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Winfoil Airfoils - Total Number: 277
Name T/C % T/C % Chord Position Camber % Camber Chord % CL Max CD Min
<< First < Prev 1 2 3 4 5 Next > Last >>
AG14 5.37 20.1855 2.326 26.9742 0.897 0.0068
AG18 5.87 20.705 2.158 42.7408 0.982 0.0064
AG12 6.23 20.8004 2.102 27.6418 0.878 0.0065
AG13 5.83 21.2982 2.209 28.1134 0.887 0.0074
AG04 6.42 21.8852 1.703 39.3636 0.931 0.0077
Coordinates
XUpper YUpper XLower YLower
0.0001 0.0099 0.0001 0.0099
0.0323 0.1647 0.0271 -0.1386
0.1202 0.3381 0.1281 -0.2806
0.2704 0.5389 0.3035 -0.4061
0.5109 0.7828 0.565 -0.5271
0.8995 1.0888 0.963 -0.6579
1.5128 1.4652 1.5964 -0.8033
2.3704 1.876 2.5442 -0.9472
3.4018 2.2662 3.7184 -1.0613
4.5367 2.6132 4.9858 -1.1373
5.7345 2.9157 6.2925 -1.1822
6.9741 3.1785 7.6214 -1.2038
8.2422 3.4067 8.9637 -1.208
9.5308 3.6048 10.3143 -1.1986
10.8351 3.7766 11.6711 -1.1785
12.1509 3.9255 13.0326 -1.1498
13.4757 4.0539 14.3975 -1.1143
14.8076 4.1641 15.765 -1.0734
16.1454 4.2577 17.1348 -1.028
17.4882 4.3362 18.5063 -0.9791
18.8351 4.4014 19.8792 -0.9274
20.1855 4.4543 21.2536 -0.8735
21.5388 4.4959 22.6289 -0.818
22.8948 4.5274 24.0052 -0.7614
24.2529 4.5494 25.3822 -0.7038
25.6127 4.5629 26.7597 -0.6459
26.9742 4.5683 28.1378 -0.5876
28.337 4.5663 29.5159 -0.5294
29.7009 4.5575 30.8937 -0.4713
31.066 4.5422 32.2711 -0.4137
32.432 4.5211 33.648 -0.3566
33.7988 4.4943 35.0246 -0.3002
35.1664 4.4624 36.4008 -0.2449
36.5347 4.4256 37.7766 -0.1905
37.9035 4.3843 39.152 -0.1375
39.2729 4.339 40.5271 -0.086
40.6427 4.2895 41.9018 -0.0361
42.013 4.2365 43.2762 0.012
43.3837 4.1799 44.6504 0.058
44.7546 4.1202 46.0245 0.1022
46.1257 4.0572 47.3985 0.1441
47.4972 3.9914 48.7723 0.1838
48.8687 3.9228 50.1461 0.2212
50.2405 3.8514 51.5198 0.2563
51.6123 3.7777 52.8935 0.2892
52.9844 3.7014 54.2672 0.3195
54.3565 3.6229 55.6409 0.3475
55.7286 3.542 57.0147 0.3731
57.1009 3.4592 58.3884 0.3962
58.4732 3.3741 59.7622 0.4169
59.8456 3.2872 61.136 0.4352
61.2179 3.1982 62.5099 0.4509
62.5903 3.1074 63.8837 0.4643
63.9628 3.0149 65.2577 0.4752
65.3352 2.9206 66.6317 0.4837
66.7077 2.8247 68.0057 0.4899
68.0802 2.7271 69.3798 0.4935
69.4527 2.628 70.7538 0.4949
70.8253 2.5274 72.128 0.4939
72.1979 2.4254 73.5021 0.4905
73.5706 2.3219 74.8762 0.4847
74.9432 2.2173 76.2503 0.4767
76.316 2.1112 77.6244 0.4662
77.6887 2.004 78.9983 0.4534
79.0615 1.8957 80.3722 0.4381
80.4341 1.7862 81.746 0.4205
81.8069 1.6757 83.1198 0.4003
83.1794 1.5641 84.4934 0.3776
84.5517 1.4514 85.8669 0.3525
85.924 1.3375 87.2403 0.3248
87.2957 1.2225 88.6136 0.2946
88.6671 1.1061 89.9868 0.2617
90.0374 0.9882 91.36 0.2264
91.4064 0.8684 92.7331 0.1884
92.7745 0.746 94.1061 0.1479
94.1417 0.6212 95.4791 0.1047
