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.
Numerical simulation of shock boundary layer interaction using a shock fitting technique / Assonitis, A.; Paciorri, R.; Bonfiglioli, A.. - (2021). (Intervento presentato al convegno 14th WCCM-ECCOMAS, virtual congress, January, 11-15, 2021. tenutosi a virtual congress) [10.23967/wccm-eccomas.2020.243].
Numerical simulation of shock boundary layer interaction using a shock fitting technique
Assonitis, A.
Primo
Software
;Paciorri, R.Secondo
Methodology
;
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.| File | Dimensione | Formato | |
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Assonitis_Preprint_Numerical_2021.pdf
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Note: https://www.scipedia.com/public/Assonitis_et_al_2021a
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3.03 MB | Adobe PDF |
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