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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 51 52 53 54 55 Next > Last >>
P-51D ROOT (BL17.5) 16.45 1.266 68.267 1.482 0.0063
EPPLER 1200 16.93 3.48 40.77 1.818 0.0072
EPPLER 266 17.3 3.062 39.79 1.483 0.0066
NACA 65-218 17.95 1.123 50 1.399 0.0076
NACA 2418 17.96 1.95 40 1.367 0.0128
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.558 1.52 0.558 -1.33
2.221 3.03 2.221 -2.64
4.952 4.47 4.952 -3.69
8.688 5.84 8.688 -4.67
13.347 6.97 13.347 -5.47
18.826 7.98 18.826 -6.14
25 8.73 25 -6.72
31.733 9.32 31.733 -7
38.874 9.47 38.874 -7.04
46.264 9 46.264 -6.73
53.736 8.14 53.736 -5.94
61.126 7.16 61.126 -4.79
68.267 6.15 68.267 -3.62
75 5.07 75 -2.65
81.175 3.81 81.175 -1.81
86.653 2.45 86.653 -1.05
91.312 1.37 91.312 -0.53
95.049 0.67 95.049 -0.25
97.779 0.28 97.779 -0.1
100 0 100 0
V 1.0