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| − | The unstructured shock-fitting algorithm originally proposed in Ref. [3] has been further developed to make it capable of dealing with shock-wave/boundary-layer interactions (SWBLIs). This paper illustrates the algorithmic features of the technique and its application to | + | The unstructured shock-fitting algorithm originally proposed in Ref. [3] has been further developed to make it capable of dealing with shock-wave/boundary-layer interactions (SWBLIs). This paper illustrates the algorithmic features of the technique and its application to 2D flow-configurations featuring different SWBLIs, including the transonic turbulent flow past a symmetrical airfoil and a laminar oblique-shock reflection. |
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<pdf>Media:Draft_Content_102882671p2377.pdf</pdf> | <pdf>Media:Draft_Content_102882671p2377.pdf</pdf> | ||
Latest revision as of 19:44, 11 March 2021
Abstract
The unstructured shock-fitting algorithm originally proposed in Ref. [3] has been further developed to make it capable of dealing with shock-wave/boundary-layer interactions (SWBLIs). This paper illustrates the algorithmic features of the technique and its application to 2D flow-configurations featuring different SWBLIs, including the transonic turbulent flow past a symmetrical airfoil and a laminar oblique-shock reflection.
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Published on 10/03/21
Submitted on 10/03/21
Volume 200 - Advanced Discretization Techniques, 2021
DOI: 10.23967/wccm-eccomas.2020.243
Licence: CC BY-NC-SA license
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