TY  - Type of reference 
TI  - Analyse CFD de l’écoulement transsonique autour d’un profil d’aile NACA 0012 
AU  - R. El Maani 
AU  - B. Radi 
AU  - A. El Hami 
AB  - Computational Fluid Dynamics (CFD) incorporates mathematical relations and algorithms to analyze and solve the problems regarding fluid flow. CFD analysis of an airfoil produces results such as lift and drag forces which determines the ability of an airfoil. In this paper a transonic flow will be modelled over a NACA 0012 airfoil for which experimental data has been published, so that a comparison can be made. The flow to be considered is compressible and turbulent and the solver used is the density based implicit solver, which gives good results for high speed compressible
flows. The results show that the predicted lift, drag and pressure coefficients are in good agreement with experimental data. 
DO  - 10.21494/ISTE.OP.2018.0307 
JF  - Incertitudes et fiabilité des systèmes multiphysiques 
KW  - CFD,  aerodynamic,  NACA 0012,  pressure coefficient,  airfoil, CFD,  aerodynamic,  NACA 0012,  pressure coefficient,  airfoil,  
L1  - https://www.openscience.fr/IMG/pdf/iste_incertfia18v2n2_5.pdf 
LA  - fr 
PB  - ISTE OpenScience 
DA  - 2018/12/14 
SN  - 2514-569X 
TT  - CFD Analysis of the Transonic Flow over a NACA 0012 Airfoil 
UR  - https://www.openscience.fr/Analyse-CFD-de-l-ecoulement-transsonique-autour-d-un-profil-d-aile-NACA-0012 
IS  - Numéro 2 
VL  - 2 
ER  -