NACA 16-015 (naca16015-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 16-015 (naca16015-il) Reynolds number: 1,000,000 Max Cl/Cd: 50.55 at α=10.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca16015-il-1000000-n5.txt Download as CSV file: xf-naca16015-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1066 0.08681 0.08379 -0.0692 1.0000 0.0049
-19.500 -1.1393 0.07796 0.07475 -0.0732 1.0000 0.0048
-19.250 -1.1638 0.07116 0.06779 -0.0757 1.0000 0.0048
-19.000 -1.1830 0.06571 0.06220 -0.0770 1.0000 0.0049
-18.750 -1.1993 0.06111 0.05747 -0.0774 1.0000 0.0049
-18.500 -1.2129 0.05719 0.05342 -0.0772 1.0000 0.0049
-18.250 -1.2247 0.05381 0.04993 -0.0764 1.0000 0.0050
-18.000 -1.2352 0.05083 0.04684 -0.0750 1.0000 0.0050
-17.750 -1.2366 0.04789 0.04378 -0.0752 0.9996 0.0051
-17.500 -1.2357 0.04523 0.04099 -0.0752 0.9990 0.0052
-17.250 -1.2330 0.04282 0.03847 -0.0750 0.9984 0.0052
-17.000 -1.2285 0.04068 0.03621 -0.0748 0.9977 0.0053
-16.750 -1.2231 0.03871 0.03414 -0.0743 0.9971 0.0054
-16.500 -1.2158 0.03696 0.03229 -0.0738 0.9964 0.0054
-16.250 -1.2096 0.03517 0.03038 -0.0731 0.9958 0.0056
-16.000 -1.2024 0.03347 0.02858 -0.0724 0.9953 0.0058
-15.750 -1.1924 0.03200 0.02703 -0.0718 0.9948 0.0060
-15.500 -1.1803 0.03069 0.02564 -0.0713 0.9943 0.0061
-15.250 -1.1693 0.02953 0.02441 -0.0702 0.9932 0.0064
-15.000 -1.1572 0.02845 0.02325 -0.0692 0.9920 0.0065
-14.750 -1.1437 0.02745 0.02217 -0.0684 0.9910 0.0068
-14.500 -1.1286 0.02649 0.02114 -0.0678 0.9899 0.0070
-14.250 -1.1124 0.02557 0.02014 -0.0672 0.9890 0.0072
-14.000 -1.0949 0.02472 0.01920 -0.0668 0.9882 0.0074
-13.750 -1.0767 0.02392 0.01834 -0.0665 0.9875 0.0075
-13.500 -1.0592 0.02303 0.01738 -0.0660 0.9869 0.0079
-13.250 -1.0400 0.02223 0.01654 -0.0658 0.9863 0.0083
-13.000 -1.0198 0.02150 0.01576 -0.0657 0.9857 0.0088
-12.750 -0.9988 0.02083 0.01503 -0.0656 0.9851 0.0092
-12.500 -0.9817 0.02025 0.01439 -0.0645 0.9832 0.0097
-12.250 -0.9635 0.01970 0.01379 -0.0636 0.9813 0.0101
-12.000 -0.9443 0.01911 0.01316 -0.0629 0.9796 0.0107
-11.750 -0.9236 0.01854 0.01257 -0.0625 0.9782 0.0117
-11.500 -0.9021 0.01801 0.01202 -0.0622 0.9769 0.0125
-11.250 -0.8803 0.01752 0.01149 -0.0619 0.9758 0.0133
-11.000 -0.8584 0.01704 0.01097 -0.0616 0.9747 0.0143
-10.750 -0.8391 0.01663 0.01055 -0.0607 0.9726 0.0156
-10.500 -0.8197 0.01625 0.01016 -0.0597 0.9700 0.0168
-10.250 -0.7987 0.01589 0.00977 -0.0590 0.9678 0.0179
-10.000 -0.7775 0.01550 0.00937 -0.0583 0.9659 0.0193
-9.750 -0.7555 0.01514 0.00901 -0.0578 0.9643 0.0208
-9.500 -0.7325 0.01481 0.00865 -0.0575 0.9627 0.0221
-9.250 -0.7118 0.01453 0.00834 -0.0566 0.9603 0.0230
-9.000 -0.6906 0.01428 0.00806 -0.0558 0.9576 0.0237
-8.750 -0.6699 0.01395 0.00770 -0.0549 0.9553 0.0248
-8.500 -0.6488 0.01360 0.00734 -0.0540 0.9530 0.0262
-8.250 -0.6266 0.01329 0.00700 -0.0534 0.9510 0.0274
