Numerical Simulation of the Boundary Layer Control on the NACA 0015 Airfoil Through Vortex Generators
This paper studies the influence caused by a vortex generator (VG) on a wing section with NACA 0015 airfoil when this generator is located before and after a recirculation bubble caused by the boundary layer detachment. The study was numerically carried out and concentrated under conditions of flow...
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| Format: | Artikel |
| Sprache: | English |
| Veröffentlicht: |
Instituto de Aeronáutica e Espaço (IAE)
2020-05-01
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| Schriftenreihe: | Journal of Aerospace Technology and Management |
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| Online Zugang: | https://www.jatm.com.br/jatm/article/view/1102 |