NACA 0012-64 (naca001264-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: NACA 0012-64 (naca001264-il) Reynolds number: 500,000 Max Cl/Cd: 53.21 at α=9.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-naca001264-il-500000-n5.txt Download as CSV file: xf-naca001264-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NACA 0012-64
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -1.1137 0.10212 0.09899 -0.0206 1.0000 0.0147
-18.000 -1.1675 0.08763 0.08425 -0.0288 1.0000 0.0145
-17.750 -1.2008 0.07746 0.07387 -0.0347 1.0000 0.0145
-17.500 -1.2231 0.06970 0.06593 -0.0391 1.0000 0.0145
-17.250 -1.2384 0.06357 0.05964 -0.0424 1.0000 0.0147
-17.000 -1.2488 0.05858 0.05452 -0.0448 1.0000 0.0148
-16.750 -1.2555 0.05443 0.05023 -0.0465 1.0000 0.0151
-16.500 -1.2595 0.05090 0.04657 -0.0476 1.0000 0.0154
-16.250 -1.2619 0.04775 0.04329 -0.0482 1.0000 0.0157
-16.000 -1.2626 0.04497 0.04037 -0.0485 1.0000 0.0160
-15.750 -1.2620 0.04247 0.03774 -0.0485 1.0000 0.0164
-15.500 -1.2603 0.04020 0.03533 -0.0481 1.0000 0.0168
-15.250 -1.2571 0.03816 0.03314 -0.0475 1.0000 0.0172
-15.000 -1.2537 0.03627 0.03113 -0.0466 1.0000 0.0175
-14.750 -1.2480 0.03467 0.02947 -0.0457 1.0000 0.0179
-14.500 -1.2400 0.03334 0.02806 -0.0447 1.0000 0.0182
-14.250 -1.2306 0.03216 0.02680 -0.0436 1.0000 0.0186
-14.000 -1.2206 0.03106 0.02561 -0.0424 1.0000 0.0191
-13.750 -1.2102 0.03002 0.02448 -0.0411 1.0000 0.0196
-13.500 -1.1992 0.02904 0.02339 -0.0397 1.0000 0.0201
-13.250 -1.1876 0.02811 0.02236 -0.0382 1.0000 0.0207
-13.000 -1.1752 0.02726 0.02138 -0.0367 1.0000 0.0212
-12.750 -1.1627 0.02644 0.02045 -0.0351 1.0000 0.0216
-12.500 -1.1532 0.02544 0.01940 -0.0330 1.0000 0.0221
-12.250 -1.1411 0.02470 0.01861 -0.0312 1.0000 0.0225
-12.000 -1.1278 0.02409 0.01795 -0.0293 1.0000 0.0230
-11.750 -1.1147 0.02354 0.01734 -0.0273 1.0000 0.0236
-11.500 -1.1023 0.02301 0.01675 -0.0250 1.0000 0.0242
-11.250 -1.0912 0.02250 0.01617 -0.0223 1.0000 0.0247
-11.000 -1.0805 0.02201 0.01560 -0.0195 1.0000 0.0253
-10.750 -1.0679 0.02152 0.01503 -0.0170 1.0000 0.0257
-10.500 -1.0548 0.02110 0.01453 -0.0145 1.0000 0.0262
-10.250 -1.0425 0.02064 0.01400 -0.0119 1.0000 0.0266
-10.000 -1.0339 0.01992 0.01325 -0.0086 1.0000 0.0272
-9.750 -1.0231 0.01941 0.01270 -0.0057 1.0000 0.0278
-9.500 -1.0086 0.01896 0.01223 -0.0034 0.9998 0.0284
-9.250 -0.9809 0.01844 0.01167 -0.0040 0.9980 0.0291
-9.000 -0.9528 0.01793 0.01110 -0.0046 0.9962 0.0299
-8.750 -0.9242 0.01741 0.01054 -0.0053 0.9945 0.0306
-8.500 -0.8960 0.01695 0.01001 -0.0058 0.9927 0.0314
-8.250 -0.8684 0.01651 0.00951 -0.0062 0.9902 0.0320
-8.000 -0.8401 0.01603 0.00898 -0.0067 0.9880 0.0324
