GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 776 AIRFOIL (goe776-il) Reynolds number: 200,000 Max Cl/Cd: 41.19 at α=10.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe776-il-200000.txt Download as CSV file: xf-goe776-il-200000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 776 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1498 0.09093 0.08445 -0.0532 1.0000 0.1299
-19.500 -1.1478 0.08825 0.08175 -0.0541 1.0000 0.1322
-19.250 -1.1685 0.08271 0.07603 -0.0560 1.0000 0.1346
-19.000 -1.2032 0.07573 0.06873 -0.0582 1.0000 0.1368
-18.750 -1.1825 0.07540 0.06852 -0.0579 1.0000 0.1392
-18.500 -1.1703 0.07408 0.06725 -0.0581 1.0000 0.1416
-18.250 -1.1738 0.07095 0.06405 -0.0588 1.0000 0.1442
-18.000 -1.1901 0.06649 0.05938 -0.0597 1.0000 0.1467
-17.750 -1.1935 0.06353 0.05632 -0.0601 1.0000 0.1491
-17.500 -1.1763 0.06276 0.05567 -0.0599 1.0000 0.1517
-17.250 -1.1714 0.06077 0.05365 -0.0600 1.0000 0.1544
-17.000 -1.1767 0.05779 0.05055 -0.0602 1.0000 0.1572
-16.750 -1.1911 0.05412 0.04665 -0.0602 1.0000 0.1596
-16.500 -1.1693 0.05369 0.04637 -0.0599 1.0000 0.1625
-16.250 -1.1606 0.05221 0.04491 -0.0597 1.0000 0.1654
-16.000 -1.1596 0.05009 0.04273 -0.0593 1.0000 0.1684
-15.750 -1.1664 0.04745 0.03991 -0.0588 1.0000 0.1712
-15.500 -1.1527 0.04637 0.03888 -0.0583 1.0000 0.1744
-15.250 -1.1425 0.04515 0.03771 -0.0577 1.0000 0.1774
-15.000 -1.1385 0.04354 0.03606 -0.0569 1.0000 0.1807
-14.750 -1.1414 0.04155 0.03394 -0.0558 1.0000 0.1839
-14.500 -1.1303 0.04043 0.03285 -0.0549 1.0000 0.1873
-14.250 -1.1203 0.03940 0.03187 -0.0539 1.0000 0.1906
-14.000 -1.1161 0.03812 0.03056 -0.0526 1.0000 0.1942
-13.750 -1.1184 0.03662 0.02893 -0.0506 1.0000 0.1978
-13.500 -1.1078 0.03570 0.02808 -0.0492 1.0000 0.2015
-13.250 -1.1011 0.03483 0.02725 -0.0473 1.0000 0.2051
-13.000 -1.0999 0.03385 0.02625 -0.0449 1.0000 0.2090
-12.750 -1.1051 0.03276 0.02505 -0.0416 1.0000 0.2127
-12.500 -1.0963 0.03208 0.02446 -0.0395 1.0000 0.2167
-12.250 -1.0951 0.03141 0.02384 -0.0364 1.0000 0.2205
-12.000 -1.0993 0.03072 0.02312 -0.0325 1.0000 0.2245
-11.750 -1.1095 0.03003 0.02233 -0.0276 1.0000 0.2281
-11.500 -1.1066 0.02951 0.02190 -0.0243 1.0000 0.2321
-11.250 -1.1112 0.02907 0.02151 -0.0199 1.0000 0.2358
-11.000 -1.1204 0.02864 0.02106 -0.0148 1.0000 0.2396
-10.750 -1.1338 0.02823 0.02058 -0.0089 1.0000 0.2432
-10.500 -1.1403 0.02783 0.02019 -0.0041 1.0000 0.2470
-10.250 -1.1170 0.02729 0.01973 -0.0046 0.9967 0.2528
-10.000 -1.0880 0.02672 0.01907 -0.0063 0.9917 0.2600
-9.750 -1.0557 0.02611 0.01855 -0.0081 0.9865 0.2666
-9.500 -1.0260 0.02561 0.01804 -0.0096 0.9803 0.2738
-9.250 -0.9909 0.02507 0.01746 -0.0119 0.9762 0.2814
-9.000 -0.9643 0.02459 0.01706 -0.0124 0.9680 0.2880
-8.750 -0.9340 0.02412 0.01650 -0.0137 0.9620 0.2957
-8.500 -0.8904 0.02354 0.01605 -0.0173 0.9592 0.3037
