NACA 0024 (naca0024-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 0024 (naca0024-il) Reynolds number: 500,000 Max Cl/Cd: 52.1 at α=10.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca0024-il-500000.txt Download as CSV file: xf-naca0024-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 0024
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2119 0.08663 0.08133 -0.0434 1.0000 0.0959
-19.500 -1.2128 0.08353 0.07821 -0.0443 1.0000 0.0976
-19.250 -1.2140 0.08032 0.07494 -0.0453 1.0000 0.0994
-19.000 -1.2126 0.07743 0.07196 -0.0461 1.0000 0.1011
-18.750 -1.2135 0.07441 0.06890 -0.0468 1.0000 0.1029
-18.500 -1.2149 0.07138 0.06588 -0.0474 1.0000 0.1048
-18.250 -1.2158 0.06837 0.06283 -0.0481 1.0000 0.1067
-18.000 -1.2132 0.06574 0.06014 -0.0486 1.0000 0.1086
-17.750 -1.2100 0.06318 0.05749 -0.0491 1.0000 0.1104
-17.500 -1.2112 0.06034 0.05465 -0.0494 1.0000 0.1125
-17.250 -1.2116 0.05753 0.05183 -0.0498 1.0000 0.1146
-17.000 -1.2093 0.05501 0.04926 -0.0501 1.0000 0.1168
-16.750 -1.2034 0.05287 0.04706 -0.0503 1.0000 0.1191
-16.500 -1.2013 0.05044 0.04458 -0.0504 1.0000 0.1213
-16.250 -1.2007 0.04792 0.04207 -0.0504 1.0000 0.1237
-16.000 -1.1967 0.04574 0.03986 -0.0503 1.0000 0.1263
-15.750 -1.1895 0.04387 0.03793 -0.0503 1.0000 0.1288
-15.500 -1.1841 0.04191 0.03594 -0.0501 1.0000 0.1314
-15.250 -1.1819 0.03973 0.03376 -0.0497 1.0000 0.1341
-15.000 -1.1758 0.03792 0.03193 -0.0493 1.0000 0.1371
-14.750 -1.1656 0.03651 0.03046 -0.0490 1.0000 0.1400
-14.500 -1.1609 0.03472 0.02866 -0.0483 1.0000 0.1430
-14.250 -1.1557 0.03303 0.02698 -0.0475 1.0000 0.1461
-14.000 -1.1469 0.03170 0.02562 -0.0467 1.0000 0.1495
-13.750 -1.1361 0.03057 0.02443 -0.0459 1.0000 0.1526
-13.500 -1.1329 0.02905 0.02294 -0.0444 1.0000 0.1560
-13.250 -1.1266 0.02786 0.02175 -0.0429 1.0000 0.1595
-13.000 -1.1182 0.02695 0.02081 -0.0413 1.0000 0.1630
-12.750 -1.1148 0.02595 0.01980 -0.0390 1.0000 0.1664
-12.500 -1.1147 0.02496 0.01884 -0.0360 1.0000 0.1698
-12.250 -1.1143 0.02421 0.01808 -0.0327 1.0000 0.1733
-12.000 -1.1132 0.02368 0.01751 -0.0292 1.0000 0.1764
-11.750 -1.1217 0.02300 0.01683 -0.0244 1.0000 0.1795
-11.500 -1.1177 0.02225 0.01610 -0.0217 0.9991 0.1835
-11.250 -1.0870 0.02154 0.01538 -0.0236 0.9965 0.1890
-11.000 -1.0580 0.02071 0.01457 -0.0253 0.9937 0.1946
-10.750 -1.0270 0.01999 0.01387 -0.0273 0.9915 0.2007
-10.500 -0.9962 0.01939 0.01325 -0.0288 0.9882 0.2063
-10.250 -0.9686 0.01862 0.01254 -0.0300 0.9838 0.2127
-10.000 -0.9344 0.01811 0.01201 -0.0321 0.9809 0.2189
-9.750 -0.9019 0.01740 0.01135 -0.0341 0.9784 0.2258
-9.500 -0.8668 0.01685 0.01081 -0.0363 0.9760 0.2327
-9.250 -0.8425 0.01634 0.01031 -0.0362 0.9680 0.2387
-9.000 -0.8145 0.01578 0.00979 -0.0369 0.9622 0.2456
-8.750 -0.7893 0.01542 0.00940 -0.0368 0.9540 0.2516
-8.500 -0.7700 0.01489 0.00892 -0.0355 0.9443 0.2583
-8.250 -0.7508 0.01453 0.00855 -0.0341 0.9335 0.2647
