NACA 64-215 AIRFOIL (n64215-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 64-215 AIRFOIL (n64215-il) Reynolds number: 1,000,000 Max Cl/Cd: 79.32 at α=3.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-n64215-il-1000000-n5.txt Download as CSV file: xf-n64215-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 64-215 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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0763 0.10913 0.10629 -0.0234 1.0000 0.0106
-19.500 -1.1001 0.10061 0.09763 -0.0283 1.0000 0.0106
-19.250 -1.1193 0.09314 0.09002 -0.0325 1.0000 0.0107
-19.000 -1.1397 0.08578 0.08251 -0.0366 1.0000 0.0106
-18.750 -1.1513 0.08012 0.07674 -0.0396 1.0000 0.0107
-18.500 -1.1625 0.07471 0.07121 -0.0424 1.0000 0.0108
-18.250 -1.1677 0.07040 0.06679 -0.0445 1.0000 0.0109
-18.000 -1.1771 0.06567 0.06194 -0.0467 1.0000 0.0109
-17.750 -1.1815 0.06178 0.05795 -0.0484 1.0000 0.0109
-17.500 -1.1816 0.05855 0.05464 -0.0497 1.0000 0.0110
-17.250 -1.1858 0.05495 0.05092 -0.0510 1.0000 0.0111
-17.000 -1.1858 0.05193 0.04781 -0.0520 1.0000 0.0111
-16.750 -1.1866 0.04894 0.04473 -0.0529 1.0000 0.0112
-16.500 -1.1880 0.04599 0.04169 -0.0536 1.0000 0.0113
-16.250 -1.1897 0.04312 0.03874 -0.0542 1.0000 0.0114
-16.000 -1.1884 0.04070 0.03625 -0.0545 1.0000 0.0115
-15.750 -1.1870 0.03834 0.03381 -0.0546 1.0000 0.0117
-15.500 -1.1821 0.03637 0.03178 -0.0547 1.0000 0.0118
-15.250 -1.1767 0.03452 0.02985 -0.0546 1.0000 0.0118
-15.000 -1.1676 0.03302 0.02831 -0.0545 1.0000 0.0121
-14.750 -1.1586 0.03155 0.02680 -0.0543 1.0000 0.0123
-14.500 -1.1517 0.02994 0.02511 -0.0539 1.0000 0.0123
-14.250 -1.1406 0.02872 0.02385 -0.0535 1.0000 0.0126
-14.000 -1.1304 0.02746 0.02253 -0.0530 1.0000 0.0127
-13.750 -1.1210 0.02617 0.02118 -0.0524 1.0000 0.0129
-13.500 -1.1096 0.02508 0.02004 -0.0517 1.0000 0.0130
-13.250 -1.0990 0.02396 0.01886 -0.0510 1.0000 0.0132
-13.000 -1.0871 0.02297 0.01782 -0.0501 1.0000 0.0134
-12.750 -1.0756 0.02200 0.01679 -0.0492 1.0000 0.0135
-12.500 -1.0638 0.02110 0.01584 -0.0481 1.0000 0.0136
-12.250 -1.0509 0.02031 0.01500 -0.0470 1.0000 0.0138
-12.000 -1.0199 0.01945 0.01407 -0.0495 0.9630 0.0139
-11.750 -0.9920 0.01846 0.01296 -0.0516 0.9285 0.0143
-11.500 -0.9805 0.01789 0.01227 -0.0497 0.9003 0.0147
-11.250 -0.9710 0.01734 0.01162 -0.0474 0.8806 0.0150
-11.000 -0.9602 0.01691 0.01110 -0.0450 0.8649 0.0152
-10.750 -0.9451 0.01647 0.01059 -0.0434 0.8519 0.0155
-10.500 -0.9270 0.01605 0.01010 -0.0422 0.8409 0.0158
-10.250 -0.9081 0.01565 0.00962 -0.0411 0.8308 0.0161
-10.000 -0.8879 0.01525 0.00916 -0.0402 0.8207 0.0165
-9.750 -0.8670 0.01488 0.00871 -0.0394 0.8116 0.0168
-9.500 -0.8451 0.01454 0.00830 -0.0387 0.8019 0.0171
-9.250 -0.8237 0.01412 0.00783 -0.0380 0.7933 0.0176
-9.000 -0.8011 0.01376 0.00744 -0.0374 0.7845 0.0182
