'NACA 64015A Swept Back Wing' simulation project by j_martins


I created a new simulation project called 'NACA 64015A Swept Back Wing':

CFD analysis to verify the experimental results carried out on NACA 64015A Swpetback wing at AoA zero degree and Sweep angle 20 degrees.

Reference: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19980227185.pdf

More of my public projects can be found here.