NASA/LANGLEY NLF(1)-0416 AIRFOIL (nlf416-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA/LANGLEY NLF(1)-0416 AIRFOIL (nlf416-il) Reynolds number: 1,000,000 Max Cl/Cd: 108.37 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-nlf416-il-1000000-n5.txt Download as CSV file: xf-nlf416-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NASA/LANGLEY NLF(1)-0416 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-18.500 -0.7425 0.13733 0.13491 -0.0255 1.0000 0.0054
-18.250 -0.7673 0.12784 0.12530 -0.0302 1.0000 0.0054
-18.000 -0.7966 0.11786 0.11521 -0.0352 1.0000 0.0055
-17.750 -0.8168 0.10992 0.10716 -0.0391 1.0000 0.0055
-17.500 -0.8366 0.10226 0.09939 -0.0430 1.0000 0.0055
-17.250 -0.8570 0.09467 0.09169 -0.0468 1.0000 0.0054
-17.000 -0.8742 0.08782 0.08473 -0.0503 1.0000 0.0054
-16.750 -0.8924 0.08094 0.07774 -0.0539 1.0000 0.0054
-16.500 -0.9087 0.07457 0.07125 -0.0572 1.0000 0.0054
-16.250 -0.9240 0.06855 0.06511 -0.0603 1.0000 0.0054
-16.000 -0.9330 0.06367 0.06012 -0.0627 1.0000 0.0054
-15.750 -0.9447 0.05863 0.05496 -0.0651 1.0000 0.0054
-15.500 -0.9558 0.05393 0.05014 -0.0671 1.0000 0.0054
-15.250 -0.9695 0.04922 0.04530 -0.0688 1.0000 0.0056
-15.000 -0.9740 0.04592 0.04191 -0.0696 1.0000 0.0055
-14.750 -0.9761 0.04315 0.03904 -0.0700 1.0000 0.0055
-14.500 -0.9837 0.04008 0.03588 -0.0701 1.0000 0.0056
-14.250 -0.9844 0.03787 0.03360 -0.0697 1.0000 0.0057
-14.000 -0.9867 0.03568 0.03132 -0.0690 1.0000 0.0056
-13.750 -0.9859 0.03387 0.02945 -0.0681 1.0000 0.0057
-13.500 -0.9854 0.03215 0.02767 -0.0670 1.0000 0.0058
-13.250 -0.9833 0.03065 0.02610 -0.0656 1.0000 0.0058
-13.000 -0.9826 0.02915 0.02454 -0.0640 1.0000 0.0058
-12.750 -0.9685 0.02771 0.02304 -0.0647 0.9992 0.0059
-12.500 -0.9434 0.02629 0.02155 -0.0672 0.9972 0.0060
-12.250 -0.9187 0.02491 0.02011 -0.0695 0.9950 0.0061
-12.000 -0.8952 0.02379 0.01893 -0.0712 0.9930 0.0062
-11.750 -0.8779 0.02272 0.01781 -0.0715 0.9903 0.0062
-11.500 -0.8583 0.02166 0.01670 -0.0722 0.9873 0.0063
-11.250 -0.8344 0.02075 0.01574 -0.0735 0.9847 0.0064
-11.000 -0.8162 0.01982 0.01476 -0.0736 0.9807 0.0065
-10.750 -0.7964 0.01886 0.01376 -0.0739 0.9750 0.0066
-10.500 -0.7699 0.01801 0.01285 -0.0753 0.9707 0.0068
-10.000 -0.7310 0.01655 0.01130 -0.0746 0.9524 0.0070
-9.750 -0.6997 0.01586 0.01057 -0.0763 0.9438 0.0072
-9.500 -0.6567 0.01520 0.00986 -0.0801 0.9336 0.0074
-9.250 -0.5877 0.01429 0.00886 -0.0895 0.9189 0.0078
-9.000 -0.5352 0.01363 0.00804 -0.0954 0.8784 0.0082
-8.750 -0.5123 0.01339 0.00757 -0.0950 0.8295 0.0083
-8.500 -0.4925 0.01317 0.00718 -0.0939 0.7903 0.0086
-8.250 -0.4717 0.01295 0.00681 -0.0929 0.7564 0.0089
-8.000 -0.4498 0.01274 0.00646 -0.0921 0.7263 0.0091
-7.750 -0.4266 0.01253 0.00612 -0.0916 0.6994 0.0094
