NACA 0024 (naca0024-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 0024 (naca0024-il) Reynolds number: 200,000 Max Cl/Cd: 42.99 at α=10° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca0024-il-200000.txt Download as CSV file: xf-naca0024-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2026 0.08451 0.07774 -0.0536 1.0000 0.1207
-19.500 -1.1773 0.08485 0.07824 -0.0531 1.0000 0.1228
-19.250 -1.1728 0.08250 0.07588 -0.0538 1.0000 0.1250
-19.000 -1.1838 0.07823 0.07147 -0.0552 1.0000 0.1272
-18.750 -1.2059 0.07277 0.06576 -0.0568 1.0000 0.1293
-18.500 -1.1994 0.07079 0.06378 -0.0570 1.0000 0.1316
-18.250 -1.1860 0.06961 0.06267 -0.0571 1.0000 0.1339
-18.000 -1.1845 0.06706 0.06008 -0.0575 1.0000 0.1364
-17.750 -1.1934 0.06344 0.05630 -0.0582 1.0000 0.1389
-17.500 -1.2041 0.05978 0.05245 -0.0587 1.0000 0.1412
-17.250 -1.1847 0.05922 0.05203 -0.0584 1.0000 0.1439
-17.000 -1.1786 0.05734 0.05015 -0.0584 1.0000 0.1466
-16.750 -1.1804 0.05473 0.04744 -0.0585 1.0000 0.1494
-16.500 -1.1905 0.05150 0.04399 -0.0584 1.0000 0.1519
-16.250 -1.1721 0.05078 0.04341 -0.0580 1.0000 0.1550
-16.000 -1.1645 0.04922 0.04186 -0.0577 1.0000 0.1580
-15.750 -1.1632 0.04716 0.03972 -0.0573 1.0000 0.1612
-15.500 -1.1694 0.04464 0.03700 -0.0566 1.0000 0.1640
-15.250 -1.1514 0.04388 0.03638 -0.0561 1.0000 0.1675
-15.000 -1.1440 0.04250 0.03501 -0.0554 1.0000 0.1708
-14.750 -1.1420 0.04078 0.03321 -0.0545 1.0000 0.1743
-14.500 -1.1415 0.03904 0.03134 -0.0532 1.0000 0.1777
-14.250 -1.1265 0.03820 0.03062 -0.0525 1.0000 0.1813
-14.000 -1.1203 0.03698 0.02940 -0.0513 1.0000 0.1851
-13.750 -1.1193 0.03556 0.02787 -0.0496 1.0000 0.1889
-13.500 -1.1104 0.03451 0.02684 -0.0481 1.0000 0.1928
-13.250 -1.1021 0.03361 0.02600 -0.0465 1.0000 0.1966
-13.000 -1.0993 0.03261 0.02496 -0.0443 1.0000 0.2007
-12.750 -1.1029 0.03154 0.02376 -0.0412 1.0000 0.2045
-12.500 -1.0909 0.03087 0.02323 -0.0394 1.0000 0.2088
-12.250 -1.0888 0.03016 0.02254 -0.0364 1.0000 0.2127
-12.000 -1.0916 0.02945 0.02178 -0.0327 1.0000 0.2169
-11.750 -1.0954 0.02879 0.02106 -0.0286 1.0000 0.2208
-11.500 -1.0918 0.02829 0.02067 -0.0253 1.0000 0.2248
-11.250 -1.0971 0.02784 0.02023 -0.0206 1.0000 0.2287
-11.000 -1.1065 0.02742 0.01976 -0.0153 1.0000 0.2326
-10.750 -1.1174 0.02704 0.01930 -0.0096 1.0000 0.2362
-10.500 -1.1189 0.02666 0.01904 -0.0053 1.0000 0.2402
-10.250 -1.1294 0.02640 0.01879 0.0004 1.0000 0.2438
-10.000 -1.1149 0.02596 0.01827 0.0016 0.9966 0.2499
-9.750 -1.0804 0.02541 0.01780 -0.0007 0.9922 0.2570
-9.500 -1.0517 0.02496 0.01733 -0.0019 0.9861 0.2642
-9.250 -1.0195 0.02444 0.01681 -0.0036 0.9802 0.2717
-9.000 -0.9827 0.02402 0.01643 -0.0061 0.9762 0.2797
-8.750 -0.9590 0.02358 0.01590 -0.0060 0.9670 0.2871
-8.500 -0.9197 0.02305 0.01551 -0.0088 0.9625 0.2953
-8.250 -0.8881 0.02263 0.01500 -0.0101 0.9561 0.3038
