NACA 23024 (naca23024-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 23024 (naca23024-il) Reynolds number: 1,000,000 Max Cl/Cd: 54.4 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca23024-il-1000000-n5.txt Download as CSV file: xf-naca23024-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 23024
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 -1.1663 0.06917 0.06417 -0.0654 1.0000 0.0564
-19.500 -1.1686 0.06641 0.06137 -0.0654 1.0000 0.0574
-19.250 -1.1708 0.06370 0.05859 -0.0654 1.0000 0.0583
-19.000 -1.1746 0.06085 0.05570 -0.0654 1.0000 0.0592
-18.750 -1.1770 0.05822 0.05302 -0.0652 1.0000 0.0600
-18.500 -1.1807 0.05548 0.05024 -0.0649 1.0000 0.0611
-18.250 -1.1819 0.05307 0.04778 -0.0645 1.0000 0.0620
-18.000 -1.1817 0.05083 0.04550 -0.0640 1.0000 0.0631
-17.750 -1.1812 0.04865 0.04327 -0.0634 1.0000 0.0641
-17.500 -1.1807 0.04656 0.04114 -0.0626 1.0000 0.0650
-17.250 -1.1819 0.04436 0.03890 -0.0618 1.0000 0.0662
-17.000 -1.1820 0.04232 0.03683 -0.0608 1.0000 0.0674
-16.750 -1.1781 0.04056 0.03503 -0.0599 0.9999 0.0688
-16.500 -1.1641 0.03876 0.03319 -0.0609 0.9992 0.0702
-16.250 -1.1505 0.03683 0.03125 -0.0620 0.9982 0.0724
-16.000 -1.1338 0.03509 0.02949 -0.0634 0.9969 0.0747
-15.750 -1.1149 0.03359 0.02797 -0.0646 0.9954 0.0767
-15.500 -1.0986 0.03203 0.02640 -0.0656 0.9939 0.0787
-15.250 -1.0816 0.03058 0.02493 -0.0664 0.9926 0.0813
-15.000 -1.0614 0.02939 0.02372 -0.0674 0.9914 0.0833
-14.750 -1.0519 0.02787 0.02220 -0.0667 0.9894 0.0866
-14.500 -1.0358 0.02668 0.02100 -0.0667 0.9874 0.0894
-14.250 -1.0186 0.02551 0.01982 -0.0668 0.9852 0.0922
-14.000 -1.0009 0.02436 0.01868 -0.0671 0.9831 0.0961
-13.750 -0.9800 0.02335 0.01766 -0.0676 0.9811 0.0996
-13.500 -0.9587 0.02233 0.01666 -0.0683 0.9794 0.1036
-13.000 -0.9322 0.02050 0.01484 -0.0659 0.9698 0.1114
-12.750 -0.9139 0.01961 0.01396 -0.0655 0.9654 0.1173
-12.500 -0.9048 0.01884 0.01321 -0.0632 0.9562 0.1214
-12.000 -0.8652 0.01731 0.01171 -0.0624 0.9408 0.1323
-11.750 -0.8344 0.01657 0.01098 -0.0641 0.9345 0.1390
-11.500 -0.7954 0.01584 0.01027 -0.0673 0.9286 0.1470
-11.250 -0.7530 0.01508 0.00954 -0.0712 0.9182 0.1567
-11.000 -0.7130 0.01453 0.00897 -0.0745 0.9057 0.1639
-10.750 -0.6776 0.01408 0.00848 -0.0767 0.8877 0.1725
-10.500 -0.6525 0.01365 0.00803 -0.0770 0.8700 0.1813
-10.250 -0.6302 0.01330 0.00764 -0.0765 0.8534 0.1878
-10.000 -0.6075 0.01299 0.00729 -0.0760 0.8353 0.1948
-9.750 -0.5858 0.01270 0.00696 -0.0753 0.8176 0.2023
-9.500 -0.5649 0.01243 0.00665 -0.0743 0.7976 0.2103
-9.250 -0.5439 0.01218 0.00635 -0.0734 0.7775 0.2172
-9.000 -0.5215 0.01197 0.00609 -0.0727 0.7597 0.2244
-8.750 -0.4981 0.01178 0.00585 -0.0721 0.7427 0.2310
-8.500 -0.4750 0.01157 0.00561 -0.0714 0.7275 0.2381
-8.000 -0.4317 0.01123 0.00519 -0.0694 0.6971 0.2515
