An unstructured, shock-fitting algorithm, originally developed to simulate Eulerian flows, has being further developed to make it capable of dealing with shock/boundary-layer interactions. This paper illustrates the algorithmic features of this technique and the results achieved in the computation of hypersonic flows past compression ramps.
Numerical simulation of shock boundary layer interaction using shock fitting technique / Assonitis, A.; Paciorri, R.; Bonfiglioli, A.. - (2020), pp. 124-134. (Intervento presentato al convegno 24th Conference of the Italian Association of Theoretical and Applied Mechanics, AIMETA 2019 tenutosi a Rome; Italy) [10.1007/978-3-030-41057-5_10].
Numerical simulation of shock boundary layer interaction using shock fitting technique
Assonitis A.Primo
Software
;Paciorri R.Secondo
Methodology
;
2020
Abstract
An unstructured, shock-fitting algorithm, originally developed to simulate Eulerian flows, has being further developed to make it capable of dealing with shock/boundary-layer interactions. This paper illustrates the algorithmic features of this technique and the results achieved in the computation of hypersonic flows past compression ramps.| File | Dimensione | Formato | |
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