-8.000 -0.7302 0.01419 0.00818 -0.0328 0.9235 0.2708
-7.750 -0.7135 0.01382 0.00784 -0.0309 0.9111 0.2776
-7.500 -0.6924 0.01354 0.00751 -0.0296 0.9007 0.2843
-7.250 -0.6737 0.01324 0.00722 -0.0280 0.8879 0.2909
-7.000 -0.6538 0.01295 0.00692 -0.0266 0.8766 0.2981
-6.750 -0.6313 0.01278 0.00669 -0.0255 0.8640 0.3047
-6.500 -0.6126 0.01248 0.00641 -0.0238 0.8519 0.3123
-6.250 -0.5916 0.01229 0.00619 -0.0225 0.8390 0.3198
-6.000 -0.5711 0.01212 0.00599 -0.0210 0.8266 0.3268
-5.750 -0.5521 0.01195 0.00580 -0.0193 0.8138 0.3345
-5.500 -0.5298 0.01185 0.00566 -0.0181 0.8009 0.3419
-5.250 -0.5089 0.01167 0.00546 -0.0167 0.7884 0.3499
-5.000 -0.4862 0.01154 0.00533 -0.0157 0.7753 0.3582
-4.750 -0.4628 0.01144 0.00518 -0.0148 0.7628 0.3659
-4.500 -0.4404 0.01129 0.00505 -0.0137 0.7497 0.3745
-4.250 -0.4156 0.01125 0.00493 -0.0130 0.7374 0.3824
-4.000 -0.3932 0.01110 0.00480 -0.0119 0.7244 0.3910
-3.750 -0.3689 0.01103 0.00470 -0.0111 0.7123 0.3997
-3.500 -0.3450 0.01095 0.00459 -0.0102 0.6994 0.4080
-3.250 -0.3212 0.01086 0.00451 -0.0094 0.6875 0.4170
-3.000 -0.2961 0.01084 0.00442 -0.0087 0.6750 0.4253
-2.750 -0.2726 0.01073 0.00435 -0.0078 0.6633 0.4345
-2.500 -0.2477 0.01072 0.00428 -0.0071 0.6510 0.4435
-2.250 -0.2233 0.01063 0.00422 -0.0063 0.6396 0.4525
-2.000 -0.1989 0.01061 0.00416 -0.0055 0.6276 0.4621
-1.750 -0.1737 0.01057 0.00412 -0.0049 0.6165 0.4711
-1.500 -0.1496 0.01054 0.00407 -0.0041 0.6048 0.4809
-1.250 -0.1238 0.01053 0.00404 -0.0036 0.5939 0.4901
-1.000 -0.1000 0.01048 0.00401 -0.0027 0.5826 0.5001
-0.750 -0.0743 0.01049 0.00400 -0.0021 0.5721 0.5098
-0.500 -0.0500 0.01045 0.00397 -0.0013 0.5609 0.5196
-0.250 -0.0248 0.01046 0.00397 -0.0007 0.5508 0.5300
0.000 0.0000 0.01045 0.00396 0.0000 0.5399 0.5399
0.250 0.0248 0.01046 0.00397 0.0007 0.5300 0.5508
0.500 0.0501 0.01045 0.00397 0.0013 0.5196 0.5609
0.750 0.0743 0.01049 0.00400 0.0021 0.5098 0.5721
1.000 0.1000 0.01048 0.00401 0.0027 0.5001 0.5826
1.250 0.1239 0.01053 0.00404 0.0036 0.4900 0.5939
1.500 0.1497 0.01054 0.00407 0.0041 0.4809 0.6048
1.750 0.1738 0.01057 0.00412 0.0049 0.4711 0.6165
2.000 0.1990 0.01061 0.00416 0.0055 0.4621 0.6276
2.250 0.2234 0.01063 0.00422 0.0063 0.4525 0.6396
2.500 0.2477 0.01072 0.00428 0.0071 0.4435 0.6510
2.750 0.2726 0.01073 0.00435 0.0078 0.4345 0.6633
3.000 0.2962 0.01084 0.00442 0.0087 0.4252 0.6750
3.250 0.3213 0.01086 0.00451 0.0093 0.4170 0.6875
3.500 0.3451 0.01095 0.00459 0.0102 0.4079 0.6994
3.750 0.3691 0.01103 0.00470 0.0110 0.3997 0.7123
4.000 0.3934 0.01110 0.00480 0.0118 0.3910 0.7244
4.250 0.4157 0.01125 0.00493 0.0129 0.3824 0.7374
4.500 0.4406 0.01129 0.00505 0.0136 0.3745 0.7498
4.750 0.4630 0.01144 0.00518 0.0147 0.3659 0.7628
5.000 0.4864 0.01154 0.00533 0.0157 0.3582 0.7753
5.250 0.5092 0.01167 0.00546 0.0167 0.3499 0.7884
5.500 0.5302 0.01185 0.00566 0.0181 0.3419 0.8009
