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...
Main Authors: | , |
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Format: | Article |
Language: | English |
Published: |
MDPI AG
2023-04-01
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Series: | Aerospace |
Subjects: | |
Online Access: | https://www.mdpi.com/2226-4310/10/4/377 |