NACA 16-015 (naca16015-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 16-015 (naca16015-il) Reynolds number: 500,000 Max Cl/Cd: 39.67 at α=10.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca16015-il-500000-n5.txt Download as CSV file: xf-naca16015-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 16-015
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
------ -------- --------- --------- -------- -------- --------
-19.000 -0.8458 0.12828 0.12548 -0.0481 1.0000 0.0080
-18.750 -0.9138 0.11017 0.10709 -0.0565 1.0000 0.0077
-18.500 -0.9535 0.09834 0.09505 -0.0621 1.0000 0.0076
-18.250 -0.9841 0.08882 0.08534 -0.0668 1.0000 0.0075
-18.000 -1.0119 0.08049 0.07684 -0.0706 1.0000 0.0075
-17.750 -1.0347 0.07371 0.06989 -0.0731 1.0000 0.0075
-17.500 -1.0540 0.06809 0.06410 -0.0745 1.0000 0.0075
-17.250 -1.0727 0.06313 0.05900 -0.0750 1.0000 0.0076
-17.000 -1.0903 0.05877 0.05449 -0.0747 1.0000 0.0076
-16.750 -1.1057 0.05506 0.05065 -0.0737 1.0000 0.0077
-16.500 -1.1190 0.05190 0.04736 -0.0721 1.0000 0.0078
-16.250 -1.1305 0.04914 0.04449 -0.0700 1.0000 0.0079
-16.000 -1.1398 0.04677 0.04201 -0.0676 1.0000 0.0080
-15.750 -1.1430 0.04446 0.03958 -0.0661 0.9996 0.0081
-15.500 -1.1396 0.04226 0.03724 -0.0655 0.9988 0.0083
-15.250 -1.1341 0.04029 0.03515 -0.0649 0.9979 0.0085
-15.000 -1.1268 0.03850 0.03323 -0.0644 0.9969 0.0087
-14.750 -1.1181 0.03684 0.03144 -0.0637 0.9960 0.0089
-14.500 -1.1083 0.03530 0.02977 -0.0631 0.9952 0.0092
-14.250 -1.0974 0.03388 0.02821 -0.0624 0.9945 0.0095
-14.000 -1.0867 0.03258 0.02678 -0.0613 0.9934 0.0098
-13.750 -1.0747 0.03142 0.02549 -0.0602 0.9920 0.0101
-13.500 -1.0631 0.03015 0.02412 -0.0592 0.9905 0.0105
-13.250 -1.0488 0.02904 0.02294 -0.0584 0.9892 0.0110
-13.000 -1.0322 0.02811 0.02194 -0.0579 0.9880 0.0115
-12.750 -1.0145 0.02725 0.02100 -0.0575 0.9871 0.0121
-12.500 -0.9962 0.02640 0.02004 -0.0571 0.9862 0.0127
-12.250 -0.9768 0.02556 0.01910 -0.0569 0.9855 0.0133
-12.000 -0.9567 0.02471 0.01817 -0.0568 0.9849 0.0140
-11.750 -0.9431 0.02404 0.01745 -0.0550 0.9819 0.0148
-11.500 -0.9240 0.02345 0.01683 -0.0544 0.9802 0.0157
-11.250 -0.9030 0.02289 0.01622 -0.0541 0.9789 0.0168
-11.000 -0.8809 0.02233 0.01557 -0.0540 0.9777 0.0179
-10.750 -0.8587 0.02168 0.01488 -0.0539 0.9767 0.0190
-10.500 -0.8342 0.02116 0.01434 -0.0543 0.9759 0.0203
-10.250 -0.8089 0.02067 0.01380 -0.0548 0.9752 0.0217
-10.000 -0.7832 0.02021 0.01327 -0.0553 0.9747 0.0231
-9.750 -0.7660 0.01988 0.01288 -0.0538 0.9718 0.0239
-9.500 -0.7488 0.01926 0.01223 -0.0525 0.9692 0.0255
-9.250 -0.7256 0.01879 0.01174 -0.0523 0.9676 0.0269
-9.000 -0.7010 0.01838 0.01128 -0.0525 0.9663 0.0284
-8.750 -0.6761 0.01797 0.01083 -0.0526 0.9652 0.0298
-8.500 -0.6505 0.01759 0.01039 -0.0529 0.9643 0.0308
-8.250 -0.6270 0.01701 0.00976 -0.0528 0.9633 0.0327
