Winfoil Airfoils - Total Number: 277
| Name | T/C % | Camber % | Camber Chord % | CL Max | CD Min |
|---|---|---|---|---|---|
| << First < Prev 5 6 7 8 9 Next > Last >> | |||||
| AG45ct -02f | 6.9 | 1.866 | 31.835 | 1.013 | 0.0075 |
| AG46c -03f | 6.03 | 1.717 | 30.3006 | 0.944 | 0.0067 |
| AG46ct -02f rot. | 6.08 | 1.704 | 31.7373 | 0.982 | 0.0076 |
| AG47c -03f | 5.06 | 1.365 | 32.0337 | 0.851 | 0.0064 |
| AG47ct -02f rot. | 4.99 | 1.326 | 32.0736 | 0.867 | 0.0075 |
Coordinates
| XUpper | YUpper | XLower | YLower |
|---|---|---|---|
| 0.0012 | -0.0341 | 0.0012 | -0.0341 |
| 0.0108 | 0.1102 | 0.0323 | -0.1724 |
| 0.0641 | 0.2824 | 0.12 | -0.3122 |
| 0.1719 | 0.4837 | 0.2797 | -0.4458 |
| 0.3508 | 0.7194 | 0.5165 | -0.5785 |
| 0.6324 | 1.0038 | 0.8624 | -0.7213 |
| 1.0753 | 1.3553 | 1.3835 | -0.8829 |
| 1.7464 | 1.7772 | 2.1627 | -1.0619 |
| 2.6537 | 2.2321 | 3.1916 | -1.2345 |
| 3.7266 | 2.6672 | 4.3766 | -1.3786 |
| 4.8949 | 3.0569 | 5.6391 | -1.4905 |
| 6.1195 | 3.3986 | 6.9386 | -1.5756 |
| 7.382 | 3.6962 | 8.2602 | -1.6393 |
| 8.6695 | 3.9554 | 9.5968 | -1.6868 |
| 9.9775 | 4.1815 | 10.9435 | -1.72 |
| 11.3001 | 4.378 | 12.2981 | -1.7412 |
| 12.6354 | 4.5491 | 13.6584 | -1.7525 |
| 13.9793 | 4.6967 | 15.0238 | -1.7559 |
| 15.3309 | 4.8233 | 16.3923 | -1.7527 |
| 16.6888 | 4.9307 | 17.7645 | -1.7443 |
| 18.0507 | 5.0204 | 19.139 | -1.7314 |
| 19.4176 | 5.0937 | 20.5156 | -1.7148 |
| 20.7871 | 5.152 | 21.8951 | -1.6951 |
| 22.1593 | 5.1963 | 23.2789 | -1.6727 |
| 23.5341 | 5.2278 | 24.6662 | -1.6479 |
| 24.9109 | 5.2477 | 26.0584 | -1.6211 |
| 26.2911 | 5.2567 | 27.4554 | -1.5926 |
| 27.6746 | 5.256 | 28.857 | -1.5627 |
| 29.0601 | 5.2459 | 30.2626 | -1.5315 |
| 30.4472 | 5.2274 | 31.6706 | -1.499 |
| 31.835 | 5.2011 | 33.08 | -1.4657 |
| 33.2237 | 5.1674 | 34.4916 | -1.4315 |
| 34.6152 | 5.1266 | 35.9042 | -1.3965 |
| 36.0112 | 5.0788 | 37.3168 | -1.361 |
| 37.4125 | 5.0243 | 38.731 | -1.3247 |
| 38.8199 | 4.9631 | 40.1465 | -1.2878 |
| 40.2335 | 4.8957 | 41.5627 | -1.2504 |
| 41.6527 | 4.8221 | 42.9771 | -1.2126 |
| 43.0752 | 4.7427 | 44.3898 | -1.1743 |
| 44.4998 | 4.658 | 45.8005 | -1.1357 |
| 45.9248 | 4.5684 | 47.2101 | -1.0967 |
| 47.3459 | 4.4743 | 48.6182 | -1.0574 |
| 48.7635 | 4.3762 | 50.0232 | -1.0178 |
| 50.1782 | 4.274 | 51.4274 | -0.9778 |
| 51.5878 | 4.1683 | 52.8296 | -0.9379 |
| 52.9917 | 4.059 | 54.2309 | -0.8976 |
| 54.3968 | 3.9459 | 54.9868 | -0.8761 |
| 55.2085 | 3.8789 | 55.9467 | -0.8487 |
| 56.1159 | 3.8028 | 56.9774 | -0.8195 |
| 57.2386 | 3.7063 | 58.3198 | -0.7814 |
| 58.6534 | 3.5819 | 59.6337 | -0.7448 |
| 60.0711 | 3.4541 | 61.0185 | -0.7068 |
| 61.2612 | 3.3445 | 62.3741 | -0.6703 |
| 62.9239 | 3.1878 | 63.7286 | -0.6344 |
| 64.3558 | 3.05 | 64.6835 | -0.6099 |
| 65.4607 | 2.9418 | 65.5828 | -0.5869 |
| 66.519 | 2.8368 | 66.4399 | -0.5656 |
| 67.2246 | 2.7662 | 67.8037 | -0.5317 |
| 68.6613 | 2.6207 | 69.1677 | -0.4993 |
| 69.7239 | 2.5118 | 69.7217 | -0.4864 |
| 70.2553 | 2.4571 | 69.9989 | -0.4799 |
| 70.7082 | 2.4251 | 70.2621 | -0.4742 |
| 71.0626 | 2.4002 | 70.6923 | -0.4644 |
| 71.6793 | 2.3568 | 71.9461 | -0.4368 |
| 72.7245 | 2.2823 | 73.3337 | -0.407 |
| 74.0701 | 2.1854 | 74.7215 | -0.3781 |
| 75.4139 | 2.0871 | 76.1077 | -0.3501 |
| 76.757 | 1.9874 | 77.494 | -0.3231 |
| 78.1009 | 1.8863 | 78.8815 | -0.2969 |
| 79.4449 | 1.7838 | 80.2688 | -0.2719 |
| 80.7898 | 1.6797 | 81.6585 | -0.2478 |
| 82.1351 | 1.5742 | 83.0472 | -0.2249 |
| 83.4812 | 1.4671 | 84.4343 | -0.203 |
| 84.8292 | 1.3586 | 85.8214 | -0.1824 |
| 86.1775 | 1.2483 | 87.2063 | -0.1626 |
| 87.5271 | 1.1366 | 88.5892 | -0.1441 |
| 88.8763 | 1.0232 | 89.9731 | -0.1266 |
| 90.2251 | 0.9085 | 91.3535 | -0.1102 |
| 91.5742 | 0.7922 | 92.7344 | -0.0948 |
| 92.9204 | 0.6747 | 94.1134 | -0.0804 |
| 94.2645 | 0.5557 | 95.491 | -0.0674 |
| 95.6049 | 0.4355 | 96.8662 | -0.0551 |
| 96.9434 | 0.3139 | 98.2162 | -0.0441 |
| 98.2595 | 0.1929 | 99.4091 | -0.0353 |
| 99.4227 | 0.0847 | 99.4227 | -0.0352 |
| 100 | 0.0311 | 100 | -0.0311 |
V 1.0