-8.000 -0.6035 0.01300 0.00670 -0.0530 0.9492 0.0285
-7.750 -0.5821 0.01277 0.00645 -0.0521 0.9467 0.0296
-7.500 -0.5602 0.01255 0.00621 -0.0513 0.9440 0.0304
-7.250 -0.5377 0.01233 0.00595 -0.0507 0.9414 0.0310
-7.000 -0.5160 0.01202 0.00563 -0.0498 0.9390 0.0328
-6.750 -0.4932 0.01175 0.00535 -0.0492 0.9369 0.0347
-6.500 -0.4698 0.01150 0.00509 -0.0487 0.9350 0.0367
-6.250 -0.4477 0.01130 0.00489 -0.0479 0.9323 0.0384
-6.000 -0.4253 0.01110 0.00468 -0.0472 0.9295 0.0410
-5.750 -0.4031 0.01086 0.00447 -0.0464 0.9269 0.0462
-5.500 -0.3805 0.01062 0.00426 -0.0456 0.9244 0.0546
-5.250 -0.3580 0.01034 0.00403 -0.0449 0.9221 0.0689
-5.000 -0.3353 0.01007 0.00382 -0.0443 0.9198 0.0859
-4.750 -0.3144 0.00983 0.00366 -0.0432 0.9170 0.1036
-4.500 -0.2934 0.00958 0.00349 -0.0421 0.9140 0.1256
-4.250 -0.2725 0.00930 0.00331 -0.0410 0.9111 0.1525
-4.000 -0.2514 0.00900 0.00312 -0.0400 0.9085 0.1853
-3.750 -0.2308 0.00865 0.00291 -0.0388 0.9060 0.2277
-3.500 -0.2141 0.00828 0.00275 -0.0369 0.9028 0.2812
-3.250 -0.2007 0.00781 0.00255 -0.0342 0.8989 0.3521
-3.000 -0.1887 0.00730 0.00234 -0.0311 0.8953 0.4296
-2.750 -0.1770 0.00680 0.00210 -0.0279 0.8920 0.5040
-2.500 -0.1720 0.00636 0.00193 -0.0231 0.8877 0.5753
-2.250 -0.1748 0.00599 0.00181 -0.0163 0.8824 0.6419
-2.000 -0.1722 0.00565 0.00169 -0.0106 0.8782 0.7051
-1.750 -0.1627 0.00544 0.00166 -0.0065 0.8746 0.7544
-1.500 -0.1489 0.00533 0.00170 -0.0033 0.8706 0.7915
-1.250 -0.1291 0.00529 0.00173 -0.0015 0.8673 0.8160
-1.000 -0.1049 0.00528 0.00174 -0.0007 0.8646 0.8313
-0.750 -0.0757 0.00528 0.00175 -0.0012 0.8623 0.8389
-0.500 -0.0536 0.00529 0.00177 -0.0001 0.8589 0.8451
-0.250 -0.0288 0.00529 0.00177 0.0004 0.8554 0.8494
0.000 0.0000 0.00529 0.00178 0.0000 0.8523 0.8523
0.250 0.0288 0.00529 0.00177 -0.0004 0.8494 0.8554
0.500 0.0536 0.00529 0.00177 0.0001 0.8451 0.8589
0.750 0.0757 0.00528 0.00175 0.0012 0.8389 0.8623
1.000 0.1049 0.00528 0.00174 0.0007 0.8313 0.8645
1.250 0.1291 0.00529 0.00173 0.0015 0.8161 0.8673
1.500 0.1488 0.00533 0.00170 0.0033 0.7913 0.8706
1.750 0.1631 0.00543 0.00166 0.0064 0.7558 0.8746
2.000 0.1717 0.00565 0.00169 0.0107 0.7036 0.8783
2.250 0.1758 0.00598 0.00180 0.0161 0.6436 0.8823
2.500 0.1716 0.00637 0.00193 0.0232 0.5736 0.8877
2.750 0.1775 0.00679 0.00209 0.0278 0.5054 0.8919
3.000 0.1889 0.00730 0.00234 0.0311 0.4296 0.8953
3.250 0.2011 0.00780 0.00255 0.0341 0.3532 0.8989
3.500 0.2142 0.00828 0.00275 0.0368 0.2807 0.9028
3.750 0.2310 0.00865 0.00291 0.0388 0.2274 0.9060
4.000 0.2515 0.00900 0.00312 0.0399 0.1847 0.9085
4.250 0.2727 0.00930 0.00331 0.0410 0.1523 0.9110
4.500 0.2938 0.00957 0.00348 0.0420 0.1263 0.9140
4.750 0.3146 0.00984 0.00366 0.0431 0.1032 0.9170
5.000 0.3356 0.01007 0.00382 0.0442 0.0858 0.9198
5.250 0.3583 0.01034 0.00403 0.0449 0.0687 0.9221
5.500 0.3809 0.01062 0.00425 0.0456 0.0545 0.9244