-8.000 -0.6015 0.01654 0.00928 -0.0531 0.9624 0.0345
-7.750 -0.5897 0.01629 0.00902 -0.0501 0.9576 0.0358
-7.500 -0.5680 0.01596 0.00865 -0.0494 0.9553 0.0374
-7.250 -0.5441 0.01562 0.00826 -0.0492 0.9536 0.0388
-7.000 -0.5197 0.01523 0.00784 -0.0490 0.9521 0.0409
-6.750 -0.4949 0.01483 0.00744 -0.0490 0.9508 0.0441
-6.500 -0.4692 0.01448 0.00708 -0.0491 0.9497 0.0474
-6.250 -0.4525 0.01426 0.00685 -0.0471 0.9462 0.0514
-6.000 -0.4346 0.01399 0.00661 -0.0454 0.9427 0.0592
-5.750 -0.4131 0.01364 0.00632 -0.0446 0.9403 0.0731
-5.500 -0.3906 0.01326 0.00602 -0.0439 0.9384 0.0920
-5.250 -0.3671 0.01288 0.00571 -0.0435 0.9369 0.1151
-5.000 -0.3437 0.01246 0.00541 -0.0432 0.9354 0.1447
-4.750 -0.3310 0.01218 0.00526 -0.0403 0.9311 0.1753
-4.500 -0.3164 0.01181 0.00505 -0.0379 0.9274 0.2164
-4.250 -0.2999 0.01130 0.00476 -0.0360 0.9247 0.2740
-4.000 -0.2836 0.01071 0.00444 -0.0341 0.9224 0.3425
-3.750 -0.2713 0.00999 0.00406 -0.0313 0.9202 0.4277
-3.500 -0.2798 0.00962 0.00396 -0.0235 0.9129 0.4944
-3.250 -0.2851 0.00895 0.00364 -0.0163 0.9084 0.5805
-3.000 -0.2894 0.00834 0.00343 -0.0092 0.9049 0.6725
-2.750 -0.2913 0.00821 0.00352 -0.0024 0.8984 0.7249
-2.500 -0.2692 0.00809 0.00355 -0.0011 0.8960 0.7672
-2.250 -0.2412 0.00805 0.00359 -0.0012 0.8944 0.7962
-2.000 -0.2127 0.00809 0.00369 -0.0012 0.8929 0.8225
-1.750 -0.1819 0.00821 0.00384 -0.0018 0.8917 0.8415
-1.500 -0.1638 0.00834 0.00398 0.0004 0.8880 0.8513
-1.250 -0.1399 0.00842 0.00405 0.0012 0.8846 0.8566
-1.000 -0.1212 0.00836 0.00396 0.0031 0.8814 0.8627
-0.750 -0.0854 0.00838 0.00397 0.0011 0.8800 0.8645
-0.500 -0.0505 0.00838 0.00396 -0.0008 0.8786 0.8664
-0.250 -0.0164 0.00836 0.00394 -0.0024 0.8773 0.8686
0.000 -0.0001 0.00840 0.00399 0.0000 0.8728 0.8729
0.250 0.0164 0.00836 0.00394 0.0024 0.8686 0.8773
0.500 0.0505 0.00838 0.00396 0.0008 0.8664 0.8786
0.750 0.0854 0.00838 0.00397 -0.0011 0.8645 0.8800
1.000 0.1212 0.00836 0.00396 -0.0031 0.8627 0.8814
1.250 0.1399 0.00842 0.00405 -0.0012 0.8566 0.8846
1.500 0.1638 0.00834 0.00398 -0.0004 0.8513 0.8880
1.750 0.1820 0.00821 0.00385 0.0018 0.8416 0.8917
2.000 0.2127 0.00809 0.00369 0.0012 0.8225 0.8929
2.250 0.2412 0.00805 0.00359 0.0012 0.7960 0.8944
2.500 0.2692 0.00809 0.00355 0.0011 0.7667 0.8960
2.750 0.2914 0.00821 0.00353 0.0024 0.7255 0.8984
3.000 0.2894 0.00834 0.00343 0.0092 0.6728 0.9049
3.250 0.2859 0.00894 0.00364 0.0162 0.5821 0.9083
3.500 0.2799 0.00962 0.00396 0.0235 0.4942 0.9129
3.750 0.2713 0.01000 0.00406 0.0313 0.4268 0.9202
4.000 0.2836 0.01071 0.00444 0.0341 0.3418 0.9224
4.250 0.3000 0.01130 0.00476 0.0360 0.2736 0.9247
4.500 0.3167 0.01180 0.00505 0.0379 0.2171 0.9274
4.750 0.3311 0.01218 0.00525 0.0403 0.1749 0.9311
5.000 0.3439 0.01246 0.00541 0.0431 0.1449 0.9354
5.250 0.3674 0.01287 0.00571 0.0435 0.1151 0.9369
