NACA 64-210 (naca64210-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 64-210 (naca64210-il) Reynolds number: 1,000,000 Max Cl/Cd: 72.87 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca64210-il-1000000-n5.txt Download as CSV file: xf-naca64210-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 64-210
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
------ -------- --------- --------- -------- -------- --------
-14.500 -1.0280 0.05482 0.05277 -0.0422 1.0000 0.0043
-14.250 -1.0734 0.04498 0.04264 -0.0484 1.0000 0.0043
-14.000 -1.0832 0.04110 0.03862 -0.0499 1.0000 0.0043
-13.750 -1.1009 0.03686 0.03417 -0.0506 1.0000 0.0043
-13.500 -1.1001 0.03486 0.03207 -0.0502 1.0000 0.0044
-13.250 -1.1074 0.03243 0.02947 -0.0489 1.0000 0.0045
-13.000 -1.1125 0.03054 0.02743 -0.0466 1.0000 0.0046
-12.750 -1.1076 0.02896 0.02570 -0.0450 1.0000 0.0046
-12.500 -1.0997 0.02726 0.02381 -0.0437 1.0000 0.0047
-12.250 -1.0870 0.02591 0.02232 -0.0427 1.0000 0.0049
-12.000 -1.0721 0.02469 0.02096 -0.0418 1.0000 0.0050
-11.750 -1.0569 0.02338 0.01949 -0.0409 1.0000 0.0051
-11.500 -1.0398 0.02223 0.01819 -0.0401 1.0000 0.0053
-11.250 -1.0213 0.02119 0.01702 -0.0394 1.0000 0.0054
-11.000 -1.0009 0.02039 0.01611 -0.0388 1.0000 0.0055
-10.750 -0.9826 0.01919 0.01477 -0.0381 1.0000 0.0058
-10.500 -0.9599 0.01869 0.01424 -0.0377 1.0000 0.0061
-10.250 -0.9372 0.01818 0.01367 -0.0373 1.0000 0.0063
-10.000 -0.9145 0.01765 0.01308 -0.0368 1.0000 0.0066
-9.750 -0.8920 0.01707 0.01243 -0.0364 1.0000 0.0069
-9.500 -0.8696 0.01646 0.01174 -0.0358 1.0000 0.0072
-9.250 -0.8472 0.01587 0.01107 -0.0352 1.0000 0.0074
-9.000 -0.8181 0.01522 0.01033 -0.0361 0.9929 0.0077
-8.750 -0.7859 0.01469 0.00971 -0.0375 0.9842 0.0080
-8.500 -0.7539 0.01390 0.00881 -0.0390 0.9739 0.0083
-8.250 -0.7225 0.01327 0.00812 -0.0403 0.9624 0.0089
-8.000 -0.6931 0.01293 0.00773 -0.0410 0.9489 0.0093
-7.750 -0.6664 0.01265 0.00740 -0.0410 0.9343 0.0098
-7.500 -0.6411 0.01235 0.00702 -0.0407 0.9204 0.0103
-7.250 -0.6162 0.01197 0.00653 -0.0403 0.9075 0.0107
-7.000 -0.5909 0.01163 0.00610 -0.0400 0.8954 0.0110
-6.750 -0.5654 0.01130 0.00569 -0.0397 0.8838 0.0113
-6.500 -0.5396 0.01098 0.00529 -0.0394 0.8730 0.0115
-6.250 -0.5145 0.01050 0.00472 -0.0391 0.8621 0.0124
-6.000 -0.4882 0.01021 0.00437 -0.0390 0.8513 0.0131
-5.750 -0.4616 0.00994 0.00405 -0.0389 0.8412 0.0136
-5.500 -0.4349 0.00970 0.00374 -0.0388 0.8314 0.0142
-5.250 -0.4080 0.00948 0.00346 -0.0387 0.8215 0.0149
-5.000 -0.3808 0.00929 0.00320 -0.0387 0.8122 0.0157
-4.750 -0.3537 0.00905 0.00290 -0.0386 0.8032 0.0166
-4.500 -0.3264 0.00882 0.00264 -0.0386 0.7941 0.0184
-4.250 -0.2989 0.00865 0.00244 -0.0387 0.7858 0.0202
-4.000 -0.2713 0.00851 0.00225 -0.0387 0.7766 0.0219
-3.750 -0.2436 0.00835 0.00206 -0.0388 0.7676 0.0244
-3.500 -0.2159 0.00820 0.00189 -0.0388 0.7590 0.0280
-3.250 -0.1880 0.00809 0.00175 -0.0389 0.7503 0.0308
-3.000 -0.1601 0.00795 0.00160 -0.0390 0.7424 0.0373
-2.750 -0.1323 0.00781 0.00147 -0.0391 0.7340 0.0486
-2.500 -0.1045 0.00758 0.00133 -0.0392 0.7259 0.0797
-2.000 -0.0500 0.00674 0.00101 -0.0397 0.7090 0.2479
-1.750 -0.0229 0.00629 0.00085 -0.0399 0.7011 0.3501
-1.500 0.0045 0.00586 0.00076 -0.0401 0.6933 0.4586
-1.250 0.0324 0.00569 0.00073 -0.0403 0.6860 0.5106
-1.000 0.0602 0.00549 0.00072 -0.0404 0.6785 0.5758
-0.750 0.0882 0.00540 0.00073 -0.0405 0.6713 0.6154
-0.500 0.1166 0.00538 0.00072 -0.0406 0.6634 0.6286
