n10 Airfoil
N-10 airfoil N-10 airfoil (x,y) Co-ordinates 1 0.0034 0.95 0.0174 0.9 0.0296 0.8 0.051 0.7 0.0712 0.6 0.0874 0.5 0.101 0.4 0.1088 0.3 0.1124 0.2 0.1096 0.15 0.1022 0.1 0.0914…
n0012 Airfoil
NACA 0012 airfoil n0012 Airfoil (x,y) Co-ordinates 0 0 0.0005839 0.0042603 0.0023342 0.0084289 0.0052468 0.0125011 0.0093149 0.0164706 0.0145291 0.02033 0.0208771 0.0240706 0.0283441 0.0276827 0.0369127 0.0311559 0.0465628 0.0344792 0.057272 0.0376414 0.0690152…