Udo Rumpf 15.3 Airfoil (Modified)

 

Tab delimited coordinates file.

Udo15.3 (2000 Version)
X Axis Y (Top) Y (Bottom)
0 0 0
0.000987 0.004757 -0.001331
0.003943 0.010743 -0.003741
0.008856 0.017932 -0.006111
0.015708 0.025339 -0.008082
0.024472 0.033005 -0.01025
0.035112 0.040825 -0.012339
0.047586 0.048516 -0.014347
0.061847 0.05633 -0.016334
0.077836 0.06407 -0.018195
0.095492 0.071608 -0.019985
0.114743 0.078926 -0.021607
0.135516 0.08599 -0.02309
0.157726 0.092661 -0.024447
0.181288 0.098816 -0.025581
0.206107 0.104402 -0.026574
0.232087 0.109367 -0.027447
0.259123 0.113573 -0.028098
0.28711 0.117095 -0.028597
0.315938 0.12003 -0.028961
0.345492 0.122214 -0.029024
0.375655 0.123623 -0.02893
0.406309 0.124291 -0.028709
0.437333 0.124207 -0.028207
0.468605 0.123346 -0.027605
0.5 0.12162 -0.026705
0.531395 0.118933 -0.025709
0.562667 0.115371 -0.02442
0.593691 0.111166 -0.023022
0.624345 0.106272 -0.021451
0.654509 0.100197 -0.019568
0.684062 0.092364 -0.017575
0.71289 0.08333 -0.015237
0.740877 0.073708 -0.012648
0.767913 0.063888 -0.009918
0.793893 0.054069 -0.007295
0.818712 0.04525 -0.004853
0.842274 0.037777 -0.002783
0.864484 0.031391 -0.001171
0.885257 0.025983 0.000099
0.904509 0.021298 0.001012
0.922164 0.017197 0.00155
0.938153 0.01361 0.001765
0.952414 0.010489 0.001764
0.964888 0.007806 0.001595
0.975528 0.005522 0.001262
0.984292 0.003638 0.000864
0.991144 0.002164 0.000545
0.996057 0.00101 0.000302
0.999013 0.000252 0.000088
1 0 0