NACA 23024 (naca23024-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 23024 (naca23024-il) Reynolds number: 1,000,000 Max Cl/Cd: 56.88 at α=8.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca23024-il-1000000.txt Download as CSV file: xf-naca23024-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1752 0.06826 0.06346 -0.0657 1.0000 0.0679
-19.500 -1.1789 0.06535 0.06050 -0.0658 1.0000 0.0691
-19.250 -1.1790 0.06291 0.05799 -0.0657 1.0000 0.0701
-19.000 -1.1861 0.05973 0.05477 -0.0657 1.0000 0.0715
-18.750 -1.1912 0.05684 0.05184 -0.0654 1.0000 0.0725
-18.500 -1.1950 0.05416 0.04912 -0.0651 1.0000 0.0740
-18.250 -1.1968 0.05170 0.04662 -0.0646 1.0000 0.0753
-18.000 -1.1951 0.04964 0.04450 -0.0640 1.0000 0.0765
-17.750 -1.1989 0.04712 0.04194 -0.0633 1.0000 0.0781
-17.500 -1.2022 0.04470 0.03949 -0.0625 1.0000 0.0796
-17.250 -1.2031 0.04259 0.03735 -0.0615 1.0000 0.0814
-17.000 -1.2006 0.04085 0.03556 -0.0604 1.0000 0.0831
-16.750 -1.2012 0.03889 0.03357 -0.0592 1.0000 0.0848
-16.500 -1.2027 0.03697 0.03163 -0.0577 1.0000 0.0869
-16.250 -1.2018 0.03533 0.02997 -0.0561 1.0000 0.0892
-16.000 -1.1990 0.03388 0.02848 -0.0545 1.0000 0.0912
-15.750 -1.2005 0.03225 0.02684 -0.0524 1.0000 0.0934
-15.500 -1.2013 0.03079 0.02537 -0.0502 1.0000 0.0962
-15.250 -1.2001 0.02957 0.02412 -0.0478 1.0000 0.0986
-15.000 -1.1832 0.02814 0.02270 -0.0485 0.9989 0.1023
-14.750 -1.1626 0.02689 0.02145 -0.0496 0.9973 0.1069
-14.500 -1.1419 0.02566 0.02023 -0.0506 0.9953 0.1111
-14.250 -1.1191 0.02461 0.01918 -0.0518 0.9935 0.1164
-14.000 -1.0975 0.02348 0.01808 -0.0528 0.9921 0.1223
-13.750 -1.0768 0.02247 0.01707 -0.0532 0.9898 0.1277
-13.500 -1.0578 0.02140 0.01604 -0.0533 0.9869 0.1337
-13.250 -1.0359 0.02044 0.01510 -0.0538 0.9843 0.1409
-12.750 -0.9862 0.01875 0.01348 -0.0555 0.9805 0.1559
-12.500 -0.9590 0.01802 0.01279 -0.0565 0.9792 0.1636
-12.250 -0.9372 0.01732 0.01211 -0.0563 0.9758 0.1705
-12.000 -0.9196 0.01654 0.01136 -0.0554 0.9702 0.1779
-11.750 -0.8921 0.01598 0.01081 -0.0560 0.9673 0.1849
-11.500 -0.8652 0.01529 0.01018 -0.0567 0.9650 0.1934
-11.250 -0.8489 0.01476 0.00965 -0.0550 0.9570 0.1997
-11.000 -0.8257 0.01416 0.00909 -0.0547 0.9517 0.2071
-10.750 -0.7973 0.01364 0.00859 -0.0553 0.9477 0.2151
-10.500 -0.7760 0.01314 0.00811 -0.0545 0.9385 0.2219
-10.250 -0.7397 0.01267 0.00767 -0.0566 0.9342 0.2305
-10.000 -0.7025 0.01221 0.00723 -0.0588 0.9275 0.2388
-9.750 -0.6625 0.01187 0.00688 -0.0616 0.9190 0.2458
-9.500 -0.6222 0.01148 0.00651 -0.0645 0.9092 0.2553
-9.250 -0.5841 0.01126 0.00624 -0.0667 0.8960 0.2617
-9.000 -0.5545 0.01096 0.00595 -0.0674 0.8817 0.2700
-8.750 -0.5190 0.01081 0.00573 -0.0691 0.8674 0.2767
-8.500 -0.4957 0.01059 0.00550 -0.0685 0.8529 0.2836
-8.250 -0.4668 0.01041 0.00530 -0.0689 0.8381 0.2910
