GOE 562 AIRFOIL (goe562-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 562 AIRFOIL (goe562-il) Reynolds number: 500,000 Max Cl/Cd: 96.65 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe562-il-500000-n5.txt Download as CSV file: xf-goe562-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 562 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-10.750 0.0146 0.09025 0.08659 -0.1145 0.7199 0.0120
-10.500 0.0220 0.08728 0.08351 -0.1165 0.6987 0.0127
-10.250 0.0249 0.08359 0.07974 -0.1184 0.6823 0.0132
-10.000 0.0265 0.07983 0.07592 -0.1203 0.6687 0.0133
-9.750 0.0235 0.07539 0.07146 -0.1226 0.6601 0.0141
-9.500 0.0312 0.07320 0.06920 -0.1238 0.6473 0.0142
-9.250 0.0369 0.07074 0.06671 -0.1251 0.6375 0.0145
-9.000 0.0402 0.06797 0.06392 -0.1265 0.6312 0.0147
-8.750 0.0419 0.06517 0.06111 -0.1279 0.6227 0.0152
-8.500 0.0343 0.06136 0.05730 -0.1300 0.6170 0.0155
-8.250 0.0203 0.05773 0.05369 -0.1306 0.6119 0.0156
-8.000 0.0020 0.05310 0.04903 -0.1309 0.6073 0.0162
-7.750 -0.0352 0.04399 0.03975 -0.1305 0.6047 0.0173
-7.500 -0.0238 0.04281 0.03849 -0.1295 0.5989 0.0177
-7.250 -0.0143 0.04108 0.03668 -0.1282 0.5934 0.0180
-6.750 -0.0580 0.02635 0.02094 -0.1166 0.5872 0.0213
-6.500 -0.0405 0.02594 0.02044 -0.1151 0.5817 0.0216
-6.250 -0.0233 0.02531 0.01970 -0.1134 0.5760 0.0219
-6.000 -0.0068 0.02453 0.01878 -0.1116 0.5708 0.0222
-5.750 0.0104 0.02382 0.01793 -0.1098 0.5658 0.0227
-5.500 0.0263 0.02269 0.01663 -0.1077 0.5612 0.0234
-5.250 0.0400 0.02112 0.01478 -0.1050 0.5565 0.0245
-5.000 0.0525 0.01921 0.01246 -0.1019 0.5522 0.0256
-4.750 0.0710 0.01821 0.01118 -0.0999 0.5475 0.0261
-4.500 0.0895 0.01721 0.01002 -0.0981 0.5426 0.0268
-4.250 0.1105 0.01675 0.00946 -0.0968 0.5377 0.0272
-4.000 0.1324 0.01630 0.00890 -0.0956 0.5334 0.0276
-3.750 0.1549 0.01581 0.00831 -0.0945 0.5290 0.0281
-3.500 0.1773 0.01530 0.00768 -0.0933 0.5244 0.0285
-3.250 0.1998 0.01491 0.00717 -0.0922 0.5201 0.0290
-3.000 0.2234 0.01448 0.00667 -0.0912 0.5156 0.0296
-2.750 0.2465 0.01417 0.00626 -0.0902 0.5098 0.0304
-2.500 0.2691 0.01383 0.00582 -0.0890 0.5046 0.0309
-2.250 0.2928 0.01349 0.00541 -0.0881 0.4999 0.0314
-2.000 0.3160 0.01318 0.00503 -0.0871 0.4951 0.0316
-1.750 0.3387 0.01296 0.00475 -0.0860 0.4907 0.0320
-1.500 0.3618 0.01281 0.00454 -0.0849 0.4868 0.0324
-1.250 0.3839 0.01245 0.00415 -0.0837 0.4822 0.0328
-1.000 0.4043 0.01222 0.00387 -0.0821 0.4756 0.0333
-0.750 0.4253 0.01205 0.00368 -0.0807 0.4708 0.0342
-0.500 0.4474 0.01193 0.00355 -0.0794 0.4666 0.0350
-0.250 0.4691 0.01183 0.00344 -0.0781 0.4626 0.0360
0.000 0.4902 0.01177 0.00333 -0.0767 0.4588 0.0367
0.250 0.5119 0.01169 0.00323 -0.0754 0.4547 0.0376
0.500 0.5340 0.01162 0.00315 -0.0741 0.4503 0.0386
0.750 0.5551 0.01159 0.00307 -0.0727 0.4452 0.0395
1.000 0.5763 0.01158 0.00303 -0.0713 0.4412 0.0403
1.250 0.5986 0.01151 0.00296 -0.0702 0.4366 0.0427
1.500 0.6201 0.01151 0.00294 -0.0689 0.4313 0.0446
1.750 0.6413 0.01155 0.00295 -0.0675 0.4272 0.0484
