GOE 775 AIRFOIL (goe775-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 775 AIRFOIL (goe775-il) Reynolds number: 200,000 Max Cl/Cd: 43.4 at α=9.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe775-il-200000-n5.txt Download as CSV file: xf-goe775-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 775 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -1.0841 0.10448 0.09806 -0.0346 1.0000 0.0731
-19.000 -1.0886 0.10042 0.09392 -0.0363 1.0000 0.0746
-18.750 -1.0933 0.09637 0.08975 -0.0380 1.0000 0.0762
-18.500 -1.0958 0.09273 0.08605 -0.0394 1.0000 0.0776
-18.250 -1.0986 0.08908 0.08237 -0.0408 1.0000 0.0790
-18.000 -1.1015 0.08541 0.07864 -0.0421 1.0000 0.0806
-17.750 -1.1039 0.08186 0.07499 -0.0434 1.0000 0.0823
-17.500 -1.1054 0.07844 0.07145 -0.0445 1.0000 0.0841
-17.250 -1.1065 0.07520 0.06819 -0.0455 1.0000 0.0856
-17.000 -1.1080 0.07191 0.06486 -0.0464 1.0000 0.0872
-16.750 -1.1088 0.06874 0.06162 -0.0473 1.0000 0.0891
-16.500 -1.1080 0.06581 0.05858 -0.0480 1.0000 0.0911
-16.250 -1.1070 0.06297 0.05568 -0.0487 1.0000 0.0930
-16.000 -1.1075 0.06004 0.05272 -0.0493 1.0000 0.0948
-15.750 -1.1064 0.05730 0.04992 -0.0497 1.0000 0.0969
-15.500 -1.1034 0.05483 0.04737 -0.0501 1.0000 0.0992
-15.250 -1.0999 0.05248 0.04494 -0.0503 1.0000 0.1014
-15.000 -1.0988 0.04996 0.04240 -0.0504 1.0000 0.1034
-14.750 -1.0959 0.04765 0.04005 -0.0505 1.0000 0.1057
-14.500 -1.0907 0.04563 0.03795 -0.0504 1.0000 0.1083
-14.250 -1.0851 0.04371 0.03596 -0.0502 1.0000 0.1107
-14.000 -1.0823 0.04160 0.03386 -0.0498 1.0000 0.1130
-13.750 -1.0775 0.03974 0.03195 -0.0494 1.0000 0.1157
-13.500 -1.0701 0.03815 0.03029 -0.0489 1.0000 0.1187
-13.250 -1.0640 0.03651 0.02862 -0.0482 1.0000 0.1214
-13.000 -1.0590 0.03487 0.02697 -0.0473 1.0000 0.1243
-12.750 -1.0518 0.03346 0.02553 -0.0464 1.0000 0.1276
-12.500 -1.0426 0.03226 0.02426 -0.0454 1.0000 0.1310
-12.250 -1.0378 0.03086 0.02289 -0.0440 1.0000 0.1341
-12.000 -1.0308 0.02970 0.02171 -0.0425 1.0000 0.1378
-11.750 -1.0218 0.02875 0.02072 -0.0409 1.0000 0.1417
-11.500 -1.0173 0.02770 0.01968 -0.0387 1.0000 0.1453
-11.250 -1.0123 0.02681 0.01879 -0.0363 1.0000 0.1494
-11.000 -1.0064 0.02611 0.01806 -0.0337 1.0000 0.1537
-10.750 -1.0055 0.02535 0.01733 -0.0304 1.0000 0.1576
-10.500 -1.0049 0.02474 0.01672 -0.0267 1.0000 0.1620
-10.250 -1.0039 0.02426 0.01621 -0.0228 1.0000 0.1664
-10.000 -1.0088 0.02377 0.01574 -0.0179 1.0000 0.1703
-9.750 -1.0068 0.02329 0.01526 -0.0142 0.9991 0.1753
-9.500 -0.9801 0.02267 0.01463 -0.0150 0.9948 0.1826
-9.250 -0.9536 0.02205 0.01403 -0.0159 0.9907 0.1906
-9.000 -0.9285 0.02149 0.01347 -0.0162 0.9851 0.1983
-8.750 -0.9008 0.02095 0.01294 -0.0170 0.9803 0.2068
-8.500 -0.8734 0.02043 0.01244 -0.0177 0.9754 0.2148
