NACA 23015 (naca23015-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 23015 (naca23015-il) Reynolds number: 500,000 Max Cl/Cd: 72.04 at α=10.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca23015-il-500000.txt Download as CSV file: xf-naca23015-il-500000.csv |
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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -1.0086 0.11078 0.10773 -0.0205 0.9999 0.0257
-18.250 -1.0776 0.09326 0.08983 -0.0318 0.9999 0.0255
-18.000 -1.1072 0.08424 0.08059 -0.0372 0.9999 0.0256
-17.750 -1.1295 0.07689 0.07304 -0.0413 0.9999 0.0258
-17.500 -1.1477 0.07054 0.06649 -0.0447 0.9999 0.0261
-17.250 -1.1627 0.06500 0.06076 -0.0473 0.9999 0.0263
-17.000 -1.1755 0.06003 0.05559 -0.0494 0.9999 0.0266
-16.750 -1.1861 0.05559 0.05093 -0.0510 0.9999 0.0269
-16.500 -1.1927 0.05194 0.04716 -0.0517 0.9999 0.0272
-16.250 -1.1919 0.04930 0.04448 -0.0520 0.9999 0.0276
-16.000 -1.1885 0.04703 0.04218 -0.0522 0.9999 0.0279
-15.750 -1.1848 0.04491 0.04001 -0.0522 0.9999 0.0283
-15.500 -1.1813 0.04285 0.03787 -0.0520 0.9999 0.0287
-15.250 -1.1785 0.04078 0.03569 -0.0516 0.9999 0.0292
-15.000 -1.1764 0.03873 0.03350 -0.0508 0.9999 0.0297
-14.750 -1.1745 0.03679 0.03138 -0.0498 0.9999 0.0303
-14.500 -1.1719 0.03496 0.02938 -0.0484 0.9999 0.0309
-14.250 -1.1640 0.03367 0.02810 -0.0471 0.9999 0.0314
-14.000 -1.1547 0.03273 0.02715 -0.0457 0.9999 0.0319
-13.750 -1.1458 0.03184 0.02622 -0.0440 0.9999 0.0325
-13.500 -1.1381 0.03091 0.02521 -0.0420 0.9999 0.0332
-13.250 -1.1318 0.02992 0.02410 -0.0395 0.9999 0.0339
-13.000 -1.1266 0.02900 0.02301 -0.0367 0.9999 0.0346
-12.750 -1.1152 0.02791 0.02187 -0.0348 0.9999 0.0354
-12.500 -1.1003 0.02731 0.02128 -0.0332 0.9999 0.0360
-12.250 -1.0845 0.02682 0.02077 -0.0316 0.9999 0.0367
-12.000 -1.0682 0.02629 0.02018 -0.0301 0.9999 0.0376
-11.750 -1.0513 0.02569 0.01946 -0.0286 0.9999 0.0387
-11.500 -1.0340 0.02491 0.01854 -0.0272 0.9999 0.0397
-11.250 -1.0142 0.02425 0.01793 -0.0262 0.9999 0.0406
-11.000 -0.9939 0.02382 0.01751 -0.0251 0.9999 0.0415
-10.750 -0.9735 0.02335 0.01698 -0.0241 0.9999 0.0425
-10.500 -0.9526 0.02286 0.01640 -0.0230 0.9999 0.0437
-10.250 -0.9317 0.02227 0.01569 -0.0220 0.9999 0.0448
-10.000 -0.9102 0.02151 0.01499 -0.0212 0.9999 0.0459
-9.750 -0.8881 0.02109 0.01458 -0.0203 0.9999 0.0470
-9.500 -0.8659 0.02066 0.01412 -0.0194 0.9999 0.0482
-9.250 -0.8437 0.02026 0.01365 -0.0184 0.9999 0.0495
-9.000 -0.8215 0.01995 0.01325 -0.0174 0.9999 0.0505
-8.750 -0.8012 0.01897 0.01233 -0.0163 0.9999 0.0518
-8.500 -0.7804 0.01856 0.01195 -0.0151 0.9999 0.0529
-8.250 -0.7600 0.01820 0.01159 -0.0138 0.9999 0.0542
-8.000 -0.7401 0.01786 0.01122 -0.0124 0.9999 0.0555
-7.750 -0.7208 0.01761 0.01092 -0.0108 0.9999 0.0566
