NACA 0024 (naca0024-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 0024 (naca0024-il) Reynolds number: 1,000,000 Max Cl/Cd: 64.15 at α=9.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca0024-il-1000000-n5.txt Download as CSV file: xf-naca0024-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2886 0.07903 0.07417 -0.0422 1.0000 0.0675
-19.500 -1.2956 0.07522 0.07031 -0.0432 1.0000 0.0687
-19.250 -1.2991 0.07189 0.06692 -0.0439 1.0000 0.0698
-19.000 -1.3010 0.06874 0.06372 -0.0446 1.0000 0.0710
-18.750 -1.3026 0.06564 0.06055 -0.0452 1.0000 0.0719
-18.500 -1.3045 0.06258 0.05744 -0.0457 1.0000 0.0731
-18.250 -1.3076 0.05943 0.05424 -0.0462 1.0000 0.0743
-18.000 -1.3092 0.05645 0.05121 -0.0466 1.0000 0.0756
-17.750 -1.3073 0.05389 0.04861 -0.0469 1.0000 0.0769
-17.500 -1.3047 0.05141 0.04608 -0.0471 1.0000 0.0781
-17.250 -1.3025 0.04894 0.04355 -0.0472 1.0000 0.0793
-17.000 -1.3010 0.04646 0.04105 -0.0473 1.0000 0.0809
-16.750 -1.2981 0.04414 0.03869 -0.0473 1.0000 0.0826
-16.500 -1.2934 0.04201 0.03652 -0.0472 1.0000 0.0842
-16.250 -1.2859 0.04020 0.03467 -0.0471 1.0000 0.0856
-16.000 -1.2808 0.03821 0.03265 -0.0469 1.0000 0.0872
-15.750 -1.2753 0.03629 0.03070 -0.0465 1.0000 0.0889
-15.500 -1.2674 0.03464 0.02902 -0.0462 1.0000 0.0907
-15.250 -1.2586 0.03308 0.02744 -0.0458 1.0000 0.0924
-15.000 -1.2492 0.03164 0.02597 -0.0452 1.0000 0.0942
-14.750 -1.2415 0.03012 0.02444 -0.0445 1.0000 0.0963
-14.500 -1.2328 0.02873 0.02303 -0.0438 1.0000 0.0986
-14.250 -1.2219 0.02758 0.02186 -0.0430 1.0000 0.1007
-14.000 -1.2120 0.02643 0.02069 -0.0420 1.0000 0.1027
-13.750 -1.2043 0.02527 0.01953 -0.0406 1.0000 0.1052
-13.500 -1.1963 0.02430 0.01855 -0.0390 1.0000 0.1077
-13.250 -1.1845 0.02340 0.01763 -0.0378 0.9991 0.1100
-13.000 -1.1634 0.02240 0.01664 -0.0385 0.9961 0.1129
-12.750 -1.1419 0.02143 0.01567 -0.0392 0.9929 0.1164
-12.500 -1.1188 0.02067 0.01489 -0.0398 0.9891 0.1194
-12.250 -1.0993 0.01982 0.01406 -0.0398 0.9822 0.1226
-12.000 -1.0773 0.01906 0.01330 -0.0401 0.9759 0.1264
-11.750 -1.0585 0.01843 0.01265 -0.0395 0.9662 0.1295
-11.500 -1.0410 0.01776 0.01198 -0.0387 0.9563 0.1331
-11.250 -1.0249 0.01716 0.01137 -0.0374 0.9441 0.1367
-11.000 -1.0074 0.01666 0.01083 -0.0363 0.9322 0.1401
-10.750 -0.9912 0.01613 0.01028 -0.0348 0.9195 0.1439
-10.500 -0.9742 0.01563 0.00977 -0.0335 0.9060 0.1480
-10.250 -0.9551 0.01525 0.00933 -0.0324 0.8933 0.1516
-10.000 -0.9375 0.01481 0.00886 -0.0311 0.8794 0.1557
-9.750 -0.9184 0.01441 0.00845 -0.0300 0.8656 0.1603
-9.500 -0.8978 0.01410 0.00808 -0.0290 0.8522 0.1642
-9.250 -0.8792 0.01372 0.00768 -0.0277 0.8375 0.1691
-9.000 -0.8585 0.01342 0.00734 -0.0267 0.8238 0.1739
-8.750 -0.8372 0.01316 0.00703 -0.0258 0.8099 0.1781
-8.500 -0.8171 0.01284 0.00670 -0.0247 0.7957 0.1836
