NACA64 airfoil - Clark Y external flap with an aspect ratio of 17. Original Cl, Cd, and Cm get from CFD using Fluent, created by Xiao Sun 3-18-3015 Cl and Cd values corrected for rotational stall delay and Cd values corrected using the Viterna method for 0 to 90deg AOA using AirfoilPrep 3 Number of airfoil tables in this file -5.0 0.0 5.0 Table ID parameter 11.4 11.9 12.4 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 0.0 -1.2394 -3.2023 -5.3040 7.4890 7.8301 7.8602 1.6455 2.0640 2.4287 -0.5318 -0.3739 -0.1029 -0.5800 -2.7500 -3.2900 0.0094 0.0088 0.0088 -180.00 0.0000 0.3298 0.0000 0.0000 0.1427 0.0000 0.0000 0.4135 0.0000 -170.00 0.3330 0.3746 0.4000 0.3880 0.1903 0.4000 0.4560 0.4570 0.4000 -160.00 0.6670 0.5029 0.2291 0.7770 0.3271 0.3885 0.9120 0.5816 0.4316 -150.00 0.8350 0.6981 0.2946 0.9520 0.5361 0.4323 1.0940 0.7706 0.4951 -140.00 0.7730 0.9344 0.3208 0.8430 0.7911 0.4249 0.9300 0.9985 0.4936 -130.00 0.6890 1.1803 0.3569 0.7310 1.0600 0.4433 0.7820 1.2341 0.5130 -120.00 0.5650 1.4024 0.3920 0.5870 1.3089 0.4684 0.6140 1.4442 0.5373 -110.00 0.3990 1.5698 0.4183 0.4090 1.5058 0.4888 0.4210 1.5984 0.5563 -100.00 0.2040 1.6575 0.4297 0.2070 1.6250 0.4968 0.2100 1.6720 0.5626 -90.00 0.0000 1.6500 0.4227 0.0000 1.6500 0.4873 0.0000 1.6500 0.5514 -80.00 -0.2040 1.6575 0.4246 -0.2070 1.6250 0.4710 -0.2100 1.6720 0.5567 -70.00 -0.3990 1.5698 0.4079 -0.4090 1.5058 0.4383 -0.4210 1.5984 0.5444 -60.00 -0.5650 1.4024 0.3768 -0.5870 1.3089 0.3948 -0.6140 1.4442 0.5195 -50.00 -0.6890 1.1803 0.3370 -0.7310 1.0600 0.3473 -0.7820 1.2341 0.4889 -40.00 -0.7730 0.9344 0.2958 -0.8430 0.7911 0.3021 -0.9300 0.9985 0.4615 -30.00 -0.8350 0.6981 0.2619 -0.9520 0.5361 0.2635 -1.0940 0.7706 0.4493 -20.00 -0.7670 0.4326 0.2062 -0.8190 0.3146 0.1867 -0.8600 0.4849 0.3559 -10.00 -0.6000 0.1311 0.1330 -0.5020 0.0967 0.0733 -0.3190 0.1452 0.2047 -6.00 -0.5340 0.0105 0.0076 -0.3750 0.0096 -0.0505 -0.1020 0.0093 -0.1323 -5.46 -0.4870 0.0104 0.0082 -0.3040 0.0094 -0.0552 -0.0270 0.0091 -0.1372 -4.92 -0.4390 0.0103 0.0086 -0.2320 0.0093 -0.0600 0.0490 0.0090 -0.1421 -4.37 -0.3880 0.0102 0.0084 -0.1600 0.0091 -0.0647 0.1250 0.0089 -0.1469 -3.83 -0.3330 0.0100 0.0072 -0.0870 0.0090 -0.0694 0.2010 0.0088 -0.1517 -3.29 -0.2740 0.0099 0.0050 -0.0130 0.0089 -0.0740 0.2760 0.0088 -0.1564 -2.75 -0.2100 0.0098 0.0020 0.0610 0.0088 -0.0787 0.3520 0.0089 -0.1610 -2.20 -0.1430 0.0097 -0.0017 0.1360 0.0088 -0.0832 0.4270 0.0090 -0.1656 -1.66 -0.0730 0.0096 -0.0058 0.2100 0.0089 -0.0878 0.5020 0.0092 -0.1701 -1.12 -0.0010 0.0095 -0.0101 0.2850 0.0089 -0.0923 0.5770 0.0093 -0.1746 -0.58 0.0720 0.0094 -0.0146 0.3600 0.0090 -0.0968 0.6520 0.0095 -0.1790 -0.03 0.1460 0.0095 -0.0192 0.4340 0.0092 -0.1012 0.7270 0.0098 -0.1834 0.51 0.2200 0.0096 -0.0238 0.5090 0.0094 -0.1057 0.8010 0.0101 -0.1877 1.05 0.2940 0.0096 -0.0284 0.5830 0.0096 -0.1101 0.8750 0.0104 -0.1920 1.59 0.3680 0.0098 -0.0331 0.6570 0.0099 -0.1146 0.9490 0.0108 -0.1963 2.14 0.4420 0.0100 -0.0377 0.7310 0.0102 -0.1190 1.0230 0.0112 -0.2006 2.68 0.5160 0.0103 -0.0423 0.8050 0.0106 -0.1235 1.0960 0.0117 -0.2049 3.22 0.5900 0.0106 -0.0470 0.8790 0.0110 -0.1280 1.1700 0.0122 -0.2092 3.76 0.6640 0.0109 -0.0517 0.9530 0.0114 -0.1325 1.2430 0.0128 -0.2136 4.31 0.7370 0.0113 -0.0565 1.0260 0.0119 -0.1371 1.3170 0.0134 -0.2181 4.85 0.8110 0.0117 -0.0614 1.1000 0.0125 -0.1418 1.3900 0.0141 -0.2226 5.39 0.8850 0.0121 -0.0663 1.1730 0.0131 -0.1466 1.4640 0.0148 -0.2272 5.93 0.9590 0.0126 -0.0713 1.2460 0.0138 -0.1515 1.5380 0.0156 -0.2319 6.47 1.0350 0.0132 -0.0764 1.3190 0.0146 -0.1566 1.6110 0.0164 -0.2367 7.02 1.1120 0.0138 -0.0819 1.3930 0.0155 -0.1619 1.6850 0.0173 -0.2416 7.56 1.1920 0.0144 -0.0879 1.4680 0.0163 -0.1673 1.7580 0.0184 -0.2466 8.10 1.2730 0.0150 -0.0948 1.5460 0.0171 -0.1729 1.8320 0.0196 -0.2516 8.64 1.3550 0.0157 -0.1026 1.6260 0.0177 -0.1786 1.9060 0.0210 -0.2568 9.19 1.4340 0.0174 -0.1110 1.7050 0.0185 -0.1837 1.9810 0.0224 -0.2622 9.73 1.5020 0.0206 -0.1195 1.7780 0.0194 -0.1878 2.0580 0.0238 -0.2678 10.27 1.5550 0.0262 -0.1275 1.8400 0.0206 -0.1902 2.1360 0.0250 -0.2739 10.81 1.5900 0.0343 -0.1342 1.8890 0.0233 -0.1924 2.2110 0.0263 -0.2806 11.36 1.6070 0.0446 -0.1379 1.9200 0.0299 -0.1976 2.2730 0.0282 -0.2883 11.90 1.6060 0.0566 -0.1371 1.9300 0.0428 -0.2092 2.3100 0.0315 -0.2972 12.44 1.5880 0.0699 -0.1306 1.9160 0.0638 -0.2296 2.3140 0.0364 -0.3074 12.98 1.5580 0.0831 -0.1202 1.8830 0.0905 -0.2549 2.2880 0.0438 -0.3172 13.53 1.5220 0.0943 -0.1086 1.8350 0.1187 -0.2788 2.2360 0.0541 -0.3241 14.07 1.4860 0.1018 -0.0989 1.7820 0.1444 -0.2945 2.1670 0.0681 -0.3255 14.61 1.4540 0.1048 -0.0934 1.7280 0.1643 -0.2985 2.0860 0.0857 -0.3203 15.15 1.4270 0.1052 -0.0932 1.6770 0.1785 -0.2948 2.0050 0.1053 -0.3111 15.69 1.4020 0.1056 -0.0992 1.6340 0.1871 -0.2889 1.9340 0.1249 -0.3012 16.24 1.3790 0.1082 -0.1123 1.6000 0.1907 -0.2860 1.8820 0.1428 -0.2940 16.78 1.3590 0.1144 -0.1310 