-7.750 -0.4112 0.01109 0.00502 -0.0681 0.6814 0.2581
-7.500 -0.3912 0.01097 0.00485 -0.0666 0.6672 0.2627
-7.250 -0.3739 0.01080 0.00467 -0.0646 0.6544 0.2710
-7.000 -0.3541 0.01069 0.00453 -0.0630 0.6422 0.2770
-6.750 -0.3364 0.01056 0.00438 -0.0611 0.6298 0.2834
-6.500 -0.3186 0.01045 0.00425 -0.0591 0.6176 0.2902
-6.250 -0.3002 0.01038 0.00413 -0.0571 0.6052 0.2957
-6.000 -0.2832 0.01026 0.00401 -0.0549 0.5954 0.3024
-5.750 -0.2659 0.01017 0.00390 -0.0528 0.5834 0.3096
-5.500 -0.2472 0.01013 0.00382 -0.0508 0.5727 0.3138
-5.250 -0.2313 0.01002 0.00371 -0.0483 0.5624 0.3214
-5.000 -0.2152 0.00996 0.00363 -0.0458 0.5519 0.3275
-4.750 -0.1967 0.00992 0.00356 -0.0438 0.5409 0.3328
-4.500 -0.1813 0.00988 0.00349 -0.0412 0.5299 0.3391
-4.250 -0.1646 0.00981 0.00342 -0.0388 0.5203 0.3458
-4.000 -0.1488 0.00980 0.00337 -0.0362 0.5096 0.3521
-3.750 -0.1337 0.00974 0.00332 -0.0334 0.4993 0.3587
-3.500 -0.1197 0.00973 0.00327 -0.0304 0.4867 0.3655
-3.250 -0.1031 0.00971 0.00323 -0.0280 0.4775 0.3719
-3.000 -0.0886 0.00970 0.00320 -0.0251 0.4664 0.3777
-2.750 -0.0758 0.00967 0.00317 -0.0218 0.4585 0.3849
-2.500 -0.0635 0.00964 0.00314 -0.0184 0.4516 0.3923
-2.250 -0.0541 0.00965 0.00312 -0.0144 0.4421 0.3975
-2.000 -0.0434 0.00961 0.00309 -0.0106 0.4358 0.4049
-1.750 -0.0309 0.00959 0.00308 -0.0073 0.4285 0.4125
-1.500 -0.0198 0.00962 0.00308 -0.0036 0.4190 0.4188
-1.250 -0.0074 0.00959 0.00307 -0.0002 0.4142 0.4266
-1.000 0.0051 0.00960 0.00307 0.0031 0.4054 0.4341
-0.750 0.0164 0.00966 0.00309 0.0068 0.3966 0.4395
-0.500 0.0278 0.00963 0.00309 0.0104 0.3905 0.4481
-0.250 0.0384 0.00966 0.00312 0.0141 0.3830 0.4560
0.000 0.0483 0.00971 0.00315 0.0180 0.3760 0.4621
0.250 0.0609 0.00970 0.00317 0.0213 0.3702 0.4713
0.500 0.0765 0.00974 0.00320 0.0240 0.3632 0.4790
0.750 0.0902 0.00979 0.00325 0.0270 0.3548 0.4877
1.000 0.1068 0.00980 0.00328 0.0294 0.3491 0.4965
1.250 0.1228 0.00986 0.00333 0.0320 0.3418 0.5051
1.500 0.1368 0.00992 0.00339 0.0349 0.3342 0.5136
1.750 0.1537 0.00996 0.00345 0.0372 0.3273 0.5230
2.000 0.1701 0.01003 0.00351 0.0396 0.3204 0.5321
2.250 0.1862 0.01008 0.00358 0.0420 0.3144 0.5434
2.500 0.2044 0.01015 0.00366 0.0440 0.3079 0.5522
2.750 0.2197 0.01022 0.00375 0.0466 0.3011 0.5627
3.000 0.2369 0.01031 0.00385 0.0487 0.2948 0.5747
3.250 0.2544 0.01038 0.00394 0.0508 0.2883 0.5851
3.500 0.2713 0.01050 0.00406 0.0529 0.2812 0.5976
3.750 0.2887 0.01058 0.00418 0.0549 0.2753 0.6087
4.000 0.3074 0.01068 0.00430 0.0567 0.2699 0.6205
4.250 0.3242 0.01081 0.00445 0.0588 0.2630 0.6336
4.500 0.3439 0.01092 0.00458 0.0603 0.2574 0.6461
4.750 0.3616 0.01106 0.00475 0.0621 0.2504 0.6596
5.000 0.3807 0.01123 0.00493 0.0636 0.2452 0.6731
5.250 0.4013 0.01133 0.00509 0.0648 0.2405 0.6876
5.500 0.4222 0.01149 0.00527 0.0659 0.2354 0.7015