-8.250 -0.8713 0.02316 0.01564 -0.0162 0.9481 0.3106
-8.000 -0.8312 0.02257 0.01506 -0.0190 0.9439 0.3188
-7.750 -0.7870 0.02200 0.01455 -0.0226 0.9411 0.3274
-7.500 -0.7714 0.02166 0.01409 -0.0205 0.9287 0.3343
-7.250 -0.7291 0.02106 0.01365 -0.0234 0.9245 0.3425
-7.000 -0.7009 0.02065 0.01319 -0.0236 0.9173 0.3507
-6.750 -0.6753 0.02020 0.01279 -0.0232 0.9072 0.3580
-6.500 -0.6423 0.01974 0.01236 -0.0241 0.9015 0.3662
-6.250 -0.6282 0.01952 0.01203 -0.0214 0.8887 0.3736
-6.000 -0.5950 0.01901 0.01166 -0.0222 0.8815 0.3816
-5.750 -0.5745 0.01877 0.01138 -0.0207 0.8709 0.3896
-5.500 -0.5503 0.01840 0.01099 -0.0198 0.8606 0.3975
-5.250 -0.5241 0.01810 0.01074 -0.0193 0.8515 0.4054
-5.000 -0.5049 0.01790 0.01046 -0.0175 0.8392 0.4136
-4.750 -0.4758 0.01753 0.01014 -0.0174 0.8304 0.4217
-4.500 -0.4553 0.01737 0.00999 -0.0159 0.8174 0.4297
-4.250 -0.4298 0.01712 0.00962 -0.0152 0.8082 0.4384
-4.000 -0.4067 0.01693 0.00954 -0.0141 0.7949 0.4462
-3.750 -0.3813 0.01675 0.00924 -0.0134 0.7853 0.4554
-3.500 -0.3587 0.01657 0.00913 -0.0123 0.7722 0.4636
-3.250 -0.3319 0.01641 0.00892 -0.0118 0.7621 0.4725
-3.000 -0.3117 0.01632 0.00879 -0.0102 0.7493 0.4815
-2.750 -0.2831 0.01614 0.00864 -0.0101 0.7389 0.4902
-2.500 -0.2620 0.01608 0.00855 -0.0087 0.7265 0.4998
-2.250 -0.2347 0.01592 0.00840 -0.0083 0.7158 0.5088
-2.000 -0.2118 0.01588 0.00837 -0.0072 0.7037 0.5184
-1.750 -0.1866 0.01578 0.00820 -0.0065 0.6928 0.5282
-1.500 -0.1620 0.01573 0.00821 -0.0057 0.6811 0.5376
-1.250 -0.1389 0.01569 0.00806 -0.0046 0.6699 0.5483
-1.000 -0.1124 0.01562 0.00809 -0.0041 0.6585 0.5576
-0.750 -0.0894 0.01560 0.00800 -0.0030 0.6473 0.5688
-0.500 -0.0630 0.01556 0.00801 -0.0025 0.6364 0.5786
-0.250 -0.0397 0.01555 0.00798 -0.0015 0.6249 0.5897
0.000 -0.0135 0.01554 0.00795 -0.0009 0.6145 0.6001
0.250 0.0098 0.01554 0.00798 0.0001 0.6029 0.6112
0.500 0.0361 0.01556 0.00793 0.0006 0.5930 0.6222
0.750 0.0593 0.01556 0.00802 0.0017 0.5815 0.6331
1.000 0.0851 0.01560 0.00796 0.0023 0.5719 0.6447
1.250 0.1089 0.01562 0.00809 0.0033 0.5607 0.6554
1.500 0.1330 0.01565 0.00804 0.0042 0.5511 0.6674
1.750 0.1586 0.01572 0.00819 0.0048 0.5408 0.6781
2.000 0.1811 0.01575 0.00818 0.0060 0.5310 0.6904
2.250 0.2086 0.01586 0.00833 0.0063 0.5216 0.7009
2.750 0.2592 0.01607 0.00850 0.0077 0.5028 0.7238
3.000 0.2790 0.01612 0.00861 0.0093 0.4933 0.7366
3.250 0.3065 0.01625 0.00876 0.0097 0.4843 0.7468
3.500 0.3288 0.01639 0.00889 0.0108 0.4756 0.7597
3.750 0.3543 0.01652 0.00910 0.0115 0.4664 0.7698
4.000 0.3797 0.01674 0.00920 0.0122 0.4583 0.7826
4.250 0.4029 0.01688 0.00949 0.0133 0.4492 0.7927
4.500 0.4260 0.01705 0.00962 0.0144 0.4411 0.8053
4.750 0.4521 0.01732 0.00991 0.0149 0.4328 0.8154
5.000 0.4734 0.01751 0.01013 0.0164 0.4244 0.8276
5.250 0.5015 0.01782 0.01035 0.0165 0.4165 0.8374
5.500 0.5223 0.01807 0.01070 0.0181 0.4084 0.8487
