GOE 559 AIRFOIL (goe559-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 559 AIRFOIL (goe559-il) Reynolds number: 500,000 Max Cl/Cd: 66.32 at α=1.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe559-il-500000.txt Download as CSV file: xf-goe559-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 559 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-9.000 -0.2387 0.08459 0.08275 -0.0400 1.0000 0.0030
-8.750 -0.2396 0.08126 0.07944 -0.0403 1.0000 0.0030
-8.500 -0.2414 0.07787 0.07608 -0.0405 1.0000 0.0030
-8.250 -0.2366 0.07349 0.07172 -0.0432 0.9946 0.0031
-8.000 -0.2295 0.06869 0.06693 -0.0467 0.9860 0.0032
-7.750 -0.2198 0.06368 0.06191 -0.0512 0.9756 0.0032
-7.500 -0.2083 0.05800 0.05622 -0.0572 0.9603 0.0032
-7.250 -0.1927 0.05193 0.05012 -0.0653 0.9381 0.0033
-7.000 -0.1868 0.04646 0.04454 -0.0733 0.9024 0.0032
-6.750 -0.1901 0.04260 0.04050 -0.0755 0.8609 0.0033
-6.500 -0.1913 0.03924 0.03693 -0.0761 0.8141 0.0032
-6.250 -0.1895 0.03577 0.03320 -0.0763 0.7757 0.0033
-6.000 -0.1840 0.03258 0.02977 -0.0763 0.7496 0.0034
-5.750 -0.1748 0.02943 0.02639 -0.0760 0.7298 0.0034
-5.500 -0.1622 0.02648 0.02320 -0.0754 0.7136 0.0035
-5.250 -0.1481 0.02376 0.02021 -0.0745 0.6989 0.0036
-5.000 -0.1324 0.02121 0.01740 -0.0733 0.6848 0.0036
-4.750 -0.1164 0.01865 0.01458 -0.0722 0.6708 0.0036
-4.500 -0.1072 0.01454 0.01029 -0.0716 0.6581 0.0039
-4.250 -0.0935 0.01176 0.00730 -0.0708 0.6441 0.0042
-4.000 -0.0749 0.00986 0.00513 -0.0698 0.6300 0.0045
-3.750 -0.0514 0.00873 0.00371 -0.0684 0.6158 0.0060
-3.500 -0.0242 0.00867 0.00325 -0.0666 0.6013 0.0066
-3.250 -0.0064 0.00632 0.00058 -0.0655 0.5911 0.0070
-3.000 -0.0360 0.14401 0.14018 -0.0445 0.5770 0.0122
-1.750 0.1425 0.01431 0.00683 -0.0649 0.5481 0.0160
-1.500 0.1690 0.01430 0.00655 -0.0642 0.5410 0.0217
-0.500 0.2670 0.01087 0.00287 -0.0610 0.5183 0.0163
-0.250 0.2921 0.01061 0.00247 -0.0604 0.5134 0.0099
0.000 0.3176 0.01034 0.00208 -0.0600 0.5086 0.0084
0.250 0.3438 0.01022 0.00179 -0.0597 0.5040 0.0097
0.500 0.3521 0.00835 0.00169 -0.0566 0.5006 0.6552
0.750 0.4905 0.00797 0.00204 -0.0807 0.4934 1.0000
1.000 0.5133 0.00801 0.00206 -0.0800 0.4896 1.0000
1.250 0.5365 0.00809 0.00213 -0.0795 0.4861 1.0000
1.500 0.5455 0.00880 0.00192 -0.0764 0.3013 1.0000
1.750 0.5505 0.01053 0.00284 -0.0726 0.0092 1.0000
2.000 0.5720 0.01076 0.00318 -0.0715 0.0084 1.0000
2.250 0.5922 0.01112 0.00369 -0.0700 0.0096 1.0000
2.500 0.6130 0.01144 0.00409 -0.0687 0.0137 1.0000
2.750 0.6359 0.01161 0.00436 -0.0674 0.0257 1.0000
3.000 0.6563 0.01202 0.00497 -0.0657 0.0347 1.0000
3.250 0.6712 0.01281 0.00587 -0.0632 0.0349 1.0000
3.500 0.6875 0.01347 0.00658 -0.0608 0.0297 1.0000
3.750 0.6947 0.01466 0.00783 -0.0572 0.0223 1.0000
4.000 0.7006 0.01595 0.00918 -0.0532 0.0173 1.0000
4.250 0.7132 0.01691 0.01017 -0.0504 0.0141 1.0000
4.500 0.7244 0.01896 0.01206 -0.0476 0.0118 1.0000
4.750 0.7448 0.01958 0.01283 -0.0458 0.0077 1.0000
5.000 0.7865 0.02446 0.01735 -0.0488 0.0060 1.0000
5.250 0.8044 0.02430 0.01747 -0.0461 0.0057 1.0000
5.500 0.8288 0.02465 0.01800 -0.0444 0.0047 1.0000
5.750 0.8564 0.02655 0.01999 -0.0438 0.0040 1.0000
6.000 0.8814 0.02932 0.02283 -0.0435 0.0036 1.0000
6.250 0.9067 0.03441 0.02795 -0.0435 0.0033 1.0000
6.500 0.9251 0.03572 0.02949 -0.0412 0.0033 1.0000
6.750 0.9453 0.03632 0.03035 -0.0385 0.0031 1.0000
7.000 0.9674 0.03767 0.03192 -0.0362 0.0029 1.0000
7.250 0.9858 0.03988 0.03433 -0.0341 0.0026 1.0000
7.500 1.0009 0.04234 0.03700 -0.0317 0.0024 1.0000
7.750 1.0136 0.04490 0.03977 -0.0292 0.0023 1.0000
8.000 1.0240 0.04765 0.04273 -0.0266 0.0021 1.0000
8.250 1.0322 0.05033 0.04562 -0.0240 0.0020 1.0000
8.500 1.0371 0.05325 0.04873 -0.0212 0.0019 1.0000
8.750 1.0382 0.05636 0.05205 -0.0183 0.0019 1.0000
9.000 1.0371 0.05946 0.05533 -0.0155 0.0018 1.0000
9.250 1.0326 0.06272 0.05876 -0.0128 0.0018 1.0000
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Polar data table (+)
Polar graphs
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