S1048 14% (Danny Howell) (s1048-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: S1048 14% (Danny Howell) (s1048-il) Reynolds number: 50,000 Max Cl/Cd: 28.26 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-s1048-il-50000-n5.txt Download as CSV file: xf-s1048-il-50000-n5.csv |
XFOIL Version 6.96
Calculated polar for: S1048 14% (Danny Howell)
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-14.500 -0.7333 0.12351 0.11638 -0.0009 1.0000 0.0536
-14.250 -0.7618 0.11175 0.10457 -0.0074 1.0000 0.0528
-14.000 -0.7901 0.10115 0.09382 -0.0134 1.0000 0.0523
-13.750 -0.8129 0.09255 0.08501 -0.0182 1.0000 0.0521
-13.500 -0.8311 0.08539 0.07762 -0.0220 1.0000 0.0527
-13.250 -0.8456 0.07921 0.07117 -0.0250 1.0000 0.0537
-13.000 -0.8557 0.07392 0.06558 -0.0272 1.0000 0.0548
-12.750 -0.8548 0.07062 0.06232 -0.0277 1.0000 0.0572
-12.500 -0.8552 0.06722 0.05885 -0.0284 1.0000 0.0598
-12.250 -0.8576 0.06355 0.05501 -0.0293 1.0000 0.0629
-12.000 -0.8606 0.05974 0.05091 -0.0300 1.0000 0.0669
-11.750 -0.8605 0.05694 0.04823 -0.0302 1.0000 0.0713
-11.500 -0.8607 0.05388 0.04502 -0.0304 1.0000 0.0767
-11.250 -0.8602 0.05105 0.04216 -0.0302 1.0000 0.0822
-11.000 -0.8614 0.04822 0.03925 -0.0300 1.0000 0.0897
-10.750 -0.8634 0.04556 0.03663 -0.0297 1.0000 0.0975
-10.500 -0.8653 0.04300 0.03405 -0.0290 1.0000 0.1074
-10.250 -0.8678 0.04065 0.03168 -0.0279 1.0000 0.1193
-10.000 -0.8704 0.03857 0.02962 -0.0263 1.0000 0.1323
-9.750 -0.8734 0.03677 0.02788 -0.0241 1.0000 0.1468
-9.500 -0.8744 0.03520 0.02640 -0.0217 1.0000 0.1632
-9.250 -0.8722 0.03380 0.02500 -0.0195 1.0000 0.1829
-9.000 -0.8670 0.03256 0.02377 -0.0173 1.0000 0.2037
-8.750 -0.8591 0.03154 0.02278 -0.0152 1.0000 0.2248
-8.500 -0.8490 0.03062 0.02181 -0.0132 1.0000 0.2462
-8.250 -0.8365 0.02990 0.02108 -0.0112 1.0000 0.2667
-8.000 -0.8236 0.02914 0.02021 -0.0094 1.0000 0.2878
-7.750 -0.8075 0.02863 0.01971 -0.0076 1.0000 0.3067
-7.500 -0.7912 0.02809 0.01907 -0.0059 1.0000 0.3254
-7.250 -0.7746 0.02752 0.01839 -0.0042 1.0000 0.3437
-7.000 -0.7572 0.02700 0.01778 -0.0026 1.0000 0.3611
-6.750 -0.7385 0.02659 0.01732 -0.0010 1.0000 0.3774
-6.500 -0.7199 0.02616 0.01683 0.0005 1.0000 0.3931
-6.250 -0.7013 0.02576 0.01634 0.0021 1.0000 0.4086
-6.000 -0.6828 0.02535 0.01587 0.0037 1.0000 0.4236
-5.750 -0.6645 0.02496 0.01542 0.0054 1.0000 0.4382
-5.500 -0.6465 0.02458 0.01499 0.0070 1.0000 0.4525
-5.250 -0.6289 0.02422 0.01458 0.0086 1.0000 0.4665
-5.000 -0.6119 0.02388 0.01419 0.0104 1.0000 0.4804
-4.750 -0.5956 0.02356 0.01380 0.0122 1.0000 0.4941
-4.500 -0.5801 0.02328 0.01347 0.0140 1.0000 0.5077
-4.250 -0.5645 0.02308 0.01327 0.0159 1.0000 0.5201
-4.000 -0.5497 0.02290 0.01307 0.0178 1.0000 0.5327
-3.750 -0.5266 0.02276 0.01287 0.0181 0.9954 0.5467
-3.500 -0.4849 0.02267 0.01271 0.0150 0.9805 0.5634
-3.250 -0.4444 0.02258 0.01254 0.0122 0.9654 0.5797
-3.000 -0.4036 0.02248 0.01235 0.0095 0.9510 0.5958
-2.750 -0.3621 0.02239 0.01221 0.0067 0.9373 0.6117
-2.500 -0.3198 0.02230 0.01208 0.0040 0.9243 0.6271
-2.250 -0.2804 0.02221 0.01195 0.0019 0.9102 0.6423
-2.000 -0.2431 0.02211 0.01182 0.0003 0.8955 0.6572
-1.750 -0.2075 0.02202 0.01170 -0.0009 0.8806 0.6720
-1.500 -0.1735 0.02194 0.01158 -0.0017 0.8656 0.6867
-1.250 -0.1418 0.02187 0.01149 -0.0020 0.8502 0.7013
