XFOIL Version 6.96 Calculated polar for: NACA 23024 1 1 Reynolds number fixed Mach number fixed xtrf = 1.000 (top) 1.000 (bottom) Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000 alpha CL CD CDp CM Top_Xtr Bot_Xtr ------ -------- --------- --------- -------- -------- -------- -19.500 -0.7868 0.11309 0.10534 -0.0606 1.0000 0.1124 -19.250 -0.8322 0.10310 0.09506 -0.0648 1.0000 0.1160 -19.000 -0.8255 0.10130 0.09330 -0.0648 1.0000 0.1182 -18.750 -0.8231 0.09889 0.09090 -0.0651 1.0000 0.1208 -18.500 -0.8373 0.09401 0.08591 -0.0666 1.0000 0.1240 -18.250 -0.8487 0.08967 0.08146 -0.0676 1.0000 0.1271 -18.000 -0.8428 0.08789 0.07975 -0.0675 1.0000 0.1299 -17.750 -0.8490 0.08439 0.07619 -0.0681 1.0000 0.1332 -17.500 -0.8623 0.08001 0.07167 -0.0689 1.0000 0.1369 -17.250 -0.8569 0.07830 0.07004 -0.0686 1.0000 0.1400 -17.000 -0.8620 0.07519 0.06689 -0.0687 1.0000 0.1437 -16.750 -0.8729 0.07141 0.06298 -0.0690 1.0000 0.1479 -16.500 -0.8697 0.06954 0.06119 -0.0685 1.0000 0.1514 -16.250 -0.8757 0.06659 0.05819 -0.0684 1.0000 0.1557 -16.000 -0.8825 0.06361 0.05514 -0.0680 1.0000 0.1601 -15.750 -0.8828 0.06153 0.05312 -0.0673 1.0000 0.1641 -15.500 -0.8904 0.05870 0.05021 -0.0667 1.0000 0.1691 -15.250 -0.8940 0.05640 0.04790 -0.0658 1.0000 0.1736 -15.000 -0.8973 0.05428 0.04579 -0.0647 1.0000 0.1783 -14.750 -0.9046 0.05182 0.04323 -0.0635 1.0000 0.1836 -14.500 -0.9071 0.05000 0.04147 -0.0619 1.0000 0.1883 -14.250 -0.9125 0.04803 0.03948 -0.0602 1.0000 0.1937 -14.000 -0.9184 0.04609 0.03747 -0.0583 1.0000 0.1990 -13.750 -0.9213 0.04461 0.03605 -0.0561 1.0000 0.2039 -13.500 -0.9274 0.04296 0.03435 -0.0537 1.0000 0.2095 -13.250 -0.9330 0.04150 0.03288 -0.0510 1.0000 0.2149 -13.000 -0.9379 0.04027 0.03168 -0.0481 1.0000 0.2200 -12.750 -0.9455 0.03896 0.03031 -0.0447 1.0000 0.2257 -12.500 -0.9516 0.03791 0.02928 -0.0412 1.0000 0.2309 -12.250 -0.9584 0.03697 0.02836 -0.0375 1.0000 0.2359 -12.000 -0.9674 0.03602 0.02735 -0.0333 1.0000 0.2415 -11.750 -0.9754 0.03523 0.02657 -0.0291 1.0000 0.2464 -11.500 -0.9587 0.03434 0.02568 -0.0291 0.9958 0.2538 -11.250 -0.9366 0.03341 0.02468 -0.0300 0.9896 0.2622 -11.000 -0.9149 0.03265 0.02394 -0.0305 0.9829 0.2700 -10.750 -0.8934 0.03184 0.02302 -0.0311 0.9765 0.2788 -10.500 -0.8719 0.03120 0.02245 -0.0310 0.9685 0.2860 -10.250 -0.8524 0.03048 0.02161 -0.0309 0.9610 0.2947 -10.000 -0.8302 0.02992 0.02111 -0.0306 0.9526 0.3019 -9.750 -0.8098 0.02932 0.02047 -0.0302 0.9448 0.3100 -9.250 -0.7635 0.02826 0.01940 -0.0297 0.9294 