XFOIL Version 6.96 Calculated polar for: NACA 23015 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -15.500 -0.9350 0.07554 0.07059 -0.0413 1.0000 0.0300 -15.250 -0.9674 0.06721 0.06199 -0.0462 1.0000 0.0302 -15.000 -0.9904 0.06092 0.05543 -0.0493 1.0000 0.0305 -14.750 -1.0102 0.05555 0.04977 -0.0513 1.0000 0.0310 -14.500 -1.0292 0.05067 0.04453 -0.0523 1.0000 0.0316 -14.250 -1.0357 0.04753 0.04119 -0.0522 1.0000 0.0321 -14.000 -1.0307 0.04587 0.03949 -0.0518 1.0000 0.0324 -13.750 -1.0265 0.04423 0.03779 -0.0512 1.0000 0.0328 -13.500 -1.0228 0.04259 0.03606 -0.0502 1.0000 0.0333 -13.250 -1.0197 0.04091 0.03426 -0.0490 1.0000 0.0339 -13.000 -1.0171 0.03919 0.03236 -0.0474 1.0000 0.0346 -12.750 -1.0155 0.03735 0.03027 -0.0453 1.0000 0.0356 -12.500 -1.0123 0.03568 0.02835 -0.0431 1.0000 0.0364 -12.250 -1.0021 0.03485 0.02753 -0.0412 1.0000 0.0370 -12.000 -0.9929 0.03408 0.02672 -0.0391 1.0000 0.0376 -11.750 -0.9837 0.03325 0.02581 -0.0367 1.0000 0.0383 -11.500 -0.9727 0.03228 0.02473 -0.0346 1.0000 0.0392 -11.250 -0.9612 0.03119 0.02344 -0.0325 1.0000 0.0404 -11.000 -0.9486 0.03014 0.02221 -0.0304 1.0000 0.0414 -10.750 -0.9333 0.02944 0.02154 -0.0287 1.0000 0.0421 -10.500 -0.9186 0.02879 0.02086 -0.0268 1.0000 0.0430 -10.250 -0.9040 0.02809 0.02010 -0.0248 1.0000 0.0440 -10.000 -0.8894 0.02736 0.01926 -0.0227 1.0000 0.0452 -9.750 -0.8749 0.02662 0.01835 -0.0205 1.0000 0.0464 -9.500 -0.8593 0.02586 0.01757 -0.0186 1.0000 0.0474 -9.250 -0.8438 0.02525 0.01698 -0.0166 1.0000 0.0483 -9.000 -0.8287 0.02468 0.01641 -0.0145 1.0000 0.0493 -8.750 -0.8135 0.02412 0.01580 -0.0123 1.0000 0.0505 -8.500 -0.7984 0.02356 0.01516 -0.0101 1.0000 0.0518 -8.250 -0.7831 0.02303 0.01453 -0.0079 1.0000 0.0529 -8.000 -0.7684 0.02238 0.01390 -0.0057 1.0000 0.0539 -7.750 -0.7383 0.02170 0.01326 -0.0066 0.9968 0.0553 -7.500 -0.7036 0.02106 0.01261 -0.0083 0.9930 0.0571 -7.250 -0.6705 0.02041 0.01192 -0.0096 0.9878 0.0587 -7.000 -0.6353 0.01982 0.01126 -0.0113 0.9834 0.0604 -6.750 -0.6036 0.01908 0.01059 -0.0125 0.9776 0.0622 -6.500 -0.5697 0.01850 0.01002 -0.0140 0.9721 0.0642 -6.250 -0.5360 0.01794 0.00945 -0.0154 0.9666 0.0662 -6.000 -0.5042 0.01747 0.00893 -0.0162 0.9590 0.0684 -5.750 -0.4734 0.01685 0.00836 -0.0170 0.9516 0.0709 -5.500 -0.4432 0.01638 0.00789 -0.0176 0.9426 0.0736 -5.250 -0.4135 0.01596 0.00744 -0.0179 