NACA 0024 (naca0024-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 0024 (naca0024-il) Reynolds number: 1,000,000 Max Cl/Cd: 68.81 at α=9° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca0024-il-1000000.txt Download as CSV file: xf-naca0024-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.3130 0.07618 0.07152 -0.0430 1.0000 0.0813
-19.500 -1.3173 0.07279 0.06808 -0.0437 1.0000 0.0827
-19.250 -1.3203 0.06954 0.06477 -0.0444 1.0000 0.0841
-19.000 -1.3200 0.06667 0.06184 -0.0450 1.0000 0.0854
-18.750 -1.3216 0.06364 0.05876 -0.0455 1.0000 0.0867
-18.500 -1.3283 0.06010 0.05517 -0.0460 1.0000 0.0883
-18.250 -1.3312 0.05700 0.05203 -0.0465 1.0000 0.0898
-18.000 -1.3296 0.05442 0.04941 -0.0467 1.0000 0.0914
-17.750 -1.3267 0.05198 0.04691 -0.0470 1.0000 0.0928
-17.500 -1.3240 0.04957 0.04445 -0.0471 1.0000 0.0943
-17.250 -1.3255 0.04681 0.04166 -0.0471 1.0000 0.0962
-17.000 -1.3238 0.04437 0.03918 -0.0471 1.0000 0.0980
-16.750 -1.3191 0.04225 0.03703 -0.0471 1.0000 0.0999
-16.500 -1.3105 0.04055 0.03528 -0.0470 1.0000 0.1015
-16.250 -1.3080 0.03832 0.03302 -0.0467 1.0000 0.1036
-16.000 -1.3041 0.03627 0.03096 -0.0463 1.0000 0.1058
-15.750 -1.2965 0.03459 0.02925 -0.0459 1.0000 0.1080
-15.500 -1.2870 0.03310 0.02772 -0.0455 1.0000 0.1099
-15.250 -1.2792 0.03153 0.02612 -0.0450 1.0000 0.1121
-15.000 -1.2727 0.02992 0.02451 -0.0442 1.0000 0.1148
-14.750 -1.2638 0.02854 0.02311 -0.0435 1.0000 0.1173
-14.500 -1.2515 0.02747 0.02201 -0.0428 1.0000 0.1196
-14.250 -1.2438 0.02615 0.02068 -0.0417 1.0000 0.1225
-14.000 -1.2361 0.02495 0.01949 -0.0404 1.0000 0.1255
-13.750 -1.2262 0.02402 0.01855 -0.0390 1.0000 0.1283
-13.500 -1.2178 0.02317 0.01767 -0.0371 1.0000 0.1307
-13.250 -1.2159 0.02222 0.01673 -0.0343 1.0000 0.1340
-13.000 -1.2150 0.02148 0.01599 -0.0310 1.0000 0.1368
-12.750 -1.2173 0.02090 0.01539 -0.0269 1.0000 0.1393
-12.500 -1.1937 0.02010 0.01459 -0.0276 0.9985 0.1432
-12.250 -1.1680 0.01923 0.01375 -0.0287 0.9964 0.1479
-12.000 -1.1387 0.01861 0.01313 -0.0302 0.9945 0.1518
-11.750 -1.1115 0.01782 0.01236 -0.0315 0.9927 0.1569
-11.500 -1.0816 0.01717 0.01173 -0.0330 0.9913 0.1619
-11.250 -1.0534 0.01658 0.01115 -0.0341 0.9884 0.1665
-11.000 -1.0278 0.01593 0.01053 -0.0347 0.9838 0.1718
-10.750 -0.9996 0.01545 0.01005 -0.0355 0.9792 0.1764
-10.500 -0.9761 0.01489 0.00952 -0.0355 0.9731 0.1819
-10.250 -0.9568 0.01442 0.00906 -0.0344 0.9638 0.1869
-10.000 -0.9362 0.01407 0.00869 -0.0334 0.9549 0.1909
-9.750 -0.9203 0.01360 0.00823 -0.0316 0.9439 0.1966
-9.500 -0.9019 0.01325 0.00787 -0.0301 0.9333 0.2018
-9.250 -0.8824 0.01295 0.00753 -0.0288 0.9225 0.2064
-9.000 -0.8640 0.01257 0.00717 -0.0273 0.9108 0.2124
-8.750 -0.8436 0.01230 0.00687 -0.0261 0.8998 0.2177
-8.500 -0.8227 0.01202 0.00658 -0.0250 0.8879 0.2234
-8.250 -0.8025 0.01173 0.00628 -0.0237 0.8764 0.2296
