GOE 776 AIRFOIL (goe776-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 776 AIRFOIL (goe776-il) Reynolds number: 500,000 Max Cl/Cd: 50.01 at α=8.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe776-il-500000.txt Download as CSV file: xf-goe776-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.2029 0.08721 0.08194 -0.0458 1.0000 0.1048
-19.500 -1.2042 0.08398 0.07862 -0.0468 1.0000 0.1067
-19.250 -1.2032 0.08112 0.07569 -0.0476 1.0000 0.1085
-19.000 -1.2047 0.07809 0.07268 -0.0483 1.0000 0.1106
-18.750 -1.2047 0.07516 0.06973 -0.0490 1.0000 0.1126
-18.500 -1.2043 0.07226 0.06676 -0.0497 1.0000 0.1145
-18.250 -1.2013 0.06965 0.06407 -0.0503 1.0000 0.1165
-18.000 -1.2008 0.06692 0.06132 -0.0508 1.0000 0.1185
-17.750 -1.2008 0.06416 0.05856 -0.0512 1.0000 0.1206
-17.500 -1.1998 0.06145 0.05581 -0.0516 1.0000 0.1227
-17.250 -1.1954 0.05913 0.05344 -0.0520 1.0000 0.1249
-17.000 -1.1904 0.05685 0.05107 -0.0523 1.0000 0.1268
-16.750 -1.1899 0.05435 0.04859 -0.0523 1.0000 0.1292
-16.500 -1.1883 0.05187 0.04609 -0.0524 1.0000 0.1314
-16.250 -1.1835 0.04973 0.04392 -0.0525 1.0000 0.1338
-16.000 -1.1766 0.04781 0.04194 -0.0525 1.0000 0.1361
-15.750 -1.1719 0.04579 0.03988 -0.0523 1.0000 0.1385
-15.500 -1.1697 0.04358 0.03768 -0.0520 1.0000 0.1410
-15.250 -1.1648 0.04162 0.03570 -0.0518 1.0000 0.1436
-15.000 -1.1562 0.04003 0.03406 -0.0514 1.0000 0.1463
-14.750 -1.1485 0.03842 0.03240 -0.0510 1.0000 0.1489
-14.500 -1.1456 0.03652 0.03053 -0.0503 1.0000 0.1518
-14.250 -1.1398 0.03490 0.02890 -0.0495 1.0000 0.1548
-14.000 -1.1310 0.03358 0.02753 -0.0487 1.0000 0.1579
-13.750 -1.1231 0.03230 0.02623 -0.0477 1.0000 0.1608
-13.500 -1.1214 0.03076 0.02471 -0.0461 1.0000 0.1640
-13.250 -1.1172 0.02957 0.02352 -0.0443 1.0000 0.1673
-13.000 -1.1116 0.02861 0.02253 -0.0424 1.0000 0.1705
-12.750 -1.1098 0.02763 0.02153 -0.0398 1.0000 0.1736
-12.500 -1.1137 0.02659 0.02051 -0.0364 1.0000 0.1769
-12.250 -1.1177 0.02578 0.01970 -0.0326 1.0000 0.1801
-12.000 -1.1217 0.02515 0.01905 -0.0286 1.0000 0.1832
-11.750 -1.1159 0.02441 0.01829 -0.0263 0.9992 0.1868
-11.500 -1.0910 0.02330 0.01721 -0.0279 0.9966 0.1923
-11.250 -1.0606 0.02256 0.01645 -0.0298 0.9941 0.1978
-11.000 -1.0327 0.02161 0.01554 -0.0316 0.9918 0.2036
-10.750 -1.0042 0.02083 0.01477 -0.0331 0.9889 0.2098
-10.500 -0.9751 0.02015 0.01408 -0.0345 0.9848 0.2155
-10.250 -0.9463 0.01932 0.01330 -0.0361 0.9813 0.2220
-10.000 -0.9114 0.01876 0.01272 -0.0384 0.9789 0.2282
-9.750 -0.8796 0.01798 0.01200 -0.0404 0.9765 0.2349
-9.500 -0.8541 0.01741 0.01143 -0.0407 0.9695 0.2412
-9.250 -0.8255 0.01688 0.01090 -0.0416 0.9634 0.2472
-9.000 -0.8025 0.01627 0.01033 -0.0414 0.9559 0.2535
-8.750 -0.7820 0.01585 0.00989 -0.0403 0.9454 0.2595
-8.500 -0.7630 0.01541 0.00944 -0.0390 0.9351 0.2653
-8.250 -0.7462 0.01496 0.00901 -0.0372 0.9236 0.2714