95.5059 0.4933 96.8507 0.0592
96.869 0.3612 98.2058 0.0121
98.2137 0.2278 99.4155 -0.0295
99.4163 0.1055 99.4163 -0.029
100 0.0478 100 -0.0478
X Y
1 0.000478
0.994163 0.001055
0.982137 0.002278
0.96869 0.003612
0.955059 0.004933
0.941417 0.006212
0.927745 0.00746
0.914064 0.008684
0.900374 0.009882
0.886671 0.011061
0.872957 0.012225
0.85924 0.013375
0.845517 0.014514
0.831794 0.015641
0.818069 0.016757
0.804341 0.017862
0.790615 0.018957
0.776887 0.02004
0.76316 0.021112
0.749432 0.022173
0.735706 0.023219
0.721979 0.024254
0.708253 0.025274
0.694527 0.02628
0.680802 0.027271
0.667077 0.028247
0.653352 0.029206
0.639628 0.030149
0.625903 0.031074
0.612179 0.031982
0.598456 0.032872
0.584732 0.033741
0.571009 0.034592
0.557286 0.03542
0.543565 0.036229
0.529844 0.037014
0.516123 0.037777
0.502405 0.038514
0.488687 0.039228
0.474972 0.039914
0.461257 0.040572
0.447546 0.041202
0.433837 0.041799
0.42013 0.042365
0.406427 0.042895
0.392729 0.04339
0.379035 0.043843
0.365347 0.044256
0.351664 0.044624
0.337988 0.044943
0.32432 0.045211
0.31066 0.045422
0.297009 0.045575
0.28337 0.045663
0.269742 0.045683
0.256127 0.045629
0.242529 0.045494
0.228948 0.045274
0.215388 0.044959
0.201855 0.044543
0.188351 0.044014
0.174882 0.043362
0.161454 0.042577
0.148076 0.041641
0.134757 0.040539
0.121509 0.039255
0.108351 0.037766
0.095308 0.036048
0.082422 0.034067
0.069741 0.031785
0.057345 0.029157
0.045367 0.026132
0.034018 0.022662
0.023704 0.01876
0.015128 0.014652
0.008995 0.010888
0.005109 0.007828
0.002704 0.005389
0.001202 0.003381
0.000323 0.001647
1E-06 9.9E-05
1E-06 9.9E-05
0.000271 -0.001386
0.001281 -0.002806
0.003035 -0.004061
0.00565 -0.005271
0.00963 -0.006579
0.015964 -0.008033
0.025442 -0.009472
0.037184 -0.010613
0.049858 -0.011373
0.062925 -0.011822
0.076214 -0.012038
0.089637 -0.01208
0.103143 -0.011986
0.116711 -0.011785
0.130326 -0.011498
0.143975 -0.011143
0.15765 -0.010734
0.171348 -0.01028
0.185063 -0.009791
0.198792 -0.009274
0.212536 -0.008735
0.226289 -0.00818
0.240052 -0.007614
0.253822 -0.007038
0.267597 -0.006459
0.281378 -0.005876
0.295159 -0.005294
0.308937 -0.004713
0.322711 -0.004137
0.33648 -0.003566
0.350246 -0.003002
0.364008 -0.002449
0.377766 -0.001905
0.39152 -0.001375
0.405271 -0.00086
0.419018 -0.000361
0.432762 0.00012
0.446504 0.00058
0.460245 0.001022
0.473985 0.001441
0.487723 0.001838
0.501461 0.002212
0.515198 0.002563
0.528935 0.002892
0.542672 0.003195
0.556409 0.003475
0.570147 0.003731
0.583884 0.003962
0.597622 0.004169
0.61136 0.004352
0.625099 0.004509
0.638837 0.004643
0.652577 0.004752
0.666317 0.004837
0.680057 0.004899
0.693798 0.004935
0.707538 0.004949
0.72128 0.004939
0.735021 0.004905
0.748762 0.004847
0.762503 0.004767
0.776244 0.004662