-8.000 -0.4361 0.01032 0.00513 -0.0695 0.8213 0.2964
-7.750 -0.4127 0.01011 0.00491 -0.0688 0.8039 0.3047
-7.500 -0.3887 0.01000 0.00474 -0.0681 0.7866 0.3108
-7.250 -0.3667 0.00991 0.00459 -0.0669 0.7700 0.3174
-7.000 -0.3483 0.00977 0.00442 -0.0651 0.7532 0.3250
-6.750 -0.3281 0.00969 0.00430 -0.0635 0.7384 0.3313
-6.500 -0.3102 0.00962 0.00417 -0.0615 0.7224 0.3378
-6.250 -0.2933 0.00949 0.00404 -0.0592 0.7083 0.3453
-6.000 -0.2744 0.00944 0.00394 -0.0573 0.6950 0.3517
-5.750 -0.2571 0.00936 0.00383 -0.0551 0.6811 0.3588
-5.500 -0.2409 0.00928 0.00373 -0.0527 0.6685 0.3655
-5.250 -0.2234 0.00924 0.00365 -0.0504 0.6556 0.3724
-5.000 -0.2070 0.00917 0.00357 -0.0480 0.6438 0.3793
-4.750 -0.1920 0.00911 0.00349 -0.0452 0.6305 0.3867
-4.500 -0.1739 0.00908 0.00343 -0.0431 0.6191 0.3933
-4.250 -0.1589 0.00905 0.00336 -0.0403 0.6065 0.4003
-4.000 -0.1446 0.00898 0.00330 -0.0374 0.5958 0.4084
-3.750 -0.1288 0.00898 0.00325 -0.0347 0.5829 0.4152
-3.500 -0.1143 0.00894 0.00320 -0.0318 0.5714 0.4227
-3.250 -0.1005 0.00891 0.00316 -0.0287 0.5598 0.4308
-3.000 -0.0844 0.00892 0.00313 -0.0261 0.5490 0.4375
-2.750 -0.0720 0.00887 0.00309 -0.0227 0.5388 0.4456
-2.500 -0.0630 0.00886 0.00307 -0.0186 0.5294 0.4539
-2.250 -0.0486 0.00886 0.00305 -0.0156 0.5204 0.4603
-2.000 -0.0416 0.00883 0.00302 -0.0110 0.5110 0.4691
-1.750 -0.0297 0.00882 0.00301 -0.0075 0.5030 0.4778
-1.500 -0.0164 0.00883 0.00300 -0.0043 0.4934 0.4852
-1.250 -0.0087 0.00883 0.00300 0.0001 0.4847 0.4943
-1.000 0.0060 0.00882 0.00300 0.0030 0.4767 0.5028
-0.750 0.0165 0.00884 0.00301 0.0068 0.4673 0.5108
-0.500 0.0257 0.00884 0.00302 0.0109 0.4594 0.5202
-0.250 0.0396 0.00887 0.00304 0.0140 0.4516 0.5286
0.000 0.0464 0.00888 0.00306 0.0186 0.4434 0.5381
0.250 0.0600 0.00890 0.00309 0.0217 0.4360 0.5481
0.500 0.0757 0.00892 0.00312 0.0244 0.4286 0.5571
0.750 0.0873 0.00897 0.00316 0.0279 0.4192 0.5683
1.250 0.1197 0.00900 0.00323 0.0330 0.4050 0.5894
1.500 0.1341 0.00909 0.00330 0.0358 0.3961 0.5991
1.750 0.1505 0.00909 0.00334 0.0383 0.3895 0.6107
2.000 0.1668 0.00916 0.00341 0.0407 0.3816 0.6222
2.250 0.1818 0.00920 0.00348 0.0434 0.3743 0.6344
2.500 0.2004 0.00925 0.00355 0.0454 0.3673 0.6462
2.750 0.2150 0.00932 0.00364 0.0481 0.3595 0.6585
3.000 0.2322 0.00940 0.00373 0.0503 0.3525 0.6719
3.250 0.2496 0.00944 0.00381 0.0525 0.3454 0.6849
3.500 0.2662 0.00957 0.00393 0.0547 0.3371 0.6984
3.750 0.2842 0.00962 0.00404 0.0567 0.3306 0.7133
4.000 0.3024 0.00972 0.00416 0.0586 0.3237 0.7272
4.250 0.3191 0.00985 0.00431 0.0607 0.3157 0.7436
4.500 0.3401 0.00991 0.00444 0.0620 0.3094 0.7594
4.750 0.3591 0.01006 0.00461 0.0636 0.3010 0.7759
5.000 0.3801 0.01019 0.00478 0.0648 0.2944 0.7934
5.250 0.4067 0.01032 0.00496 0.0648 0.2870 0.8104
