NACA 23024 (naca23024-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 23024 (naca23024-il) Reynolds number: 500,000 Max Cl/Cd: 43.4 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca23024-il-500000-n5.txt Download as CSV file: xf-naca23024-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0452 0.08245 0.07690 -0.0641 1.0000 0.0685
-19.500 -1.0470 0.07955 0.07394 -0.0645 1.0000 0.0697
-19.250 -1.0496 0.07658 0.07092 -0.0648 1.0000 0.0706
-19.000 -1.0552 0.07330 0.06760 -0.0652 1.0000 0.0720
-18.750 -1.0597 0.07019 0.06446 -0.0654 1.0000 0.0735
-18.500 -1.0621 0.06741 0.06162 -0.0655 1.0000 0.0747
-18.250 -1.0635 0.06476 0.05892 -0.0654 1.0000 0.0762
-18.000 -1.0660 0.06204 0.05615 -0.0653 1.0000 0.0774
-17.750 -1.0699 0.05924 0.05331 -0.0651 1.0000 0.0789
-17.500 -1.0726 0.05661 0.05064 -0.0648 1.0000 0.0805
-17.250 -1.0735 0.05424 0.04823 -0.0643 1.0000 0.0824
-17.000 -1.0739 0.05198 0.04592 -0.0637 1.0000 0.0841
-16.750 -1.0769 0.04951 0.04342 -0.0630 1.0000 0.0858
-16.500 -1.0780 0.04731 0.04119 -0.0622 1.0000 0.0880
-16.250 -1.0774 0.04534 0.03917 -0.0612 1.0000 0.0901
-16.000 -1.0780 0.04332 0.03712 -0.0601 1.0000 0.0920
-15.750 -1.0788 0.04139 0.03517 -0.0588 1.0000 0.0939
-15.500 -1.0790 0.03958 0.03334 -0.0573 1.0000 0.0966
-15.250 -1.0777 0.03799 0.03170 -0.0558 1.0000 0.0988
-15.000 -1.0761 0.03619 0.02990 -0.0546 0.9997 0.1019
-14.750 -1.0587 0.03455 0.02823 -0.0558 0.9984 0.1054
-14.500 -1.0415 0.03292 0.02659 -0.0570 0.9965 0.1093
-14.250 -1.0238 0.03141 0.02508 -0.0580 0.9943 0.1140
-14.000 -1.0050 0.02999 0.02365 -0.0591 0.9919 0.1185
-13.750 -0.9891 0.02860 0.02226 -0.0594 0.9894 0.1239
-13.500 -0.9721 0.02729 0.02096 -0.0597 0.9864 0.1286
-13.250 -0.9532 0.02610 0.01977 -0.0602 0.9833 0.1342
-13.000 -0.9331 0.02495 0.01863 -0.0609 0.9806 0.1402
-12.750 -0.9097 0.02396 0.01764 -0.0619 0.9784 0.1465
-12.500 -0.8983 0.02291 0.01661 -0.0604 0.9718 0.1515
-12.250 -0.8784 0.02200 0.01571 -0.0605 0.9670 0.1584
-12.000 -0.8621 0.02105 0.01479 -0.0598 0.9611 0.1657
-11.750 -0.8463 0.02029 0.01403 -0.0587 0.9528 0.1721
-11.500 -0.8271 0.01946 0.01322 -0.0584 0.9472 0.1798
-11.250 -0.8095 0.01882 0.01258 -0.0573 0.9381 0.1853
-11.000 -0.7852 0.01803 0.01183 -0.0577 0.9329 0.1941
-10.750 -0.7591 0.01738 0.01118 -0.0582 0.9259 0.2017
-10.500 -0.7266 0.01673 0.01056 -0.0599 0.9195 0.2105
-10.250 -0.6886 0.01606 0.00990 -0.0628 0.9136 0.2196
-9.750 -0.6099 0.01501 0.00886 -0.0687 0.8948 0.2370
-9.500 -0.5708 0.01464 0.00845 -0.0714 0.8828 0.2449
-9.250 -0.5317 0.01422 0.00802 -0.0743 0.8696 0.2536
-9.000 -0.4970 0.01396 0.00771 -0.0761 0.8545 0.2609
-8.750 -0.4614 0.01360 0.00733 -0.0782 0.8395 0.2696
