NACA 64(2)-415 (naca642415-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: NACA 64(2)-415 (naca642415-il) Reynolds number: 1,000,000 Max Cl/Cd: 120.62 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-naca642415-il-1000000.txt Download as CSV file: xf-naca642415-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: NACA 64(2)-415
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -0.8389 0.10377 0.10146 -0.0444 1.0000 0.0140
-17.500 -0.8981 0.08830 0.08575 -0.0534 1.0000 0.0138
-17.250 -0.9231 0.07967 0.07695 -0.0587 1.0000 0.0138
-17.000 -0.9353 0.07364 0.07080 -0.0625 1.0000 0.0139
-16.750 -0.9570 0.06663 0.06363 -0.0665 1.0000 0.0139
-16.500 -0.9660 0.06182 0.05868 -0.0693 1.0000 0.0140
-16.250 -0.9764 0.05710 0.05383 -0.0718 1.0000 0.0140
-16.000 -0.9833 0.05307 0.04966 -0.0738 1.0000 0.0141
-15.750 -1.0013 0.04808 0.04450 -0.0756 1.0000 0.0143
-15.500 -1.0117 0.04422 0.04050 -0.0767 1.0000 0.0144
-15.250 -1.0152 0.04126 0.03745 -0.0774 1.0000 0.0146
-15.000 -1.0122 0.03907 0.03521 -0.0779 1.0000 0.0148
-14.750 -1.0094 0.03691 0.03298 -0.0781 1.0000 0.0149
-14.500 -1.0053 0.03495 0.03095 -0.0782 1.0000 0.0151
-14.250 -0.9972 0.03347 0.02943 -0.0783 1.0000 0.0153
-14.000 -0.9919 0.03175 0.02763 -0.0780 1.0000 0.0154
-13.750 -0.9843 0.03032 0.02614 -0.0777 1.0000 0.0157
-13.500 -0.9774 0.02889 0.02463 -0.0771 1.0000 0.0159
-13.250 -0.9701 0.02757 0.02324 -0.0763 1.0000 0.0161
-13.000 -0.9624 0.02637 0.02196 -0.0753 1.0000 0.0163
-12.750 -0.9540 0.02533 0.02086 -0.0741 1.0000 0.0166
-12.500 -0.9467 0.02436 0.01983 -0.0726 1.0000 0.0168
-12.250 -0.9424 0.02343 0.01882 -0.0704 1.0000 0.0169
-11.750 -0.9036 0.02100 0.01621 -0.0718 0.9847 0.0177
-11.500 -0.8722 0.01986 0.01504 -0.0746 0.9766 0.0182
-11.250 -0.8362 0.01904 0.01418 -0.0777 0.9690 0.0187
-11.000 -0.8015 0.01828 0.01336 -0.0803 0.9576 0.0192
-10.750 -0.7720 0.01763 0.01262 -0.0817 0.9417 0.0196
-10.500 -0.7502 0.01712 0.01199 -0.0814 0.9239 0.0201
-10.250 -0.7308 0.01669 0.01145 -0.0804 0.9082 0.0205
-10.000 -0.7101 0.01636 0.01103 -0.0796 0.8949 0.0208
-9.750 -0.6951 0.01547 0.01004 -0.0781 0.8822 0.0214
-9.500 -0.6761 0.01491 0.00942 -0.0771 0.8714 0.0220
-9.250 -0.6545 0.01451 0.00897 -0.0764 0.8610 0.0226
-9.000 -0.6320 0.01414 0.00854 -0.0759 0.8519 0.0231
-8.750 -0.6090 0.01379 0.00812 -0.0753 0.8427 0.0238
-8.500 -0.5854 0.01343 0.00770 -0.0749 0.8343 0.0244
-8.250 -0.5609 0.01316 0.00735 -0.0746 0.8261 0.0249
-8.000 -0.5389 0.01256 0.00669 -0.0740 0.8180 0.0259
-7.750 -0.5149 0.01217 0.00626 -0.0737 0.8100 0.0269
-7.500 -0.4895 0.01187 0.00593 -0.0735 0.8026 0.0279
-7.250 -0.4638 0.01160 0.00560 -0.0733 0.7951 0.0288
-7.000 -0.4377 0.01137 0.00531 -0.0732 0.7883 0.0297