0.9328 0.0765 -5.000 -0.3829 0.01548 0.00698 -0.0184 0.9233 0.0803 -4.750 -0.3556 0.01510 0.00660 -0.0182 0.9107 0.0851 -4.500 -0.3273 0.01470 0.00620 -0.0182 0.8984 0.0912 -4.250 -0.2989 0.01429 0.00582 -0.0181 0.8856 0.1018 -4.000 -0.2735 0.01380 0.00544 -0.0175 0.8703 0.1271 -3.750 -0.2537 0.01280 0.00495 -0.0163 0.8540 0.2315 -3.500 -0.2331 0.01205 0.00466 -0.0150 0.8373 0.3454 -3.250 -0.2099 0.01163 0.00447 -0.0139 0.8203 0.4109 -3.000 -0.1857 0.01134 0.00431 -0.0129 0.8032 0.4601 -2.750 -0.1610 0.01112 0.00418 -0.0119 0.7856 0.4999 -2.500 -0.1366 0.01093 0.00408 -0.0109 0.7675 0.5424 -2.250 -0.1124 0.01077 0.00400 -0.0097 0.7460 0.5840 -2.000 -0.0878 0.01068 0.00392 -0.0086 0.7219 0.6154 -1.750 -0.0628 0.01064 0.00384 -0.0076 0.6979 0.6437 -1.500 -0.0377 0.01059 0.00382 -0.0067 0.6756 0.6724 -1.250 -0.0124 0.01057 0.00381 -0.0057 0.6550 0.7015 -1.000 0.0132 0.01058 0.00381 -0.0049 0.6341 0.7270 -0.750 0.0392 0.01062 0.00381 -0.0041 0.6130 0.7486 -0.500 0.0654 0.01068 0.00381 -0.0034 0.5918 0.7667 -0.250 0.0918 0.01076 0.00382 -0.0028 0.5704 0.7835 0.000 0.1182 0.01086 0.00385 -0.0022 0.5494 0.7999 0.250 0.1448 0.01097 0.00389 -0.0016 0.5290 0.8161 0.500 0.1715 0.01110 0.00395 -0.0011 0.5085 0.8322 0.750 0.1984 0.01126 0.00403 -0.0006 0.4876 0.8473 1.000 0.2262 0.01143 0.00413 -0.0003 0.4671 0.8611 1.250 0.2542 0.01161 0.00423 -0.0001 0.4480 0.8743 1.500 0.2817 0.01180 0.00433 0.0002 0.4289 0.8876 1.750 0.3112 0.01203 0.00447 0.0001 0.4092 0.8989 2.000 0.3406 0.01226 0.00460 -0.0001 0.3898 0.9096 2.250 0.3683 0.01248 0.00473 0.0000 0.3720 0.9215 2.500 0.4014 0.01274 0.00491 -0.0010 0.3548 0.9290 2.750 0.4298 0.01297 0.00506 -0.0011 0.3395 0.9396 3.000 0.4642 0.01325 0.00525 -0.0024 0.3235 0.9459 3.250 0.4932 0.01352 0.00543 -0.0027 0.3095 0.9551 3.500 0.5290 0.01381 0.00563 -0.0045 0.2957 0.9600 3.750 0.5621 0.01406 0.00584 -0.0057 0.2844 0.9668 4.000 0.5971 0.01435 0.00606 -0.0073 0.2742 0.9717 4.250 0.6327 0.01462 0.00628 -0.0091 0.2642 0.9766 4.500 0.6657 0.01490 0.00652 -0.0104 0.2560 0.9824 4.750 0.7022 0.01517 0.00676 -0.0124 0.2481 0.9863 5.000 0.7365 0.01549 0.00703 -0.0141 0.2419 0.9911 5.250 0.7718 0.01575 0.00729 -0.0159 0.2355 0.9950 5.500 0.8069 0.01606 0.00757 -0.0177 0.2294 0.9989 5.750 0.8305 0.01636 0.00784 -0.0172 0.2249 1.0000 6.000 0.8498 0.01658 0.00809 -0.0157 0.2205 1.0000 