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…

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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…

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