Airfoil:

mm

Job Status

Please wait while the PDF is generated...

Plot Number:

File:

Search for Airfoil
Winfoil Airfoils - Total Number: 277
Name T/C % Camber % Camber Chord % CL Max CD Min
<< First < Prev 51 52 53 54 55 Next > Last >>
AG17 6.49 2.013 45.4997 0.959 0.0072
AG16 7.11 1.869 45.4885 0.975 0.008
AG14 5.37 2.326 26.9742 0.897 0.0068
AG13 5.83 2.209 28.1134 0.887 0.0074
AG12 6.23 2.102 27.6418 0.878 0.0065
Coordinates
XUpper YUpper XLower YLower
0 -0.0158 0 -0.0158
0.0232 0.1348 0.0353 -0.1632
0.0966 0.2984 0.1387 -0.3053
0.2198 0.4819 0.3064 -0.4384
0.4076 0.6955 0.5465 -0.574
0.6944 0.9528 0.8937 -0.7231
1.1377 1.272 1.4154 -0.8951
1.8045 1.6557 2.1949 -1.0873
2.7028 2.0699 3.2246 -1.2732
3.7643 2.4669 4.4105 -1.4262
4.9192 2.8241 5.6736 -1.545
6.1297 3.1395 6.9736 -1.6335
7.3782 3.4165 8.2955 -1.6967
8.6527 3.6593 9.6323 -1.7399
9.9488 3.8723 10.9792 -1.7665
11.2599 4.0587 12.3336 -1.7797
12.5846 4.2218 13.6936 -1.7812
13.9184 4.3639 15.0585 -1.7728
15.2607 4.4871 16.4266 -1.7555
16.6099 4.5935 17.7981 -1.7301
17.9639 4.6842 19.1719 -1.6977
19.3233 4.761 20.5476 -1.6593
20.686 4.825 21.9253 -1.6155
22.0519 4.8772 23.3046 -1.5669
23.4209 4.9186 24.685 -1.5141
24.7916 4.95 26.0671 -1.4578
26.1644 4.9721 27.4503 -1.3983
27.5394 4.9856 28.8347 -1.3366
28.915 4.9911 30.2207 -1.2732
30.2923 4.9888 31.6079 -1.208
31.6712 4.9797 32.9962 -1.1417
33.0505 4.9638 34.3862 -1.0744
34.431 4.9414 35.7774 -1.0065
35.8127 4.913 37.1698 -0.9382
37.1948 4.879 38.5636 -0.8701
38.5774 4.8396 39.9584 -0.8019
39.961 4.7949 41.3536 -0.7342
41.3451 4.7453 42.7477 -0.6673
42.7293 4.691 44.1406 -0.6013
44.1142 4.632 45.5325 -0.5363
45.4997 4.5687 46.9238 -0.4729
46.8851 4.5013 48.314 -0.4112
48.2711 4.4298 49.7034 -0.3513
49.6577 4.3544 51.0923 -0.2931
51.0442 4.2754 52.4811 -0.2372
52.4307 4.1927 53.8693 -0.1834
53.8178 4.1065 55.2571 -0.1319
55.2052 4.017 56.6445 -0.0828
56.5925 3.9244 58.0319 -0.0364
57.9799 3.8286 59.4185 0.0075
59.3678 3.73 60.8049 0.0486
60.7557 3.6286 62.1908 0.087
62.1435 3.5246 63.5763 0.1224
63.5318 3.418 64.9612 0.1549
64.9202 3.309 66.346 0.1844
66.3082 3.1975 67.7307 0.2109
67.6966 3.0839 69.1153 0.2342
69.0854 2.9685 70.4999 0.2543
70.4739 2.8513 71.8847 0.2714
71.8624 2.7325 73.2698 0.2851
73.2513 2.6123 74.6549 0.2956
74.6399 2.4905 76.0403 0.3032
76.0282 2.3672 77.4259 0.3071
77.4167 2.2424 78.8116 0.308
78.805 2.1162 80.1978 0.3057
80.193 1.9883 81.5846 0.2999
81.5815 1.8589 82.9713 0.2909
82.9697 1.7281 84.3583 0.2787
84.3579 1.596 85.7456 0.2632
85.7464 1.4625 87.1329 0.2447
87.1348 1.328 88.5203 0.2232
88.5237 1.1924 89.9081 0.1983
89.9126 1.0558 91.2957 0.1702
91.3017 0.9183 92.6835 0.1395
92.6907 0.7801 94.0713 0.1061
94.0794 0.6406 95.4593 0.0693
95.4679 0.4997 96.8446 0.0298
96.8523 0.357 98.2051 -0.0118
98.2067 0.2158 99.4064 -0.0501
99.406 0.0877 99.9985 -0.0684
99.9985 0.0254 100.0004 -0.0685
V 1.0