0.789983 0.004534
0.803722 0.004381
0.81746 0.004205
0.831198 0.004003
0.844934 0.003776
0.858669 0.003525
0.872403 0.003248
0.886136 0.002946
0.899868 0.002617
0.9136 0.002264
0.927331 0.001884
0.941061 0.001479
0.954791 0.001047
0.968507 0.000592
0.982058 0.000121
0.994155 -0.000295
0.994163 -0.00029
1 -0.000478
X Y
100 0.0478
99.4163 0.1055
98.2137 0.2278
96.869 0.3612
95.5059 0.4933
94.1417 0.6212
92.7745 0.746
91.4064 0.8684
90.0374 0.9882
88.6671 1.1061
87.2957 1.2225
85.924 1.3375
84.5517 1.4514
83.1794 1.5641
81.8069 1.6757
80.4341 1.7862
79.0615 1.8957
77.6887 2.004
76.316 2.1112
74.9432 2.2173
73.5706 2.3219
72.1979 2.4254
70.8253 2.5274
69.4527 2.628
68.0802 2.7271
66.7077 2.8247
65.3352 2.9206
63.9628 3.0149
62.5903 3.1074
61.2179 3.1982
59.8456 3.2872
58.4732 3.3741
57.1009 3.4592
55.7286 3.542
54.3565 3.6229
52.9844 3.7014
51.6123 3.7777
50.2405 3.8514
48.8687 3.9228
47.4972 3.9914
46.1257 4.0572
44.7546 4.1202
43.3837 4.1799
42.013 4.2365
40.6427 4.2895
39.2729 4.339
37.9035 4.3843
36.5347 4.4256
35.1664 4.4624
33.7988 4.4943
32.432 4.5211
31.066 4.5422
29.7009 4.5575
28.337 4.5663
26.9742 4.5683
25.6127 4.5629
24.2529 4.5494
22.8948 4.5274
21.5388 4.4959
20.1855 4.4543
18.8351 4.4014
17.4882 4.3362
16.1454 4.2577
14.8076 4.1641
13.4757 4.0539
12.1509 3.9255
10.8351 3.7766
9.5308 3.6048
8.2422 3.4067
6.9741 3.1785
5.7345 2.9157
4.5367 2.6132
3.4018 2.2662
2.3704 1.876
1.5128 1.4652
0.8995 1.0888
0.5109 0.7828
0.2704 0.5389
0.1202 0.3381
0.0323 0.1647
0.0001 0.0099
0.0001 0.0099
0.0271 -0.1386
0.1281 -0.2806
0.3035 -0.4061
0.565 -0.5271
0.963 -0.6579
1.5964 -0.8033
2.5442 -0.9472
3.7184 -1.0613
4.9858 -1.1373
6.2925 -1.1822
7.6214 -1.2038
8.9637 -1.208
10.3143 -1.1986
11.6711 -1.1785
13.0326 -1.1498
14.3975 -1.1143
15.765 -1.0734
17.1348 -1.028
18.5063 -0.9791
19.8792 -0.9274
21.2536 -0.8735
22.6289 -0.818
24.0052 -0.7614
25.3822 -0.7038
26.7597 -0.6459
28.1378 -0.5876
29.5159 -0.5294
30.8937 -0.4713
32.2711 -0.4137
33.648 -0.3566
35.0246 -0.3002
36.4008 -0.2449
37.7766 -0.1905
39.152 -0.1375
40.5271 -0.086
41.9018 -0.0361
43.2762 0.012
44.6504 0.058
46.0245 0.1022
47.3985 0.1441
48.7723 0.1838
50.1461 0.2212
51.5198 0.2563
52.8935 0.2892
54.2672 0.3195
55.6409 0.3475
57.0147 0.3731
58.3884 0.3962
59.7622 0.4169
61.136 0.4352
62.5099 0.4509
63.8837 0.4643
65.2577 0.4752
66.6317 0.4837
68.0057 0.4899
69.3798 0.4935
70.7538 0.4949
72.128 0.4939
73.5021 0.4905
74.8762 0.4847
76.2503 0.4767
77.6244 0.4662
78.9983 0.4534
80.3722 0.4381
81.746 0.4205
83.1198 0.4003
84.4934 0.3776
85.8669 0.3525
87.2403 0.3248
88.6136 0.2946
89.9868 0.2617
91.36 0.2264
92.7331 0.1884
94.1061 0.1479
95.4791 0.1047
96.8507 0.0592
98.2058 0.0121
99.4155 -0.0295
99.4163 -0.029
100 -0.0478
V 1.1