-0.250 0.1451 0.00538 0.00072 -0.0408 0.6561 0.6385
0.000 0.1736 0.00540 0.00073 -0.0409 0.6488 0.6466
0.250 0.2021 0.00541 0.00074 -0.0410 0.6422 0.6540
0.500 0.2306 0.00543 0.00076 -0.0412 0.6339 0.6617
0.750 0.2589 0.00545 0.00078 -0.0413 0.6247 0.6700
1.000 0.2872 0.00549 0.00082 -0.0414 0.6145 0.6777
1.250 0.3152 0.00555 0.00085 -0.0415 0.5957 0.6858
1.500 0.3426 0.00568 0.00089 -0.0414 0.5661 0.6934
1.750 0.3697 0.00587 0.00095 -0.0413 0.5254 0.7017
2.000 0.3968 0.00604 0.00103 -0.0413 0.4882 0.7100
2.250 0.4223 0.00649 0.00117 -0.0411 0.4026 0.7190
2.500 0.4464 0.00714 0.00143 -0.0407 0.2968 0.7280
2.750 0.4716 0.00766 0.00167 -0.0406 0.2182 0.7366
3.000 0.4965 0.00822 0.00194 -0.0403 0.1376 0.7456
3.250 0.5220 0.00868 0.00219 -0.0401 0.0803 0.7542
3.750 0.5750 0.00925 0.00262 -0.0399 0.0352 0.7731
4.000 0.6019 0.00943 0.00281 -0.0398 0.0303 0.7827
4.500 0.6558 0.00979 0.00323 -0.0397 0.0240 0.8020
4.750 0.6824 0.01000 0.00347 -0.0396 0.0210 0.8116
5.250 0.7351 0.01044 0.00399 -0.0392 0.0166 0.8326
5.500 0.7611 0.01069 0.00426 -0.0390 0.0151 0.8435
5.750 0.7866 0.01098 0.00460 -0.0386 0.0136 0.8547
6.000 0.8118 0.01129 0.00498 -0.0382 0.0129 0.8669
6.500 0.8612 0.01186 0.00570 -0.0372 0.0120 0.8942
6.750 0.8851 0.01215 0.00606 -0.0366 0.0115 0.9095
7.000 0.9080 0.01246 0.00645 -0.0357 0.0111 0.9265
7.250 0.9301 0.01278 0.00685 -0.0347 0.0107 0.9480
7.500 0.9574 0.01317 0.00730 -0.0349 0.0104 1.0000
7.750 0.9818 0.01365 0.00782 -0.0346 0.0101 1.0000
8.000 1.0052 0.01426 0.00849 -0.0341 0.0095 1.0000
8.250 1.0272 0.01503 0.00933 -0.0334 0.0092 1.0000
8.500 1.0509 0.01553 0.00989 -0.0330 0.0090 1.0000
8.750 1.0744 0.01605 0.01046 -0.0325 0.0089 1.0000
9.000 1.0974 0.01661 0.01109 -0.0320 0.0087 1.0000
9.250 1.1201 0.01718 0.01172 -0.0315 0.0085 1.0000
9.500 1.1425 0.01776 0.01237 -0.0309 0.0082 1.0000
9.750 1.1647 0.01833 0.01301 -0.0304 0.0079 1.0000
10.000 1.1868 0.01887 0.01361 -0.0298 0.0076 1.0000
10.250 1.2087 0.01939 0.01417 -0.0292 0.0073 1.0000
10.500 1.2297 0.02000 0.01483 -0.0285 0.0071 1.0000
10.750 1.2498 0.02065 0.01554 -0.0277 0.0069 1.0000
11.000 1.2681 0.02147 0.01643 -0.0267 0.0067 1.0000
11.250 1.2810 0.02285 0.01794 -0.0251 0.0063 1.0000
11.500 1.2983 0.02364 0.01884 -0.0240 0.0062 1.0000
11.750 1.3144 0.02447 0.01977 -0.0227 0.0061 1.0000
12.000 1.3274 0.02534 0.02074 -0.0210 0.0060 1.0000
12.250 1.3391 0.02614 0.02164 -0.0191 0.0059 1.0000
12.500 1.3478 0.02718 0.02278 -0.0170 0.0057 1.0000
12.750 1.3558 0.02829 0.02401 -0.0150 0.0056 1.0000
13.000 1.3679 0.02907 0.02485 -0.0136 0.0053 1.0000
13.250 1.3761 0.03024 0.02610 -0.0121 0.0052 1.0000
13.500 1.3833 0.03154 0.02750 -0.0106 0.0050 1.0000
13.750 1.3896 0.03298 0.02904 -0.0094 0.0049 1.0000
14.000 1.3956 0.03450 0.03066 -0.0083 0.0048 1.0000
14.250 1.4000 0.03626 0.03253 -0.0073 0.0047 1.0000
14.500 1.4024 0.03831 0.03469 -0.0066 0.0046 1.0000
14.750 1.4065 0.04026 0.03672 -0.0061 0.0045 1.0000
15.000 1.4056 0.04288 0.03946 -0.0058 0.0045 1.0000
15.250 1.4066 0.04540 0.04207 -0.0058 0.0043 1.0000
15.500 1.4000 0.04897 0.04578 -0.0063 0.0043 1.0000
15.750 1.3901 0.05320 0.05017 -0.0072 0.0042 1.0000
16.000 1.3784 0.05796 0.05507 -0.0088 0.0042 1.0000
16.250 1.3616 0.06382 0.06110 -0.0113 0.0041 1.0000
16.500 1.3481 0.06962 0.06705 -0.0141 0.0041 1.0000
16.750 1.3221 0.07821 0.07584 -0.0189 0.0041 1.0000
17.000 1.2936 0.08830 0.08611 -0.0251 0.0041 1.0000
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