XFOIL Version 6.96 Calculated polar for: NACA 64(2)-415 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.500 -0.9114 0.12058 0.11809 -0.0342 1.0000 0.0107 -19.250 -0.9623 0.10698 0.10431 -0.0416 1.0000 0.0106 -19.000 -1.0042 0.09538 0.09253 -0.0480 1.0000 0.0106 -18.750 -1.0358 0.08597 0.08297 -0.0533 1.0000 0.0106 -18.500 -1.0593 0.07827 0.07512 -0.0576 1.0000 0.0106 -18.250 -1.0749 0.07205 0.06877 -0.0611 1.0000 0.0107 -18.000 -1.0920 0.06590 0.06249 -0.0645 1.0000 0.0106 -17.750 -1.1042 0.06081 0.05729 -0.0672 1.0000 0.0108 -17.500 -1.1140 0.05622 0.05260 -0.0694 1.0000 0.0109 -17.250 -1.1203 0.05230 0.04858 -0.0713 1.0000 0.0110 -17.000 -1.1231 0.04896 0.04515 -0.0727 1.0000 0.0111 -16.750 -1.1245 0.04595 0.04206 -0.0738 1.0000 0.0112 -16.500 -1.1235 0.04334 0.03937 -0.0746 1.0000 0.0114 -16.250 -1.1220 0.04085 0.03680 -0.0753 1.0000 0.0115 -16.000 -1.1188 0.03860 0.03449 -0.0758 1.0000 0.0116 -15.750 -1.1141 0.03657 0.03238 -0.0762 1.0000 0.0117 -15.500 -1.1084 0.03468 0.03043 -0.0764 1.0000 0.0119 -15.250 -1.1015 0.03297 0.02865 -0.0764 1.0000 0.0120 -15.000 -1.0939 0.03136 0.02697 -0.0764 1.0000 0.0122 -14.750 -1.0860 0.02984 0.02539 -0.0762 1.0000 0.0124 -14.500 -1.0780 0.02839 0.02386 -0.0758 1.0000 0.0125 -14.250 -1.0692 0.02706 0.02247 -0.0754 1.0000 0.0127 -14.000 -1.0595 0.02586 0.02121 -0.0748 1.0000 0.0129 -13.750 -1.0493 0.02477 0.02006 -0.0741 1.0000 0.0130 -13.500 -1.0374 0.02388 0.01911 -0.0732 1.0000 0.0132 -13.250 -1.0294 0.02280 0.01797 -0.0720 1.0000 0.0134 -13.000 -1.0171 0.02165 0.01677 -0.0716 0.9867 0.0136 -12.750 -0.9806 0.02055 0.01562 -0.0756 0.9733 0.0140 -12.500 -0.9401 0.01957 0.01457 -0.0802 0.9586 0.0143 -12.250 -0.9050 0.01875 0.01367 -0.0833 0.9372 0.0147 -12.000 -0.8865 0.01814 0.01292 -0.0830 0.9119 0.0149 -11.750 -0.8768 0.01760 0.01226 -0.0808 0.8909 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0.00124 -0.0765 0.6036 0.5083 -1.500 0.1695 0.00649 0.00125 -0.0768 0.5986 0.5313 -1.250 0.1985 0.00650 0.00125 -0.0771 0.5942 0.5427 -1.000 0.2278 0.00649 0.00125 -0.0774 0.5900 0.5485 -0.750 0.2570 0.00651 0.00125 -0.0777 0.5855 0.5542 -0.500 0.2861 0.00653 0.00125 -0.0779 0.5811 0.5588 -0.250 0.3152 0.00655 0.00126 -0.0782 0.5773 0.5628 0.000 0.3444 0.00656 0.00128 -0.0785 0.5736 0.5667 0.250 0.3736 0.00659 0.00130 -0.0788 0.5694 0.5706 0.500 0.4025 0.00663 0.00132 -0.0791 0.5652 0.5743 0.750 0.4315 0.00666 0.00135 -0.0794 0.5614 0.5789 1.000 0.4607 0.00667 0.00139 -0.0797 0.5580 0.5837 1.250 0.4898 0.00671 0.00143 -0.0799 0.5539 0.5882 1.500 0.5185 0.00676 0.00148 -0.0802 0.5492 0.5923 1.750 0.5473 0.00680 0.00153 -0.0804 0.5445 0.5971 2.000 0.5763 0.00683 0.00158 -0.0807 0.5397 0.6020 2.250 0.6051 0.00689 0.00164 -0.0809 0.5348 0.6067 2.500 0.6335 0.00695 0.00171 -0.0811 0.5291 0.6115 2.750 0.6621 0.00700 0.00178 -0.0813 0.5199 0.6170 3.000 0.6902 0.00709 0.00185 -0.0814 0.5094 0.6222 3.250 0.7178 0.00721 0.00194 -0.0815 0.4952 0.6273 3.500 0.7452 0.00734 0.00204 -0.0815 0.4775 0.6334 3.750 0.7725 0.00749 0.00215 -0.0815 0.4596 0.6395 4.000 