-8.500 -0.4315 0.01339 0.00705 -0.0789 0.8218 0.2768
-8.250 -0.4088 0.01313 0.00676 -0.0783 0.8034 0.2838
-8.000 -0.3864 0.01295 0.00651 -0.0775 0.7851 0.2907
-7.750 -0.3650 0.01281 0.00629 -0.0763 0.7681 0.2970
-7.500 -0.3486 0.01260 0.00605 -0.0743 0.7515 0.3036
-7.250 -0.3308 0.01246 0.00586 -0.0724 0.7353 0.3106
-7.000 -0.3133 0.01236 0.00567 -0.0704 0.7187 0.3165
-6.750 -0.2991 0.01221 0.00549 -0.0678 0.7031 0.3228
-6.500 -0.2822 0.01209 0.00534 -0.0657 0.6897 0.3293
-6.250 -0.2658 0.01203 0.00520 -0.0634 0.6757 0.3352
-6.000 -0.2517 0.01188 0.00505 -0.0607 0.6626 0.3418
-5.750 -0.2367 0.01181 0.00492 -0.0581 0.6500 0.3480
-5.000 -0.1906 0.01156 0.00460 -0.0503 0.6150 0.3676
-4.750 -0.1751 0.01154 0.00452 -0.0477 0.6028 0.3739
-4.500 -0.1605 0.01144 0.00443 -0.0450 0.5925 0.3803
-4.250 -0.1467 0.01139 0.00435 -0.0420 0.5815 0.3873
-4.000 -0.1309 0.01136 0.00429 -0.0394 0.5707 0.3940
-3.750 -0.1184 0.01131 0.00422 -0.0362 0.5596 0.4006
-3.500 -0.1049 0.01127 0.00416 -0.0332 0.5502 0.4077
-3.250 -0.0897 0.01125 0.00412 -0.0304 0.5390 0.4148
-3.000 -0.0787 0.01123 0.00407 -0.0268 0.5286 0.4220
-2.750 -0.0661 0.01119 0.00403 -0.0236 0.5182 0.4296
-2.250 -0.0426 0.01118 0.00398 -0.0166 0.4985 0.4441
-2.000 -0.0339 0.01118 0.00397 -0.0125 0.4880 0.4517
-1.750 -0.0237 0.01119 0.00396 -0.0087 0.4798 0.4587
-1.500 -0.0155 0.01117 0.00395 -0.0044 0.4721 0.4658
-1.250 -0.0121 0.01119 0.00394 0.0008 0.4625 0.4742
-1.000 -0.0008 0.01119 0.00395 0.0044 0.4558 0.4821
-0.750 0.0067 0.01118 0.00395 0.0088 0.4480 0.4896
-0.500 0.0148 0.01121 0.00396 0.0130 0.4404 0.4982
0.000 0.0394 0.01123 0.00400 0.0197 0.4241 0.5156
0.250 0.0512 0.01127 0.00403 0.0231 0.4170 0.5247
0.500 0.0662 0.01128 0.00406 0.0259 0.4097 0.5332
0.750 0.0783 0.01132 0.00411 0.0292 0.4015 0.5431
1.250 0.1066 0.01139 0.00421 0.0350 0.3872 0.5628
1.500 0.1203 0.01146 0.00427 0.0379 0.3798 0.5734
1.750 0.1341 0.01151 0.00434 0.0408 0.3731 0.5837
2.000 0.1493 0.01156 0.00441 0.0434 0.3650 0.5954
2.250 0.1628 0.01165 0.00451 0.0463 0.3576 0.6059
2.500 0.1776 0.01171 0.00460 0.0490 0.3515 0.6184
2.750 0.1931 0.01179 0.00469 0.0515 0.3434 0.6291
3.000 0.2063 0.01190 0.00482 0.0544 0.3363 0.6417
3.250 0.2231 0.01197 0.00493 0.0566 0.3301 0.6535
3.500 0.2379 0.01207 0.00506 0.0591 0.3232 0.6675
3.750 0.2520 0.01221 0.00522 0.0617 0.3166 0.6802
4.000 0.2687 0.01230 0.00535 0.0638 0.3096 0.6954
4.250 0.2841 0.01243 0.00553 0.0661 0.3025 0.7092
4.750 0.3180 0.01271 0.00590 0.0701 0.2907 0.7400
5.000 0.3350 0.01288 0.00612 0.0719 0.2834 0.7567
5.250 0.3530 0.01308 0.00635 0.0735 0.2779 0.7735
5.500 0.3745 0.01324 0.00658 0.0744 0.2714 0.7919
5.750 0.3974 0.01347 0.00687 0.0749 0.2648 0.8103
