References in periodicals archive ?
Airfoil considered in this study is NACA 0012 airfoil with chord length of 1m.
Sitaram, "Grid and turbulence model based exhaustive analysis of NACA 0012 airfoil," Journal of Advanced Research in Applied Mechanics & Computational Fluid Dynamics, vol.
0 X 106 Of Three Airfoil Sections Formed By Cutting Off Various Amounts From The Rear Portion Of The NACA 0012 Airfoil Section".
The stereolithography process it was experimented (Landrum, 1997) to manufacturing a NACA 0012 airfoil section.
z] of two NACA 0012 airfoils crossing over time traveling at M = 0.