GOE 344 (PFALZ 71) AIRFOIL (goe344-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 344 (PFALZ 71) AIRFOIL (goe344-il) Reynolds number: 1,000,000 Max Cl/Cd: 89 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe344-il-1000000-n5.txt Download as CSV file: xf-goe344-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 344 (PFALZ 71) 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
------ -------- --------- --------- -------- -------- --------
-13.000 -0.6290 0.13110 0.12931 0.0041 1.0000 0.0076
-12.750 -0.6254 0.12749 0.12571 0.0026 1.0000 0.0078
-12.250 -1.0588 0.02848 0.02528 -0.0506 1.0000 0.0070
-12.000 -1.0464 0.02566 0.02219 -0.0497 1.0000 0.0071
-11.750 -1.0300 0.02382 0.02015 -0.0487 1.0000 0.0073
-11.500 -1.0132 0.02200 0.01814 -0.0477 1.0000 0.0076
-11.250 -0.9946 0.02058 0.01656 -0.0467 1.0000 0.0080
-11.000 -0.9747 0.01943 0.01528 -0.0457 1.0000 0.0085
-10.750 -0.9537 0.01848 0.01421 -0.0448 1.0000 0.0090
-10.500 -0.9321 0.01766 0.01327 -0.0439 1.0000 0.0094
-10.250 -0.9100 0.01694 0.01242 -0.0429 1.0000 0.0098
-10.000 -0.8879 0.01617 0.01155 -0.0420 1.0000 0.0106
-9.750 -0.8652 0.01553 0.01085 -0.0412 1.0000 0.0114
-9.500 -0.8422 0.01498 0.01023 -0.0403 1.0000 0.0122
-9.250 -0.8190 0.01449 0.00965 -0.0395 1.0000 0.0130
-9.000 -0.7954 0.01406 0.00918 -0.0386 1.0000 0.0140
-8.750 -0.7715 0.01375 0.00886 -0.0378 1.0000 0.0152
-8.500 -0.7476 0.01346 0.00854 -0.0370 1.0000 0.0163
-8.250 -0.7230 0.01317 0.00819 -0.0363 0.9999 0.0171
-8.000 -0.6935 0.01283 0.00782 -0.0368 0.9994 0.0180
-7.750 -0.6633 0.01261 0.00759 -0.0373 0.9987 0.0189
-7.500 -0.6323 0.01240 0.00736 -0.0380 0.9978 0.0198
-7.250 -0.6007 0.01218 0.00711 -0.0389 0.9969 0.0207
-7.000 -0.5685 0.01197 0.00686 -0.0398 0.9960 0.0215
-6.750 -0.5356 0.01175 0.00660 -0.0409 0.9951 0.0221
-6.500 -0.5025 0.01154 0.00634 -0.0420 0.9940 0.0225
-6.250 -0.4712 0.01114 0.00588 -0.0428 0.9920 0.0231
-6.000 -0.4394 0.01066 0.00535 -0.0437 0.9901 0.0242
-5.750 -0.4069 0.01037 0.00505 -0.0447 0.9885 0.0251
-5.500 -0.3746 0.01013 0.00479 -0.0457 0.9871 0.0259
-5.250 -0.3424 0.00987 0.00450 -0.0466 0.9861 0.0266
-5.000 -0.3116 0.00960 0.00420 -0.0472 0.9844 0.0272
-4.750 -0.2820 0.00935 0.00392 -0.0475 0.9809 0.0278
-4.500 -0.2488 0.00909 0.00363 -0.0486 0.9777 0.0283
-4.250 -0.2166 0.00883 0.00334 -0.0494 0.9734 0.0287
-4.000 -0.1868 0.00859 0.00308 -0.0497 0.9662 0.0290
-3.750 -0.1554 0.00836 0.00283 -0.0503 0.9581 0.0293
-3.500 -0.1213 0.00814 0.00258 -0.0516 0.9466 0.0295
-3.250 -0.0875 0.00792 0.00230 -0.0527 0.9290 0.0299
-3.000 -0.0578 0.00775 0.00203 -0.0529 0.9049 0.0310
-2.750 -0.0306 0.00767 0.00185 -0.0524 0.8790 0.0325
-2.500 -0.0044 0.00763 0.00170 -0.0518 0.8421 0.0344
-2.250 0.0196 0.00779 0.00157 -0.0507 0.7627 0.0360
-2.000 0.0449 0.00794 0.00150 -0.0500 0.7077 0.0377
-1.750 0.0716 0.00797 0.00143 -0.0497 0.6759 0.0425
-1.500 0.0984 0.00796 0.00136 -0.0494 0.6438 0.0541
-1.250 0.1252 0.00797 0.00131 -0.0491 0.6090 0.0699
-1.000 0.1523 0.00801 0.00128 -0.0489 0.5770 0.0798
-0.750 0.1795 0.00806 0.00125 -0.0487 0.5490 0.0889
-0.500 0.2067 0.00810 0.00125 -0.0485 0.5219 0.1017
-0.250 0.2340 0.00815 0.00125 -0.0483 0.4965 0.1161
0.000 0.2615 0.00820 0.00126 -0.0482 0.4738 0.1262
0.250 0.2888 0.00829 0.00127 -0.0480 0.4444 0.1335
0.500 0.3158 0.00843 0.00129 -0.0478 0.4056 0.1419
0.750 0.3428 0.00855 0.00133 -0.0476 0.3718 0.1519
1.000 0.3700 0.00865 0.00137 -0.0474 0.3462 0.1644
1.250 0.3973 0.00874 0.00141 -0.0473 0.3265 0.1752