1.5760 0.1904 -0.2874 1.8520 0.1587 -0.2922 17.32 1.3430 0.1242 -0.1515 1.5600 0.1886 -0.2899 1.8360 0.1753 -0.2985 17.86 1.3350 0.1374 -0.1696 1.5490 0.1874 -0.2898 1.8270 0.1945 -0.3150 18.41 1.3340 0.1542 -0.1817 1.5380 0.1890 -0.2844 1.8170 0.2185 -0.3437 18.95 1.3390 0.1757 -0.1884 1.5300 0.1937 -0.2775 1.8050 0.2461 -0.3800 19.49 1.3410 0.2032 -0.1923 1.5240 0.2008 -0.2765 1.7900 0.2742 -0.4165 20.03 1.3340 0.2385 -0.1961 1.5230 0.2097 -0.2888 1.7750 0.2999 -0.4456 20.58 1.3130 0.2813 -0.2018 1.5280 0.2207 -0.3184 1.7590 0.3219 -0.4618 21.12 1.2870 0.3259 -0.2089 1.5340 0.2371 -0.3590 1.7440 0.3430 -0.4661 21.66 1.2620 0.3651 -0.2165 1.5400 0.2625 -0.4021 1.7310 0.3676 -0.4610 22.20 1.2500 0.3921 -0.2236 1.5400 0.3007 -0.4391 1.7190 0.3997 -0.4489 22.75 1.2510 0.4064 -0.2303 1.5340 0.3498 -0.4641 1.7090 0.4401 -0.4341 23.29 1.2590 0.4167 -0.2383 1.5220 0.4001 -0.4751 1.7020 0.4854 -0.4231 23.83 1.2670 0.4323 -0.2493 1.5080 0.4412 -0.4701 1.6970 0.5316 -0.4224 24.37 1.2690 0.4614 -0.2647 1.4920 0.4638 -0.4478 1.6940 0.5749 -0.4381 24.92 1.2630 0.5044 -0.2843 1.4760 0.4679 -0.4106 1.6930 0.6148 -0.4693 25.46 1.2520 0.5567 -0.3067 1.4590 0.4598 -0.3634 1.6920 0.6524 -0.5109 26.00 1.2380 0.6135 -0.3306 1.4420 0.4454 -0.3113 1.6930 0.6887 -0.5577 30.00 1.1930 0.6981 -0.3346 1.3590 0.5361 -0.3245 1.5630 0.7706 -0.5438 40.00 1.1040 0.9344 -0.3565 1.2050 0.7911 -0.3566 1.3290 0.9985 -0.5343 50.00 0.9840 1.1803 -0.3831 1.0440 1.0600 -0.3901 1.1180 1.2341 -0.5410 60.00 0.8070 1.4024 -0.4064 0.8390 1.3089 -0.4230 0.8780 1.4442 -0.5517 70.00 0.5700 1.5698 -0.4223 0.5840 1.5058 -0.4523 0.6010 1.5984 -0.5596 80.00 0.2920 1.6575 -0.4283 0.2950 1.6250 -0.4748 0.2990 1.6720 -0.5606 90.00 0.0000 1.6500 -0.4227 0.0000 1.6500 -0.4873 0.0000 1.6500 -0.5514 100.00 -0.2040 1.6575 -0.4297 -0.2070 1.6250 -0.4968 -0.2100 1.6720 -0.5626 110.00 -0.3990 1.5698 -0.4183 -0.4090 1.5058 -0.4888 -0.4210 1.5984 -0.5563 120.00 -0.5650 1.4024 -0.3920 -0.5870 1.3089 -0.4684 -0.6140 1.4442 -0.5373 130.00 -0.6890 1.1803 -0.3569 -0.7310 1.0600 -0.4433 -0.7820 1.2341 -0.5130 140.00 -0.7730 0.9344 -0.3208 -0.8430 0.7911 -0.4249 -0.9300 0.9985 -0.4936 150.00 -0.8350 0.6981 -0.2946 -0.9520 0.5361 -0.4323 -1.0940 0.7706 -0.4951 160.00 -0.6670 0.5029 -0.2291 -0.7770 0.3271 -0.3885 -0.9120 0.5816 -0.4316 170.00 -0.3330 0.3746 -0.5000 -0.3880 0.1903 -0.5000 -0.4560 0.4570 -0.5000 180.00 0.0000 0.3298 0.0000 0.0000 0.1427 0.0000 0.0000 0.4135 0.0000