-7.500 -0.7042 0.01699 0.01030 -0.0089 0.9999 0.0578
-7.250 -0.6881 0.01653 0.00989 -0.0070 0.9999 0.0590
-7.000 -0.6674 0.01621 0.00958 -0.0059 0.9994 0.0603
-6.750 -0.6323 0.01576 0.00913 -0.0073 0.9970 0.0622
-6.500 -0.5967 0.01534 0.00869 -0.0087 0.9946 0.0637
-6.250 -0.5624 0.01469 0.00803 -0.0101 0.9924 0.0655
-6.000 -0.5285 0.01413 0.00752 -0.0113 0.9886 0.0677
-5.750 -0.4926 0.01370 0.00710 -0.0129 0.9855 0.0698
-5.500 -0.4559 0.01331 0.00669 -0.0145 0.9826 0.0719
-5.250 -0.4234 0.01281 0.00620 -0.0154 0.9760 0.0745
-5.000 -0.3904 0.01241 0.00583 -0.0163 0.9693 0.0776
-4.750 -0.3615 0.01213 0.00554 -0.0163 0.9578 0.0805
-4.500 -0.3347 0.01182 0.00523 -0.0159 0.9450 0.0840
-4.250 -0.3092 0.01154 0.00497 -0.0151 0.9311 0.0891
-4.000 -0.2844 0.01129 0.00472 -0.0142 0.9164 0.0960
-3.750 -0.2601 0.01097 0.00446 -0.0133 0.9005 0.1121
-3.500 -0.2398 0.00984 0.00398 -0.0122 0.8826 0.2677
-3.250 -0.2178 0.00910 0.00374 -0.0112 0.8625 0.4071
-3.000 -0.1933 0.00879 0.00361 -0.0104 0.8408 0.4702
-2.750 -0.1677 0.00860 0.00350 -0.0097 0.8193 0.5177
-2.500 -0.1414 0.00846 0.00343 -0.0092 0.7997 0.5570
-2.250 -0.1151 0.00834 0.00336 -0.0087 0.7801 0.5936
-2.000 -0.0884 0.00825 0.00331 -0.0082 0.7607 0.6255
-1.750 -0.0619 0.00817 0.00328 -0.0077 0.7408 0.6610
-1.500 -0.0354 0.00810 0.00326 -0.0072 0.7200 0.6968
-1.250 -0.0086 0.00808 0.00325 -0.0067 0.6992 0.7254
-1.000 0.0184 0.00808 0.00324 -0.0063 0.6783 0.7495
-0.750 0.0451 0.00809 0.00324 -0.0057 0.6563 0.7740
-0.500 0.0717 0.00813 0.00325 -0.0052 0.6337 0.7976
-0.250 0.0984 0.00817 0.00327 -0.0047 0.6113 0.8196
0.000 0.1248 0.00823 0.00330 -0.0042 0.5897 0.8408
0.250 0.1509 0.00831 0.00334 -0.0035 0.5680 0.8617
0.500 0.1767 0.00840 0.00339 -0.0028 0.5458 0.8795
0.750 0.2024 0.00851 0.00344 -0.0021 0.5239 0.8945
1.000 0.2280 0.00863 0.00349 -0.0014 0.5029 0.9092
1.250 0.2537 0.00875 0.00355 -0.0007 0.4825 0.9236
1.500 0.2792 0.00889 0.00361 0.0000 0.4622 0.9381
1.750 0.3059 0.00903 0.00367 0.0005 0.4413 0.9501
2.000 0.3346 0.00920 0.00375 0.0005 0.4196 0.9605
2.250 0.3647 0.00940 0.00385 0.0002 0.3978 0.9702
2.500 0.3984 0.00964 0.00398 -0.0009 0.3763 0.9763
2.750 0.4320 0.00990 0.00412 -0.0021 0.3560 0.9824
3.000 0.4691 0.01018 0.00429 -0.0039 0.3359 0.9849
3.250 0.5058 0.01046 0.00447 -0.0057 0.3173 0.9878
3.500 0.5413 0.01075 0.00466 -0.0073 0.3008 0.9913
3.750 0.5774 0.01100 0.00485 -0.0090 0.2876 0.9941
4.000 0.6140 0.01124 0.00504 -0.0108 0.2766 0.9963
4.250 0.6498 0.01156 0.00526 -0.0125 0.2665 0.9988
4.500 0.6789 0.01168 0.00538 -0.0129 0.2592 1.0001
4.750 0.6989 0.01180 0.00545 -0.0117 0.2528 1.0001
5.000 0.7194 0.01193 0.00555 -0.0104 0.2475 1.0001
5.250 0.7406 0.01203 0.00564 -0.0093 0.2423 1.0001
