NACA 0024 (naca0024-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 0024 (naca0024-il) Reynolds number: 500,000 Max Cl/Cd: 50.79 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca0024-il-500000-n5.txt Download as CSV file: xf-naca0024-il-500000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1682 0.09290 0.08750 -0.0405 1.0000 0.0801
-19.500 -1.1741 0.08903 0.08357 -0.0417 1.0000 0.0815
-19.250 -1.1766 0.08565 0.08015 -0.0427 1.0000 0.0830
-19.000 -1.1786 0.08231 0.07674 -0.0437 1.0000 0.0846
-18.750 -1.1771 0.07945 0.07382 -0.0445 1.0000 0.0859
-18.500 -1.1827 0.07576 0.07008 -0.0454 1.0000 0.0873
-18.250 -1.1862 0.07235 0.06664 -0.0462 1.0000 0.0888
-18.000 -1.1873 0.06928 0.06351 -0.0469 1.0000 0.0904
-17.750 -1.1874 0.06632 0.06049 -0.0475 1.0000 0.0921
-17.500 -1.1843 0.06377 0.05788 -0.0480 1.0000 0.0937
-17.250 -1.1875 0.06056 0.05463 -0.0485 1.0000 0.0954
-17.000 -1.1884 0.05763 0.05166 -0.0489 1.0000 0.0972
-16.750 -1.1863 0.05508 0.04907 -0.0492 1.0000 0.0991
-16.500 -1.1827 0.05270 0.04663 -0.0494 1.0000 0.1010
-16.250 -1.1802 0.05025 0.04414 -0.0495 1.0000 0.1028
-16.000 -1.1788 0.04775 0.04161 -0.0496 1.0000 0.1049
-15.750 -1.1755 0.04548 0.03931 -0.0496 1.0000 0.1070
-15.500 -1.1696 0.04349 0.03727 -0.0495 1.0000 0.1093
-15.250 -1.1636 0.04156 0.03530 -0.0493 1.0000 0.1114
-15.000 -1.1601 0.03946 0.03318 -0.0490 1.0000 0.1137
-14.750 -1.1543 0.03764 0.03133 -0.0486 1.0000 0.1162
-14.500 -1.1460 0.03606 0.02972 -0.0482 1.0000 0.1188
-14.250 -1.1389 0.03445 0.02808 -0.0476 1.0000 0.1212
-14.000 -1.1330 0.03283 0.02645 -0.0468 1.0000 0.1239
-13.750 -1.1251 0.03145 0.02505 -0.0459 1.0000 0.1268
-13.500 -1.1161 0.03023 0.02380 -0.0450 1.0000 0.1295
-13.250 -1.1098 0.02895 0.02251 -0.0436 1.0000 0.1322
-13.000 -1.1044 0.02778 0.02134 -0.0419 1.0000 0.1353
-12.750 -1.0992 0.02679 0.02033 -0.0399 1.0000 0.1383
-12.250 -1.0862 0.02493 0.01846 -0.0361 0.9988 0.1442
-12.000 -1.0631 0.02391 0.01744 -0.0371 0.9955 0.1485
-11.750 -1.0373 0.02306 0.01657 -0.0384 0.9927 0.1525
-11.500 -1.0143 0.02208 0.01560 -0.0393 0.9891 0.1569
-11.250 -0.9916 0.02128 0.01480 -0.0398 0.9831 0.1615
-11.000 -0.9665 0.02053 0.01405 -0.0407 0.9778 0.1659
-10.750 -0.9456 0.01976 0.01330 -0.0407 0.9705 0.1708
-10.500 -0.9220 0.01914 0.01266 -0.0410 0.9627 0.1756
-10.250 -0.9019 0.01849 0.01201 -0.0406 0.9537 0.1800
-10.000 -0.8820 0.01789 0.01142 -0.0400 0.9435 0.1852
-9.750 -0.8627 0.01742 0.01092 -0.0390 0.9324 0.1899
-9.500 -0.8453 0.01687 0.01036 -0.0377 0.9209 0.1946
-9.250 -0.8276 0.01641 0.00990 -0.0364 0.9079 0.1999
-9.000 -0.8080 0.01604 0.00948 -0.0353 0.8959 0.2046
-8.750 -0.7909 0.01559 0.00901 -0.0338 0.8821 0.2099
-8.500 -0.7717 0.01523 0.00863 -0.0325 0.8692 0.2155
-8.250 -0.7514 0.01492 0.00826 -0.0314 0.8560 0.2205