0.3257 -9.000 -0.7500 0.02771 0.01873 -0.0277 0.9187 0.3337 -8.750 -0.7163 0.02724 0.01835 -0.0290 0.9137 0.3416 -8.500 -0.7041 0.02683 0.01790 -0.0264 0.9022 0.3491 -8.250 -0.6766 0.02630 0.01736 -0.0265 0.8955 0.3572 -8.000 -0.6415 0.02578 0.01685 -0.0279 0.8912 0.3657 -7.750 -0.6368 0.02547 0.01646 -0.0238 0.8769 0.3730 -7.500 -0.6002 0.02499 0.01605 -0.0253 0.8712 0.3808 -7.250 -0.5793 0.02463 0.01566 -0.0240 0.8615 0.3888 -7.000 -0.5601 0.02425 0.01521 -0.0224 0.8510 0.3967 -6.750 -0.5172 0.02377 0.01480 -0.0250 0.8455 0.4052 -6.500 -0.5077 0.02354 0.01451 -0.0215 0.8324 0.4128 -6.250 -0.4716 0.02311 0.01410 -0.0229 0.8242 0.4212 -6.000 -0.4386 0.02275 0.01373 -0.0237 0.8157 0.4301 -5.750 -0.4266 0.02248 0.01337 -0.0206 0.8028 0.4383 -5.500 -0.3764 0.02204 0.01299 -0.0246 0.7959 0.4473 -5.250 -0.3691 0.02191 0.01283 -0.0205 0.7816 0.4551 -5.000 -0.3294 0.02151 0.01240 -0.0226 0.7730 0.4646 -4.750 -0.3140 0.02139 0.01231 -0.0199 0.7595 0.4724 -4.500 -0.2849 0.02107 0.01187 -0.0200 0.7497 0.4827 -4.250 -0.2626 0.02096 0.01184 -0.0186 0.7368 0.4903 -4.000 -0.2323 0.02072 0.01154 -0.0188 0.7261 0.5002 -3.750 -0.2173 0.02062 0.01142 -0.0162 0.7136 0.5088 -3.500 -0.1857 0.02046 0.01126 -0.0166 0.7026 0.5180 -3.250 -0.1734 0.02037 0.01111 -0.0134 0.6906 0.5277 -3.000 -0.1440 0.02026 0.01103 -0.0133 0.6793 0.5367 -2.750 -0.1247 0.02019 0.01093 -0.0114 0.6680 0.5464 -2.500 -0.1062 0.02011 0.01083 -0.0094 0.6564 0.5560 -2.250 -0.0790 0.02007 0.01078 -0.0089 0.6459 0.5658 -2.000 -0.0704 0.02002 0.01068 -0.0050 0.6344 0.5762 -1.750 -0.0356 0.01998 0.01066 -0.0060 0.6240 0.5856 -1.500 -0.0262 0.01999 0.01067 -0.0022 0.6125 0.5963 -1.250 0.0034 0.01995 0.01059 -0.0022 0.6023 0.6064 -1.000 0.0167 0.01999 0.01068 0.0009 0.5908 0.6168 -0.750 0.0372 0.01997 0.01061 0.0026 0.5806 0.6278 -0.500 0.0587 0.02004 0.01071 0.0041 0.5696 0.6383 -0.250 0.0709 0.02002 0.01065 0.0073 0.5595 0.6501 0.000 0.1006 0.02012 0.01078 0.0073 0.5487 0.6602 0.250 0.1090 0.02013 0.01077 0.0113 0.5385 0.6728 0.500 0.1430 0.02025 0.01088 0.0104 0.5283 0.6829 0.750 0.1524 0.02031 0.01098 0.0141 0.5181 0.6954 1.000 0.1850 0.02045 0.01108 0.0135 0.5083 0.7061 1.250 0.1978 0.02056 0.01123 0.0165 0.4984 0.7186 1.500 0.2253 0.02073 0.01140 0.0168 0.4884 0.7295 1.750 0.2459 0.02088 0.01155 0.0184 0.4791 0.7418 2.000 0.2696 0.02109 0.01179 0.0193 0.4690 0.7528 2.250 0.2977 0.02131 0.01195 0.0195 0.4602 0.7646 2.500 0.3167 0.02155 0.01226 0.0213 0.4503 0.7760 2.750 0.3469 0.02182 0.01247 