-8.000 -0.8549 0.02210 0.01461 -0.0115 0.9488 0.3117
-7.750 -0.8158 0.02163 0.01409 -0.0141 0.9443 0.3212
-7.500 -0.7698 0.02103 0.01360 -0.0180 0.9420 0.3305
-7.250 -0.7497 0.02073 0.01327 -0.0167 0.9305 0.3385
-7.000 -0.7109 0.02018 0.01277 -0.0190 0.9258 0.3476
-6.750 -0.6721 0.01970 0.01230 -0.0212 0.9220 0.3573
-6.500 -0.6547 0.01940 0.01199 -0.0192 0.9091 0.3651
-6.250 -0.6199 0.01893 0.01160 -0.0204 0.9036 0.3743
-5.750 -0.5699 0.01823 0.01094 -0.0190 0.8842 0.3916
-5.500 -0.5468 0.01797 0.01062 -0.0179 0.8745 0.4008
-5.250 -0.5211 0.01761 0.01033 -0.0172 0.8639 0.4093
-5.000 -0.4948 0.01732 0.01002 -0.0167 0.8552 0.4187
-4.750 -0.4731 0.01708 0.00977 -0.0153 0.8425 0.4274
-4.500 -0.4451 0.01679 0.00950 -0.0150 0.8336 0.4366
-4.250 -0.4258 0.01665 0.00928 -0.0131 0.8200 0.4459
-4.000 -0.3965 0.01635 0.00906 -0.0131 0.8105 0.4550
-3.750 -0.3759 0.01624 0.00890 -0.0115 0.7969 0.4647
-3.500 -0.3481 0.01600 0.00868 -0.0112 0.7864 0.4739
-3.250 -0.3258 0.01589 0.00856 -0.0099 0.7731 0.4838
-3.000 -0.2996 0.01572 0.00836 -0.0094 0.7621 0.4935
-2.750 -0.2757 0.01561 0.00828 -0.0084 0.7490 0.5032
-2.500 -0.2509 0.01551 0.00810 -0.0076 0.7376 0.5135
-2.250 -0.2256 0.01539 0.00804 -0.0068 0.7249 0.5232
-2.000 -0.2020 0.01535 0.00789 -0.0058 0.7133 0.5340
-1.750 -0.1754 0.01523 0.00785 -0.0053 0.7009 0.5436
-1.500 -0.1516 0.01521 0.00775 -0.0043 0.6893 0.5548
-1.250 -0.1253 0.01510 0.00771 -0.0038 0.6771 0.5646
-1.000 -0.1010 0.01510 0.00765 -0.0029 0.6657 0.5760
-0.750 -0.0751 0.01503 0.00761 -0.0023 0.6538 0.5861
-0.500 -0.0505 0.01504 0.00759 -0.0014 0.6425 0.5977
-0.250 -0.0250 0.01499 0.00757 -0.0008 0.6308 0.6082
0.000 0.0000 0.01502 0.00757 0.0000 0.6198 0.6198
0.250 0.0251 0.01499 0.00757 0.0008 0.6082 0.6308
0.500 0.0505 0.01504 0.00759 0.0014 0.5977 0.6425
0.750 0.0751 0.01503 0.00761 0.0023 0.5861 0.6538
1.000 0.1011 0.01510 0.00765 0.0029 0.5760 0.6657
1.250 0.1253 0.01510 0.00771 0.0038 0.5646 0.6771
1.500 0.1517 0.01521 0.00775 0.0043 0.5548 0.6893
1.750 0.1755 0.01523 0.00785 0.0053 0.5436 0.7009
2.000 0.2020 0.01535 0.00789 0.0058 0.5340 0.7133
2.250 0.2257 0.01539 0.00804 0.0068 0.5231 0.7249
2.500 0.2509 0.01551 0.00810 0.0075 0.5135 0.7376
2.750 0.2758 0.01561 0.00827 0.0083 0.5032 0.7490
3.000 0.2996 0.01572 0.00836 0.0093 0.4935 0.7621
3.250 0.3259 0.01589 0.00856 0.0099 0.4838 0.7731
3.500 0.3481 0.01600 0.00868 0.0112 0.4739 0.7864
3.750 0.3760 0.01624 0.00890 0.0115 0.4647 0.7969
4.000 0.3966 0.01635 0.00906 0.0131 0.4549 0.8105
4.250 0.4259 0.01665 0.00928 0.0131 0.4459 0.8200
4.500 0.4452 0.01679 0.00950 0.0149 0.4366 0.8337
4.750 0.4732 0.01708 0.00977 0.0152 0.4274 0.8425
5.000 0.4949 0.01732 0.01002 0.0166 0.4187 0.8552
5.250 0.5212 0.01761 0.01033 0.0172 0.4093 0.8639
5.500 0.5469 0.01797 0.01062 0.0179 0.4008 0.8745