-8.000 -0.7327 0.01455 0.00789 -0.0300 0.8419 0.2264
-7.750 -0.7121 0.01427 0.00756 -0.0289 0.8290 0.2324
-7.500 -0.6915 0.01400 0.00725 -0.0278 0.8148 0.2379
-7.250 -0.6713 0.01371 0.00694 -0.0266 0.8017 0.2443
-7.000 -0.6495 0.01350 0.00668 -0.0256 0.7882 0.2505
-6.750 -0.6288 0.01324 0.00641 -0.0244 0.7746 0.2567
-6.500 -0.6074 0.01303 0.00616 -0.0233 0.7617 0.2636
-6.250 -0.5851 0.01286 0.00594 -0.0224 0.7478 0.2697
-6.000 -0.5648 0.01264 0.00571 -0.0210 0.7353 0.2767
-5.750 -0.5436 0.01251 0.00554 -0.0198 0.7219 0.2836
-5.500 -0.5232 0.01236 0.00538 -0.0184 0.7093 0.2901
-5.250 -0.5035 0.01224 0.00522 -0.0168 0.6964 0.2975
-5.000 -0.4809 0.01214 0.00509 -0.0158 0.6842 0.3045
-4.750 -0.4599 0.01201 0.00494 -0.0145 0.6715 0.3118
-4.500 -0.4365 0.01190 0.00482 -0.0136 0.6595 0.3196
-4.250 -0.4136 0.01182 0.00470 -0.0127 0.6474 0.3265
-4.000 -0.3905 0.01170 0.00458 -0.0117 0.6356 0.3346
-3.750 -0.3665 0.01165 0.00449 -0.0109 0.6240 0.3420
-3.500 -0.3432 0.01153 0.00438 -0.0100 0.6125 0.3497
-3.250 -0.3195 0.01148 0.00430 -0.0092 0.6013 0.3578
-3.000 -0.2948 0.01141 0.00422 -0.0085 0.5904 0.3653
-2.500 -0.2462 0.01130 0.00408 -0.0070 0.5688 0.3817
-2.250 -0.2228 0.01124 0.00402 -0.0061 0.5579 0.3899
-2.000 -0.1978 0.01119 0.00397 -0.0055 0.5479 0.3988
-1.750 -0.1733 0.01117 0.00392 -0.0047 0.5372 0.4067
-1.500 -0.1489 0.01112 0.00388 -0.0040 0.5277 0.4158
-1.250 -0.1235 0.01112 0.00385 -0.0035 0.5170 0.4240
-1.000 -0.0996 0.01107 0.00382 -0.0026 0.5077 0.4330
-0.750 -0.0742 0.01106 0.00380 -0.0021 0.4977 0.4420
-0.500 -0.0500 0.01106 0.00378 -0.0013 0.4879 0.4505
-0.250 -0.0248 0.01103 0.00377 -0.0007 0.4786 0.4602
0.000 0.0000 0.01106 0.00377 0.0000 0.4688 0.4688
0.250 0.0248 0.01103 0.00377 0.0007 0.4602 0.4787
0.500 0.0500 0.01106 0.00378 0.0013 0.4505 0.4880
0.750 0.0742 0.01106 0.00380 0.0020 0.4420 0.4977
1.000 0.0996 0.01107 0.00382 0.0026 0.4330 0.5078
1.250 0.1235 0.01112 0.00385 0.0035 0.4240 0.5170
1.500 0.1489 0.01112 0.00388 0.0040 0.4157 0.5276
1.750 0.1733 0.01117 0.00392 0.0047 0.4067 0.5372
2.000 0.1978 0.01119 0.00397 0.0055 0.3988 0.5478
2.250 0.2228 0.01124 0.00402 0.0061 0.3900 0.5579
2.500 0.2462 0.01130 0.00408 0.0070 0.3817 0.5688
3.000 0.2949 0.01141 0.00422 0.0085 0.3653 0.5904
3.250 0.3196 0.01148 0.00430 0.0091 0.3578 0.6013
3.500 0.3433 0.01153 0.00438 0.0100 0.3497 0.6125
3.750 0.3666 0.01165 0.00449 0.0109 0.3420 0.6240
4.000 0.3906 0.01170 0.00458 0.0117 0.3345 0.6356
4.250 0.4137 0.01182 0.00470 0.0126 0.3265 0.6474
4.500 0.4367 0.01190 0.00482 0.0136 0.3196 0.6595
4.750 0.4601 0.01201 0.00494 0.0144 0.3118 0.6715
5.000 0.4812 0.01214 0.00509 0.0157 0.3044 0.6842
5.250 0.5039 0.01224 0.00522 0.0167 0.2975 0.6964
5.500 0.5237 0.01236 0.00538 0.0183 0.2901 0.7094
