XFOIL Version 6.96 Calculated polar for: NACA 65(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 = 9.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -16.500 -0.8295 0.07759 0.07523 -0.0679 1.0000 0.0122 -16.250 -0.8556 0.06891 0.06636 -0.0735 1.0000 0.0122 -16.000 -0.8847 0.06080 0.05805 -0.0783 1.0000 0.0122 -15.750 -0.9015 0.05531 0.05243 -0.0812 1.0000 0.0123 -15.500 -0.9225 0.04981 0.04674 -0.0834 1.0000 0.0123 -15.250 -0.9270 0.04669 0.04354 -0.0844 1.0000 0.0125 -15.000 -0.9313 0.04374 0.04050 -0.0850 1.0000 0.0126 -14.750 -0.9308 0.04147 0.03815 -0.0854 1.0000 0.0127 -14.500 -0.9274 0.03959 0.03622 -0.0855 1.0000 0.0128 -14.250 -0.9244 0.03779 0.03436 -0.0853 1.0000 0.0130 -14.000 -0.9227 0.03592 0.03241 -0.0849 1.0000 0.0131 -13.750 -0.9191 0.03437 0.03079 -0.0843 1.0000 0.0133 -13.500 -0.9142 0.03309 0.02944 -0.0835 1.0000 0.0135 -13.250 -0.9126 0.03158 0.02784 -0.0823 1.0000 0.0137 -13.000 -0.9118 0.03019 0.02636 -0.0805 1.0000 0.0138 -12.750 -0.8997 0.02916 0.02527 -0.0803 0.9933 0.0142 -12.500 -0.8783 0.02742 0.02335 -0.0824 0.9846 0.0146 -12.250 -0.8509 0.02602 0.02180 -0.0852 0.9774 0.0149 -12.000 -0.8176 0.02508 0.02073 -0.0887 0.9710 0.0151 -11.750 -0.7934 0.02231 0.01776 -0.0912 0.9614 0.0158 -11.500 -0.7636 0.02143 0.01682 -0.0934 0.9485 0.0161 -11.250 -0.7430 0.02077 0.01605 -0.0935 0.9320 0.0164 -11.000 -0.7295 0.02026 0.01543 -0.0918 0.9162 0.0168 -10.750 -0.7173 0.01974 0.01479 -0.0898 0.9029 0.0171 -10.500 -0.7023 0.01921 0.01415 -0.0882 0.8922 0.0175 -10.250 -0.6847 0.01875 0.01359 -0.0870 0.8823 0.0179 -10.000 -0.6659 0.01836 0.01310 -0.0859 0.8735 0.0183 -9.750 -0.6462 0.01799 0.01263 -0.0849 0.8647 0.0186 -9.500 -0.6289 0.01675 0.01127 -0.0838 0.8569 0.0191 -9.250 -0.6102 0.01603 0.01049 -0.0828 0.8489 0.0196 -9.000 -0.5895 0.01558 0.01000 -0.0820 0.8420 0.0201 -8.750 -0.5679 0.01518 0.00955 -0.0813 0.8346 0.0205 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0.0518 -3.750 -0.0759 0.00844 0.00231 -0.0758 0.7253 0.1099 -3.500 -0.0516 0.00768 0.00199 -0.0759 0.7209 0.2371 -3.250 -0.0276 0.00667 0.00163 -0.0762 0.7169 0.4187 -3.000 -0.0004 0.00620 0.00153 -0.0766 0.7131 0.5244 -2.750 0.0282 0.00612 0.00150 -0.0769 0.7090 0.5573 -2.500 0.0569 0.00610 0.00148 -0.0772 0.7050 0.5778 -2.250 0.0859 0.00609 0.00147 -0.0775 0.7012 0.5907 -2.000 0.1149 0.00607 0.00147 -0.0779 0.6976 0.6065 -1.750 0.1438 0.00608 0.00151 -0.0781 0.6939 0.6253 -1.500 0.1726 0.00614 0.00156 -0.0784 0.6903 0.6420 -1.250 0.2016 0.00620 0.00158 -0.0787 0.6866 0.6505 -1.000 0.2307 0.00618 0.00159 -0.0790 0.6834 0.6548 -0.750 0.2599 0.00618 0.00158 -0.0794 0.6798 0.6582 -0.500 0.2890 0.00621 0.00158 -0.0798 0.6764 0.6616 -0.250 0.3181 0.00626 0.00158 -0.0801 0.6731 0.6648 0.000 0.3470 0.00626 0.00160 -0.0805 0.6698 0.6684 0.250 0.3761 0.00626 0.00162 -0.0808 0.6666 0.6717 0.500 0.4052 0.00627 0.00164 -0.0812 0.6633 0.6754 0.750 0.4342 0.00631 0.00166 -0.0816 0.6601 0.6789 1.000 0.4631 0.00637 0.00169 -0.0819 0.6567 0.6823 1.250 0.4920 0.00638 0.00174 -0.0822 0.6537 0.6859 1.500 0.5210 0.00639 0.00178 -0.0826 0.6505 0.6898 1.750 0.5499 0.00642 0.00183 -0.0829 0.6472 0.6937 2.000 0.5787 0.00648 0.00187 -0.0832 0.6430 0.6971 2.250 0.6070 0.00650 0.00192 -0.0835 0.6381 0.7011 2.500 0.6355 0.00650 0.00197 -0.0837 0.6329 0.7052 2.750 0.6637 0.00656 0.00201 -0.0839 0.6268 0.7095 3.000 0.6919 0.00659 0.00206 -0.0841 0.6190 0.7134 3.250 0.7190 0.00663 0.00210 -0.0840 0.6087 0.7178 3.500 0.7463 0.00666 0.00214 -0.0840 0.5957 0.7222 3.750 0.7736 0.00673 0.00220 -0.0840 0.5818 0.7267 4.000 0.8007 0.00682 0.00228 -0.0840 0.5672 0.7312 4.250 0.8273 0.00691 0.00238 -0.0839 0.5518 0.7361 4.500 0.8528 0.00707 0.00250 -0.0836 0.5306 0.7411 4.750 0.8766 0.00736 0.00266 -0.0830 0.4947 0.7459 5.000 0.8937 0.00799 0.00300 -0.0813 0.4222 0.7510 5.250 0.9045 0.00904 0.00360 -0.0786 0.3248 0.7567 5.500 0.9153 0.01007 0.00419 -0.0759 0.2375 0.7624 5.750 0.9259 0.01099 0.00477 -0.0732 0.1646 0.7685 6.000 0.9369 0.01184 0.00533 -0.0706 0.1060 0.7751 6.250 0.9493 0.01255 0.00586 -0.0682 0.0665 0.7813 6.500 0.9613 0.01312 0.00632 -0.0656 0.0440 0.7881 7.000 0.9909 0.01396 0.00716 -0.0613 0.0314 0.8022 7.250 1.0050 0.01446 0.00766 -0.0592 0.0281 0.8103 7.500 1.0210 0.01486 0.00813 -0.0574 0.0263 0.8183 8.000 1.0491 0.01591 0.00926 -0.0534 0.0226 0.8361 8.250 1.0637 0.01643 0.00986 -0.0516 0.0217 0.8455 8.500 1.0791 0.01692 0.01041 -0.0500 0.0208 0.8559 8.750 1.0931 0.01747 0.01103 -0.0482 0.0199 0.8671 9.000 1.1062 0.01807 0.01169 -0.0463 0.0193 0.8799 9.250 1.1151 0.01889 0.01259 -0.0438 0.0184 0.8958 9.500 1.1206 0.01986 0.01367 -0.0410 0.0179 0.9163 9.750 1.1313 0.02040 0.01433 -0.0387 0.0176 0.9451 10.000 1.1483 0.02115 0.01517 -0.0381 0.0172 1.0000 10.250 1.1627 0.02200 0.01605 -0.0371 0.0168 1.0000 10.500 1.1767 0.02288 0.01697 -0.0360 0.0162 1.0000 10.750 1.1893 0.02388 0.01800 -0.0348 0.0159 1.0000 11.000 1.2026 0.02483 0.01898 -0.0338 0.0155 1.0000 11.250 1.2137 0.02597 0.02015 -0.0326 0.0151 1.0000 11.500 1.2191 0.02757 0.02179 -0.0309 0.0146 1.0000 11.750 1.2224 0.02939 0.02369 -0.0292 0.0143 1.0000 12.000 1.2340 0.03059 0.02494 -0.0282 0.0142 1.0000 12.250 1.2472 0.03167 0.02608 -0.0275 0.0140 1.0000 12.500 1.2578 0.03299 0.02746 -0.0265 0.0138 1.0000 12.750 1.2675 0.03443 0.02896 -0.0256 0.0137 1.0000 13.000 1.2777 0.03585 0.03044 -0.0248 0.0134 1.0000 13.250 1.2868 0.03739 0.03204 -0.0240 0.0133 1.0000 13.500 1.2967 0.03889 0.03360 -0.0233 0.0130 1.0000 13.750 1.3055 0.04053 0.03531 -0.0226 0.0128 1.0000 14.000 1.3134 0.04230 0.03715 -0.0220 0.0126 1.0000 14.250 1.3224 0.04398 0.03888 -0.0215 0.0124 1.0000 14.500 1.3295 0.04589 0.04086 -0.0210 0.0123 1.0000 14.750 1.3372 0.04778 0.04281 -0.0206 0.0121 1.0000 15.000 1.3440 0.04981 0.04489 -0.0203 0.0120 1.0000 15.250 1.3488 0.05209 0.04724 -0.0200 0.0118 1.0000 15.500 1.3531 0.05448 0.04971 -0.0197 0.0117 1.0000 15.750 1.3516 0.05767 0.05302 -0.0192 0.0114 1.0000 16.000 1.3530 0.06060 0.05608 -0.0191 0.0112 1.0000 16.250 1.3559 0.06334 0.05892 -0.0193 0.0112 1.0000 16.500 1.3581 0.06625 0.06194 -0.0196 0.0111 1.0000 16.750 1.3592 0.06937 0.06518 -0.0200 0.0110 1.0000 17.000 1.3596 0.07266 0.06859 -0.0206 0.0110 1.0000 17.250 1.3589 0.07619 0.07224 -0.0215 0.0109 1.0000 17.500 1.3561 0.08010 0.07628 -0.0225 0.0108 1.0000 17.750 1.3519 0.08437 0.08068 -0.0237 0.0107 1.0000 18.000 1.3468 0.08889 0.08533 -0.0252 0.0106 1.0000 18.250 1.3400 0.09379 0.09038 -0.0270 0.0106 1.0000 18.500 1.3317 0.09905 0.09579 -0.0292 0.0105 1.0000 18.750 1.3213 0.10489 0.10177 -0.0319 0.0104 1.0000 19.000 1.3111 0.11087 0.10790 -0.0348 0.0104 1.0000 19.250 1.2971 0.11773 0.11493 -0.0384 0.0103 1.0000