5.750 0.4035 0.01086 0.00447 0.0463 0.0462 0.9269
6.000 0.4257 0.01110 0.00468 0.0471 0.0410 0.9295
6.250 0.4482 0.01130 0.00488 0.0478 0.0384 0.9323
6.500 0.4703 0.01150 0.00509 0.0486 0.0367 0.9349
6.750 0.4938 0.01175 0.00535 0.0491 0.0348 0.9369
7.000 0.5166 0.01202 0.00563 0.0497 0.0328 0.9389
7.250 0.5383 0.01233 0.00595 0.0505 0.0309 0.9414
7.500 0.5609 0.01255 0.00620 0.0512 0.0303 0.9440
7.750 0.5828 0.01277 0.00645 0.0520 0.0296 0.9467
8.000 0.6042 0.01300 0.00670 0.0528 0.0286 0.9492
8.250 0.6273 0.01328 0.00700 0.0533 0.0273 0.9510
8.500 0.6496 0.01360 0.00734 0.0539 0.0262 0.9530
8.750 0.6706 0.01395 0.00770 0.0547 0.0248 0.9552
9.000 0.6915 0.01428 0.00805 0.0556 0.0237 0.9576
9.250 0.7127 0.01453 0.00834 0.0564 0.0230 0.9602
9.500 0.7334 0.01481 0.00864 0.0573 0.0220 0.9627
9.750 0.7564 0.01514 0.00900 0.0576 0.0207 0.9642
10.000 0.7784 0.01549 0.00936 0.0581 0.0193 0.9659
10.250 0.7997 0.01588 0.00976 0.0588 0.0179 0.9677
10.500 0.8207 0.01625 0.01016 0.0595 0.0168 0.9700
10.750 0.8401 0.01662 0.01054 0.0605 0.0155 0.9726
11.000 0.8594 0.01704 0.01096 0.0614 0.0142 0.9747
11.250 0.8814 0.01752 0.01148 0.0617 0.0133 0.9758
11.500 0.9033 0.01801 0.01201 0.0620 0.0125 0.9770
11.750 0.9248 0.01853 0.01256 0.0623 0.0116 0.9783
12.000 0.9455 0.01910 0.01315 0.0627 0.0107 0.9797
12.250 0.9648 0.01969 0.01378 0.0634 0.0101 0.9813
12.500 0.9828 0.02024 0.01438 0.0643 0.0096 0.9833
12.750 1.0003 0.02082 0.01502 0.0653 0.0092 0.9851
13.000 1.0213 0.02149 0.01575 0.0654 0.0088 0.9857
13.250 1.0416 0.02222 0.01652 0.0655 0.0084 0.9863
13.500 1.0608 0.02303 0.01738 0.0657 0.0079 0.9869
13.750 1.0785 0.02391 0.01832 0.0661 0.0075 0.9876
14.000 1.0967 0.02471 0.01919 0.0665 0.0074 0.9883
14.250 1.1142 0.02555 0.02012 0.0669 0.0072 0.9891
14.500 1.1305 0.02647 0.02112 0.0674 0.0070 0.9901
14.750 1.1457 0.02742 0.02215 0.0680 0.0067 0.9911
15.000 1.1591 0.02843 0.02324 0.0689 0.0066 0.9922
15.250 1.1714 0.02950 0.02437 0.0699 0.0063 0.9934
15.500 1.1828 0.03068 0.02562 0.0708 0.0062 0.9944
15.750 1.1951 0.03198 0.02700 0.0713 0.0059 0.9949
16.000 1.2051 0.03345 0.02855 0.0719 0.0057 0.9954
16.250 1.2120 0.03516 0.03037 0.0727 0.0055 0.9959
16.500 1.2187 0.03692 0.03224 0.0733 0.0054 0.9966
16.750 1.2260 0.03867 0.03409 0.0738 0.0054 0.9972
17.000 1.2316 0.04061 0.03614 0.0743 0.0053 0.9979
17.250 1.2360 0.04276 0.03841 0.0745 0.0052 0.9985
17.500 1.2391 0.04514 0.04091 0.0747 0.0051 0.9992
17.750 1.2401 0.04782 0.04370 0.0746 0.0051 0.9997
18.000 1.2363 0.05067 0.04668 0.0750 0.0050 1.0000
18.250 1.2263 0.05360 0.04972 0.0764 0.0050 1.0000
18.500 1.2149 0.05695 0.05318 0.0772 0.0049 1.0000
18.750 1.2011 0.06088 0.05724 0.0774 0.0049 1.0000
19.000 1.1854 0.06542 0.06190 0.0770 0.0049 1.0000
19.250 1.1665 0.07083 0.06746 0.0756 0.0048 1.0000
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