-7.500 -0.4026 0.01233 0.00581 -0.0912 0.6769 0.0098
-7.250 -0.3777 0.01209 0.00548 -0.0909 0.6574 0.0102
-7.000 -0.3524 0.01185 0.00517 -0.0907 0.6405 0.0108
-6.750 -0.3264 0.01164 0.00489 -0.0906 0.6251 0.0115
-6.500 -0.2999 0.01146 0.00464 -0.0906 0.6109 0.0124
-6.250 -0.2731 0.01125 0.00439 -0.0906 0.5980 0.0139
-6.000 -0.2461 0.01105 0.00415 -0.0907 0.5861 0.0165
-5.750 -0.2191 0.01084 0.00392 -0.0908 0.5743 0.0214
-5.500 -0.1915 0.01061 0.00368 -0.0910 0.5638 0.0294
-5.250 -0.1638 0.01035 0.00345 -0.0912 0.5551 0.0428
-5.000 -0.1358 0.01008 0.00323 -0.0916 0.5468 0.0604
-4.750 -0.1076 0.00984 0.00304 -0.0919 0.5395 0.0800
-4.500 -0.0789 0.00959 0.00285 -0.0924 0.5327 0.1030
-4.250 -0.0502 0.00931 0.00267 -0.0929 0.5256 0.1351
-4.000 -0.0210 0.00897 0.00248 -0.0936 0.5194 0.1793
-3.750 0.0086 0.00857 0.00229 -0.0944 0.5132 0.2402
-3.250 0.0684 0.00799 0.00200 -0.0959 0.5030 0.3410
-3.000 0.0983 0.00779 0.00189 -0.0965 0.4977 0.3770
-2.750 0.1283 0.00760 0.00179 -0.0972 0.4925 0.4199
-2.500 0.1584 0.00742 0.00170 -0.0978 0.4882 0.4601
-2.250 0.1886 0.00725 0.00163 -0.0984 0.4839 0.4988
-2.000 0.2185 0.00712 0.00160 -0.0990 0.4792 0.5381
-1.750 0.2480 0.00709 0.00164 -0.0993 0.4748 0.5752
-1.500 0.2774 0.00713 0.00169 -0.0996 0.4710 0.5953
-1.250 0.3068 0.00717 0.00173 -0.0998 0.4672 0.6067
-1.000 0.3360 0.00724 0.00175 -0.1000 0.4629 0.6155
-0.750 0.3649 0.00731 0.00180 -0.1001 0.4587 0.6210
-0.500 0.3940 0.00738 0.00184 -0.1003 0.4550 0.6262
-0.250 0.4233 0.00744 0.00186 -0.1005 0.4515 0.6305
0.000 0.4524 0.00750 0.00190 -0.1007 0.4475 0.6340
0.250 0.4812 0.00757 0.00196 -0.1008 0.4435 0.6373
0.500 0.5099 0.00767 0.00202 -0.1009 0.4393 0.6405
0.750 0.5391 0.00772 0.00207 -0.1011 0.4360 0.6433
1.000 0.5681 0.00779 0.00211 -0.1013 0.4317 0.6459
1.250 0.5970 0.00788 0.00216 -0.1014 0.4273 0.6480
1.500 0.6254 0.00796 0.00222 -0.1015 0.4229 0.6503
1.750 0.6542 0.00801 0.00229 -0.1017 0.4191 0.6524
2.000 0.6829 0.00808 0.00236 -0.1018 0.4146 0.6545
2.250 0.7113 0.00818 0.00243 -0.1019 0.4096 0.6562
2.500 0.7398 0.00826 0.00250 -0.1020 0.4052 0.6578
2.750 0.7685 0.00833 0.00257 -0.1021 0.4002 0.6593
3.000 0.7968 0.00843 0.00265 -0.1022 0.3942 0.6609
3.250 0.8250 0.00854 0.00273 -0.1022 0.3884 0.6627
3.500 0.8533 0.00864 0.00282 -0.1023 0.3814 0.6642
3.750 0.8810 0.00876 0.00291 -0.1023 0.3735 0.6653
4.000 0.9090 0.00885 0.00299 -0.1024 0.3652 0.6663
4.250 0.9365 0.00898 0.00310 -0.1023 0.3565 0.6673
4.500 0.9638 0.00913 0.00322 -0.1023 0.3457 0.6682
4.750 0.9911 0.00928 0.00334 -0.1022 0.3353 0.6690
5.000 1.0178 0.00947 0.00349 -0.1021 0.3235 0.6697
5.250 1.0442 0.00968 0.00366 -0.1019 0.3114 0.6704
5.500 1.0706 0.00990 0.00383 -0.1017 0.2990 0.6711