0.0210 0.4409 0.7868 3.000 0.3641 0.02206 0.01276 0.0230 0.4317 0.7987 3.250 0.3958 0.02242 0.01310 0.0224 0.4220 0.8083 3.500 0.4121 0.02264 0.01329 0.0246 0.4141 0.8210 3.750 0.4494 0.02311 0.01379 0.0227 0.4034 0.8284 4.000 0.4599 0.02326 0.01385 0.0261 0.3968 0.8430 4.250 0.4989 0.02381 0.01447 0.0237 0.3859 0.8486 4.500 0.5313 0.02423 0.01483 0.0228 0.3773 0.8565 4.750 0.5439 0.02453 0.01516 0.0255 0.3697 0.8691 5.000 0.5788 0.02507 0.01569 0.0239 0.3604 0.8747 5.250 0.6053 0.02552 0.01607 0.0239 0.3529 0.8834 5.500 0.6227 0.02594 0.01655 0.0255 0.3449 0.8935 5.750 0.6556 0.02648 0.01703 0.0243 0.3373 0.8990 6.000 0.6739 0.02696 0.01752 0.0256 0.3303 0.9093 6.500 0.7305 0.02801 0.01848 0.0243 0.3163 0.9226 6.750 0.7465 0.02857 0.01912 0.0257 0.3095 0.9328 7.000 0.7754 0.02914 0.01970 0.0247 0.3024 0.9389 7.250 0.7964 0.02965 0.02009 0.0253 0.2973 0.9487 7.500 0.8233 0.03032 0.02088 0.0242 0.2904 0.9546 7.750 0.8424 0.03096 0.02152 0.0248 0.2848 0.9640 8.000 0.8746 0.03146 0.02190 0.0230 0.2794 0.9690 8.250 0.8940 0.03226 0.02283 0.0230 0.2737 0.9775 8.500 0.9213 0.03291 0.02351 0.0216 0.2679 0.9828 8.750 0.9498 0.03349 0.02402 0.0202 0.2632 0.9887 9.000 0.9746 0.03432 0.02492 0.0190 0.2578 0.9947 9.250 1.0011 0.03514 0.02580 0.0174 0.2524 0.9999 9.500 0.9998 0.03572 0.02636 0.0209 0.2493 1.0000 9.750 1.0025 0.03622 0.02677 0.0240 0.2463 1.0000 10.000 0.9981 0.03703 0.02765 0.0278 0.2430 1.0000 10.250 0.9926 0.03797 0.02866 0.0315 0.2396 1.0000 10.500 0.9901 0.03887 0.02958 0.0347 0.2363 1.0000 10.750 0.9914 0.03968 0.03038 0.0375 0.2332 1.0000 11.000 0.9991 0.04031 0.03093 0.0396 0.2303 1.0000 11.250 0.9955 0.04156 0.03225 0.0424 0.2272 1.0000 11.500 0.9895 0.04303 0.03382 0.0452 0.2238 1.0000 11.750 0.9883 0.04434 0.03516 0.0475 0.2206 1.0000 12.000 0.9919 0.04542 0.03623 0.0494 0.2176 1.0000 12.250 1.0033 0.04609 0.03682 0.0507 0.2148 1.0000 12.500 0.9941 0.04818 0.03903 0.0529 0.2118 1.0000 12.750 0.9837 0.05048 0.04146 0.0549 0.2085 1.0000 13.000 0.9809 0.05234 0.04338 0.0563 0.2054 1.0000 13.250 0.9854 0.05368 0.04471 0.0575 0.2026 1.0000 13.500 1.0012 0.05420 0.04513 0.0583 0.2001 1.0000 13.750 0.9772 0.05811 0.04926 0.0596 0.1971 1.0000 14.000 0.9553 0.06216 0.05348 0.0604 0.1938 1.0000 14.250 0.9475 0.06503 0.05642 0.0609 0.1907 1.0000 14.500 0.9571 0.06618 0.05753 0.0615 0.1882 1.0000 14.750 0.9687 0.06717 0.05847 0.0621 0.1858 1.0000 15.000 0.8161 0.08813 0.08010 0.0574 0.1782 1.0000 15.250 0.8239 0.08970 0.08165 0.0576 0.1758 1.0000