-8.250 -0.7953 0.01260 0.00643 -0.0238 0.7827 0.1885
-8.000 -0.7735 0.01237 0.00616 -0.0229 0.7682 0.1930
-7.750 -0.7522 0.01211 0.00589 -0.0219 0.7552 0.1988
-7.500 -0.7297 0.01193 0.00566 -0.0210 0.7416 0.2037
-7.250 -0.7074 0.01171 0.00542 -0.0201 0.7286 0.2090
-7.000 -0.6855 0.01151 0.00520 -0.0191 0.7157 0.2150
-6.500 -0.6406 0.01116 0.00480 -0.0173 0.6903 0.2262
-6.250 -0.6187 0.01102 0.00464 -0.0162 0.6771 0.2325
-6.000 -0.5974 0.01090 0.00450 -0.0149 0.6656 0.2379
-5.750 -0.5772 0.01077 0.00436 -0.0135 0.6525 0.2449
-5.500 -0.5544 0.01068 0.00424 -0.0124 0.6411 0.2507
-5.250 -0.5316 0.01056 0.00411 -0.0115 0.6286 0.2574
-5.000 -0.5077 0.01045 0.00399 -0.0107 0.6176 0.2645
-4.750 -0.4833 0.01037 0.00389 -0.0100 0.6056 0.2705
-4.500 -0.4595 0.01025 0.00377 -0.0092 0.5952 0.2783
-4.250 -0.4347 0.01018 0.00368 -0.0086 0.5833 0.2852
-4.000 -0.4104 0.01008 0.00358 -0.0079 0.5736 0.2928
-3.750 -0.3855 0.01000 0.00350 -0.0073 0.5622 0.3003
-3.500 -0.3602 0.00995 0.00342 -0.0068 0.5521 0.3070
-3.250 -0.3353 0.00986 0.00334 -0.0061 0.5418 0.3150
-3.000 -0.3098 0.00983 0.00328 -0.0056 0.5314 0.3220
-2.750 -0.2844 0.00975 0.00322 -0.0051 0.5216 0.3298
-2.250 -0.2328 0.00967 0.00312 -0.0041 0.5023 0.3445
-2.000 -0.2079 0.00962 0.00307 -0.0035 0.4918 0.3532
-1.750 -0.1815 0.00959 0.00303 -0.0032 0.4832 0.3607
-1.500 -0.1559 0.00956 0.00300 -0.0027 0.4731 0.3687
-1.250 -0.1302 0.00953 0.00297 -0.0022 0.4640 0.3774
-1.000 -0.1037 0.00952 0.00295 -0.0018 0.4548 0.3850
-0.750 -0.0786 0.00950 0.00293 -0.0012 0.4450 0.3942
-0.500 -0.0517 0.00949 0.00292 -0.0009 0.4370 0.4020
-0.250 -0.0263 0.00948 0.00291 -0.0004 0.4274 0.4108
0.000 0.0000 0.00947 0.00291 0.0000 0.4196 0.4196
0.250 0.0264 0.00948 0.00291 0.0004 0.4108 0.4272
0.500 0.0517 0.00949 0.00292 0.0009 0.4020 0.4371
0.750 0.0786 0.00950 0.00293 0.0012 0.3941 0.4450
1.000 0.1037 0.00952 0.00295 0.0018 0.3849 0.4547
1.250 0.1302 0.00953 0.00297 0.0022 0.3774 0.4640
1.500 0.1560 0.00955 0.00300 0.0026 0.3688 0.4732
1.750 0.1815 0.00959 0.00303 0.0032 0.3607 0.4832
2.000 0.2079 0.00962 0.00307 0.0035 0.3532 0.4918
2.250 0.2329 0.00967 0.00312 0.0041 0.3444 0.5023
2.750 0.2845 0.00975 0.00322 0.0051 0.3297 0.5216
3.000 0.3099 0.00983 0.00328 0.0056 0.3220 0.5314
3.250 0.3354 0.00986 0.00334 0.0061 0.3150 0.5418
3.500 0.3603 0.00995 0.00342 0.0067 0.3070 0.5521
3.750 0.3856 0.01000 0.00350 0.0073 0.3003 0.5622
4.000 0.4105 0.01008 0.00358 0.0079 0.2928 0.5736
4.250 0.4349 0.01018 0.00368 0.0086 0.2851 0.5834
4.500 0.4597 0.01025 0.00377 0.0092 0.2783 0.5950
4.750 0.4835 0.01037 0.00388 0.0100 0.2705 0.6057
5.000 0.5079 0.01045 0.00399 0.0107 0.2644 0.6177
5.250 0.5318 0.01056 0.00411 0.0114 0.2573 0.6287
5.500 0.5547 0.01068 0.00424 0.0124 0.2507 0.6412