1.500 0.4247 0.00878 0.00146 -0.0472 0.3124 0.1966
1.750 0.4521 0.00875 0.00154 -0.0471 0.3009 0.2484
2.000 0.4796 0.00876 0.00162 -0.0470 0.2901 0.2913
2.250 0.5068 0.00873 0.00170 -0.0469 0.2805 0.3480
2.500 0.5205 0.00727 0.00184 -0.0439 0.2718 0.9341
2.750 0.5461 0.00740 0.00193 -0.0432 0.2556 0.9654
3.000 0.5755 0.00755 0.00202 -0.0434 0.2400 0.9780
3.250 0.6058 0.00772 0.00212 -0.0439 0.2247 0.9858
3.500 0.6381 0.00788 0.00223 -0.0449 0.2126 0.9907
3.750 0.6696 0.00805 0.00235 -0.0458 0.2011 0.9947
4.000 0.7049 0.00826 0.00248 -0.0475 0.1864 0.9970
4.250 0.7384 0.00846 0.00263 -0.0488 0.1735 0.9991
4.500 0.7672 0.00867 0.00278 -0.0491 0.1593 1.0000
4.750 0.7912 0.00889 0.00293 -0.0483 0.1436 1.0000
5.000 0.8150 0.00917 0.00312 -0.0475 0.1248 1.0000
5.250 0.8386 0.00948 0.00334 -0.0466 0.1053 1.0000
5.500 0.8623 0.00980 0.00357 -0.0458 0.0879 1.0000
5.750 0.8864 0.01010 0.00381 -0.0451 0.0749 1.0000
6.000 0.9109 0.01040 0.00407 -0.0444 0.0653 1.0000
6.250 0.9356 0.01070 0.00433 -0.0438 0.0579 1.0000
6.500 0.9608 0.01095 0.00457 -0.0433 0.0526 1.0000
6.750 0.9858 0.01125 0.00484 -0.0428 0.0478 1.0000
7.000 1.0111 0.01151 0.00511 -0.0424 0.0443 1.0000
7.250 1.0365 0.01176 0.00537 -0.0419 0.0416 1.0000
7.500 1.0616 0.01206 0.00566 -0.0415 0.0386 1.0000
7.750 1.0866 0.01237 0.00598 -0.0410 0.0353 1.0000
8.000 1.1118 0.01265 0.00628 -0.0406 0.0330 1.0000
8.250 1.1365 0.01300 0.00661 -0.0401 0.0296 1.0000
8.500 1.1612 0.01333 0.00696 -0.0396 0.0267 1.0000
8.750 1.1851 0.01375 0.00735 -0.0391 0.0217 1.0000
9.000 1.2086 0.01422 0.00780 -0.0384 0.0167 1.0000
9.250 1.2320 0.01469 0.00828 -0.0378 0.0140 1.0000
9.500 1.2551 0.01519 0.00879 -0.0371 0.0119 1.0000
9.750 1.2785 0.01562 0.00927 -0.0364 0.0110 1.0000
10.000 1.3012 0.01611 0.00980 -0.0357 0.0100 1.0000
10.250 1.3233 0.01668 0.01040 -0.0349 0.0090 1.0000
10.500 1.3455 0.01719 0.01099 -0.0341 0.0085 1.0000
10.750 1.3675 0.01770 0.01154 -0.0333 0.0079 1.0000
11.000 1.3889 0.01825 0.01215 -0.0324 0.0074 1.0000
11.250 1.4094 0.01887 0.01282 -0.0314 0.0069 1.0000
11.500 1.4288 0.01958 0.01358 -0.0302 0.0065 1.0000
11.750 1.4481 0.02026 0.01434 -0.0291 0.0062 1.0000
12.000 1.4674 0.02090 0.01506 -0.0279 0.0060 1.0000
12.250 1.4858 0.02157 0.01582 -0.0266 0.0058 1.0000
12.500 1.5032 0.02229 0.01661 -0.0253 0.0056 1.0000
12.750 1.5196 0.02306 0.01746 -0.0238 0.0054 1.0000
13.000 1.5346 0.02388 0.01836 -0.0221 0.0052 1.0000
13.250 1.5478 0.02476 0.01932 -0.0201 0.0050 1.0000
13.500 1.5584 0.02571 0.02035 -0.0178 0.0048 1.0000
13.750 1.5638 0.02678 0.02151 -0.0147 0.0046 1.0000
14.000 1.5661 0.02810 0.02295 -0.0114 0.0044 1.0000
14.250 1.5721 0.02925 0.02419 -0.0089 0.0044 1.0000
14.500 1.5767 0.03056 0.02562 -0.0065 0.0043 1.0000
14.750 1.5799 0.03208 0.02724 -0.0044 0.0042 1.0000
15.000 1.5817 0.03383 0.02910 -0.0025 0.0041 1.0000
15.250 1.5819 0.03589 0.03128 -0.0010 0.0041 1.0000
15.500 1.5801 0.03834 0.03386 0.0001 0.0040 1.0000
15.750 1.5758 0.04137 0.03702 0.0004 0.0039 1.0000
16.000 1.5696 0.04509 0.04088 -0.0003 0.0039 1.0000
16.250 1.5599 0.04981 0.04575 -0.0021 0.0039 1.0000
16.500 1.5470 0.05546 0.05157 -0.0048 0.0038 1.0000
16.750 1.5283 0.06249 0.05877 -0.0085 0.0038 1.0000
17.000 1.5023 0.07099 0.06745 -0.0130 0.0038 1.0000
17.250 1.4706 0.08067 0.07731 -0.0180 0.0038 1.0000
17.500 1.4310 0.09168 0.08849 -0.0234 0.0039 1.0000
17.750 1.3907 0.10276 0.09974 -0.0287 0.0039 1.0000
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