5.750 0.5700 0.01823 0.01094 0.0190 0.3916 0.8842
6.250 0.6201 0.01892 0.01160 0.0204 0.3743 0.9036
6.500 0.6548 0.01940 0.01199 0.0191 0.3651 0.9092
6.750 0.6723 0.01969 0.01230 0.0211 0.3573 0.9220
7.000 0.7111 0.02017 0.01276 0.0190 0.3476 0.9258
7.250 0.7499 0.02072 0.01327 0.0167 0.3384 0.9305
7.500 0.7701 0.02103 0.01359 0.0180 0.3304 0.9420
7.750 0.8161 0.02162 0.01408 0.0141 0.3212 0.9444
8.000 0.8552 0.02210 0.01460 0.0115 0.3117 0.9489
8.250 0.8881 0.02262 0.01499 0.0101 0.3038 0.9563
8.500 0.9202 0.02304 0.01550 0.0087 0.2952 0.9626
8.750 0.9595 0.02357 0.01589 0.0059 0.2870 0.9670
9.000 0.9833 0.02401 0.01642 0.0060 0.2797 0.9762
9.250 1.0202 0.02444 0.01680 0.0035 0.2717 0.9802
9.500 1.0524 0.02495 0.01732 0.0018 0.2642 0.9862
9.750 1.0813 0.02539 0.01778 0.0006 0.2569 0.9923
10.000 1.1157 0.02595 0.01826 -0.0017 0.2498 0.9967
10.250 1.1295 0.02638 0.01876 -0.0004 0.2438 1.0000
10.500 1.1190 0.02664 0.01902 0.0053 0.2402 1.0000
10.750 1.1174 0.02701 0.01928 0.0096 0.2362 1.0000
11.000 1.1066 0.02740 0.01973 0.0153 0.2326 1.0000
11.250 1.0972 0.02781 0.02020 0.0206 0.2287 1.0000
11.500 1.0919 0.02826 0.02064 0.0253 0.2248 1.0000
11.750 1.0956 0.02876 0.02102 0.0285 0.2208 1.0000
12.000 1.0919 0.02942 0.02174 0.0327 0.2169 1.0000
12.250 1.0892 0.03013 0.02250 0.0364 0.2127 1.0000
12.500 1.0914 0.03084 0.02319 0.0393 0.2087 1.0000
12.750 1.1034 0.03151 0.02372 0.0411 0.2045 1.0000
13.000 1.1001 0.03257 0.02492 0.0442 0.2007 1.0000
13.250 1.1030 0.03358 0.02596 0.0464 0.1965 1.0000
13.500 1.1117 0.03447 0.02679 0.0480 0.1927 1.0000
13.750 1.1204 0.03554 0.02784 0.0494 0.1888 1.0000
14.000 1.1216 0.03695 0.02936 0.0511 0.1850 1.0000
14.250 1.1281 0.03816 0.03058 0.0523 0.1812 1.0000
14.500 1.1437 0.03898 0.03127 0.0530 0.1775 1.0000
14.750 1.1436 0.04076 0.03318 0.0542 0.1742 1.0000
15.000 1.1458 0.04246 0.03497 0.0551 0.1707 1.0000
15.250 1.1536 0.04382 0.03632 0.0558 0.1674 1.0000
15.500 1.1710 0.04464 0.03700 0.0563 0.1640 1.0000
15.750 1.1652 0.04713 0.03969 0.0570 0.1611 1.0000
16.000 1.1668 0.04917 0.04181 0.0574 0.1579 1.0000
16.250 1.1747 0.05071 0.04333 0.0577 0.1549 1.0000
16.500 1.1924 0.05151 0.04400 0.0580 0.1519 1.0000
16.750 1.1827 0.05471 0.04741 0.0581 0.1493 1.0000
17.000 1.1814 0.05728 0.05008 0.0580 0.1465 1.0000
17.250 1.1878 0.05912 0.05192 0.0580 0.1438 1.0000
17.500 1.2089 0.05954 0.05218 0.0584 0.1410 1.0000
17.750 1.1958 0.06344 0.05630 0.0578 0.1388 1.0000
18.000 1.1876 0.06700 0.06001 0.0571 0.1363 1.0000
18.250 1.1896 0.06949 0.06254 0.0567 0.1338 1.0000
18.500 1.2036 0.07060 0.06358 0.0566 0.1315 1.0000
18.750 1.2081 0.07283 0.06583 0.0564 0.1292 1.0000
19.000 1.1868 0.07821 0.07145 0.0547 0.1271 1.0000
19.250 1.1767 0.08238 0.07575 0.0534 0.1249 1.0000
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