-8.250 -0.8479 0.01996 0.01198 -0.0178 0.9689 0.2232
-8.000 -0.8171 0.01945 0.01149 -0.0190 0.9645 0.2316
-7.750 -0.7917 0.01902 0.01107 -0.0189 0.9576 0.2402
-7.500 -0.7640 0.01858 0.01065 -0.0193 0.9509 0.2484
-7.250 -0.7317 0.01813 0.01021 -0.0205 0.9463 0.2580
-7.000 -0.7103 0.01777 0.00988 -0.0195 0.9365 0.2659
-6.750 -0.6804 0.01737 0.00949 -0.0201 0.9300 0.2756
-6.500 -0.6571 0.01703 0.00918 -0.0193 0.9203 0.2839
-6.250 -0.6297 0.01668 0.00883 -0.0193 0.9119 0.2937
-6.000 -0.6062 0.01637 0.00854 -0.0185 0.9015 0.3026
-5.750 -0.5801 0.01606 0.00823 -0.0181 0.8916 0.3127
-5.500 -0.5576 0.01579 0.00799 -0.0170 0.8796 0.3218
-5.250 -0.5315 0.01551 0.00770 -0.0166 0.8691 0.3323
-5.000 -0.5097 0.01527 0.00749 -0.0153 0.8554 0.3417
-4.750 -0.4847 0.01504 0.00724 -0.0146 0.8432 0.3528
-4.500 -0.4615 0.01479 0.00702 -0.0136 0.8289 0.3640
-4.250 -0.4377 0.01460 0.00682 -0.0127 0.8138 0.3765
-4.000 -0.4138 0.01438 0.00661 -0.0118 0.7988 0.3891
-3.750 -0.3885 0.01419 0.00639 -0.0111 0.7837 0.3998
-3.500 -0.3637 0.01403 0.00621 -0.0103 0.7680 0.4107
-3.250 -0.3387 0.01388 0.00604 -0.0096 0.7530 0.4207
-3.000 -0.3134 0.01376 0.00587 -0.0089 0.7387 0.4313
-2.750 -0.2883 0.01366 0.00574 -0.0082 0.7245 0.4413
-2.500 -0.2633 0.01357 0.00563 -0.0075 0.7111 0.4525
-2.000 -0.2130 0.01343 0.00545 -0.0062 0.6852 0.4742
-1.750 -0.1878 0.01338 0.00537 -0.0055 0.6730 0.4851
-1.500 -0.1627 0.01333 0.00532 -0.0048 0.6600 0.4972
-1.250 -0.1377 0.01328 0.00527 -0.0041 0.6482 0.5085
-1.000 -0.1123 0.01326 0.00522 -0.0035 0.6352 0.5206
-0.750 -0.0874 0.01321 0.00520 -0.0027 0.6231 0.5324
-0.500 -0.0622 0.01320 0.00517 -0.0020 0.6102 0.5448
-0.250 -0.0373 0.01318 0.00516 -0.0013 0.5975 0.5578
0.000 -0.0124 0.01318 0.00514 -0.0005 0.5847 0.5704
0.250 0.0126 0.01318 0.00515 0.0002 0.5711 0.5840
0.500 0.0375 0.01318 0.00516 0.0009 0.5586 0.5967
0.750 0.0625 0.01320 0.00517 0.0016 0.5456 0.6096
1.000 0.0876 0.01321 0.00520 0.0023 0.5333 0.6226
1.250 0.1125 0.01326 0.00522 0.0031 0.5214 0.6346
1.500 0.1379 0.01328 0.00527 0.0037 0.5093 0.6476
1.750 0.1629 0.01333 0.00531 0.0044 0.4982 0.6595
2.000 0.1881 0.01337 0.00537 0.0051 0.4861 0.6726
2.250 0.2132 0.01343 0.00544 0.0058 0.4752 0.6848
2.750 0.2635 0.01357 0.00562 0.0071 0.4536 0.7107
3.000 0.2885 0.01365 0.00573 0.0078 0.4424 0.7242
3.250 0.3136 0.01376 0.00587 0.0085 0.4323 0.7384
3.500 0.3390 0.01387 0.00603 0.0092 0.4218 0.7528
3.750 0.3639 0.01402 0.00620 0.0099 0.4118 0.7678
4.000 0.3889 0.01418 0.00639 0.0107 0.4009 0.7835
4.250 0.4140 0.01437 0.00661 0.0114 0.3903 0.7987
4.500 0.4381 0.01458 0.00681 0.0123 0.3776 0.8137
4.750 0.4619 0.01478 0.00701 0.0132 0.3653 0.8288
5.000 0.4849 0.01503 0.00723 0.0142 0.3539 0.8432
5.250 0.5101 0.01525 0.00748 0.0149 0.3429 0.8554