-6.750 -0.4125 0.01094 0.00484 -0.0731 0.7810 0.0312
-6.250 -0.3593 0.01044 0.00428 -0.0730 0.7671 0.0346
-6.000 -0.3323 0.01024 0.00402 -0.0730 0.7598 0.0361
-5.750 -0.3057 0.00992 0.00369 -0.0730 0.7531 0.0392
-5.500 -0.2782 0.00973 0.00347 -0.0731 0.7458 0.0418
-5.250 -0.2510 0.00948 0.00321 -0.0732 0.7394 0.0466
-5.000 -0.2233 0.00926 0.00299 -0.0734 0.7327 0.0535
-4.750 -0.1960 0.00900 0.00277 -0.0735 0.7261 0.0675
-4.500 -0.1685 0.00868 0.00255 -0.0737 0.7199 0.0953
-4.250 -0.1413 0.00826 0.00232 -0.0740 0.7133 0.1433
-4.000 -0.1145 0.00772 0.00205 -0.0744 0.7072 0.2235
-3.750 -0.0876 0.00694 0.00173 -0.0749 0.7010 0.3480
-3.500 -0.0600 0.00647 0.00159 -0.0754 0.6947 0.4486
-3.250 -0.0311 0.00638 0.00154 -0.0757 0.6889 0.4795
-3.000 -0.0020 0.00633 0.00150 -0.0760 0.6825 0.4976
-2.750 0.0269 0.00632 0.00146 -0.0762 0.6763 0.5118
-2.500 0.0562 0.00630 0.00144 -0.0765 0.6704 0.5230
-2.250 0.0853 0.00628 0.00142 -0.0768 0.6644 0.5337
-2.000 0.1141 0.00630 0.00141 -0.0770 0.6587 0.5473
-1.750 0.1435 0.00629 0.00142 -0.0773 0.6533 0.5601
-1.250 0.2014 0.00634 0.00145 -0.0778 0.6421 0.5829
-1.000 0.2308 0.00635 0.00145 -0.0781 0.6370 0.5881
-0.750 0.2599 0.00635 0.00144 -0.0784 0.6316 0.5935
-0.500 0.2887 0.00639 0.00145 -0.0786 0.6264 0.5988
-0.250 0.3181 0.00639 0.00146 -0.0790 0.6217 0.6036
0.000 0.3472 0.00642 0.00147 -0.0792 0.6164 0.6080
0.250 0.3759 0.00645 0.00149 -0.0795 0.6113 0.6128
0.500 0.4052 0.00646 0.00152 -0.0798 0.6071 0.6178
0.750 0.4344 0.00650 0.00155 -0.0801 0.6025 0.6226
1.000 0.4633 0.00652 0.00158 -0.0803 0.5981 0.6277
1.250 0.4920 0.00658 0.00163 -0.0806 0.5935 0.6333
1.500 0.5213 0.00660 0.00167 -0.0809 0.5888 0.6390
1.750 0.5501 0.00663 0.00172 -0.0811 0.5833 0.6447
2.000 0.5785 0.00671 0.00179 -0.0813 0.5782 0.6506
2.250 0.6077 0.00673 0.00184 -0.0816 0.5741 0.6565
2.500 0.6365 0.00676 0.00190 -0.0818 0.5688 0.6625
2.750 0.6646 0.00684 0.00198 -0.0820 0.5615 0.6689
3.000 0.6935 0.00686 0.00203 -0.0822 0.5540 0.6751
3.250 0.7213 0.00694 0.00210 -0.0823 0.5448 0.6816
3.500 0.7498 0.00699 0.00217 -0.0824 0.5354 0.6885
3.750 0.7778 0.00706 0.00225 -0.0825 0.5254 0.6950
4.000 0.8053 0.00716 0.00234 -0.0825 0.5130 0.7022
4.250 0.8335 0.00724 0.00244 -0.0827 0.5029 0.7093
4.500 0.8612 0.00732 0.00256 -0.0827 0.4932 0.7166
4.750 0.8885 0.00746 0.00268 -0.0827 0.4802 0.7240
5.000 0.9155 0.00759 0.00282 -0.0827 0.4644 0.7311
5.250 0.9415 0.00781 0.00298 -0.0824 0.4385 0.7388
5.500 0.9611 0.00848 0.00333 -0.0813 0.3642 0.7460
5.750 0.9766 0.00950 0.00393 -0.0795 0.2794 0.7539
6.000 0.9931 0.01040 0.00450 -0.0779 0.2096 0.7616
6.250 1.0107 0.01117 0.00502 -0.0765 0.1590 0.7698