5.750 0.5525 0.01195 0.00580 0.0192 0.3345 0.8138
6.000 0.5716 0.01213 0.00599 0.0209 0.3267 0.8265
6.250 0.5920 0.01229 0.00619 0.0224 0.3197 0.8390
6.500 0.6131 0.01247 0.00641 0.0237 0.3122 0.8519
6.750 0.6318 0.01278 0.00669 0.0254 0.3047 0.8639
7.000 0.6543 0.01295 0.00692 0.0264 0.2981 0.8765
7.250 0.6742 0.01324 0.00722 0.0279 0.2909 0.8879
7.500 0.6930 0.01354 0.00751 0.0295 0.2843 0.9007
7.750 0.7142 0.01382 0.00784 0.0308 0.2775 0.9110
8.000 0.7308 0.01419 0.00817 0.0327 0.2708 0.9234
8.250 0.7515 0.01453 0.00855 0.0340 0.2647 0.9335
8.500 0.7707 0.01489 0.00891 0.0354 0.2582 0.9443
8.750 0.7901 0.01541 0.00939 0.0366 0.2516 0.9539
9.000 0.8153 0.01577 0.00978 0.0368 0.2456 0.9622
9.250 0.8432 0.01633 0.01030 0.0361 0.2386 0.9681
9.500 0.8677 0.01684 0.01080 0.0362 0.2327 0.9760
9.750 0.9028 0.01739 0.01134 0.0339 0.2257 0.9784
10.000 0.9353 0.01809 0.01199 0.0319 0.2189 0.9809
10.250 0.9695 0.01861 0.01252 0.0299 0.2126 0.9839
10.500 0.9971 0.01937 0.01324 0.0287 0.2063 0.9883
10.750 1.0281 0.01997 0.01385 0.0271 0.2006 0.9916
11.000 1.0592 0.02069 0.01455 0.0251 0.1945 0.9938
11.250 1.0883 0.02151 0.01535 0.0234 0.1889 0.9966
11.500 1.1191 0.02222 0.01608 0.0215 0.1834 0.9992
11.750 1.1217 0.02296 0.01679 0.0244 0.1795 1.0000
12.000 1.1132 0.02364 0.01746 0.0293 0.1765 1.0000
12.250 1.1146 0.02416 0.01803 0.0327 0.1733 1.0000
12.500 1.1152 0.02492 0.01879 0.0360 0.1698 1.0000
12.750 1.1154 0.02590 0.01975 0.0389 0.1663 1.0000
13.000 1.1192 0.02690 0.02075 0.0412 0.1630 1.0000
13.250 1.1278 0.02781 0.02170 0.0428 0.1594 1.0000
13.500 1.1344 0.02900 0.02289 0.0442 0.1559 1.0000
13.750 1.1376 0.03053 0.02439 0.0457 0.1525 1.0000
14.000 1.1489 0.03164 0.02555 0.0464 0.1494 1.0000
14.250 1.1578 0.03297 0.02691 0.0472 0.1460 1.0000
14.500 1.1629 0.03467 0.02860 0.0480 0.1429 1.0000
14.750 1.1681 0.03643 0.03038 0.0486 0.1399 1.0000
15.000 1.1784 0.03785 0.03185 0.0490 0.1370 1.0000
15.250 1.1844 0.03967 0.03369 0.0493 0.1340 1.0000
15.500 1.1866 0.04186 0.03587 0.0497 0.1313 1.0000
15.750 1.1925 0.04377 0.03783 0.0499 0.1288 1.0000
16.000 1.1997 0.04566 0.03977 0.0499 0.1262 1.0000
16.250 1.2037 0.04784 0.04198 0.0500 0.1236 1.0000
16.500 1.2043 0.05037 0.04451 0.0500 0.1212 1.0000
16.750 1.2069 0.05277 0.04695 0.0499 0.1190 1.0000
17.000 1.2128 0.05490 0.04915 0.0496 0.1167 1.0000
17.250 1.2151 0.05745 0.05174 0.0493 0.1145 1.0000
17.500 1.2146 0.06026 0.05456 0.0490 0.1124 1.0000
17.750 1.2138 0.06307 0.05738 0.0486 0.1103 1.0000
18.000 1.2171 0.06564 0.06003 0.0481 0.1085 1.0000
18.250 1.2196 0.06828 0.06273 0.0476 0.1065 1.0000
18.500 1.2187 0.07130 0.06579 0.0469 0.1047 1.0000
18.750 1.2173 0.07433 0.06881 0.0463 0.1028 1.0000
19.000 1.2166 0.07734 0.07187 0.0456 0.1010 1.0000
19.250 1.2181 0.08023 0.07484 0.0447 0.0993 1.0000
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