Towards Accurate Vortex Separation Simulations with RANS Using Improved <i>k</i>-<i>kL</i> Turbulence Model

In this study, we present our improved RANS results of the missile aerodynamic flow computation involving leading edge vortex separation. We have used our in-house tailored version of the open source finite volume solver FlowPsi. An ongoing study in the NATO STO Applied Vehicle Technologies Panel (A...

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Bibliographic Details
Main Authors: Erdem Dikbaş, Özgür Uğraş Baran
Format: Article
Language:English
Published: MDPI AG 2023-04-01
Series:Aerospace
Subjects:
Online Access:https://www.mdpi.com/2226-4310/10/4/377