-8.000 -0.7268 0.01466 0.00867 -0.0358 0.9117 0.2772
-7.750 -0.7083 0.01428 0.00827 -0.0342 0.9005 0.2831
-7.500 -0.6905 0.01395 0.00795 -0.0326 0.8874 0.2895
-7.250 -0.6689 0.01372 0.00765 -0.0314 0.8759 0.2957
-7.000 -0.6501 0.01340 0.00734 -0.0299 0.8624 0.3020
-6.750 -0.6299 0.01314 0.00706 -0.0285 0.8502 0.3085
-6.500 -0.6072 0.01297 0.00681 -0.0276 0.8369 0.3146
-6.250 -0.5876 0.01269 0.00655 -0.0261 0.8240 0.3215
-6.000 -0.5665 0.01250 0.00631 -0.0249 0.8108 0.3284
-5.750 -0.5432 0.01238 0.00613 -0.0240 0.7977 0.3344
-5.500 -0.5242 0.01216 0.00590 -0.0223 0.7847 0.3416
-5.250 -0.5038 0.01203 0.00576 -0.0209 0.7716 0.3486
-5.000 -0.4821 0.01196 0.00561 -0.0196 0.7591 0.3552
-4.750 -0.4634 0.01180 0.00548 -0.0178 0.7461 0.3627
-4.500 -0.4410 0.01173 0.00535 -0.0167 0.7343 0.3702
-4.250 -0.4182 0.01163 0.00522 -0.0157 0.7217 0.3773
-4.000 -0.3963 0.01152 0.00511 -0.0145 0.7102 0.3850
-3.750 -0.3722 0.01146 0.00501 -0.0137 0.6985 0.3924
-3.500 -0.3494 0.01137 0.00489 -0.0127 0.6873 0.3998
-3.250 -0.3263 0.01127 0.00481 -0.0117 0.6758 0.4078
-3.000 -0.3016 0.01127 0.00472 -0.0110 0.6649 0.4150
-2.750 -0.2787 0.01113 0.00464 -0.0100 0.6542 0.4234
-2.500 -0.2551 0.01111 0.00456 -0.0091 0.6430 0.4317
-2.250 -0.2303 0.01104 0.00450 -0.0084 0.6326 0.4396
-2.000 -0.2073 0.01098 0.00444 -0.0074 0.6218 0.4484
-1.750 -0.1823 0.01095 0.00439 -0.0067 0.6116 0.4570
-1.500 -0.1588 0.01089 0.00434 -0.0058 0.6005 0.4659
-1.250 -0.1347 0.01086 0.00430 -0.0049 0.5904 0.4754
-1.000 -0.1101 0.01083 0.00426 -0.0042 0.5795 0.4842
-0.750 -0.0868 0.01081 0.00424 -0.0032 0.5691 0.4942
-0.500 -0.0615 0.01079 0.00421 -0.0026 0.5584 0.5036
-0.250 -0.0388 0.01078 0.00420 -0.0015 0.5478 0.5139
0.000 -0.0134 0.01077 0.00419 -0.0009 0.5375 0.5240
0.250 0.0096 0.01077 0.00419 0.0001 0.5269 0.5344
0.500 0.0346 0.01077 0.00420 0.0008 0.5170 0.5451
0.750 0.0580 0.01078 0.00421 0.0018 0.5067 0.5554
1.000 0.0826 0.01080 0.00423 0.0025 0.4973 0.5664
1.250 0.1066 0.01081 0.00425 0.0034 0.4873 0.5766
1.500 0.1304 0.01086 0.00429 0.0042 0.4781 0.5876
1.750 0.1552 0.01088 0.00432 0.0049 0.4689 0.5977
2.000 0.1780 0.01095 0.00438 0.0060 0.4595 0.6087
2.250 0.2035 0.01098 0.00442 0.0066 0.4513 0.6191
2.500 0.2268 0.01101 0.00448 0.0075 0.4425 0.6299
2.750 0.2509 0.01110 0.00455 0.0083 0.4344 0.6406
3.000 0.2751 0.01111 0.00462 0.0092 0.4261 0.6514
3.250 0.2979 0.01123 0.00470 0.0102 0.4178 0.6625
3.500 0.3224 0.01126 0.00479 0.0109 0.4105 0.6732
3.750 0.3460 0.01133 0.00487 0.0118 0.4026 0.6849
4.000 0.3680 0.01146 0.00499 0.0130 0.3946 0.6959
4.250 0.3925 0.01149 0.00508 0.0137 0.3877 0.7078
4.500 0.4152 0.01159 0.00519 0.0147 0.3801 0.7192
4.750 0.4369 0.01172 0.00533 0.0160 0.3727 0.7317
5.000 0.4604 0.01177 0.00545 0.0169 0.3657 0.7436
5.250 0.4802 0.01190 0.00557 0.0185 0.3582 0.7566