2.000 0.6636 0.01155 0.00296 -0.0664 0.4234 0.0548
2.250 0.6859 0.01155 0.00299 -0.0653 0.4198 0.0698
2.500 0.7021 0.01086 0.00322 -0.0634 0.4161 0.4395
3.000 1.0132 0.01104 0.00443 -0.1218 0.3963 1.0000
3.250 1.0346 0.01115 0.00452 -0.1206 0.3924 1.0000
3.500 1.0558 0.01126 0.00462 -0.1193 0.3878 1.0000
3.750 1.0761 0.01141 0.00474 -0.1179 0.3831 1.0000
4.000 1.0960 0.01156 0.00486 -0.1164 0.3789 1.0000
4.250 1.1168 0.01168 0.00498 -0.1151 0.3740 1.0000
4.500 1.1363 0.01183 0.00512 -0.1135 0.3687 1.0000
4.750 1.1547 0.01200 0.00527 -0.1118 0.3636 1.0000
5.000 1.1732 0.01214 0.00541 -0.1100 0.3580 1.0000
5.250 1.1893 0.01232 0.00557 -0.1077 0.3520 1.0000
5.500 1.2062 0.01248 0.00574 -0.1057 0.3458 1.0000
5.750 1.2222 0.01267 0.00591 -0.1034 0.3388 1.0000
6.000 1.2382 0.01288 0.00611 -0.1012 0.3315 1.0000
6.250 1.2516 0.01317 0.00634 -0.0985 0.3199 1.0000
6.500 1.2660 0.01344 0.00660 -0.0961 0.3100 1.0000
6.750 1.2782 0.01380 0.00690 -0.0933 0.2968 1.0000
7.000 1.2922 0.01411 0.00719 -0.0908 0.2887 1.0000
7.250 1.3023 0.01456 0.00758 -0.0877 0.2761 1.0000
7.500 1.3144 0.01497 0.00797 -0.0850 0.2665 1.0000
7.750 1.3238 0.01548 0.00843 -0.0819 0.2550 1.0000
8.250 1.3466 0.01641 0.00933 -0.0766 0.2407 1.0000
8.500 1.3583 0.01688 0.00982 -0.0741 0.2354 1.0000
8.750 1.3682 0.01745 0.01038 -0.0714 0.2288 1.0000
9.000 1.3778 0.01805 0.01097 -0.0687 0.2210 1.0000
9.250 1.3858 0.01875 0.01166 -0.0659 0.2146 1.0000
9.500 1.3971 0.01933 0.01228 -0.0637 0.2089 1.0000
9.750 1.4018 0.02028 0.01320 -0.0607 0.2007 1.0000
10.000 1.4120 0.02100 0.01396 -0.0586 0.1930 1.0000
10.250 1.4162 0.02210 0.01504 -0.0560 0.1810 1.0000
10.500 1.3959 0.02482 0.01751 -0.0510 0.1334 1.0000
10.750 1.3676 0.02855 0.02110 -0.0463 0.0947 1.0000
11.000 1.3459 0.03227 0.02475 -0.0431 0.0629 1.0000
11.250 1.3428 0.03469 0.02721 -0.0415 0.0535 1.0000
11.500 1.3386 0.03734 0.02988 -0.0401 0.0441 1.0000
11.750 1.3276 0.04074 0.03327 -0.0387 0.0244 1.0000
12.000 1.3193 0.04399 0.03653 -0.0375 0.0183 1.0000
12.250 1.3151 0.04690 0.03951 -0.0366 0.0160 1.0000
12.500 1.3133 0.04961 0.04231 -0.0359 0.0149 1.0000
12.750 1.3120 0.05235 0.04515 -0.0353 0.0141 1.0000
13.000 1.3093 0.05527 0.04815 -0.0347 0.0133 1.0000
13.250 1.3062 0.05829 0.05126 -0.0342 0.0128 1.0000
13.500 1.2994 0.06183 0.05489 -0.0338 0.0119 1.0000
13.750 1.2938 0.06530 0.05845 -0.0335 0.0114 1.0000
14.000 1.2902 0.06857 0.06181 -0.0333 0.0112 1.0000
14.250 1.2867 0.07190 0.06523 -0.0332 0.0109 1.0000
14.500 1.2824 0.07536 0.06879 -0.0332 0.0106 1.0000
14.750 1.2773 0.07901 0.07254 -0.0332 0.0104 1.0000
15.000 1.2723 0.08266 0.07629 -0.0333 0.0102 1.0000
15.250 1.2670 0.08639 0.08009 -0.0336 0.0094 1.0000
15.500 1.2608 0.09032 0.08412 -0.0338 0.0097 1.0000
15.750 1.2534 0.09447 0.08836 -0.0342 0.0092 1.0000
16.000 1.2464 0.09859 0.09256 -0.0347 0.0090 1.0000
16.250 1.2372 0.10309 0.09716 -0.0352 0.0089 1.0000
16.500 1.2294 0.10740 0.10154 -0.0359 0.0086 1.0000
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