5.750 0.5440 0.01251 0.00554 0.0197 0.2836 0.7218
6.000 0.5652 0.01264 0.00571 0.0209 0.2766 0.7353
6.250 0.5855 0.01286 0.00594 0.0223 0.2697 0.7479
6.500 0.6079 0.01303 0.00616 0.0232 0.2636 0.7617
6.750 0.6293 0.01324 0.00640 0.0243 0.2567 0.7746
7.000 0.6501 0.01350 0.00667 0.0255 0.2505 0.7881
7.250 0.6719 0.01371 0.00694 0.0265 0.2443 0.8017
7.500 0.6922 0.01400 0.00725 0.0277 0.2379 0.8148
7.750 0.7128 0.01427 0.00756 0.0288 0.2323 0.8289
8.000 0.7335 0.01455 0.00788 0.0299 0.2264 0.8418
8.250 0.7522 0.01492 0.00826 0.0312 0.2205 0.8560
8.500 0.7725 0.01522 0.00862 0.0324 0.2154 0.8691
8.750 0.7918 0.01559 0.00901 0.0336 0.2099 0.8821
9.000 0.8090 0.01604 0.00947 0.0351 0.2046 0.8958
9.250 0.8286 0.01641 0.00989 0.0362 0.1998 0.9078
9.500 0.8463 0.01686 0.01036 0.0375 0.1946 0.9209
9.750 0.8638 0.01741 0.01091 0.0388 0.1898 0.9323
10.000 0.8831 0.01788 0.01141 0.0398 0.1851 0.9435
10.250 0.9030 0.01848 0.01200 0.0404 0.1800 0.9537
10.500 0.9231 0.01912 0.01265 0.0408 0.1755 0.9627
10.750 0.9467 0.01974 0.01328 0.0405 0.1707 0.9705
11.000 0.9677 0.02051 0.01403 0.0405 0.1658 0.9779
11.250 0.9929 0.02126 0.01478 0.0396 0.1614 0.9832
11.500 1.0156 0.02205 0.01558 0.0391 0.1568 0.9893
11.750 1.0387 0.02304 0.01654 0.0381 0.1524 0.9928
12.000 1.0647 0.02387 0.01740 0.0369 0.1484 0.9957
12.250 1.0878 0.02490 0.01842 0.0358 0.1441 0.9990
12.750 1.0999 0.02673 0.02028 0.0398 0.1382 1.0000
13.000 1.1054 0.02773 0.02128 0.0418 0.1352 1.0000
13.250 1.1111 0.02890 0.02246 0.0435 0.1321 1.0000
13.500 1.1177 0.03017 0.02374 0.0448 0.1294 1.0000
13.750 1.1269 0.03139 0.02499 0.0457 0.1267 1.0000
14.000 1.1349 0.03277 0.02639 0.0465 0.1238 1.0000
14.250 1.1410 0.03439 0.02801 0.0473 0.1211 1.0000
14.500 1.1484 0.03599 0.02964 0.0479 0.1187 1.0000
14.750 1.1568 0.03756 0.03125 0.0483 0.1161 1.0000
15.000 1.1627 0.03939 0.03310 0.0487 0.1136 1.0000
15.250 1.1662 0.04150 0.03523 0.0490 0.1113 1.0000
15.500 1.1726 0.04339 0.03716 0.0491 0.1092 1.0000
15.750 1.1784 0.04539 0.03921 0.0492 0.1069 1.0000
16.000 1.1819 0.04767 0.04152 0.0492 0.1048 1.0000
16.250 1.1833 0.05016 0.04404 0.0491 0.1027 1.0000
16.500 1.1861 0.05259 0.04651 0.0490 0.1009 1.0000
16.750 1.1898 0.05497 0.04895 0.0487 0.0990 1.0000
17.000 1.1920 0.05752 0.05155 0.0484 0.0971 1.0000
17.250 1.1910 0.06046 0.05453 0.0480 0.0953 1.0000
17.500 1.1880 0.06366 0.05777 0.0475 0.0936 1.0000
17.750 1.1914 0.06619 0.06036 0.0470 0.0920 1.0000
18.000 1.1913 0.06916 0.06339 0.0464 0.0903 1.0000
18.250 1.1903 0.07223 0.06651 0.0457 0.0887 1.0000
18.500 1.1865 0.07567 0.06999 0.0449 0.0872 1.0000
18.750 1.1815 0.07930 0.07366 0.0440 0.0859 1.0000
19.000 1.1829 0.08219 0.07662 0.0432 0.0845 1.0000
19.250 1.1809 0.08554 0.08003 0.0422 0.0830 1.0000
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