5.500 0.7618 0.01220 0.00577 -0.0082 0.2369 1.0001
5.750 0.7833 0.01244 0.00596 -0.0072 0.2317 1.0001
6.000 0.8064 0.01256 0.00611 -0.0063 0.2275 1.0001
6.250 0.8295 0.01274 0.00628 -0.0056 0.2230 1.0001
6.500 0.8525 0.01303 0.00652 -0.0048 0.2182 1.0001
6.750 0.8766 0.01326 0.00676 -0.0042 0.2141 1.0001
7.000 0.9017 0.01342 0.00695 -0.0038 0.2100 1.0001
7.250 0.9264 0.01365 0.00716 -0.0034 0.2055 1.0001
7.500 0.9500 0.01402 0.00748 -0.0028 0.2006 1.0001
7.750 0.9755 0.01420 0.00771 -0.0025 0.1971 1.0001
8.000 1.0009 0.01437 0.00792 -0.0021 0.1928 1.0001
8.250 1.0254 0.01464 0.00816 -0.0017 0.1884 1.0001
8.500 1.0489 0.01501 0.00851 -0.0012 0.1838 1.0001
8.750 1.0744 0.01517 0.00874 -0.0009 0.1802 1.0001
9.000 1.0991 0.01540 0.00899 -0.0005 0.1758 1.0001
9.250 1.1223 0.01575 0.00931 0.0000 0.1711 1.0001
9.500 1.1464 0.01602 0.00962 0.0005 0.1671 1.0001
9.750 1.1706 0.01625 0.00990 0.0009 0.1625 1.0001
10.000 1.1931 0.01660 0.01023 0.0015 0.1576 1.0001
10.250 1.2161 0.01692 0.01059 0.0021 0.1530 1.0001
10.500 1.2391 0.01720 0.01090 0.0027 0.1475 1.0001
10.750 1.2596 0.01765 0.01132 0.0035 0.1417 1.0001
11.000 1.2821 0.01794 0.01167 0.0042 0.1357 1.0001
11.250 1.3009 0.01845 0.01215 0.0052 0.1293 1.0001
11.500 1.3213 0.01885 0.01258 0.0061 0.1228 1.0001
11.750 1.3382 0.01943 0.01315 0.0074 0.1163 1.0001
12.000 1.3546 0.02000 0.01373 0.0088 0.1097 1.0001
12.250 1.3685 0.02068 0.01442 0.0105 0.1039 1.0001
12.500 1.3773 0.02146 0.01520 0.0130 0.0985 1.0001
12.750 1.3851 0.02232 0.01610 0.0154 0.0940 1.0001
13.000 1.3926 0.02328 0.01708 0.0177 0.0897 1.0001
13.250 1.3981 0.02447 0.01829 0.0199 0.0861 1.0001
13.500 1.4068 0.02553 0.01941 0.0216 0.0827 1.0001
13.750 1.4113 0.02695 0.02086 0.0233 0.0799 1.0001
14.000 1.4145 0.02858 0.02254 0.0249 0.0774 1.0001
14.250 1.4220 0.02998 0.02404 0.0260 0.0751 1.0001
14.500 1.4259 0.03176 0.02588 0.0271 0.0730 1.0001
14.750 1.4256 0.03403 0.02819 0.0279 0.0712 1.0001
15.000 1.4245 0.03651 0.03075 0.0285 0.0695 1.0001
15.250 1.4287 0.03861 0.03296 0.0288 0.0680 1.0001
15.500 1.4303 0.04107 0.03551 0.0289 0.0666 1.0001
15.750 1.4289 0.04394 0.03846 0.0287 0.0654 1.0001
16.000 1.4239 0.04730 0.04189 0.0283 0.0643 1.0001
16.250 1.4149 0.05121 0.04587 0.0277 0.0633 1.0001
16.500 1.4076 0.05501 0.04976 0.0269 0.0623 1.0001
16.750 1.4044 0.05849 0.05337 0.0260 0.0615 1.0001
17.000 1.3993 0.06228 0.05727 0.0249 0.0606 1.0001
17.250 1.3930 0.06630 0.06138 0.0237 0.0598 1.0001
17.500 1.3856 0.07053 0.06571 0.0223 0.0590 1.0001
17.750 1.3772 0.07492 0.07020 0.0208 0.0582 1.0001
18.000 1.3680 0.07946 0.07479 0.0192 0.0575 1.0001
18.250 1.3593 0.08387 0.07925 0.0177 0.0567 1.0001
18.500 1.3527 0.08784 0.08325 0.0164 0.0558 1.0001
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