-1.000 -0.1118 0.02182 0.01142 -0.0020 0.8346 0.7156
-0.750 -0.0829 0.02178 0.01138 -0.0017 0.8191 0.7298
-0.500 -0.0548 0.02176 0.01135 -0.0012 0.8038 0.7443
-0.250 -0.0273 0.02174 0.01132 -0.0006 0.7885 0.7588
0.000 0.0000 0.02174 0.01132 0.0000 0.7736 0.7736
0.250 0.0273 0.02174 0.01132 0.0006 0.7588 0.7885
0.500 0.0548 0.02176 0.01134 0.0012 0.7443 0.8037
0.750 0.0829 0.02178 0.01137 0.0017 0.7298 0.8190
1.000 0.1119 0.02182 0.01142 0.0020 0.7156 0.8346
1.250 0.1418 0.02187 0.01149 0.0020 0.7013 0.8502
1.500 0.1735 0.02194 0.01158 0.0017 0.6867 0.8656
1.750 0.2075 0.02202 0.01171 0.0009 0.6720 0.8807
2.000 0.2432 0.02211 0.01182 -0.0003 0.6572 0.8955
2.250 0.2804 0.02221 0.01195 -0.0019 0.6423 0.9102
2.500 0.3198 0.02230 0.01209 -0.0040 0.6271 0.9243
2.750 0.3621 0.02239 0.01221 -0.0067 0.6117 0.9373
3.000 0.4037 0.02248 0.01235 -0.0095 0.5958 0.9510
3.250 0.4445 0.02258 0.01254 -0.0122 0.5797 0.9655
3.500 0.4850 0.02267 0.01271 -0.0150 0.5633 0.9805
3.750 0.5266 0.02276 0.01290 -0.0181 0.5467 0.9954
4.000 0.5497 0.02289 0.01307 -0.0178 0.5327 1.0000
4.250 0.5645 0.02308 0.01327 -0.0159 0.5202 1.0000
4.500 0.5801 0.02328 0.01347 -0.0140 0.5077 1.0000
4.750 0.5956 0.02356 0.01380 -0.0122 0.4941 1.0000
5.000 0.6119 0.02388 0.01419 -0.0104 0.4804 1.0000
5.250 0.6289 0.02422 0.01458 -0.0086 0.4665 1.0000
5.500 0.6465 0.02458 0.01499 -0.0070 0.4525 1.0000
5.750 0.6646 0.02496 0.01542 -0.0054 0.4382 1.0000
6.000 0.6828 0.02535 0.01587 -0.0037 0.4236 1.0000
6.250 0.7013 0.02575 0.01633 -0.0021 0.4086 1.0000
6.500 0.7199 0.02616 0.01683 -0.0006 0.3931 1.0000
6.750 0.7386 0.02658 0.01731 0.0010 0.3773 1.0000
7.000 0.7573 0.02701 0.01779 0.0026 0.3612 1.0000
7.250 0.7746 0.02752 0.01839 0.0042 0.3437 1.0000
7.500 0.7912 0.02809 0.01907 0.0059 0.3255 1.0000
7.750 0.8076 0.02863 0.01970 0.0076 0.3067 1.0000
8.000 0.8236 0.02914 0.02021 0.0094 0.2877 1.0000
8.250 0.8365 0.02989 0.02108 0.0112 0.2667 1.0000
8.500 0.8490 0.03062 0.02181 0.0132 0.2462 1.0000
8.750 0.8591 0.03154 0.02278 0.0152 0.2247 1.0000
9.000 0.8670 0.03256 0.02377 0.0173 0.2037 1.0000
9.250 0.8722 0.03379 0.02499 0.0195 0.1828 1.0000
9.500 0.8745 0.03520 0.02640 0.0217 0.1631 1.0000
9.750 0.8734 0.03677 0.02788 0.0241 0.1466 1.0000
10.000 0.8704 0.03857 0.02961 0.0263 0.1322 1.0000
10.250 0.8679 0.04066 0.03168 0.0279 0.1191 1.0000
10.500 0.8653 0.04301 0.03404 0.0289 0.1072 1.0000
10.750 0.8639 0.04554 0.03662 0.0296 0.0975 1.0000
11.000 0.8618 0.04822 0.03925 0.0300 0.0896 1.0000
11.250 0.8608 0.05103 0.04214 0.0301 0.0822 1.0000
11.500 0.8613 0.05387 0.04501 0.0303 0.0766 1.0000
11.750 0.8611 0.05693 0.04821 0.0302 0.0712 1.0000
12.000 0.8617 0.05969 0.05086 0.0300 0.0670 1.0000
12.250 0.8580 0.06355 0.05502 0.0291 0.0628 1.0000
12.500 0.8561 0.06720 0.05883 0.0284 0.0598 1.0000
12.750 0.8559 0.07059 0.06229 0.0277 0.0573 1.0000
13.000 0.8565 0.07393 0.06560 0.0271 0.0547 1.0000
13.250 0.8461 0.07927 0.07124 0.0249 0.0536 1.0000
13.500 0.8309 0.08556 0.07779 0.0217 0.0525 1.0000
13.750 0.8130 0.09273 0.08519 0.0180 0.0520 1.0000
14.000 0.7901 0.10137 0.09404 0.0132 0.0523 1.0000
14.250 0.7618 0.11202 0.10484 0.0071 0.0528 1.0000
14.500 0.7336 0.12374 0.11662 0.0007 0.0536 1.0000
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