5.500 0.4327 0.01052 0.00518 0.0648 0.2789 0.8264
5.750 0.4586 0.01066 0.00535 0.0649 0.2730 0.8421
6.000 0.4883 0.01087 0.00559 0.0641 0.2652 0.8574
6.250 0.5156 0.01107 0.00582 0.0638 0.2588 0.8721
6.500 0.5456 0.01129 0.00606 0.0629 0.2524 0.8871
6.750 0.5795 0.01160 0.00638 0.0611 0.2448 0.8999
7.000 0.6150 0.01184 0.00665 0.0591 0.2398 0.9126
7.250 0.6589 0.01224 0.00704 0.0552 0.2329 0.9214
7.500 0.6959 0.01263 0.00743 0.0528 0.2278 0.9308
7.750 0.7366 0.01303 0.00783 0.0496 0.2230 0.9353
8.000 0.7701 0.01354 0.00832 0.0478 0.2181 0.9403
8.250 0.7917 0.01403 0.00880 0.0483 0.2134 0.9492
8.500 0.8214 0.01444 0.00923 0.0474 0.2101 0.9528
8.750 0.8451 0.01493 0.00970 0.0476 0.2063 0.9586
9.000 0.8627 0.01554 0.01029 0.0486 0.2021 0.9654
9.250 0.8927 0.01604 0.01079 0.0474 0.1985 0.9678
9.500 0.9219 0.01649 0.01125 0.0463 0.1954 0.9706
9.750 0.9357 0.01714 0.01190 0.0482 0.1925 0.9781
10.000 0.9649 0.01779 0.01252 0.0466 0.1881 0.9792
10.250 0.9953 0.01834 0.01307 0.0450 0.1850 0.9805
10.500 1.0263 0.01881 0.01356 0.0433 0.1821 0.9820
10.750 1.0542 0.01943 0.01417 0.0420 0.1787 0.9838
11.000 1.0787 0.02023 0.01495 0.0411 0.1749 0.9863
11.250 1.1041 0.02089 0.01562 0.0402 0.1721 0.9888
11.500 1.1270 0.02162 0.01637 0.0398 0.1692 0.9916
11.750 1.1551 0.02228 0.01704 0.0381 0.1663 0.9928
12.000 1.1795 0.02316 0.01789 0.0368 0.1627 0.9944
12.250 1.2059 0.02391 0.01867 0.0353 0.1598 0.9962
12.500 1.2325 0.02464 0.01941 0.0338 0.1575 0.9979
12.750 1.2576 0.02554 0.02032 0.0322 0.1540 0.9994
13.000 1.2682 0.02668 0.02145 0.0329 0.1510 1.0000
13.250 1.2718 0.02767 0.02246 0.0351 0.1492 1.0000
13.500 1.2793 0.02852 0.02335 0.0369 0.1473 1.0000
13.750 1.2846 0.02959 0.02445 0.0387 0.1452 1.0000
14.000 1.2888 0.03079 0.02566 0.0404 0.1429 1.0000
14.250 1.2891 0.03233 0.02720 0.0422 0.1404 1.0000
14.500 1.2946 0.03357 0.02848 0.0436 0.1383 1.0000
14.750 1.3008 0.03483 0.02978 0.0448 0.1365 1.0000
15.000 1.3062 0.03619 0.03116 0.0459 0.1342 1.0000
15.250 1.3077 0.03793 0.03292 0.0470 0.1320 1.0000
15.500 1.3057 0.03999 0.03500 0.0482 0.1296 1.0000
15.750 1.3126 0.04138 0.03643 0.0490 0.1279 1.0000
16.000 1.3165 0.04307 0.03817 0.0497 0.1260 1.0000
16.250 1.3191 0.04488 0.04001 0.0504 0.1238 1.0000
16.500 1.3170 0.04719 0.04233 0.0511 0.1218 1.0000
16.750 1.3130 0.04970 0.04488 0.0517 0.1198 1.0000
17.000 1.3182 0.05142 0.04666 0.0520 0.1182 1.0000
17.250 1.3187 0.05361 0.04888 0.0524 0.1162 1.0000
17.500 1.3180 0.05596 0.05127 0.0526 0.1144 1.0000
17.750 1.3092 0.05918 0.05451 0.0527 0.1117 1.0000
18.000 1.3090 0.06156 0.05693 0.0528 0.1105 1.0000
18.250 1.3094 0.06396 0.05939 0.0527 0.1088 1.0000
18.500 1.3080 0.06652 0.06200 0.0526 0.1066 1.0000
18.750 1.3002 0.06985 0.06536 0.0523 0.1045 1.0000
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