6.500 1.0289 0.01185 0.00551 -0.0752 0.1185 0.7779
6.750 1.0473 0.01247 0.00599 -0.0738 0.0889 0.7868
7.000 1.0662 0.01302 0.00645 -0.0725 0.0676 0.7957
7.250 1.0852 0.01353 0.00690 -0.0713 0.0527 0.8053
7.500 1.1041 0.01399 0.00735 -0.0700 0.0434 0.8146
8.000 1.1401 0.01489 0.00826 -0.0670 0.0338 0.8348
8.250 1.1563 0.01524 0.00867 -0.0652 0.0316 0.8458
8.500 1.1700 0.01568 0.00915 -0.0629 0.0294 0.8587
8.750 1.1818 0.01619 0.00972 -0.0604 0.0273 0.8737
9.000 1.1952 0.01659 0.01021 -0.0581 0.0258 0.8915
9.250 1.2049 0.01709 0.01078 -0.0554 0.0243 0.9166
9.500 1.2113 0.01767 0.01149 -0.0522 0.0229 1.0000
9.750 1.2278 0.01825 0.01211 -0.0510 0.0219 1.0000
10.000 1.2423 0.01895 0.01282 -0.0497 0.0209 1.0000
10.250 1.2552 0.01977 0.01366 -0.0482 0.0199 1.0000
10.500 1.2630 0.02093 0.01485 -0.0462 0.0189 1.0000
10.750 1.2771 0.02174 0.01571 -0.0451 0.0184 1.0000
11.000 1.2900 0.02265 0.01666 -0.0438 0.0178 1.0000
11.250 1.3024 0.02362 0.01767 -0.0426 0.0173 1.0000
11.500 1.3142 0.02467 0.01875 -0.0415 0.0168 1.0000
11.750 1.3239 0.02590 0.02001 -0.0402 0.0163 1.0000
12.000 1.3291 0.02752 0.02168 -0.0387 0.0158 1.0000
12.250 1.3331 0.02930 0.02353 -0.0373 0.0154 1.0000
12.500 1.3453 0.03046 0.02475 -0.0365 0.0152 1.0000
12.750 1.3542 0.03194 0.02629 -0.0356 0.0150 1.0000
13.000 1.3646 0.03332 0.02771 -0.0349 0.0146 1.0000
13.250 1.3734 0.03486 0.02932 -0.0341 0.0143 1.0000
13.500 1.3817 0.03649 0.03100 -0.0334 0.0140 1.0000
13.750 1.3892 0.03823 0.03279 -0.0328 0.0138 1.0000
14.000 1.3960 0.04009 0.03471 -0.0323 0.0136 1.0000
14.250 1.4022 0.04204 0.03671 -0.0318 0.0134 1.0000
14.500 1.4069 0.04422 0.03895 -0.0314 0.0131 1.0000
14.750 1.4094 0.04669 0.04148 -0.0310 0.0129 1.0000
15.000 1.4090 0.04954 0.04441 -0.0308 0.0127 1.0000
15.250 1.4042 0.05296 0.04793 -0.0305 0.0125 1.0000
15.500 1.4087 0.05546 0.05051 -0.0306 0.0124 1.0000
15.750 1.4145 0.05784 0.05298 -0.0307 0.0123 1.0000
16.000 1.4186 0.06048 0.05570 -0.0310 0.0122 1.0000
16.250 1.4211 0.06339 0.05869 -0.0314 0.0121 1.0000
16.500 1.4239 0.06633 0.06172 -0.0318 0.0120 1.0000
16.750 1.4261 0.06940 0.06488 -0.0324 0.0119 1.0000
17.000 1.4270 0.07272 0.06829 -0.0331 0.0118 1.0000
17.250 1.4270 0.07622 0.07188 -0.0340 0.0117 1.0000
17.500 1.4271 0.07979 0.07556 -0.0350 0.0116 1.0000
17.750 1.4267 0.08351 0.07938 -0.0361 0.0115 1.0000
18.000 1.4247 0.08753 0.08349 -0.0375 0.0114 1.0000
18.250 1.4227 0.09165 0.08771 -0.0389 0.0113 1.0000
18.500 1.4204 0.09590 0.09206 -0.0406 0.0112 1.0000
18.750 1.4172 0.10036 0.09662 -0.0424 0.0111 1.0000
19.000 1.4133 0.10501 0.10138 -0.0444 0.0110 1.0000
19.250 1.4092 0.10979 0.10625 -0.0467 0.0109 1.0000
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