OAF117 AIRFOIL 51. 51. 0.000000 0.000000 0.000987 0.006616 0.003943 0.012913 0.008856 0.018950 0.015708 0.024804 0.024472 0.030536 0.035112 0.036169 0.047586 0.041672 0.061847 0.046965 0.077836 0.051945 0.095492 0.056512 0.114743 0.060602 0.135516 0.064196 0.157726 0.067297 0.181288 0.069895 0.206107 0.071928 0.232087 0.073288 0.259123 0.073940 0.287110 0.074182 0.315938 0.073751 0.345492 0.072779 0.375655 0.071298 0.406309 0.069353 0.437333 0.066999 0.468605 0.064296 0.500000 0.061305 0.531395 0.058087 0.562667 0.054700 0.593691 0.051198 0.624345 0.047628 0.654508 0.044033 0.684062 0.040451 0.712890 0.036917 0.740877 0.033462 0.767913 0.030118 0.793893 0.026911 0.818712 0.023871 0.842274 0.021022 0.864484 0.018387 0.885257 0.015986 0.904508 0.013832 0.922164 0.011933 0.938153 0.010292 0.952414 0.008902 0.964888 0.007753 0.975528 0.006829 0.984292 0.006111 0.991144 0.005578 0.996057 0.005213 0.999013 0.005001 1.000000 0.004931 0.000000 0.000000 0.000987 -0.005216 0.003943 -0.010416 0.008856 -0.015442 0.015708 -0.020121 0.024472 -0.024348 0.035112 -0.028121 0.047586 -0.031504 0.061847 -0.034547 0.077836 -0.037201 0.095492 -0.039332 0.114743 -0.040848 0.135516 -0.041856 0.157726 -0.042549 0.181288 -0.042503 0.206107 -0.042177 0.232087 -0.041389 0.259123 -0.040161 0.287110 -0.038533 0.315938 -0.036557 0.345492 -0.034297 0.375655 -0.031821 0.406309 -0.029199 0.437333 -0.026500 0.468605 -0.023787 0.500000 -0.021117 0.531395 -0.018537 0.562667 -0.016086 0.593691 -0.013791 0.624345 -0.011674 0.654508 -0.009749 0.684062 -0.008023 0.712890 -0.006502 0.740877 -0.005189 0.767913 -0.004083 0.793893 -0.003184 0.818712 -0.002492 0.842274 -0.002001 0.864484 -0.001706 0.885257 -0.001597 0.904508 -0.001657 0.922164 -0.001865 0.938153 -0.002196 0.952414 -0.002617 0.964888 -0.003092 0.975528 -0.003583 0.984292 -0.004050 0.991144 -0.004458 0.996057 -0.004774 0.999013 -0.004974 1.000000 -0.005042