5.750 1.0967 0.01012 0.00402 -0.1015 0.2864 0.6719
6.000 1.1226 0.01037 0.00423 -0.1012 0.2740 0.6726
6.250 1.1480 0.01064 0.00445 -0.1009 0.2611 0.6735
6.500 1.1732 0.01093 0.00468 -0.1005 0.2487 0.6744
6.750 1.1983 0.01121 0.00493 -0.1001 0.2369 0.6754
7.000 1.2233 0.01148 0.00517 -0.0997 0.2252 0.6762
7.250 1.2479 0.01179 0.00543 -0.0993 0.2136 0.6769
7.500 1.2720 0.01211 0.00572 -0.0988 0.2025 0.6776
7.750 1.2958 0.01245 0.00601 -0.0982 0.1916 0.6783
8.000 1.3198 0.01276 0.00630 -0.0976 0.1815 0.6790
8.250 1.3429 0.01311 0.00662 -0.0970 0.1714 0.6797
8.500 1.3651 0.01351 0.00697 -0.0962 0.1604 0.6803
8.750 1.3876 0.01388 0.00731 -0.0954 0.1509 0.6809
9.000 1.4095 0.01425 0.00767 -0.0945 0.1422 0.6815
9.250 1.4301 0.01469 0.00807 -0.0935 0.1329 0.6825
9.500 1.4512 0.01506 0.00845 -0.0925 0.1253 0.6834
9.750 1.4707 0.01550 0.00887 -0.0913 0.1173 0.6843
10.000 1.4882 0.01603 0.00936 -0.0898 0.1077 0.6852
10.250 1.5040 0.01653 0.00984 -0.0879 0.0986 0.6861
10.500 1.5169 0.01707 0.01036 -0.0856 0.0897 0.6871
10.750 1.5289 0.01768 0.01095 -0.0832 0.0819 0.6882
11.000 1.5412 0.01829 0.01155 -0.0808 0.0753 0.6893
11.250 1.5540 0.01889 0.01215 -0.0787 0.0704 0.6904
11.500 1.5646 0.01960 0.01287 -0.0763 0.0648 0.6914
11.750 1.5756 0.02031 0.01359 -0.0741 0.0607 0.6923
12.000 1.5853 0.02110 0.01441 -0.0718 0.0564 0.6933
12.250 1.5937 0.02200 0.01532 -0.0696 0.0527 0.6943
12.500 1.6021 0.02295 0.01630 -0.0674 0.0492 0.6952
12.750 1.6070 0.02415 0.01751 -0.0651 0.0456 0.6961
13.000 1.6137 0.02533 0.01874 -0.0632 0.0424 0.6969
13.250 1.6171 0.02682 0.02025 -0.0613 0.0394 0.6977
13.500 1.6217 0.02834 0.02182 -0.0597 0.0369 0.6988
13.750 1.6249 0.03007 0.02361 -0.0583 0.0345 0.7000
14.000 1.6263 0.03210 0.02570 -0.0571 0.0323 0.7011
14.250 1.6290 0.03417 0.02783 -0.0562 0.0303 0.7023
14.500 1.6289 0.03661 0.03033 -0.0555 0.0282 0.7034
14.750 1.6288 0.03920 0.03298 -0.0550 0.0263 0.7046
15.000 1.6283 0.04196 0.03582 -0.0548 0.0246 0.7057
15.250 1.6246 0.04516 0.03907 -0.0547 0.0227 0.7069
15.500 1.6236 0.04818 0.04218 -0.0548 0.0214 0.7080
15.750 1.6198 0.05161 0.04567 -0.0551 0.0198 0.7091
16.000 1.6151 0.05524 0.04938 -0.0556 0.0187 0.7102
16.250 1.6120 0.05879 0.05300 -0.0561 0.0176 0.7112
16.500 1.6070 0.06266 0.05694 -0.0569 0.0165 0.7123
17.000 1.5965 0.07077 0.06521 -0.0588 0.0146 0.7142
17.250 1.5911 0.07501 0.06954 -0.0600 0.0137 0.7156
17.500 1.5847 0.07947 0.07409 -0.0614 0.0130 0.7169
17.750 1.5789 0.08395 0.07866 -0.0628 0.0123 0.7181
18.000 1.5743 0.08832 0.08312 -0.0643 0.0118 0.7195
18.250 1.5685 0.09299 0.08788 -0.0660 0.0112 0.7207
18.500 1.5616 0.09788 0.09286 -0.0679 0.0107 0.7220
18.750 1.5544 0.10290 0.09797 -0.0700 0.0103 0.7232
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