-8.000 -0.7798 0.01153 0.00604 -0.0228 0.8640 0.2347
-7.750 -0.7589 0.01126 0.00576 -0.0217 0.8521 0.2414
-7.500 -0.7368 0.01104 0.00553 -0.0207 0.8392 0.2478
-7.250 -0.7134 0.01087 0.00532 -0.0199 0.8272 0.2533
-7.000 -0.6924 0.01064 0.00508 -0.0187 0.8138 0.2607
-6.750 -0.6688 0.01048 0.00490 -0.0179 0.8017 0.2670
-6.500 -0.6471 0.01032 0.00471 -0.0167 0.7882 0.2737
-6.250 -0.6259 0.01016 0.00455 -0.0154 0.7756 0.2810
-6.000 -0.6032 0.01009 0.00443 -0.0144 0.7628 0.2865
-5.750 -0.5825 0.00993 0.00428 -0.0130 0.7496 0.2948
-5.500 -0.5586 0.00983 0.00415 -0.0122 0.7372 0.3019
-5.250 -0.5346 0.00972 0.00402 -0.0114 0.7240 0.3090
-5.000 -0.5109 0.00960 0.00390 -0.0106 0.7119 0.3170
-4.750 -0.4855 0.00956 0.00381 -0.0100 0.6989 0.3233
-4.500 -0.4618 0.00942 0.00369 -0.0092 0.6871 0.3323
-4.250 -0.4370 0.00936 0.00360 -0.0085 0.6741 0.3400
-4.000 -0.4119 0.00926 0.00351 -0.0080 0.6629 0.3482
-3.750 -0.3875 0.00920 0.00342 -0.0072 0.6500 0.3566
-3.500 -0.3610 0.00915 0.00336 -0.0069 0.6389 0.3638
-3.250 -0.3370 0.00907 0.00327 -0.0061 0.6265 0.3730
-3.000 -0.3105 0.00902 0.00322 -0.0057 0.6157 0.3809
-2.750 -0.2858 0.00898 0.00315 -0.0050 0.6034 0.3896
-2.500 -0.2596 0.00891 0.00310 -0.0046 0.5933 0.3983
-2.250 -0.2339 0.00891 0.00306 -0.0041 0.5812 0.4060
-2.000 -0.2083 0.00883 0.00301 -0.0036 0.5711 0.4156
-1.750 -0.1820 0.00884 0.00298 -0.0032 0.5596 0.4234
-1.500 -0.1564 0.00878 0.00294 -0.0027 0.5496 0.4330
-1.250 -0.1304 0.00877 0.00292 -0.0022 0.5385 0.4420
-1.000 -0.1043 0.00875 0.00289 -0.0018 0.5287 0.4510
-0.750 -0.0784 0.00873 0.00288 -0.0013 0.5182 0.4608
-0.500 -0.0519 0.00875 0.00287 -0.0009 0.5083 0.4691
-0.250 -0.0262 0.00870 0.00286 -0.0004 0.4986 0.4796
0.000 0.0000 0.00875 0.00286 0.0000 0.4882 0.4882
0.250 0.0262 0.00870 0.00285 0.0004 0.4796 0.4985
0.500 0.0520 0.00875 0.00287 0.0009 0.4692 0.5083
0.750 0.0784 0.00873 0.00287 0.0013 0.4608 0.5182
1.000 0.1043 0.00875 0.00289 0.0018 0.4509 0.5286
1.250 0.1304 0.00877 0.00292 0.0022 0.4420 0.5385
1.500 0.1564 0.00878 0.00294 0.0027 0.4331 0.5496
1.750 0.1820 0.00884 0.00298 0.0032 0.4234 0.5596
2.000 0.2083 0.00883 0.00301 0.0036 0.4156 0.5711
2.250 0.2339 0.00891 0.00306 0.0041 0.4059 0.5812
2.500 0.2597 0.00891 0.00310 0.0046 0.3983 0.5933
2.750 0.2859 0.00898 0.00315 0.0050 0.3895 0.6034
3.000 0.3106 0.00902 0.00322 0.0057 0.3809 0.6157
3.250 0.3371 0.00907 0.00327 0.0061 0.3730 0.6265
3.500 0.3611 0.00915 0.00336 0.0069 0.3638 0.6389
3.750 0.3876 0.00920 0.00342 0.0072 0.3566 0.6500
4.000 0.4120 0.00926 0.00351 0.0079 0.3481 0.6629
4.250 0.4372 0.00936 0.00360 0.0085 0.3400 0.6741
4.500 0.4620 0.00942 0.00369 0.0092 0.3323 0.6870
4.750 0.4857 0.00955 0.00381 0.0100 0.3233 0.6989
5.000 0.5111 0.00960 0.00390 0.0105 0.3170 0.7119
5.250 0.5349 0.00972 0.00402 0.0113 0.3089 0.7240
5.500 0.5589 0.00983 0.00415 0.0121 0.3019 0.7372
