Numerical study of flow around NACA0015 in ground effect

Numerical study of flow around NACA0015 in ground effect

The aim of this work is to present a numerical simulation of flow around a wing profile NACA0015 under the ground effect. CFD software has been used to determine the aerodynamic performance for different angles of incidence. The flow is considered two-dimensional and the adopted meshing considered t...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Malti, Khadidja, Hebow, Hanaa, Imine, Bachir
Format: Tagungsbericht
Sprache:eng
Schlagworte:
Aerodynamics
Boundary layers
Computational fluid dynamics
Computer simulation
Ground effect (aerodynamics)
Incidence angle
Mathematical models
Meshing
Simulation
Turbulence models
Two dimensional flow
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Beschreibung
Zusammenfassung:The aim of this work is to present a numerical simulation of flow around a wing profile NACA0015 under the ground effect. CFD software has been used to determine the aerodynamic performance for different angles of incidence. The flow is considered two-dimensional and the adopted meshing considered the effects of the boundary layer. The Spalart-Almaras turbulence model was adopted for the investigation of complex flow around the profile. The results obtained by CFD were compared to those obtained by the literature.
ISSN:2100-014X
2101-6275
2100-014X
DOI:10.1051/epjconf/201611402069