5.500 0.3909 0.01326 0.00601 0.0439 0.0919 0.9384
5.750 0.4133 0.01364 0.00631 0.0445 0.0730 0.9403
6.000 0.4349 0.01398 0.00660 0.0453 0.0593 0.9427
6.250 0.4528 0.01426 0.00685 0.0470 0.0515 0.9462
6.500 0.4696 0.01447 0.00708 0.0490 0.0474 0.9497
6.750 0.4953 0.01482 0.00744 0.0489 0.0441 0.9508
7.000 0.5201 0.01523 0.00784 0.0489 0.0409 0.9521
7.250 0.5445 0.01562 0.00825 0.0491 0.0388 0.9536
7.500 0.5684 0.01596 0.00864 0.0493 0.0374 0.9554
7.750 0.5901 0.01629 0.00901 0.0500 0.0358 0.9576
8.000 0.6021 0.01653 0.00928 0.0530 0.0344 0.9624
8.250 0.6275 0.01700 0.00976 0.0527 0.0326 0.9633
8.500 0.6511 0.01759 0.01038 0.0528 0.0308 0.9643
8.750 0.6767 0.01796 0.01082 0.0525 0.0298 0.9653
9.000 0.7016 0.01837 0.01127 0.0524 0.0284 0.9664
9.250 0.7262 0.01879 0.01173 0.0522 0.0269 0.9677
9.500 0.7493 0.01926 0.01222 0.0523 0.0255 0.9693
9.750 0.7661 0.01987 0.01286 0.0537 0.0239 0.9720
10.000 0.7840 0.02021 0.01326 0.0551 0.0231 0.9747
10.250 0.8098 0.02067 0.01379 0.0546 0.0217 0.9753
10.500 0.8351 0.02115 0.01433 0.0541 0.0203 0.9759
10.750 0.8596 0.02167 0.01486 0.0538 0.0190 0.9768
11.000 0.8818 0.02232 0.01556 0.0538 0.0179 0.9778
11.250 0.9039 0.02289 0.01621 0.0539 0.0168 0.9789
11.500 0.9249 0.02344 0.01683 0.0542 0.0157 0.9803
11.750 0.9441 0.02402 0.01744 0.0548 0.0147 0.9821
12.000 0.9581 0.02470 0.01816 0.0565 0.0140 0.9849
12.250 0.9782 0.02555 0.01909 0.0566 0.0133 0.9856
12.500 0.9976 0.02639 0.02003 0.0568 0.0127 0.9863
12.750 1.0159 0.02724 0.02098 0.0572 0.0121 0.9872
13.000 1.0337 0.02810 0.02193 0.0576 0.0115 0.9881
13.250 1.0503 0.02902 0.02292 0.0581 0.0110 0.9893
13.500 1.0645 0.03014 0.02411 0.0589 0.0105 0.9906
13.750 1.0764 0.03138 0.02546 0.0599 0.0101 0.9921
14.000 1.0883 0.03256 0.02676 0.0610 0.0098 0.9935
14.250 1.0992 0.03386 0.02819 0.0620 0.0095 0.9946
14.500 1.1103 0.03528 0.02975 0.0627 0.0092 0.9953
14.750 1.1201 0.03682 0.03142 0.0634 0.0089 0.9961
15.000 1.1289 0.03847 0.03320 0.0640 0.0087 0.9971
15.250 1.1363 0.04027 0.03512 0.0646 0.0085 0.9980
15.500 1.1419 0.04223 0.03721 0.0652 0.0083 0.9990
15.750 1.1454 0.04444 0.03955 0.0657 0.0081 0.9998
16.000 1.1407 0.04666 0.04189 0.0676 0.0080 1.0000
16.250 1.1312 0.04904 0.04438 0.0700 0.0079 1.0000
16.500 1.1201 0.05175 0.04721 0.0721 0.0078 1.0000
16.750 1.1066 0.05494 0.05052 0.0737 0.0077 1.0000
17.000 1.0914 0.05863 0.05435 0.0747 0.0076 1.0000
17.250 1.0739 0.06298 0.05884 0.0750 0.0076 1.0000
17.500 1.0557 0.06789 0.06389 0.0745 0.0075 1.0000
17.750 1.0365 0.07349 0.06966 0.0731 0.0075 1.0000
18.000 1.0135 0.08031 0.07665 0.0705 0.0075 1.0000
18.250 0.9860 0.08861 0.08512 0.0667 0.0075 1.0000
18.500 0.9549 0.09826 0.09498 0.0620 0.0076 1.0000
18.750 0.9156 0.11005 0.10697 0.0563 0.0077 1.0000
19.000 0.8479 0.12811 0.12531 0.0480 0.0080 1.0000
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