6.000 0.4238 0.01371 0.00716 0.0747 0.2585 0.8270
6.250 0.4524 0.01396 0.00745 0.0740 0.2524 0.8437
6.500 0.4907 0.01432 0.00783 0.0711 0.2458 0.8596
6.750 0.5283 0.01459 0.00815 0.0685 0.2405 0.8730
7.000 0.5659 0.01495 0.00854 0.0658 0.2347 0.8869
7.250 0.6074 0.01544 0.00903 0.0622 0.2286 0.8978
7.500 0.6482 0.01586 0.00948 0.0588 0.2231 0.9071
7.750 0.6871 0.01640 0.01002 0.0558 0.2183 0.9150
8.000 0.7244 0.01702 0.01063 0.0529 0.2131 0.9207
8.250 0.7577 0.01753 0.01116 0.0510 0.2092 0.9270
8.500 0.7860 0.01811 0.01174 0.0500 0.2050 0.9335
8.750 0.8115 0.01878 0.01241 0.0493 0.2014 0.9389
9.250 0.8540 0.01995 0.01360 0.0498 0.1945 0.9532
9.500 0.8700 0.02062 0.01428 0.0509 0.1913 0.9617
9.750 0.8902 0.02139 0.01504 0.0508 0.1877 0.9668
10.000 0.9129 0.02212 0.01577 0.0504 0.1850 0.9714
10.500 0.9549 0.02360 0.01729 0.0502 0.1787 0.9801
10.750 0.9782 0.02452 0.01820 0.0491 0.1751 0.9827
11.000 1.0007 0.02542 0.01911 0.0482 0.1724 0.9855
11.250 1.0238 0.02625 0.01998 0.0474 0.1696 0.9884
11.500 1.0436 0.02727 0.02101 0.0469 0.1664 0.9912
11.750 1.0650 0.02836 0.02210 0.0458 0.1631 0.9934
12.000 1.0864 0.02947 0.02322 0.0445 0.1604 0.9956
12.250 1.1105 0.03042 0.02421 0.0431 0.1581 0.9976
12.500 1.1323 0.03162 0.02543 0.0417 0.1545 0.9992
12.750 1.1467 0.03290 0.02673 0.0414 0.1519 1.0000
13.000 1.1480 0.03429 0.02812 0.0433 0.1496 1.0000
13.250 1.1545 0.03538 0.02926 0.0447 0.1478 1.0000
13.500 1.1593 0.03667 0.03059 0.0461 0.1457 1.0000
13.750 1.1637 0.03806 0.03200 0.0474 0.1435 1.0000
14.000 1.1654 0.03972 0.03368 0.0487 0.1411 1.0000
14.250 1.1665 0.04149 0.03546 0.0498 0.1390 1.0000
14.500 1.1723 0.04293 0.03696 0.0507 0.1370 1.0000
14.750 1.1760 0.04459 0.03866 0.0515 0.1349 1.0000
15.000 1.1781 0.04644 0.04054 0.0523 0.1324 1.0000
15.250 1.1785 0.04850 0.04263 0.0530 0.1307 1.0000
15.500 1.1793 0.05057 0.04472 0.0536 0.1286 1.0000
15.750 1.1826 0.05247 0.04668 0.0540 0.1267 1.0000
16.000 1.1848 0.05450 0.04875 0.0544 0.1245 1.0000
16.250 1.1836 0.05693 0.05121 0.0547 0.1222 1.0000
16.500 1.1810 0.05953 0.05384 0.0548 0.1204 1.0000
16.750 1.1821 0.06182 0.05618 0.0550 0.1184 1.0000
17.000 1.1825 0.06421 0.05863 0.0550 0.1163 1.0000
17.250 1.1815 0.06677 0.06123 0.0549 0.1146 1.0000
17.500 1.1774 0.06973 0.06423 0.0547 0.1125 1.0000
17.750 1.1738 0.07266 0.06719 0.0544 0.1109 1.0000
18.000 1.1734 0.07531 0.06991 0.0541 0.1090 1.0000
18.250 1.1726 0.07800 0.07265 0.0538 0.1072 1.0000
18.500 1.1669 0.08131 0.07600 0.0532 0.1051 1.0000
18.750 1.1626 0.08448 0.07920 0.0526 0.1035 1.0000
19.000 1.1580 0.08774 0.08252 0.0519 0.1019 1.0000
19.250 1.1571 0.09055 0.08539 0.0513 0.1002 1.0000
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