-7.750 -0.8121 0.01540 0.00832 -0.0073 0.9859 0.0334
-7.500 -0.7822 0.01491 0.00782 -0.0082 0.9844 0.0344
-7.250 -0.7536 0.01451 0.00740 -0.0087 0.9820 0.0355
-7.000 -0.7258 0.01413 0.00700 -0.0090 0.9789 0.0365
-6.750 -0.6960 0.01377 0.00660 -0.0097 0.9766 0.0375
-6.500 -0.6655 0.01342 0.00622 -0.0106 0.9745 0.0385
-6.250 -0.6346 0.01307 0.00585 -0.0115 0.9727 0.0398
-6.000 -0.6084 0.01272 0.00551 -0.0114 0.9687 0.0419
-5.750 -0.5809 0.01241 0.00520 -0.0115 0.9649 0.0444
-5.500 -0.5515 0.01212 0.00492 -0.0120 0.9619 0.0478
-5.250 -0.5219 0.01179 0.00463 -0.0126 0.9594 0.0544
-5.000 -0.4973 0.01152 0.00439 -0.0121 0.9539 0.0626
-4.750 -0.4703 0.01124 0.00416 -0.0120 0.9495 0.0723
-4.500 -0.4419 0.01098 0.00392 -0.0123 0.9460 0.0826
-4.000 -0.3906 0.01047 0.00353 -0.0116 0.9354 0.1089
-3.750 -0.3639 0.01016 0.00331 -0.0115 0.9309 0.1310
-3.500 -0.3389 0.00986 0.00314 -0.0110 0.9254 0.1596
-3.250 -0.3143 0.00955 0.00296 -0.0105 0.9191 0.1928
-3.000 -0.2888 0.00920 0.00276 -0.0101 0.9140 0.2335
-2.750 -0.2667 0.00874 0.00257 -0.0091 0.9070 0.2986
-2.500 -0.2450 0.00819 0.00236 -0.0081 0.9004 0.3850
-2.250 -0.2248 0.00762 0.00218 -0.0067 0.8936 0.4837
-2.000 -0.2037 0.00718 0.00205 -0.0053 0.8862 0.5641
-1.750 -0.1802 0.00690 0.00197 -0.0044 0.8797 0.6175
-1.500 -0.1555 0.00673 0.00191 -0.0036 0.8721 0.6542
-1.250 -0.1301 0.00657 0.00187 -0.0030 0.8656 0.6928
-1.000 -0.1052 0.00644 0.00187 -0.0022 0.8575 0.7276
-0.750 -0.0787 0.00636 0.00185 -0.0017 0.8505 0.7541
-0.500 -0.0528 0.00630 0.00188 -0.0011 0.8419 0.7792
-0.250 -0.0263 0.00627 0.00188 -0.0006 0.8329 0.8017
0.000 0.0000 0.00626 0.00188 0.0000 0.8196 0.8196
0.250 0.0264 0.00627 0.00188 0.0006 0.8018 0.8329
0.500 0.0529 0.00630 0.00188 0.0011 0.7793 0.8419
0.750 0.0788 0.00636 0.00185 0.0017 0.7537 0.8505
1.000 0.1053 0.00644 0.00187 0.0022 0.7275 0.8575
1.250 0.1302 0.00657 0.00187 0.0029 0.6928 0.8656
1.500 0.1555 0.00673 0.00191 0.0036 0.6542 0.8721
1.750 0.1803 0.00690 0.00197 0.0044 0.6180 0.8797
2.000 0.2037 0.00718 0.00205 0.0053 0.5637 0.8862
2.250 0.2248 0.00762 0.00218 0.0067 0.4839 0.8936
2.500 0.2450 0.00819 0.00236 0.0081 0.3851 0.9004
2.750 0.2668 0.00874 0.00257 0.0091 0.2983 0.9070
3.000 0.2889 0.00920 0.00276 0.0101 0.2336 0.9140
3.250 0.3144 0.00955 0.00296 0.0104 0.1928 0.9190
3.500 0.3390 0.00986 0.00314 0.0110 0.1597 0.9253
3.750 0.3639 0.01016 0.00331 0.0115 0.1310 0.9309
4.000 0.3907 0.01047 0.00353 0.0116 0.1090 0.9354
4.500 0.4419 0.01098 0.00392 0.0123 0.0826 0.9460
4.750 0.4704 0.01124 0.00416 0.0120 0.0723 0.9495
5.000 0.4973 0.01152 0.00439 0.0121 0.0626 0.9540
