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Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 3 4 5 6 7 Next > Last >>
NACA 0016 15.91 0 0 1.332 0.0106
P-51H ROOT 15.49 1.333 47.5 1.223 0.0031
KC-135 BL52.44 15.45 1.015 25 1.382 0.0079
BOEING 737 ROOT AIRFOI 15.33 0.233 4.95 1.372 0.011
NACA 0015 15.01 0 0 1.287 0.0064
Coordinates
XUpper YUpper XLower YLower
0 0 0 0
0.6161 1.8011 0.6161 -1.8011
2.4491 3.4537 2.4491 -3.4537
5.454 4.9172 5.454 -4.9172
9.5566 6.1416 9.5566 -6.1416
14.6558 7.0793 14.6558 -7.0793
20.6261 7.6963 20.6261 -7.6963
27.3202 7.9801 27.3202 -7.9801
34.5732 7.9427 34.5732 -7.9427
42.2064 7.6181 42.2064 -7.6181
50.0316 7.056 50.0316 -7.056
57.8561 6.3141 57.8561 -6.3141
65.4869 5.4513 65.4869 -5.4513
72.7361 4.5234 72.7361 -4.5234
79.4251 3.5821 79.4251 -3.5821
85.3889 2.6757 85.3889 -2.6757
90.4806 1.8503 90.4806 -1.8503
94.5747 1.1501 94.5747 -1.1501
97.5704 0.6158 97.5704 -0.6158
99.3938 0.281 99.3938 -0.281
100 0.168 100 -0.168
V 1.0