5.750 0.5829 0.00993 0.00428 0.0129 0.2948 0.7497
6.000 0.6036 0.01009 0.00443 0.0143 0.2865 0.7627
6.250 0.6264 0.01016 0.00455 0.0153 0.2809 0.7756
6.500 0.6476 0.01032 0.00471 0.0166 0.2737 0.7882
6.750 0.6693 0.01048 0.00490 0.0178 0.2670 0.8016
7.000 0.6929 0.01064 0.00508 0.0186 0.2607 0.8137
7.250 0.7140 0.01087 0.00532 0.0198 0.2532 0.8271
7.500 0.7374 0.01104 0.00553 0.0206 0.2478 0.8392
7.750 0.7595 0.01126 0.00576 0.0215 0.2414 0.8520
8.000 0.7805 0.01152 0.00604 0.0227 0.2347 0.8640
8.250 0.8032 0.01173 0.00627 0.0236 0.2295 0.8762
8.500 0.8235 0.01202 0.00657 0.0248 0.2233 0.8878
8.750 0.8444 0.01230 0.00686 0.0259 0.2177 0.8997
9.000 0.8649 0.01257 0.00717 0.0271 0.2124 0.9107
9.250 0.8833 0.01295 0.00753 0.0286 0.2063 0.9224
9.500 0.9030 0.01324 0.00786 0.0299 0.2017 0.9331
9.750 0.9214 0.01360 0.00822 0.0314 0.1966 0.9438
10.000 0.9373 0.01407 0.00868 0.0332 0.1909 0.9548
10.250 0.9579 0.01442 0.00905 0.0342 0.1868 0.9637
10.500 0.9772 0.01488 0.00951 0.0353 0.1818 0.9731
10.750 1.0007 0.01544 0.01004 0.0353 0.1764 0.9792
11.000 1.0289 0.01592 0.01051 0.0345 0.1717 0.9838
11.250 1.0544 0.01656 0.01113 0.0339 0.1664 0.9885
11.500 1.0828 0.01715 0.01171 0.0328 0.1618 0.9913
11.750 1.1128 0.01780 0.01234 0.0312 0.1569 0.9928
12.000 1.1401 0.01859 0.01310 0.0299 0.1517 0.9946
12.250 1.1695 0.01920 0.01372 0.0285 0.1478 0.9965
12.500 1.1952 0.02007 0.01456 0.0273 0.1431 0.9986
12.750 1.2171 0.02085 0.01535 0.0270 0.1393 1.0000
13.000 1.2151 0.02144 0.01594 0.0310 0.1368 1.0000
13.250 1.2165 0.02217 0.01668 0.0343 0.1340 1.0000
13.500 1.2187 0.02313 0.01762 0.0370 0.1307 1.0000
13.750 1.2275 0.02397 0.01849 0.0388 0.1282 1.0000
14.000 1.2377 0.02490 0.01943 0.0401 0.1254 1.0000
14.250 1.2456 0.02610 0.02063 0.0414 0.1224 1.0000
14.500 1.2538 0.02740 0.02194 0.0425 0.1195 1.0000
14.750 1.2660 0.02848 0.02305 0.0432 0.1172 1.0000
15.000 1.2751 0.02986 0.02445 0.0439 0.1146 1.0000
15.250 1.2817 0.03146 0.02605 0.0446 0.1120 1.0000
15.500 1.2899 0.03301 0.02763 0.0452 0.1098 1.0000
15.750 1.2995 0.03451 0.02916 0.0455 0.1079 1.0000
16.000 1.3071 0.03619 0.03087 0.0459 0.1057 1.0000
16.250 1.3110 0.03825 0.03294 0.0463 0.1035 1.0000
16.500 1.3141 0.04042 0.03515 0.0465 0.1015 1.0000
16.750 1.3227 0.04213 0.03690 0.0466 0.0998 1.0000
17.000 1.3273 0.04427 0.03908 0.0467 0.0979 1.0000
17.250 1.3291 0.04670 0.04155 0.0467 0.0961 1.0000
17.500 1.3275 0.04948 0.04436 0.0466 0.0941 1.0000
17.750 1.3309 0.05184 0.04676 0.0465 0.0927 1.0000
18.000 1.3339 0.05428 0.04926 0.0462 0.0913 1.0000
18.250 1.3354 0.05687 0.05189 0.0459 0.0897 1.0000
18.500 1.3324 0.05999 0.05506 0.0455 0.0882 1.0000
18.750 1.3255 0.06356 0.05866 0.0450 0.0866 1.0000
19.000 1.3252 0.06644 0.06161 0.0445 0.0853 1.0000
19.250 1.3250 0.06938 0.06461 0.0439 0.0840 1.0000
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