-8.750 -0.7775 0.01344 0.00708 -0.0370 0.7765 0.0189
-8.500 -0.7535 0.01315 0.00674 -0.0366 0.7682 0.0197
-8.250 -0.7289 0.01288 0.00642 -0.0363 0.7607 0.0204
-8.000 -0.7041 0.01260 0.00610 -0.0360 0.7530 0.0210
-7.750 -0.6795 0.01229 0.00576 -0.0357 0.7463 0.0221
-7.500 -0.6541 0.01202 0.00547 -0.0356 0.7392 0.0231
-7.000 -0.6023 0.01157 0.00493 -0.0353 0.7251 0.0251
-6.750 -0.5764 0.01132 0.00465 -0.0352 0.7175 0.0265
-6.500 -0.5502 0.01109 0.00440 -0.0351 0.7107 0.0281
-6.250 -0.5235 0.01089 0.00416 -0.0351 0.7036 0.0296
-6.000 -0.4967 0.01070 0.00394 -0.0350 0.6973 0.0312
-5.750 -0.4699 0.01047 0.00372 -0.0350 0.6910 0.0340
-5.500 -0.4428 0.01029 0.00351 -0.0351 0.6846 0.0369
-5.250 -0.4157 0.01008 0.00331 -0.0351 0.6788 0.0414
-5.000 -0.3885 0.00987 0.00311 -0.0352 0.6725 0.0482
-4.750 -0.3615 0.00966 0.00292 -0.0352 0.6664 0.0587
-4.500 -0.3342 0.00942 0.00273 -0.0353 0.6610 0.0735
-4.250 -0.3072 0.00915 0.00254 -0.0354 0.6549 0.0960
-3.750 -0.2534 0.00849 0.00213 -0.0357 0.6435 0.1687
-3.500 -0.2267 0.00811 0.00192 -0.0358 0.6372 0.2209
-3.250 -0.2001 0.00768 0.00171 -0.0359 0.6317 0.2831
-3.000 -0.1736 0.00716 0.00148 -0.0361 0.6265 0.3619
-2.750 -0.1464 0.00679 0.00135 -0.0363 0.6211 0.4345
-2.500 -0.1180 0.00667 0.00130 -0.0366 0.6161 0.4654
-2.250 -0.0892 0.00658 0.00126 -0.0369 0.6115 0.4907
-2.000 -0.0604 0.00649 0.00124 -0.0371 0.6064 0.5128
-1.750 -0.0316 0.00646 0.00122 -0.0374 0.6016 0.5304
-1.500 -0.0024 0.00645 0.00121 -0.0376 0.5974 0.5404
-1.250 0.0268 0.00643 0.00119 -0.0379 0.5929 0.5456
-1.000 0.0559 0.00643 0.00118 -0.0382 0.5883 0.5512
-0.500 0.1143 0.00644 0.00117 -0.0388 0.5800 0.5605
-0.250 0.1436 0.00644 0.00117 -0.0391 0.5754 0.5644
0.000 0.1727 0.00646 0.00117 -0.0394 0.5710 0.5683
0.250 0.2018 0.00649 0.00119 -0.0397 0.5672 0.5719
0.500 0.2311 0.00649 0.00120 -0.0400 0.5638 0.5758
0.750 0.2603 0.00649 0.00123 -0.0403 0.5601 0.5802
1.000 0.2895 0.00652 0.00125 -0.0406 0.5560 0.5850
1.500 0.3476 0.00657 0.00132 -0.0411 0.5465 0.5940
1.750 0.3766 0.00659 0.00136 -0.0414 0.5413 0.5989
2.000 0.4055 0.00664 0.00140 -0.0416 0.5363 0.6036
2.250 0.4345 0.00667 0.00145 -0.0419 0.5292 0.6081
2.500 0.4628 0.00674 0.00151 -0.0420 0.5181 0.6133
2.750 0.4913 0.00682 0.00156 -0.0422 0.5044 0.6186
3.000 0.5192 0.00694 0.00163 -0.0423 0.4859 0.6234
3.250 0.5471 0.00705 0.00172 -0.0424 0.4659 0.6289
3.500 0.5743 0.00724 0.00182 -0.0424 0.4372 0.6347
3.750 0.5988 0.00769 0.00202 -0.0421 0.3731 0.6399
4.000 0.6219 0.00828 0.00235 -0.0416 0.3075 0.6459
4.250 0.6451 0.00886 0.00267 -0.0411 0.2481 0.6525
4.500 0.6690 0.00934 0.00298 -0.0407 0.2022 0.6585
4.750 0.6926 0.00983 0.00329 -0.0402 0.1591 0.6651
5.000 0.7165 0.01028 0.00359 -0.0398 0.1235 0.6713
5.250 0.7405 0.01068 0.00390 -0.0394 0.0959 0.6775
