NACA 64(2)-415 (naca642415-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 64(2)-415 (naca642415-il) Reynolds number: 1,000,000 Max Cl/Cd: 103.14 at α=4° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca642415-il-1000000-n5.txt Download as CSV file: xf-naca642415-il-1000000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.9114 0.12058 0.11809 -0.0342 1.0000 0.0107
-19.250 -0.9623 0.10698 0.10431 -0.0416 1.0000 0.0106
-19.000 -1.0042 0.09538 0.09253 -0.0480 1.0000 0.0106
-18.750 -1.0358 0.08597 0.08297 -0.0533 1.0000 0.0106
-18.500 -1.0593 0.07827 0.07512 -0.0576 1.0000 0.0106
-18.250 -1.0749 0.07205 0.06877 -0.0611 1.0000 0.0107
-18.000 -1.0920 0.06590 0.06249 -0.0645 1.0000 0.0106
-17.750 -1.1042 0.06081 0.05729 -0.0672 1.0000 0.0108
-17.500 -1.1140 0.05622 0.05260 -0.0694 1.0000 0.0109
-17.250 -1.1203 0.05230 0.04858 -0.0713 1.0000 0.0110
-17.000 -1.1231 0.04896 0.04515 -0.0727 1.0000 0.0111
-16.750 -1.1245 0.04595 0.04206 -0.0738 1.0000 0.0112
-16.500 -1.1235 0.04334 0.03937 -0.0746 1.0000 0.0114
-16.250 -1.1220 0.04085 0.03680 -0.0753 1.0000 0.0115
-16.000 -1.1188 0.03860 0.03449 -0.0758 1.0000 0.0116
-15.750 -1.1141 0.03657 0.03238 -0.0762 1.0000 0.0117
-15.500 -1.1084 0.03468 0.03043 -0.0764 1.0000 0.0119
-15.250 -1.1015 0.03297 0.02865 -0.0764 1.0000 0.0120
-15.000 -1.0939 0.03136 0.02697 -0.0764 1.0000 0.0122
-14.750 -1.0860 0.02984 0.02539 -0.0762 1.0000 0.0124
-14.500 -1.0780 0.02839 0.02386 -0.0758 1.0000 0.0125
-14.250 -1.0692 0.02706 0.02247 -0.0754 1.0000 0.0127
-14.000 -1.0595 0.02586 0.02121 -0.0748 1.0000 0.0129
-13.750 -1.0493 0.02477 0.02006 -0.0741 1.0000 0.0130
-13.500 -1.0374 0.02388 0.01911 -0.0732 1.0000 0.0132
-13.250 -1.0294 0.02280 0.01797 -0.0720 1.0000 0.0134
-13.000 -1.0171 0.02165 0.01677 -0.0716 0.9867 0.0136
-12.750 -0.9806 0.02055 0.01562 -0.0756 0.9733 0.0140
-12.500 -0.9401 0.01957 0.01457 -0.0802 0.9586 0.0143
-12.250 -0.9050 0.01875 0.01367 -0.0833 0.9372 0.0147
-12.000 -0.8865 0.01814 0.01292 -0.0830 0.9119 0.0149
-11.750 -0.8768 0.01760 0.01226 -0.0808 0.8909 0.0151
-11.500 -0.8634 0.01715 0.01171 -0.0791 0.8756 0.0154
-11.000 -0.8274 0.01627 0.01065 -0.0769 0.8519 0.0159
-10.750 -0.8077 0.01588 0.01016 -0.0760 0.8421 0.0162
-10.500 -0.7881 0.01540 0.00962 -0.0752 0.8319 0.0166
-10.250 -0.7675 0.01495 0.00911 -0.0744 0.8231 0.0170
-10.000 -0.7457 0.01456 0.00866 -0.0738 0.8140 0.0174
-9.750 -0.7229 0.01420 0.00826 -0.0734 0.8060 0.0178
-9.500 -0.6996 0.01387 0.00787 -0.0729 0.7970 0.0182
-9.250 -0.6757 0.01356 0.00750 -0.0726 0.7891 0.0187
-9.000 -0.6514 0.01326 0.00714 -0.0723 0.7804 0.0192
-8.750 -0.6267 0.01297 0.00678 -0.0720 0.7729 0.0196
-8.500 -0.6022 0.01263 0.00639 -0.0718 0.7650 0.0201
-8.250 -0.5774 0.01231 0.00603 -0.0716 0.7578 0.0207
