Drela AG03 (flat aft bottom) airfoil
ag03 Airfoil (x,y) Co-ordinates
| 1 | 0.000662 |
| 0.994875 | 0.00121 |
| 0.984975 | 0.002247 |
| 0.973308 | 0.003426 |
| 0.960939 | 0.004647 |
| 0.94837 | 0.005887 |
| 0.935754 | 0.00714 |
| 0.923123 | 0.008397 |
| 0.910487 | 0.009656 |
| 0.897855 | 0.010913 |
| 0.88523 | 0.012166 |
| 0.872612 | 0.013411 |
| 0.86 | 0.014647 |
| 0.847391 | 0.015874 |
| 0.834786 | 0.017089 |
| 0.822181 | 0.018292 |
| 0.809577 | 0.019483 |
| 0.796974 | 0.02066 |
| 0.784368 | 0.021824 |
| 0.771761 | 0.022975 |
| 0.759154 | 0.024113 |
| 0.746543 | 0.025238 |
| 0.733929 | 0.02635 |
| 0.721314 | 0.027451 |
| 0.708699 | 0.028539 |
| 0.696083 | 0.029615 |
| 0.683469 | 0.030677 |
| 0.670857 | 0.031725 |
| 0.658247 | 0.032758 |
| 0.645638 | 0.033774 |
| 0.633032 | 0.034775 |
| 0.620429 | 0.035756 |
| 0.607827 | 0.03672 |
| 0.595228 | 0.037664 |
| 0.582632 | 0.038586 |
| 0.570039 | 0.039488 |
| 0.557449 | 0.040365 |
| 0.544862 | 0.041218 |
| 0.532277 | 0.042044 |
| 0.519696 | 0.042844 |
| 0.507117 | 0.043615 |
| 0.494542 | 0.044357 |
| 0.48197 | 0.04507 |
| 0.469399 | 0.045748 |
| 0.456832 | 0.046394 |
| 0.444268 | 0.047005 |
| 0.431705 | 0.047581 |
| 0.419146 | 0.048121 |
| 0.40659 | 0.048623 |
| 0.394038 | 0.049085 |
| 0.381491 | 0.049506 |
| 0.368949 | 0.049886 |
| 0.356413 | 0.050221 |
| 0.343886 | 0.050509 |
| 0.331366 | 0.050751 |
| 0.318857 | 0.05094 |
| 0.306358 | 0.051075 |
| 0.293873 | 0.051154 |
| 0.281401 | 0.051173 |
| 0.268946 | 0.051128 |
| 0.256511 | 0.051015 |
| 0.244096 | 0.05083 |
| 0.231706 | 0.050567 |
| 0.219345 | 0.050221 |
| 0.207014 | 0.049788 |
| 0.194722 | 0.049257 |
| 0.182473 | 0.048624 |
| 0.170275 | 0.047879 |
| 0.158135 | 0.047014 |
| 0.146065 | 0.046016 |
| 0.134077 | 0.044875 |
| 0.122188 | 0.043576 |
| 0.110415 | 0.042107 |
| 0.098787 | 0.040447 |
| 0.087333 | 0.038582 |
| 0.076099 | 0.03649 |
| 0.065141 | 0.034148 |
| 0.054543 | 0.031546 |
| 0.044438 | 0.028679 |
| 0.035054 | 0.02558 |
| 0.026726 | 0.022341 |
| 0.019796 | 0.019132 |
| 0.014399 | 0.016153 |
| 0.010376 | 0.013518 |
| 0.00741 | 0.011228 |
| 0.005217 | 0.009239 |
| 0.003584 | 0.007497 |
| 0.002364 | 0.005957 |
| 0.001461 | 0.004586 |
| 0.000804 | 0.003348 |
| 0.000336 | 0.002171 |
| 0.000057 | 0.001038 |
| 0.000003 | -0.000144 |
| 0.000295 | -0.001237 |
| 0.001304 | -0.002345 |
| 0.002832 | -0.003392 |
| 0.005146 | -0.00455 |
| 0.008148 | -0.0057 |
| 0.012068 | -0.006869 |
| 0.017309 | -0.008078 |
| 0.024142 | -0.009278 |
| 0.032772 | -0.010396 |
| 0.042956 | -0.011344 |
| 0.05378 | -0.012046 |
| 0.065071 | -0.012544 |
| 0.076714 | -0.01288 |
| 0.0886 | -0.013076 |
| 0.100661 | -0.013162 |
| 0.112851 | -0.013163 |
| 0.125133 | -0.013101 |
| 0.137483 | -0.012991 |
| 0.149888 | -0.012852 |
| 0.162339 | -0.012699 |
| 0.174831 | -0.012533 |
| 0.187362 | -0.012358 |
| 0.199929 | -0.012175 |
| 0.212527 | -0.011993 |
| 0.225155 | -0.011809 |
| 0.237803 | -0.011625 |
| 0.250473 | -0.011441 |
| 0.263159 | -0.011256 |
| 0.275856 | -0.011072 |
| 0.28856 | -0.010887 |
| 0.301265 | -0.010703 |
| 0.313969 | -0.010518 |
| 0.326666 | -0.010333 |
| 0.339358 | -0.010149 |
| 0.352044 | -0.009965 |
| 0.364727 | -0.00978 |
| 0.377405 | -0.009596 |
| 0.390079 | -0.009412 |
| 0.40275 | -0.009228 |
| 0.415417 | -0.009043 |
| 0.428079 | -0.00886 |
| 0.440739 | -0.008676 |
| 0.453397 | -0.008492 |
| 0.466057 | -0.008308 |
| 0.478721 | -0.008123 |
| 0.49139 | -0.00794 |
| 0.50406 | -0.007755 |
| 0.516731 | -0.007571 |
| 0.5294 | -0.007387 |
| 0.542065 | -0.007204 |
| 0.554732 | -0.007019 |
| 0.567398 | -0.006835 |
| 0.580063 | -0.006651 |
| 0.592727 | -0.006467 |
| 0.605391 | -0.006283 |
| 0.618056 | -0.006099 |
| 0.630721 | -0.005915 |
| 0.643385 | -0.00573 |
| 0.656047 | -0.005547 |
| 0.668712 | -0.005363 |
| 0.681376 | -0.005179 |
| 0.694041 | -0.004994 |
| 0.706707 | -0.00481 |
| 0.719375 | -0.004627 |
| 0.732044 | -0.004442 |
| 0.744714 | -0.004258 |
| 0.757385 | -0.004074 |
| 0.770058 | -0.00389 |
| 0.782733 | -0.003706 |
| 0.795412 | -0.003522 |
| 0.808092 | -0.003337 |
| 0.820775 | -0.003154 |
| 0.833464 | -0.002968 |
| 0.846158 | -0.002784 |
| 0.858858 | -0.002599 |
| 0.871564 | -0.002415 |
| 0.884274 | -0.00223 |
| 0.89698 | -0.002045 |
| 0.909681 | -0.00186 |
| 0.922381 | -0.001677 |
| 0.935082 | -0.001492 |
| 0.947777 | -0.001308 |
| 0.960437 | -0.001123 |
| 0.972932 | -0.000942 |
| 0.984788 | -0.000769 |
| 0.994831 | -0.000624 |
| 1 | -0.000548 |
ag03 Airfoil CAD files