5.250 0.5219 0.01179 0.00462 0.0126 0.0545 0.9594
5.500 0.5515 0.01212 0.00491 0.0120 0.0479 0.9619
5.750 0.5810 0.01241 0.00520 0.0115 0.0444 0.9649
6.000 0.6085 0.01272 0.00551 0.0114 0.0419 0.9687
6.250 0.6347 0.01307 0.00585 0.0115 0.0398 0.9727
6.500 0.6656 0.01342 0.00622 0.0106 0.0385 0.9745
6.750 0.6960 0.01376 0.00660 0.0097 0.0375 0.9766
7.000 0.7258 0.01413 0.00700 0.0090 0.0365 0.9790
7.250 0.7536 0.01451 0.00740 0.0087 0.0355 0.9821
7.500 0.7822 0.01491 0.00782 0.0082 0.0344 0.9844
7.750 0.8121 0.01540 0.00832 0.0073 0.0334 0.9859
8.000 0.8401 0.01603 0.00898 0.0067 0.0324 0.9880
8.250 0.8684 0.01650 0.00951 0.0062 0.0320 0.9903
8.500 0.8961 0.01695 0.01001 0.0058 0.0314 0.9927
8.750 0.9243 0.01741 0.01054 0.0053 0.0306 0.9946
9.000 0.9530 0.01793 0.01110 0.0046 0.0299 0.9962
9.250 0.9811 0.01845 0.01167 0.0039 0.0291 0.9981
9.500 1.0088 0.01896 0.01223 0.0034 0.0284 0.9998
9.750 1.0230 0.01941 0.01270 0.0057 0.0278 1.0000
10.000 1.0339 0.01992 0.01325 0.0086 0.0272 1.0000
10.250 1.0425 0.02064 0.01400 0.0119 0.0266 1.0000
10.500 1.0548 0.02109 0.01453 0.0145 0.0262 1.0000
10.750 1.0680 0.02152 0.01503 0.0170 0.0257 1.0000
11.000 1.0806 0.02201 0.01559 0.0195 0.0253 1.0000
11.250 1.0915 0.02250 0.01617 0.0223 0.0247 1.0000
11.500 1.1027 0.02300 0.01674 0.0249 0.0242 1.0000
11.750 1.1152 0.02353 0.01733 0.0272 0.0236 1.0000
12.000 1.1284 0.02409 0.01794 0.0292 0.0230 1.0000
12.250 1.1417 0.02470 0.01861 0.0310 0.0225 1.0000
12.500 1.1539 0.02544 0.01939 0.0329 0.0221 1.0000
12.750 1.1633 0.02644 0.02046 0.0350 0.0216 1.0000
13.000 1.1760 0.02726 0.02138 0.0366 0.0212 1.0000
13.250 1.1885 0.02811 0.02236 0.0381 0.0207 1.0000
13.500 1.2002 0.02904 0.02339 0.0395 0.0201 1.0000
13.750 1.2113 0.03001 0.02447 0.0409 0.0196 1.0000
14.000 1.2219 0.03104 0.02559 0.0422 0.0191 1.0000
14.250 1.2319 0.03214 0.02678 0.0434 0.0186 1.0000
14.500 1.2414 0.03332 0.02804 0.0445 0.0182 1.0000
14.750 1.2495 0.03465 0.02944 0.0455 0.0179 1.0000
15.000 1.2552 0.03625 0.03111 0.0464 0.0175 1.0000
15.250 1.2588 0.03814 0.03312 0.0472 0.0171 1.0000
15.500 1.2620 0.04018 0.03531 0.0478 0.0168 1.0000
15.750 1.2639 0.04243 0.03771 0.0482 0.0164 1.0000
16.000 1.2646 0.04493 0.04034 0.0482 0.0160 1.0000
16.250 1.2643 0.04768 0.04322 0.0479 0.0156 1.0000
16.500 1.2623 0.05077 0.04643 0.0473 0.0153 1.0000
16.750 1.2583 0.05431 0.05011 0.0462 0.0150 1.0000
17.000 1.2514 0.05849 0.05443 0.0445 0.0148 1.0000
17.250 1.2413 0.06344 0.05951 0.0421 0.0146 1.0000
17.500 1.2261 0.06956 0.06578 0.0388 0.0145 1.0000
17.750 1.2040 0.07730 0.07370 0.0343 0.0144 1.0000
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