-8.000 -0.5517 0.01203 0.00572 -0.0715 0.7504 0.0214
-7.750 -0.5260 0.01178 0.00542 -0.0713 0.7432 0.0221
-7.500 -0.4995 0.01154 0.00515 -0.0713 0.7363 0.0228
-7.250 -0.4730 0.01134 0.00489 -0.0713 0.7295 0.0236
-7.000 -0.4466 0.01107 0.00460 -0.0713 0.7234 0.0246
-6.750 -0.4198 0.01084 0.00434 -0.0713 0.7168 0.0257
-6.250 -0.3654 0.01046 0.00389 -0.0715 0.7045 0.0279
-6.000 -0.3381 0.01027 0.00367 -0.0715 0.6978 0.0292
-5.750 -0.3107 0.01007 0.00345 -0.0716 0.6915 0.0311
-5.500 -0.2830 0.00991 0.00326 -0.0718 0.6850 0.0330
-5.250 -0.2553 0.00975 0.00308 -0.0719 0.6786 0.0355
-5.000 -0.2274 0.00957 0.00290 -0.0721 0.6732 0.0388
-4.750 -0.1993 0.00941 0.00274 -0.0723 0.6673 0.0429
-4.500 -0.1714 0.00926 0.00258 -0.0725 0.6616 0.0492
-4.250 -0.1433 0.00907 0.00243 -0.0727 0.6565 0.0599
-4.000 -0.1151 0.00887 0.00227 -0.0730 0.6508 0.0759
-3.750 -0.0872 0.00866 0.00213 -0.0732 0.6453 0.0971
-3.500 -0.0590 0.00839 0.00197 -0.0736 0.6404 0.1319
-3.250 -0.0308 0.00807 0.00181 -0.0740 0.6349 0.1790
-3.000 -0.0029 0.00768 0.00163 -0.0744 0.6295 0.2456
-2.750 0.0251 0.00721 0.00144 -0.0749 0.6245 0.3295
-2.500 0.0535 0.00679 0.00130 -0.0755 0.6190 0.4148
-2.250 0.0823 0.00667 0.00126 -0.0758 0.6133 0.4565
-2.000 0.1113 0.00659 0.00124 -0.0762 0.6085 0.4839
-1.750 0.1405 0.00653 0.00124 -0.0765 0.6036 0.5083
-1.500 0.1695 0.00649 0.00125 -0.0768 0.5986 0.5313
-1.250 0.1985 0.00650 0.00125 -0.0771 0.5942 0.5427
-1.000 0.2278 0.00649 0.00125 -0.0774 0.5900 0.5485
-0.750 0.2570 0.00651 0.00125 -0.0777 0.5855 0.5542
-0.500 0.2861 0.00653 0.00125 -0.0779 0.5811 0.5588
-0.250 0.3152 0.00655 0.00126 -0.0782 0.5773 0.5628
0.000 0.3444 0.00656 0.00128 -0.0785 0.5736 0.5667
0.250 0.3736 0.00659 0.00130 -0.0788 0.5694 0.5706
0.500 0.4025 0.00663 0.00132 -0.0791 0.5652 0.5743
0.750 0.4315 0.00666 0.00135 -0.0794 0.5614 0.5789
1.000 0.4607 0.00667 0.00139 -0.0797 0.5580 0.5837
1.250 0.4898 0.00671 0.00143 -0.0799 0.5539 0.5882
1.500 0.5185 0.00676 0.00148 -0.0802 0.5492 0.5923
1.750 0.5473 0.00680 0.00153 -0.0804 0.5445 0.5971
2.000 0.5763 0.00683 0.00158 -0.0807 0.5397 0.6020
2.250 0.6051 0.00689 0.00164 -0.0809 0.5348 0.6067
2.500 0.6335 0.00695 0.00171 -0.0811 0.5291 0.6115
2.750 0.6621 0.00700 0.00178 -0.0813 0.5199 0.6170
3.000 0.6902 0.00709 0.00185 -0.0814 0.5094 0.6222
3.250 0.7178 0.00721 0.00194 -0.0815 0.4952 0.6273
3.500 0.7452 0.00734 0.00204 -0.0815 0.4775 0.6334
3.750 0.7725 0.00749 0.00215 -0.0815 0.4596 0.6395
4.000 0.7983 0.00774 0.00230 -0.0813 0.4266 0.6455
4.250 0.8190 0.00842 0.00264 -0.0803 0.3522 0.6519
4.500 0.8412 0.00898 0.00298 -0.0796 0.3022 0.6578
4.750 0.8630 0.00955 0.00335 -0.0788 0.2520 0.6638
5.000 0.8841 0.01016 0.00375 -0.0779 0.2033 0.6703
5.500 0.9273 0.01123 0.00449 -0.0763 0.1294 0.6830
5.750 0.9480 0.01179 0.00490 -0.0753 0.0973 0.6899