0.7983 0.00774 0.00230 -0.0813 0.4266 0.6455 4.250 0.8190 0.00842 0.00264 -0.0803 0.3522 0.6519 4.500 0.8412 0.00898 0.00298 -0.0796 0.3022 0.6578 4.750 0.8630 0.00955 0.00335 -0.0788 0.2520 0.6638 5.000 0.8841 0.01016 0.00375 -0.0779 0.2033 0.6703 5.500 0.9273 0.01123 0.00449 -0.0763 0.1294 0.6830 5.750 0.9480 0.01179 0.00490 -0.0753 0.0973 0.6899 6.000 0.9692 0.01228 0.00529 -0.0744 0.0734 0.6962 6.250 0.9908 0.01272 0.00565 -0.0736 0.0565 0.7034 6.750 1.0350 0.01346 0.00635 -0.0721 0.0392 0.7179 7.000 1.0571 0.01380 0.00669 -0.0713 0.0345 0.7260 7.250 1.0787 0.01414 0.00705 -0.0704 0.0310 0.7337 7.500 1.1000 0.01448 0.00741 -0.0695 0.0284 0.7418 7.750 1.1203 0.01484 0.00779 -0.0685 0.0262 0.7493 8.000 1.1401 0.01517 0.00816 -0.0673 0.0247 0.7576 8.250 1.1566 0.01554 0.00856 -0.0655 0.0231 0.7656 8.500 1.1724 0.01594 0.00900 -0.0637 0.0218 0.7749 8.750 1.1887 0.01633 0.00944 -0.0620 0.0207 0.7847 9.250 1.2180 0.01730 0.01050 -0.0583 0.0182 0.8064 9.500 1.2331 0.01780 0.01106 -0.0567 0.0174 0.8176 9.750 1.2473 0.01835 0.01167 -0.0550 0.0162 0.8304 10.000 1.2606 0.01897 0.01234 -0.0533 0.0155 0.8445 10.250 1.2730 0.01963 0.01308 -0.0515 0.0147 0.8601 10.500 1.2853 0.02029 0.01384 -0.0497 0.0141 0.8800 10.750 1.2956 0.02096 0.01462 -0.0476 0.0137 0.9093 11.000 1.3063 0.02164 0.01543 -0.0457 0.0131 1.0000 11.250 1.3191 0.02255 0.01636 -0.0445 0.0127 1.0000 11.500 1.3306 0.02358 0.01743 -0.0432 0.0121 1.0000 11.750 1.3427 0.02461 0.01849 -0.0421 0.0118 1.0000 12.000 1.3548 0.02567 0.01959 -0.0411 0.0116 1.0000 12.250 1.3664 0.02678 0.02075 -0.0401 0.0113 1.0000 12.500 1.3774 0.02798 0.02200 -0.0391 0.0111 1.0000 12.750 1.3882 0.02923 0.02330 -0.0381 0.0109 1.0000 13.000 1.3983 0.03056 0.02467 -0.0373 0.0107 1.0000 13.250 1.4079 0.03197 0.02613 -0.0364 0.0105 1.0000 13.500 1.4169 0.03346 0.02766 -0.0356 0.0104 1.0000 13.750 1.4252 0.03504 0.02929 -0.0349 0.0102 1.0000 14.000 1.4330 0.03671 0.03101 -0.0342 0.0100 1.0000 14.250 1.4395 0.03855 0.03290 -0.0336 0.0098 1.0000 14.500 1.4448 0.04054 0.03497 -0.0330 0.0096 1.0000 14.750 1.4493 0.04269 0.03718 -0.0325 0.0095 1.0000 15.000 1.4564 0.04464 0.03919 -0.0322 0.0095 1.0000 15.250 1.4626 0.04671 0.04133 -0.0320 0.0094 1.0000 15.500 1.4679 0.04893 0.04363 -0.0318 0.0094 1.0000 15.750 1.4726 0.05129 0.04606 -0.0317 0.0093 1.0000 16.000 1.4773 0.05369 0.04854 -0.0318 0.0092 1.0000 16.250 1.4816 0.05621 0.05114 -0.0319 0.0091 1.0000 16.500 1.4846 0.05894 0.05395 -0.0322 0.0091 1.0000 16.750 1.4878 0.06171 0.05680 -0.0325 0.0090 1.0000 17.000 1.4911 0.06451 0.05968 -0.0329 0.0089 1.0000 17.250 1.4928 0.06760 0.06286 -0.0335 0.0088 1.0000 17.500 1.4935 0.07089 0.06622 -0.0343 0.0087 1.0000 17.750 1.4929 0.07441 0.06984 -0.0351 0.0086 1.0000 18.000 1.4930 0.07792 0.07344 -0.0361 0.0085 1.0000 18.250 1.4916 0.08173 0.07733 -0.0372 0.0085 1.0000 18.500 1.4892 0.08578 0.08148 -0.0386 0.0084 1.0000 18.750 1.4866 0.08991 0.08572 -0.0401 0.0084 1.0000 19.000 1.4828 0.09433 0.09023 -0.0417 0.0083 1.0000 19.250 1.4779 0.09902 0.09503 -0.0437 0.0083 1.0000