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...

Full description

Saved in:
Bibliographic Details
Main Authors: Malti, Khadidja, Hebow, Hanaa, Imine, Bachir
Format: Conference Proceeding
Language:English
Subjects:
Aerodynamics
Boundary layers
Computational fluid dynamics
Computer simulation
Ground effect (aerodynamics)
Incidence angle
Mathematical models
Meshing
Simulation
Turbulence models
Two dimensional flow
Citations: Items that this one cites
Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
Description
Summary: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