6.000 0.9692 0.01228 0.00529 -0.0744 0.0734 0.6962
6.250 0.9908 0.01272 0.00565 -0.0736 0.0565 0.7034
6.750 1.0350 0.01346 0.00635 -0.0721 0.0392 0.7179
7.000 1.0571 0.01380 0.00669 -0.0713 0.0345 0.7260
7.250 1.0787 0.01414 0.00705 -0.0704 0.0310 0.7337
7.500 1.1000 0.01448 0.00741 -0.0695 0.0284 0.7418
7.750 1.1203 0.01484 0.00779 -0.0685 0.0262 0.7493
8.000 1.1401 0.01517 0.00816 -0.0673 0.0247 0.7576
8.250 1.1566 0.01554 0.00856 -0.0655 0.0231 0.7656
8.500 1.1724 0.01594 0.00900 -0.0637 0.0218 0.7749
8.750 1.1887 0.01633 0.00944 -0.0620 0.0207 0.7847
9.250 1.2180 0.01730 0.01050 -0.0583 0.0182 0.8064
9.500 1.2331 0.01780 0.01106 -0.0567 0.0174 0.8176
9.750 1.2473 0.01835 0.01167 -0.0550 0.0162 0.8304
10.000 1.2606 0.01897 0.01234 -0.0533 0.0155 0.8445
10.250 1.2730 0.01963 0.01308 -0.0515 0.0147 0.8601
10.500 1.2853 0.02029 0.01384 -0.0497 0.0141 0.8800
10.750 1.2956 0.02096 0.01462 -0.0476 0.0137 0.9093
11.000 1.3063 0.02164 0.01543 -0.0457 0.0131 1.0000
11.250 1.3191 0.02255 0.01636 -0.0445 0.0127 1.0000
11.500 1.3306 0.02358 0.01743 -0.0432 0.0121 1.0000
11.750 1.3427 0.02461 0.01849 -0.0421 0.0118 1.0000
12.000 1.3548 0.02567 0.01959 -0.0411 0.0116 1.0000
12.250 1.3664 0.02678 0.02075 -0.0401 0.0113 1.0000
12.500 1.3774 0.02798 0.02200 -0.0391 0.0111 1.0000
12.750 1.3882 0.02923 0.02330 -0.0381 0.0109 1.0000
13.000 1.3983 0.03056 0.02467 -0.0373 0.0107 1.0000
13.250 1.4079 0.03197 0.02613 -0.0364 0.0105 1.0000
13.500 1.4169 0.03346 0.02766 -0.0356 0.0104 1.0000
13.750 1.4252 0.03504 0.02929 -0.0349 0.0102 1.0000
14.000 1.4330 0.03671 0.03101 -0.0342 0.0100 1.0000
14.250 1.4395 0.03855 0.03290 -0.0336 0.0098 1.0000
14.500 1.4448 0.04054 0.03497 -0.0330 0.0096 1.0000
14.750 1.4493 0.04269 0.03718 -0.0325 0.0095 1.0000
15.000 1.4564 0.04464 0.03919 -0.0322 0.0095 1.0000
15.250 1.4626 0.04671 0.04133 -0.0320 0.0094 1.0000
15.500 1.4679 0.04893 0.04363 -0.0318 0.0094 1.0000
15.750 1.4726 0.05129 0.04606 -0.0317 0.0093 1.0000
16.000 1.4773 0.05369 0.04854 -0.0318 0.0092 1.0000
16.250 1.4816 0.05621 0.05114 -0.0319 0.0091 1.0000
16.500 1.4846 0.05894 0.05395 -0.0322 0.0091 1.0000
16.750 1.4878 0.06171 0.05680 -0.0325 0.0090 1.0000
17.000 1.4911 0.06451 0.05968 -0.0329 0.0089 1.0000
17.250 1.4928 0.06760 0.06286 -0.0335 0.0088 1.0000
17.500 1.4935 0.07089 0.06622 -0.0343 0.0087 1.0000
17.750 1.4929 0.07441 0.06984 -0.0351 0.0086 1.0000
18.000 1.4930 0.07792 0.07344 -0.0361 0.0085 1.0000
18.250 1.4916 0.08173 0.07733 -0.0372 0.0085 1.0000
18.500 1.4892 0.08578 0.08148 -0.0386 0.0084 1.0000
18.750 1.4866 0.08991 0.08572 -0.0401 0.0084 1.0000
19.000 1.4828 0.09433 0.09023 -0.0417 0.0083 1.0000
19.250 1.4779 0.09902 0.09503 -0.0437 0.0083 1.0000
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