Winfoil Airfoils - Total Number: 277
| Name | T/C % | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|
| << First < Prev 48 49 50 51 52 Next > Last >> | |||||
| AG46c -03f | 6.03 | 1.717 | 30.3006 | 0.944 | 0.0067 |
| AG45ct -02f | 6.9 | 1.866 | 31.835 | 1.013 | 0.0075 |
| AG45c -03f | 6.93 | 2.04 | 30.3656 | 1.053 | 0.0077 |
| AG455ct -02f rot. | 6.47 | 1.846 | 31.8804 | 1.009 | 0.0078 |
| AG44ct -02f | 7.29 | 1.955 | 33.0081 | 1.039 | 0.0074 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0.0249 | -0.0173 | 0.0249 | -0.0173 |
| 0.032 | 0.1211 | 0.0568 | -0.1462 |
| 0.0806 | 0.2861 | 0.1444 | -0.2774 |
| 0.182 | 0.4794 | 0.3038 | -0.4026 |
| 0.3524 | 0.7058 | 0.5412 | -0.5244 |
| 0.6238 | 0.9784 | 0.8878 | -0.6518 |
| 1.0536 | 1.3142 | 1.4099 | -0.7911 |
| 1.7095 | 1.7148 | 2.1901 | -0.9375 |
| 2.6016 | 2.1433 | 3.2206 | -1.0701 |
| 3.6616 | 2.5498 | 4.4072 | -1.1717 |
| 4.8194 | 2.9114 | 5.6713 | -1.2409 |
| 6.036 | 3.2269 | 6.9722 | -1.2838 |
| 7.2916 | 3.501 | 8.2949 | -1.3064 |
| 8.5735 | 3.7402 | 9.6323 | -1.3136 |
| 9.8766 | 3.9502 | 10.9795 | -1.3086 |
| 11.1948 | 4.1349 | 12.3342 | -1.2938 |
| 12.5262 | 4.2979 | 13.6945 | -1.2713 |
| 13.8667 | 4.4413 | 15.0596 | -1.2425 |
| 15.2152 | 4.5673 | 16.4277 | -1.2085 |
| 16.5703 | 4.6775 | 17.7995 | -1.1702 |
| 17.93 | 4.7732 | 19.1733 | -1.1285 |
| 19.295 | 4.8556 | 20.5499 | -1.085 |
| 20.6629 | 4.9257 | 21.9297 | -1.0409 |
| 22.0339 | 4.9844 | 23.3118 | -0.9964 |
| 23.4078 | 5.0325 | 24.6958 | -0.9513 |
| 24.7831 | 5.0707 | 26.0828 | -0.9058 |
| 26.1605 | 5.0996 | 27.4725 | -0.8598 |
| 27.5398 | 5.1197 | 28.8648 | -0.8133 |
| 28.9197 | 5.1317 | 30.2596 | -0.7663 |
| 30.3006 | 5.1359 | 31.6566 | -0.719 |
| 31.683 | 5.1328 | 33.055 | -0.6713 |
| 33.0658 | 5.1229 | 34.4548 | -0.6232 |
| 34.4495 | 5.1065 | 35.856 | -0.5747 |
| 35.8341 | 5.0839 | 37.2579 | -0.526 |
| 37.2187 | 5.0554 | 38.6614 | -0.4769 |
| 38.6037 | 5.0215 | 40.0668 | -0.4276 |
| 39.9894 | 4.9821 | 41.4731 | -0.3779 |
| 41.3755 | 4.9376 | 42.8787 | -0.3281 |
| 42.761 | 4.888 | 44.2832 | -0.2781 |
| 44.147 | 4.8338 | 45.6863 | -0.228 |
| 45.5335 | 4.7748 | 47.0885 | -0.1778 |
| 46.9192 | 4.7116 | 48.4891 | -0.1275 |
| 48.3062 | 4.644 | 49.8881 | -0.0771 |
| 49.6939 | 4.5721 | 51.2865 | -0.0267 |
| 51.08 | 4.4961 | 52.6832 | 0.0238 |
| 52.4636 | 4.4165 | 54.0786 | 0.0743 |
| 53.8476 | 4.3329 | 54.8323 | 0.1016 |
| 54.6455 | 4.2829 | 55.7895 | 0.1363 |
| 55.5362 | 4.2259 | 56.8168 | 0.1736 |
| 56.6365 | 4.1533 | 58.157 | 0.2222 |
| 58.0199 | 4.0589 | 59.4962 | 0.2708 |
| 59.4041 | 3.961 | 60.1303 | 0.2937 |
| 61.0035 | 3.8435 | 60.8574 | 0.3201 |
| 62.1787 | 3.7546 | 62.2228 | 0.3696 |
| 63.5666 | 3.6467 | 63.5882 | 0.419 |
| 64.6148 | 3.563 | 64.583 | 0.455 |
| 65.1965 | 3.5167 | 65.0807 | 0.473 |
| 65.6278 | 3.4806 | 65.4978 | 0.488 |
| 66.3422 | 3.4217 | 66.3319 | 0.5181 |
| 67.73 | 3.3049 | 67.7052 | 0.5676 |
| 69.118 | 3.1853 | 69.0787 | 0.617 |
| 69.7919 | 3.1263 | 69.6952 | 0.6391 |
| 70.1288 | 3.0971 | 70.0094 | 0.6503 |
| 70.3136 | 3.0904 | 70.6384 | 0.6729 |
| 70.6832 | 3.0764 | 71.8717 | 0.717 |
| 71.789 | 3.0352 | 73.2647 | 0.7665 |
| 73.1816 | 2.9808 | 74.6569 | 0.816 |
| 74.5739 | 2.9242 | 76.0475 | 0.8651 |
| 75.9661 | 2.8653 | 77.4369 | 0.914 |
| 77.3584 | 2.8043 | 78.8242 | 0.9626 |
| 78.7506 | 2.7412 | 80.2105 | 1.0109 |
| 80.1427 | 2.6764 | 81.5966 | 1.0589 |
| 81.5353 | 2.6096 | 82.9827 | 1.106 |
| 82.9276 | 2.5411 | 84.369 | 1.1511 |
| 84.3198 | 2.4703 | 85.756 | 1.1951 |
| 85.7123 | 2.3982 | 87.143 | 1.237 |
| 87.1047 | 2.324 | 88.53 | 1.2774 |
| 88.4978 | 2.2482 | 89.9177 | 1.3149 |
| 89.8906 | 2.1707 | 91.3056 | 1.3502 |
| 91.2837 | 2.0917 | 92.6936 | 1.3831 |
| 92.6766 | 2.0115 | 94.082 | 1.4128 |
| 94.0696 | 1.9304 | 95.4706 | 1.4394 |
| 95.4624 | 1.8494 | 96.8568 | 1.463 |
| 96.8515 | 1.7692 | 98.2183 | 1.4824 |
| 98.2105 | 1.688 | 99.4205 | 1.4989 |
| 99.4142 | 1.6169 | 100.009 | 1.5054 |
| 100.009 | 1.5848 | 100.0151 | 1.5055 |
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