5.500 0.5318 0.01550 0.00769 0.0162 0.3334 0.8692
5.750 0.5580 0.01577 0.00797 0.0166 0.3229 0.8797
6.000 0.5804 0.01605 0.00822 0.0177 0.3138 0.8916
6.250 0.6066 0.01635 0.00853 0.0180 0.3038 0.9015
6.500 0.6300 0.01666 0.00882 0.0188 0.2948 0.9120
6.750 0.6576 0.01701 0.00916 0.0188 0.2849 0.9204
7.000 0.6809 0.01735 0.00948 0.0196 0.2766 0.9301
7.250 0.7110 0.01775 0.00986 0.0190 0.2669 0.9366
7.500 0.7323 0.01811 0.01019 0.0200 0.2590 0.9464
7.750 0.7648 0.01855 0.01063 0.0187 0.2493 0.9510
8.000 0.7921 0.01901 0.01105 0.0185 0.2412 0.9578
8.250 0.8181 0.01943 0.01147 0.0184 0.2325 0.9646
8.500 0.8486 0.01994 0.01195 0.0172 0.2242 0.9691
8.750 0.8744 0.02040 0.01241 0.0171 0.2157 0.9756
9.000 0.9018 0.02092 0.01292 0.0164 0.2077 0.9805
9.250 0.9299 0.02145 0.01343 0.0155 0.1992 0.9852
9.500 0.9546 0.02202 0.01400 0.0152 0.1917 0.9909
9.750 0.9817 0.02262 0.01459 0.0143 0.1836 0.9949
10.000 1.0081 0.02325 0.01522 0.0135 0.1762 0.9992
10.250 1.0092 0.02370 0.01568 0.0174 0.1713 1.0000
10.750 1.0051 0.02468 0.01666 0.0262 0.1629 1.0000
11.000 1.0063 0.02528 0.01726 0.0298 0.1585 1.0000
11.500 1.0131 0.02675 0.01873 0.0358 0.1503 1.0000
11.750 1.0186 0.02762 0.01960 0.0381 0.1461 1.0000
12.250 1.0322 0.02963 0.02164 0.0418 0.1385 1.0000
12.500 1.0396 0.03077 0.02279 0.0433 0.1348 1.0000
12.750 1.0449 0.03214 0.02414 0.0447 0.1316 1.0000
13.000 1.0536 0.03338 0.02543 0.0457 0.1283 1.0000
13.250 1.0613 0.03476 0.02686 0.0466 0.1249 1.0000
13.500 1.0667 0.03637 0.02848 0.0475 0.1220 1.0000
13.750 1.0722 0.03805 0.03018 0.0481 0.1193 1.0000
14.000 1.0800 0.03961 0.03182 0.0487 0.1163 1.0000
14.250 1.0853 0.04144 0.03369 0.0491 0.1135 1.0000
14.500 1.0885 0.04351 0.03577 0.0494 0.1112 1.0000
14.750 1.0936 0.04548 0.03779 0.0496 0.1088 1.0000
15.000 1.0992 0.04747 0.03986 0.0497 0.1062 1.0000
15.250 1.1024 0.04974 0.04218 0.0496 0.1038 1.0000
15.500 1.1039 0.05223 0.04469 0.0495 0.1018 1.0000
15.750 1.1070 0.05462 0.04714 0.0493 0.0997 1.0000
16.000 1.1103 0.05706 0.04967 0.0489 0.0974 1.0000
16.250 1.1117 0.05976 0.05244 0.0485 0.0952 1.0000
16.500 1.1116 0.06267 0.05537 0.0479 0.0934 1.0000
16.750 1.1122 0.06554 0.05829 0.0472 0.0916 1.0000
17.000 1.1133 0.06845 0.06131 0.0465 0.0895 1.0000
17.250 1.1128 0.07158 0.06452 0.0456 0.0876 1.0000
17.500 1.1116 0.07484 0.06783 0.0447 0.0859 1.0000
17.750 1.1101 0.07812 0.07112 0.0437 0.0845 1.0000
18.000 1.1089 0.08151 0.07463 0.0426 0.0827 1.0000
18.250 1.1067 0.08504 0.07825 0.0413 0.0809 1.0000
18.500 1.1037 0.08873 0.08202 0.0400 0.0793 1.0000
18.750 1.1008 0.09241 0.08573 0.0386 0.0779 1.0000
19.000 1.0985 0.09601 0.08938 0.0372 0.0765 1.0000
19.250 1.0938 0.10008 0.09356 0.0355 0.0749 1.0000
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