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.
|Titolo:||Simulation of Shock Boundary Layer Interaction Using Shock Fitting Technique|
|Data di pubblicazione:||2019|
|Appare nelle tipologie:||4.1 Contributo in atti di Convegno|