5.500 0.7644 0.01108 0.00420 -0.0390 0.0735 0.6842
6.000 0.8127 0.01179 0.00480 -0.0382 0.0452 0.6973
6.250 0.8372 0.01210 0.00509 -0.0378 0.0386 0.7042
6.500 0.8619 0.01236 0.00536 -0.0374 0.0346 0.7108
6.750 0.8863 0.01265 0.00566 -0.0370 0.0314 0.7182
7.000 0.9105 0.01292 0.00596 -0.0366 0.0292 0.7253
7.250 0.9339 0.01324 0.00629 -0.0361 0.0270 0.7334
7.500 0.9577 0.01351 0.00660 -0.0356 0.0255 0.7411
7.750 0.9806 0.01381 0.00693 -0.0350 0.0239 0.7492
8.000 1.0025 0.01418 0.00731 -0.0342 0.0222 0.7569
8.250 1.0248 0.01447 0.00766 -0.0335 0.0212 0.7646
8.500 1.0463 0.01480 0.00803 -0.0327 0.0202 0.7729
8.750 1.0666 0.01516 0.00843 -0.0317 0.0190 0.7817
9.250 1.1034 0.01591 0.00927 -0.0290 0.0173 0.8010
9.500 1.1185 0.01629 0.00970 -0.0271 0.0166 0.8114
9.750 1.1327 0.01672 0.01019 -0.0251 0.0160 0.8231
10.000 1.1459 0.01722 0.01075 -0.0231 0.0153 0.8357
10.250 1.1581 0.01779 0.01138 -0.0211 0.0147 0.8495
10.500 1.1713 0.01832 0.01200 -0.0193 0.0144 0.8649
10.750 1.1835 0.01889 0.01268 -0.0174 0.0141 0.8841
11.000 1.1942 0.01947 0.01337 -0.0152 0.0137 0.9117
11.250 1.2102 0.02010 0.01413 -0.0143 0.0134 0.9661
11.500 1.2243 0.02089 0.01496 -0.0133 0.0131 1.0000
11.750 1.2372 0.02176 0.01586 -0.0121 0.0128 1.0000
12.000 1.2494 0.02271 0.01685 -0.0110 0.0124 1.0000
12.250 1.2608 0.02376 0.01792 -0.0099 0.0122 1.0000
12.500 1.2720 0.02483 0.01904 -0.0088 0.0120 1.0000
12.750 1.2815 0.02608 0.02034 -0.0078 0.0118 1.0000
13.000 1.2923 0.02726 0.02157 -0.0069 0.0117 1.0000
13.250 1.3036 0.02843 0.02279 -0.0061 0.0115 1.0000
13.500 1.3143 0.02968 0.02410 -0.0053 0.0113 1.0000
13.750 1.3241 0.03103 0.02550 -0.0046 0.0112 1.0000
14.000 1.3327 0.03252 0.02705 -0.0039 0.0110 1.0000
14.250 1.3411 0.03405 0.02865 -0.0034 0.0110 1.0000
14.500 1.3489 0.03568 0.03033 -0.0028 0.0108 1.0000
14.750 1.3568 0.03733 0.03204 -0.0024 0.0106 1.0000
15.000 1.3638 0.03911 0.03388 -0.0020 0.0105 1.0000
15.250 1.3698 0.04103 0.03587 -0.0017 0.0104 1.0000
15.500 1.3751 0.04308 0.03799 -0.0015 0.0103 1.0000
15.750 1.3811 0.04511 0.04008 -0.0014 0.0102 1.0000
16.000 1.3852 0.04742 0.04246 -0.0014 0.0101 1.0000
16.250 1.3892 0.04979 0.04490 -0.0016 0.0100 1.0000
16.500 1.3913 0.05245 0.04763 -0.0018 0.0099 1.0000
16.750 1.3943 0.05507 0.05033 -0.0022 0.0098 1.0000
17.000 1.3942 0.05816 0.05350 -0.0027 0.0097 1.0000
17.250 1.3947 0.06125 0.05667 -0.0034 0.0096 1.0000
17.500 1.3929 0.06471 0.06022 -0.0043 0.0096 1.0000
17.750 1.3892 0.06855 0.06416 -0.0054 0.0095 1.0000
18.000 1.3834 0.07280 0.06851 -0.0068 0.0094 1.0000
18.250 1.3785 0.07703 0.07283 -0.0083 0.0093 1.0000
18.500 1.3774 0.08081 0.07671 -0.0098 0.0093 1.0000
18.750 1.3714 0.08546 0.08147 -0.0117 0.0093 1.0000
19.000 1.3660 0.09015 0.08627 -0.0138 0.0092 1.0000
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