 nd - order ) for vortex-dominant flows enhances accuracy and potential efficiency of the overall numerical method. 41…”
Section: Cfd Methodologymentioning
confidence: 99%
“…2nd-order) for vortex-dominant flows enhances accuracy and potential efficiency of the overall numerical method. 41 The CFD model consists of a rotating wheel equivalent to the conditions as in Fackrell's 9 experiment. The flow around the wheel is simulated with a Reynolds number of Re d = 5:3 Á 10 5 based on the wheel diameter.…”
Section: Governing Equationsmentioning
confidence: 99%
“…Despite the fact that unstructured high-order finite volume methods (FVM) have been very promising and popular in the computational fluid dynamics (CFD) research community [1,2,3,4], the second-order FVM is still a prominent and dominating numerical method for simulating complex flows in both scientific and industrial scenarios, and it is still developing with much effort, aiming at further improvements regarding both accurate approximation and/or computational efficiency. An extensive overview of unstructured FVM discretizations and solvers was given by Mavriplis [5].…”
Section: Introductionmentioning
confidence: 99%