XFOIL Version 6.96 Calculated polar for: NLF(1)-0115 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -12.750 -0.6252 0.06378 0.06090 -0.0713 1.0000 0.0101 -12.500 -0.6617 0.05729 0.05422 -0.0726 1.0000 0.0101 -12.250 -0.6912 0.05266 0.04943 -0.0718 1.0000 0.0101 -12.000 -0.7103 0.04829 0.04486 -0.0721 0.9990 0.0101 -11.750 -0.7214 0.04359 0.03987 -0.0739 0.9957 0.0101 -11.500 -0.7260 0.03994 0.03596 -0.0747 0.9919 0.0101 -11.250 -0.7246 0.03689 0.03264 -0.0753 0.9879 0.0101 -11.000 -0.7190 0.03377 0.02926 -0.0761 0.9846 0.0102 -10.750 -0.7108 0.03169 0.02698 -0.0756 0.9796 0.0103 -10.500 -0.6945 0.03004 0.02519 -0.0759 0.9754 0.0105 -10.250 -0.6742 0.02787 0.02277 -0.0768 0.9726 0.0105 -10.000 -0.6607 0.02660 0.02136 -0.0755 0.9653 0.0107 -9.750 -0.6373 0.02542 0.02004 -0.0760 0.9607 0.0108 -9.500 -0.6202 0.02451 0.01903 -0.0749 0.9526 0.0111 -9.000 -0.5787 0.02229 0.01654 -0.0739 0.9352 0.0115 -8.750 -0.5557 0.02118 0.01528 -0.0736 0.9240 0.0117 -8.500 -0.5297 0.02009 0.01403 -0.0738 0.9101 0.0119 -8.250 -0.5021 0.01907 0.01285 -0.0742 0.8926 0.0121 -8.000 -0.4759 0.01821 0.01181 -0.0743 0.8719 0.0123 -7.750 -0.4531 0.01751 0.01094 -0.0736 0.8506 0.0125 -7.500 -0.4321 0.01694 0.01021 -0.0726 0.8313 0.0127 -7.250 -0.4118 0.01641 0.00955 -0.0714 0.8151 0.0128 -7.000 -0.3915 0.01597 0.00898 -0.0703 0.8012 0.0130 -6.750 -0.3712 0.01556 0.00846 -0.0691 0.7895 0.0132 -6.500 -0.3537 0.01490 0.00774 -0.0675 0.7788 0.0135 -6.250 -0.3345 0.01442 0.00720 -0.0662 0.7697 0.0138 -6.000 -0.3146 0.01403 0.00675 -0.0650 0.7612 0.0141 -5.750 -0.2937 0.01366 0.00635 -0.0640 0.7537 0.0145 -5.500 -0.2724 0.01333 0.00596 -0.0629 0.7466 0.0149 -5.250 -0.2504 0.01303 0.00561 -0.0620 0.7403 0.0155 -5.000 -0.2280 0.01275 0.00528 -0.0612 0.7338 0.0161 -4.500 -0.1828 0.01217 0.00460 -0.0596 0.7229 0.0173 -4.250 -0.1596 0.01189 0.00430 -0.0588 0.7179 0.0180 -4.000 -0.1358 0.01168 0.00403 -0.0582 0.7135 0.0190 -3.750 -0.1112 0.01148 0.00380 -0.0577 0.7094 0.0203 -3.500 -0.0864 0.01128 0.00358 -0.0573 0.7053 0.0219 -3.250 -0.0618 0.01107 0.00338 -0.0568 0.7013 0.0264 -3.000 -0.0380 0.01082 0.00319 -0.0562 0.6977 0.0459 -2.750 -0.0146 0.01049 0.00300 -0.0556 0.6941 0.0840 -2.500 0.0068 0.00999 0.00279 -0.0548 0.6904 0.1631 -2.250 0.0064 0.00788 0.00227 -0.0507 0.6868 0.5883 -2.000 0.0333 0.00797 0.00238 -0.0504 0.6839 0.6297 -1.750 0.0608 0.00808 0.00246 -0.0502 0.6812 0.6476 -1.500 0.0881 0.00826 0.00265 -0.0500 0.6786 0.6664 -1.250 0.1157 0.00838 0.00276 -0.0498 0.6757 0.6774 -1.000 0.1438 0.00844 0.00280 -0.0498 0.6726 0.6824 -0.750 0.1722 0.00845 0.00276 -0.0500 0.6698 0.6837 -0.500 0.2007 0.00846 0.00272 -0.0502 0.6674 0.6846 -0.250 0.2293 0.00849 0.00269 -0.0504 0.6652 0.6854 0.000 0.2578 0.00849 0.00267 -0.0507 0.6627 0.6863 0.250 0.2859 0.00849 0.00265 -0.0508 0.6587 0.6872 0.500 0.3132 0.00851 0.00261 -0.0507 0.6515 0.6883 0.750 0.3401 0.00852 0.00258 -0.0506 0.6424 0.6892 1.000 0.3668 0.00855 0.00253 -0.0504 0.6332 0.6900 1.250 0.3935 0.00853 0.00252 -0.0502 0.6232 0.6908 1.500 0.4203 0.00856 0.00251 -0.0501 0.6151 0.6916 1.750 0.4475 0.00857 0.00253 -0.0500 0.6075 0.6924 2.000 0.4744 0.00861 0.00254 -0.0499 0.6010 0.6933 2.250 0.5017 0.00863 0.00258 -0.0498 0.5930 0.6942 2.500 0.5281 0.00868 0.00260 -0.0496 0.5844 0.6951 2.750 0.5548 0.00871 0.00264 -0.0495 0.5743 0.6961 3.000 0.5807 0.00877 0.00269 -0.0491 0.5607 0.6972 3.250 0.6050 0.00886 0.00272 -0.0485 0.5401 0.6983 3.500 0.6273 0.00903 0.00278 -0.0475 0.5071 0.6996 3.750 0.6421 0.00950 0.00294 -0.0451 0.4422 0.7010 4.000 0.6562 0.01009 0.00324 -0.0427 0.3808 0.7024 4.250 0.6728 0.01060 0.00353 -0.0408 0.3336 0.7036 4.500 0.6913 0.01101 0.00378 -0.0393 0.2992 0.7048 4.750 0.7103 0.01138 0.00403 -0.0378 0.2718 0.7059 5.000 0.7293 0.01171 0.00427 -0.0364 0.2483 0.7071 5.250 0.7485 0.01203 0.00451 -0.0350 0.2285 0.7083 5.500 0.7678 0.01230 0.00474 -0.0335 0.2138 0.7097 5.750 0.7857 0.01257 0.00497 -0.0319 0.2006 0.7111 6.000 0.8040 0.01283 0.00520 -0.0303 0.1887 0.7126 6.250 0.8223 0.01310 0.00545 -0.0287 0.1782 0.7142 6.500 0.8404 0.01341 0.00573 -0.0271 0.1695 0.7158 6.750 0.8594 0.01370 0.00602 -0.0257 0.1615 0.7175 7.000 0.8775 0.01403 0.00633 -0.0242 0.1540 0.7192 7.250 0.8962 0.01435 0.00665 -0.0228 0.1467 0.7210 7.500 0.9137 0.01469 0.00699 -0.0213 0.1405 0.7228 7.750 0.9323 0.01499 0.00734 -0.0199 0.1349 0.7249 8.000 0.9493 0.01537 0.00772 -0.0184 0.1291 0.7272 8.250 0.9672 0.01572 0.00810 -0.0170 0.1241 0.7296 8.500 0.9847 0.01610 0.00850 -0.0156 0.1192 0.7320 8.750 1.0007 0.01655 0.00895 -0.0140 0.1144 0.7345 9.000 1.0185 0.01694 0.00938 -0.0127 0.1104 0.7370 9.250 1.0350 0.01736 0.00985 -0.0112 0.1062 0.7396 9.500 1.0504 0.01786 0.01036 -0.0097 0.1023 0.7426 9.750 1.0664 0.01833 0.01090 -0.0083 0.0989 0.7460 10.000 1.0828 0.01881 0.01143 -0.0070 0.0952 0.7497 10.500 1.1116 0.02000 0.01267 -0.0040 0.0878 0.7576 10.750 1.1275 0.02052 0.01329 -0.0028 0.0849 0.7627 11.000 1.1422 0.02114 0.01396 -0.0015 0.0818 0.7681 11.250 1.1557 0.02182 0.01469 -0.0001 0.0788 0.7740 11.500 1.1684 0.02258 0.01551 0.0013 0.0758 0.7815 11.750 1.1831 0.02321 0.01624 0.0025 0.0729 0.7902 12.250 1.2072 0.02480 0.01798 0.0052 0.0662 0.8169 12.500 1.2192 0.02555 0.01887 0.0066 0.0636 0.8403 12.750 1.2390 0.02629 0.01987 0.0063 0.0593 0.9131 13.000 1.2622 0.02744 0.02107 0.0046 0.0556 1.0000 13.250 1.2749 0.02842 0.02210 0.0055 0.0533 1.0000 13.500 1.2868 0.02949 0.02322 0.0063 0.0504 1.0000 13.750 1.2973 0.03068 0.02444 0.0072 0.0480 1.0000 14.000 1.3073 0.03192 0.02571 0.0080 0.0455 1.0000 14.250 1.3179 0.03315 0.02699 0.0088 0.0429 1.0000 14.500 1.3275 0.03448 0.02836 0.0095 0.0409 1.0000 14.750 1.3350 0.03602 0.02992 0.0103 0.0381 1.0000 15.000 1.3442 0.03744 0.03141 0.0109 0.0360 1.0000 15.250 1.3521 0.03899 0.03303 0.0115 0.0342 1.0000 15.500 1.3580 0.04076 0.03483 0.0121 0.0321 1.0000 15.750 1.3648 0.04249 0.03663 0.0125 0.0304 1.0000 16.000 1.3706 0.04435 0.03856 0.0129 0.0283 1.0000 16.250 1.3751 0.04638 0.04065 0.0133 0.0267 1.0000 16.500 1.3785 0.04858 0.04291 0.0135 0.0252 1.0000 16.750 1.3820 0.05082 0.04522 0.0137 0.0232 1.0000 17.000 1.3826 0.05344 0.04790 0.0137 0.0212 1.0000 17.250 1.3837 0.05606 0.05062 0.0136 0.0200 1.0000 17.500 1.3825 0.05904 0.05367 0.0133 0.0179 1.0000 17.750 1.3791 0.06237 0.05708 0.0129 0.0163 1.0000 18.000 1.3760 0.06580 0.06061 0.0122 0.0148 1.0000 18.250 1.3683 0.06994 0.06482 0.0112 0.0131 1.0000 18.500 1.3620 0.07403 0.06903 0.0100 0.0121 1.0000 18.750 1.3506 0.07904 0.07415 0.0083 0.0109 1.0000 19.000 1.3390 0.08431 0.07954 0.0063 0.0102 1.0000 19.250 1.3265 0.08988 0.08524 0.0040 0.0097 1.0000