5.500 0.5004 0.01201 0.00573 0.0200 0.3514 0.7690
5.750 0.5216 0.01212 0.00587 0.0213 0.3445 0.7824
6.000 0.5411 0.01229 0.00607 0.0229 0.3374 0.7952
6.500 0.5851 0.01263 0.00650 0.0251 0.3243 0.8214
6.750 0.6046 0.01290 0.00674 0.0265 0.3174 0.8347
7.000 0.6268 0.01309 0.00700 0.0276 0.3112 0.8478
7.250 0.6479 0.01332 0.00726 0.0288 0.3047 0.8602
7.500 0.6659 0.01366 0.00759 0.0304 0.2980 0.8737
7.750 0.6878 0.01389 0.00788 0.0315 0.2922 0.8853
8.000 0.7067 0.01418 0.00819 0.0330 0.2857 0.8984
8.250 0.7235 0.01462 0.00861 0.0349 0.2793 0.9098
8.500 0.7437 0.01487 0.00891 0.0362 0.2739 0.9220
8.750 0.7621 0.01528 0.00934 0.0377 0.2677 0.9328
9.000 0.7783 0.01579 0.00981 0.0395 0.2616 0.9442
9.250 0.8009 0.01616 0.01023 0.0402 0.2559 0.9539
9.500 0.8230 0.01670 0.01074 0.0407 0.2497 0.9624
9.750 0.8502 0.01731 0.01132 0.0400 0.2435 0.9686
10.000 0.8758 0.01781 0.01184 0.0397 0.2374 0.9761
10.250 0.9074 0.01859 0.01255 0.0377 0.2305 0.9787
10.500 0.9424 0.01916 0.01314 0.0354 0.2244 0.9810
10.750 0.9730 0.01990 0.01385 0.0336 0.2179 0.9842
11.000 1.0007 0.02068 0.01462 0.0323 0.2120 0.9885
11.250 1.0303 0.02137 0.01531 0.0308 0.2061 0.9915
11.500 1.0572 0.02238 0.01626 0.0290 0.1999 0.9938
11.750 1.0885 0.02307 0.01699 0.0270 0.1946 0.9963
12.000 1.1154 0.02405 0.01794 0.0254 0.1892 0.9989
12.250 1.1204 0.02500 0.01887 0.0274 0.1851 1.0000
12.500 1.1179 0.02554 0.01946 0.0314 0.1822 1.0000
12.750 1.1155 0.02626 0.02019 0.0350 0.1789 1.0000
13.000 1.1131 0.02720 0.02111 0.0383 0.1757 1.0000
13.250 1.1101 0.02840 0.02229 0.0413 0.1723 1.0000
13.500 1.1178 0.02923 0.02316 0.0432 0.1693 1.0000
13.750 1.1233 0.03034 0.02429 0.0449 0.1659 1.0000
14.000 1.1270 0.03174 0.02568 0.0464 0.1627 1.0000
14.250 1.1312 0.03325 0.02718 0.0476 0.1594 1.0000
14.500 1.1415 0.03447 0.02845 0.0483 0.1565 1.0000
14.750 1.1490 0.03595 0.02995 0.0490 0.1534 1.0000
15.000 1.1533 0.03775 0.03175 0.0497 0.1505 1.0000
15.250 1.1575 0.03961 0.03361 0.0503 0.1477 1.0000
15.500 1.1675 0.04109 0.03516 0.0506 0.1450 1.0000
15.750 1.1736 0.04295 0.03705 0.0508 0.1423 1.0000
16.000 1.1774 0.04502 0.03912 0.0511 0.1397 1.0000
16.250 1.1789 0.04732 0.04141 0.0513 0.1371 1.0000
16.500 1.1871 0.04912 0.04329 0.0513 0.1349 1.0000
16.750 1.1925 0.05122 0.04543 0.0512 0.1324 1.0000
17.000 1.1951 0.05359 0.04783 0.0511 0.1301 1.0000
17.250 1.1954 0.05617 0.05039 0.0510 0.1278 1.0000
17.500 1.1993 0.05849 0.05278 0.0508 0.1257 1.0000
17.750 1.2041 0.06078 0.05513 0.0504 0.1235 1.0000
18.000 1.2057 0.06342 0.05781 0.0500 0.1213 1.0000
18.250 1.2061 0.06617 0.06056 0.0496 0.1192 1.0000
18.500 1.2057 0.06898 0.06338 0.0492 0.1170 1.0000
18.750 1.2089 0.07156 0.06604 0.0486 0.1152 1.0000
19.000 1.2096 0.07444 0.06899 0.0479 0.1131 1.0000
19.250 1.2100 0.07733 0.07190 0.0472 0.1111 1.0000
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