6.250 0.8684 0.01684 0.00836 -0.0142 0.2160 1.0000 6.500 0.8862 0.01716 0.00864 -0.0125 0.2118 1.0000 6.750 0.9047 0.01746 0.00894 -0.0109 0.2079 1.0000 7.000 0.9239 0.01771 0.00925 -0.0094 0.2036 1.0000 7.250 0.9424 0.01801 0.00956 -0.0078 0.1995 1.0000 7.500 0.9601 0.01837 0.00989 -0.0061 0.1956 1.0000 7.750 0.9786 0.01871 0.01025 -0.0046 0.1917 1.0000 8.000 0.9978 0.01899 0.01060 -0.0031 0.1874 1.0000 8.250 1.0160 0.01931 0.01094 -0.0015 0.1830 1.0000 8.500 1.0331 0.01972 0.01131 0.0002 0.1791 1.0000 8.750 1.0521 0.02005 0.01172 0.0016 0.1750 1.0000 9.000 1.0709 0.02038 0.01212 0.0030 0.1705 1.0000 9.250 1.0885 0.02077 0.01252 0.0045 0.1662 1.0000 9.500 1.1060 0.02121 0.01297 0.0060 0.1621 1.0000 9.750 1.1249 0.02158 0.01343 0.0073 0.1573 1.0000 10.000 1.1418 0.02201 0.01390 0.0088 0.1528 1.0000 10.250 1.1575 0.02250 0.01441 0.0104 0.1486 1.0000 10.500 1.1744 0.02294 0.01494 0.0119 0.1437 1.0000 10.750 1.1878 0.02345 0.01549 0.0139 0.1390 1.0000 11.000 1.2009 0.02403 0.01611 0.0158 0.1347 1.0000 11.250 1.2155 0.02461 0.01678 0.0173 0.1296 1.0000 11.500 1.2271 0.02534 0.01752 0.0191 0.1250 1.0000 11.750 1.2405 0.02607 0.01834 0.0205 0.1202 1.0000 12.000 1.2520 0.02692 0.01924 0.0220 0.1152 1.0000 12.250 1.2620 0.02791 0.02027 0.0235 0.1106 1.0000 12.500 1.2725 0.02895 0.02138 0.0247 0.1057 1.0000 13.000 1.2883 0.03154 0.02409 0.0270 0.0974 1.0000 13.250 1.2942 0.03310 0.02571 0.0280 0.0937 1.0000 13.500 1.2979 0.03493 0.02759 0.0287 0.0907 1.0000 13.750 1.3032 0.03674 0.02951 0.0293 0.0875 1.0000 14.000 1.3054 0.03892 0.03176 0.0296 0.0846 1.0000 14.250 1.3042 0.04153 0.03442 0.0296 0.0823 1.0000 14.500 1.3057 0.04402 0.03702 0.0295 0.0799 1.0000 14.750 1.3050 0.04683 0.03995 0.0292 0.0777 1.0000 15.000 1.3015 0.05005 0.04326 0.0285 0.0758 1.0000 15.250 1.2953 0.05371 0.04699 0.0276 0.0742 1.0000 15.500 1.2887 0.05750 0.05087 0.0265 0.0728 1.0000 15.750 1.2839 0.06122 0.05474 0.0253 0.0712 1.0000 16.000 1.2770 0.06532 0.05896 0.0239 0.0698 1.0000 16.250 1.2684 0.06973 0.06348 0.0223 0.0686 1.0000 16.500 1.2587 0.07441 0.06825 0.0205 0.0674 1.0000 16.750 1.2485 0.07920 0.07311 0.0185 0.0663 1.0000 17.000 1.2392 0.08386 0.07781 0.0167 0.0653 1.0000 17.250 1.2299 0.08877 0.08288 0.0146 0.0642 1.0000 17.500 1.2202 0.09380 0.08804 0.0124 0.0631 1.0000 17.750 1.2103 0.09890 0.09326 0.0102 0.0620 1.0000