NACA 66,2-(1.8)12 A=.6 P-51 TIP AIRFOIL 49.0 49.0 0.000000 0.000000 0.001859 0.006812 0.004112 0.009583 0.006512 0.011638 0.008943 0.013306 0.011393 0.014734 0.018795 0.018227 0.023749 0.020217 0.048596 0.028646 0.073528 0.035398 0.098509 0.041094 0.123521 0.046061 0.148558 0.050417 0.173613 0.054241 0.198683 0.057614 0.223765 0.060595 0.248857 0.063218 0.273958 0.065507 0.299067 0.067478 0.324183 0.069148 0.349305 0.070531 0.374432 0.071632 0.399566 0.072452 0.424704 0.072998 0.449848 0.073258 0.474998 0.073235 0.500154 0.072920 0.525318 0.072297 0.550494 0.071343 0.575689 0.070027 0.600951 0.068244 0.626185 0.065839 0.651298 0.062766 0.676347 0.059107 0.701348 0.055022 0.726309 0.050640 0.751239 0.046002 0.776140 0.041128 0.801018 0.036064 0.825880 0.030891 0.850731 0.025693 0.875577 0.020538 0.900424 0.015492 0.925280 0.010663 0.950152 0.006221 0.975052 0.002442 0.985023 0.001227 0.990012 0.000715 1.000000 0.000000 0.000000 0.000000 0.003141 -0.006166 0.005888 -0.008416 0.008488 -0.009997 0.011057 -0.011222 0.013607 -0.012230 0.021205 -0.014561 0.026251 -0.015837 0.051404 -0.021157 0.076472 -0.025298 0.101491 -0.028721 0.126479 -0.031672 0.151442 -0.034228 0.176387 -0.036436 0.201317 -0.038359 0.226235 -0.040042 0.251143 -0.041506 0.276042 -0.042768 0.300933 -0.043840 0.325817 -0.044733 0.350695 -0.045457 0.375568 -0.046017 0.400434 -0.046414 0.425296 -0.046652 0.450152 -0.046726 0.475002 -0.046638 0.499846 -0.046386 0.524682 -0.045961 0.549506 -0.045352 0.574311 -0.044546 0.599049 -0.043476 0.623815 -0.042061 0.648702 -0.040170 0.673653 -0.037840 0.698652 -0.035198 0.723691 -0.032354 0.748761 -0.029328 0.773860 -0.026125 0.798982 -0.022776 0.824120 -0.019344 0.849269 -0.015901 0.874423 -0.012499 0.899576 -0.009187 0.924720 -0.006055 0.949848 -0.003252 0.974948 -0.001024 0.984977 -0.000398 0.989988 -0.000170 1.000000 0.000000