n66021 Airfoil

NACA 66(4)-021 airfoil n66021 Airfoil (x,y) Coordinates 0 0 0.005 0.01525 0.0075 0.01804 0.0125 0.0224 0.025 0.03045 0.05 0.04269 0.075 0.05233 0.1 0.06052 0.15 0.07369 0.2 0.08376 0.25 0.09153 0.3…

Continue Readingn66021 Airfoil

n642415 Airfoil

ACA 64(2)-415 [NACA 6a series from Theory of Wing Sections] n642415 Airfoil (x,y) Coordinates 100 0 95.032 0.976 90.066 1.982 85.092 3.02 80.109 4.062 75.115 5.084 70.111 6.055 65.096 6.954…

Continue Readingn642415 Airfoil