5.750 0.5775 0.01077 0.00436 0.0134 0.2448 0.6526
6.000 0.5979 0.01090 0.00450 0.0148 0.2379 0.6656
6.250 0.6192 0.01102 0.00464 0.0161 0.2325 0.6771
6.500 0.6411 0.01116 0.00480 0.0172 0.2263 0.6904
7.000 0.6860 0.01151 0.00520 0.0190 0.2150 0.7157
7.250 0.7080 0.01171 0.00542 0.0200 0.2089 0.7286
7.500 0.7303 0.01193 0.00565 0.0209 0.2037 0.7416
7.750 0.7529 0.01211 0.00588 0.0217 0.1988 0.7552
8.000 0.7742 0.01237 0.00615 0.0227 0.1930 0.7682
8.250 0.7960 0.01260 0.00642 0.0237 0.1884 0.7826
8.500 0.8179 0.01284 0.00670 0.0245 0.1835 0.7956
8.750 0.8380 0.01316 0.00703 0.0257 0.1780 0.8099
9.000 0.8594 0.01341 0.00734 0.0266 0.1738 0.8237
9.250 0.8801 0.01372 0.00768 0.0275 0.1690 0.8374
9.500 0.8989 0.01410 0.00808 0.0288 0.1641 0.8522
9.750 0.9195 0.01441 0.00844 0.0297 0.1603 0.8655
10.000 0.9387 0.01480 0.00885 0.0308 0.1558 0.8793
10.250 0.9563 0.01524 0.00933 0.0322 0.1515 0.8931
10.500 0.9755 0.01563 0.00976 0.0332 0.1479 0.9060
10.750 0.9925 0.01612 0.01027 0.0346 0.1438 0.9194
11.000 1.0088 0.01665 0.01082 0.0360 0.1400 0.9320
11.250 1.0264 0.01715 0.01135 0.0372 0.1367 0.9439
11.500 1.0425 0.01775 0.01197 0.0384 0.1330 0.9561
11.750 1.0601 0.01841 0.01263 0.0393 0.1295 0.9661
12.000 1.0787 0.01905 0.01328 0.0399 0.1262 0.9759
12.250 1.1009 0.01980 0.01403 0.0395 0.1225 0.9823
12.500 1.1205 0.02064 0.01486 0.0396 0.1194 0.9892
12.750 1.1436 0.02141 0.01564 0.0389 0.1162 0.9930
13.000 1.1653 0.02237 0.01660 0.0382 0.1128 0.9963
13.250 1.1865 0.02336 0.01759 0.0375 0.1100 0.9993
13.500 1.1974 0.02425 0.01849 0.0388 0.1077 1.0000
13.750 1.2058 0.02522 0.01947 0.0404 0.1051 1.0000
14.000 1.2137 0.02639 0.02064 0.0417 0.1027 1.0000
14.250 1.2240 0.02752 0.02179 0.0427 0.1006 1.0000
14.500 1.2350 0.02868 0.02297 0.0435 0.0985 1.0000
14.750 1.2436 0.03008 0.02439 0.0442 0.0962 1.0000
15.000 1.2516 0.03158 0.02590 0.0449 0.0941 1.0000
15.250 1.2613 0.03301 0.02736 0.0454 0.0924 1.0000
15.500 1.2702 0.03455 0.02894 0.0458 0.0906 1.0000
15.750 1.2783 0.03621 0.03061 0.0461 0.0888 1.0000
16.000 1.2837 0.03813 0.03256 0.0464 0.0871 1.0000
16.250 1.2893 0.04009 0.03455 0.0467 0.0855 1.0000
16.500 1.2968 0.04190 0.03641 0.0468 0.0841 1.0000
16.750 1.3015 0.04403 0.03858 0.0468 0.0825 1.0000
17.000 1.3046 0.04635 0.04093 0.0468 0.0808 1.0000
17.250 1.3063 0.04882 0.04343 0.0468 0.0793 1.0000
17.500 1.3087 0.05129 0.04594 0.0466 0.0780 1.0000
17.750 1.3115 0.05374 0.04845 0.0464 0.0768 1.0000
18.000 1.3133 0.05632 0.05108 0.0461 0.0755 1.0000
18.250 1.3118 0.05930 0.05411 0.0457 0.0742 1.0000
18.500 1.3089 0.06244 0.05729 0.0452 0.0730 1.0000
18.750 1.3073 0.06547 0.06038 0.0447 0.0719 1.0000
19.000 1.3057 0.06859 0.06355 0.0440 0.0709 1.0000
19.250 1.3042 0.07170 0.06672 0.0434 0.0698 1.0000
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