5.750 0.5449 0.01830 0.01093 0.0193 0.4004 0.8593
6.000 0.5733 0.01873 0.01130 0.0194 0.3926 0.8684
6.250 0.5907 0.01893 0.01158 0.0215 0.3847 0.8804
6.500 0.6216 0.01937 0.01194 0.0211 0.3767 0.8876
6.750 0.6383 0.01965 0.01224 0.0233 0.3695 0.9005
7.000 0.6701 0.02010 0.01272 0.0226 0.3609 0.9062
7.250 0.7031 0.02061 0.01311 0.0216 0.3533 0.9139
7.500 0.7240 0.02095 0.01354 0.0229 0.3456 0.9238
7.750 0.7627 0.02148 0.01399 0.0206 0.3374 0.9284
8.000 0.7819 0.02188 0.01440 0.0221 0.3306 0.9406
8.250 0.8245 0.02243 0.01497 0.0188 0.3217 0.9435
8.500 0.8683 0.02305 0.01548 0.0153 0.3136 0.9469
8.750 0.8923 0.02347 0.01597 0.0155 0.3061 0.9563
9.000 0.9285 0.02396 0.01635 0.0133 0.2986 0.9615
9.250 0.9616 0.02447 0.01693 0.0115 0.2908 0.9668
9.500 0.9853 0.02492 0.01737 0.0115 0.2841 0.9759
9.750 1.0238 0.02547 0.01786 0.0086 0.2766 0.9794
10.000 1.0530 0.02596 0.01841 0.0072 0.2692 0.9856
10.250 1.0857 0.02654 0.01884 0.0054 0.2626 0.9911
10.500 1.1146 0.02711 0.01954 0.0037 0.2556 0.9959
10.750 1.1397 0.02767 0.02008 0.0028 0.2493 1.0000
11.000 1.1406 0.02805 0.02033 0.0065 0.2452 1.0000
11.250 1.1246 0.02844 0.02084 0.0128 0.2418 1.0000
11.500 1.1139 0.02887 0.02131 0.0181 0.2380 1.0000
11.750 1.1068 0.02932 0.02175 0.0229 0.2343 1.0000
12.000 1.1095 0.02978 0.02209 0.0263 0.2304 1.0000
12.250 1.1035 0.03043 0.02279 0.0307 0.2267 1.0000
12.500 1.0972 0.03115 0.02357 0.0349 0.2227 1.0000
12.750 1.0964 0.03184 0.02426 0.0382 0.2189 1.0000
13.000 1.1057 0.03244 0.02472 0.0403 0.2148 1.0000
13.250 1.1040 0.03345 0.02580 0.0433 0.2111 1.0000
13.500 1.1029 0.03450 0.02692 0.0460 0.2072 1.0000
13.750 1.1070 0.03546 0.02787 0.0481 0.2034 1.0000
14.000 1.1250 0.03604 0.02828 0.0490 0.1994 1.0000
14.250 1.1200 0.03763 0.03003 0.0512 0.1961 1.0000
14.500 1.1220 0.03902 0.03148 0.0527 0.1924 1.0000
14.750 1.1293 0.04019 0.03265 0.0538 0.1890 1.0000
15.000 1.1487 0.04083 0.03313 0.0543 0.1853 1.0000
15.250 1.1429 0.04295 0.03543 0.0557 0.1823 1.0000
15.500 1.1446 0.04471 0.03727 0.0565 0.1789 1.0000
15.750 1.1523 0.04610 0.03865 0.0571 0.1758 1.0000
16.000 1.1747 0.04654 0.03891 0.0575 0.1724 1.0000
16.250 1.1650 0.04936 0.04195 0.0581 0.1698 1.0000
16.500 1.1637 0.05167 0.04436 0.0585 0.1667 1.0000
16.750 1.1698 0.05338 0.04608 0.0587 0.1637 1.0000
17.000 1.1872 0.05414 0.04672 0.0590 0.1609 1.0000
17.250 1.1838 0.05684 0.04955 0.0591 0.1582 1.0000
17.500 1.1762 0.06004 0.05290 0.0589 0.1554 1.0000
17.750 1.1784 0.06231 0.05521 0.0587 0.1527 1.0000
18.000 1.1917 0.06347 0.05630 0.0588 0.1501 1.0000
18.250 1.1998 0.06522 0.05804 0.0588 0.1475 1.0000
18.500 1.1813 0.06989 0.06293 0.0578 0.1451 1.0000
18.750 1.1752 0.07331 0.06646 0.0571 0.1425 1.0000
19.000 1.1834 0.07510 0.06823 0.0567 0.1400 1.0000
19.250 1.2143 0.07426 0.06719 0.0574 0.1375 1.0000
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