5.750 0.4437 0.01167 0.00549 0.0667 0.2302 0.7171
6.000 0.4685 0.01181 0.00569 0.0670 0.2264 0.7322
6.250 0.4925 0.01199 0.00591 0.0673 0.2212 0.7490
6.500 0.5154 0.01219 0.00616 0.0679 0.2167 0.7675
6.750 0.5381 0.01238 0.00641 0.0684 0.2124 0.7839
7.000 0.5612 0.01257 0.00667 0.0689 0.2089 0.8012
7.250 0.5832 0.01280 0.00695 0.0695 0.2044 0.8201
7.500 0.6058 0.01306 0.00726 0.0699 0.2008 0.8391
7.750 0.6312 0.01328 0.00755 0.0698 0.1976 0.8568
8.000 0.6573 0.01353 0.00787 0.0695 0.1946 0.8732
8.250 0.6848 0.01384 0.00823 0.0688 0.1908 0.8906
8.500 0.7219 0.01424 0.00868 0.0661 0.1866 0.9069
8.750 0.7655 0.01463 0.00910 0.0621 0.1829 0.9185
9.000 0.8107 0.01514 0.00962 0.0577 0.1783 0.9280
9.250 0.8511 0.01576 0.01023 0.0541 0.1739 0.9339
9.500 0.8861 0.01629 0.01078 0.0518 0.1710 0.9396
9.750 0.9104 0.01682 0.01132 0.0515 0.1684 0.9478
10.000 0.9343 0.01742 0.01191 0.0512 0.1649 0.9534
10.500 0.9674 0.01866 0.01316 0.0532 0.1598 0.9681
10.750 0.9879 0.01925 0.01376 0.0535 0.1573 0.9728
11.000 0.9986 0.01999 0.01451 0.0554 0.1548 0.9786
11.250 1.0231 0.02077 0.01527 0.0544 0.1513 0.9801
11.500 1.0474 0.02150 0.01601 0.0535 0.1485 0.9818
11.750 1.0712 0.02225 0.01677 0.0526 0.1465 0.9838
12.000 1.0926 0.02308 0.01761 0.0521 0.1432 0.9859
12.250 1.1101 0.02412 0.01864 0.0519 0.1401 0.9881
12.500 1.1288 0.02503 0.01958 0.0517 0.1384 0.9900
12.750 1.1465 0.02601 0.02057 0.0517 0.1361 0.9917
13.000 1.1676 0.02704 0.02161 0.0506 0.1333 0.9930
13.250 1.1878 0.02818 0.02275 0.0495 0.1304 0.9945
13.500 1.2088 0.02935 0.02394 0.0482 0.1280 0.9960
13.750 1.2304 0.03046 0.02508 0.0469 0.1253 0.9974
14.000 1.2481 0.03186 0.02649 0.0457 0.1227 0.9986
14.250 1.2627 0.03339 0.02803 0.0449 0.1198 0.9995
14.500 1.2780 0.03475 0.02942 0.0443 0.1179 1.0000
14.750 1.2832 0.03612 0.03082 0.0455 0.1160 1.0000
15.000 1.2850 0.03781 0.03253 0.0466 0.1137 1.0000
15.250 1.2858 0.03964 0.03439 0.0477 0.1117 1.0000
15.500 1.2894 0.04130 0.03608 0.0486 0.1101 1.0000
15.750 1.2923 0.04307 0.03789 0.0494 0.1082 1.0000
16.000 1.2942 0.04495 0.03980 0.0501 0.1062 1.0000
16.250 1.2931 0.04718 0.04206 0.0508 0.1044 1.0000
16.500 1.2919 0.04944 0.04435 0.0513 0.1026 1.0000
16.750 1.2941 0.05145 0.04642 0.0517 0.1015 1.0000
17.000 1.2940 0.05371 0.04873 0.0521 0.0997 1.0000
17.250 1.2923 0.05615 0.05120 0.0523 0.0976 1.0000
17.500 1.2890 0.05885 0.05394 0.0525 0.0963 1.0000
17.750 1.2844 0.06170 0.05683 0.0525 0.0939 1.0000
18.000 1.2835 0.06422 0.05940 0.0525 0.0931 1.0000
18.250 1.2799 0.06707 0.06231 0.0523 0.0915 1.0000
18.500 1.2734 0.07025 0.06552 0.0521 0.0893 1.0000
18.750 1.2640 0.07386 0.06917 0.0516 0.0875 1.0000
19.000 1.2627 0.07658 0.07195 0.0513 0.0865 1.0000
19.250 1.2567 0.07986 0.07529 0.0507 0.0847 1.0000
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