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...
| Hlavní autoři: | , |
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| Médium: | Článek |
| Jazyk: | English |
| Vydáno: |
Instituto de Aeronáutica e Espaço (IAE)
2020-05-01
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| Edice: | Journal of Aerospace Technology and Management |
| Témata: | |
| On-line přístup: | https://www.scielo.br/pdf/jatm/v12/2175-9146-jatm-12-e1920.pdf |