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== Abstract ==2
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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 2D flow-configurations featuring different SWBLIs, including the transonic turbulent flow past a symmetrical airfoil and a laminar oblique-shock reflection.4
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== Full document ==6
<pdf>Media:Draft_Content_102882671p2377.pdf</pdf>7
Return to Assonitis et al 2021a.
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