GOE 600 AIRFOIL (goe600-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 600 AIRFOIL (goe600-il) Reynolds number: 1,000,000 Max Cl/Cd: 86.04 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe600-il-1000000-n5.txt Download as CSV file: xf-goe600-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 600 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.250 -1.0598 0.09369 0.09089 -0.0215 1.0000 0.0055
-17.000 -1.1221 0.07867 0.07566 -0.0297 1.0000 0.0054
-16.750 -1.1667 0.06717 0.06397 -0.0363 1.0000 0.0053
-16.500 -1.1959 0.05852 0.05513 -0.0416 1.0000 0.0053
-16.250 -1.2159 0.05161 0.04807 -0.0460 1.0000 0.0053
-16.000 -1.2279 0.04616 0.04247 -0.0494 1.0000 0.0053
-15.750 -1.2353 0.04156 0.03773 -0.0523 1.0000 0.0054
-15.500 -1.2383 0.03780 0.03384 -0.0545 1.0000 0.0054
-15.250 -1.2379 0.03475 0.03066 -0.0560 1.0000 0.0055
-15.000 -1.2358 0.03222 0.02802 -0.0567 1.0000 0.0055
-14.750 -1.2318 0.03020 0.02589 -0.0568 1.0000 0.0056
-14.500 -1.2308 0.02821 0.02379 -0.0560 1.0000 0.0057
-14.250 -1.2283 0.02662 0.02209 -0.0544 1.0000 0.0058
-14.000 -1.2232 0.02539 0.02078 -0.0523 1.0000 0.0059
-13.750 -1.2126 0.02435 0.01966 -0.0507 1.0000 0.0061
-13.500 -1.1983 0.02339 0.01863 -0.0496 1.0000 0.0062
-13.250 -1.1822 0.02252 0.01769 -0.0486 1.0000 0.0064
-13.000 -1.1647 0.02171 0.01681 -0.0476 1.0000 0.0065
-12.750 -1.1462 0.02096 0.01598 -0.0468 1.0000 0.0067
-12.500 -1.1268 0.02024 0.01520 -0.0460 1.0000 0.0069
-12.250 -1.1068 0.01957 0.01447 -0.0453 1.0000 0.0071
-12.000 -1.0830 0.01891 0.01375 -0.0453 0.9948 0.0073
-11.750 -1.0560 0.01828 0.01304 -0.0459 0.9854 0.0075
-11.500 -1.0294 0.01766 0.01234 -0.0463 0.9752 0.0076
-11.250 -1.0050 0.01695 0.01157 -0.0463 0.9635 0.0080
-11.000 -0.9817 0.01640 0.01095 -0.0459 0.9518 0.0084
-10.750 -0.9587 0.01591 0.01040 -0.0453 0.9412 0.0088
-10.500 -0.9354 0.01548 0.00990 -0.0447 0.9315 0.0092
-10.250 -0.9114 0.01506 0.00942 -0.0442 0.9229 0.0096
-10.000 -0.8872 0.01469 0.00896 -0.0437 0.9146 0.0100
-9.750 -0.8628 0.01424 0.00845 -0.0434 0.9066 0.0106
-9.500 -0.8384 0.01381 0.00796 -0.0429 0.8990 0.0113
-9.250 -0.8129 0.01343 0.00753 -0.0427 0.8918 0.0120
-9.000 -0.7873 0.01309 0.00713 -0.0425 0.8847 0.0127
-8.750 -0.7611 0.01277 0.00675 -0.0423 0.8776 0.0134
-8.500 -0.7354 0.01240 0.00634 -0.0421 0.8698 0.0150
-8.250 -0.7091 0.01208 0.00599 -0.0420 0.8617 0.0167
-8.000 -0.6828 0.01176 0.00564 -0.0418 0.8532 0.0192
-7.750 -0.6560 0.01148 0.00533 -0.0418 0.8442 0.0222
-7.500 -0.6293 0.01120 0.00504 -0.0417 0.8354 0.0262
-7.250 -0.6021 0.01097 0.00477 -0.0417 0.8253 0.0292
-7.000 -0.5748 0.01073 0.00453 -0.0417 0.8148 0.0328
-6.750 -0.5472 0.01057 0.00431 -0.0417 0.8036 0.0348
-6.500 -0.5199 0.01035 0.00405 -0.0417 0.7917 0.0379
-6.250 -0.4923 0.01017 0.00383 -0.0418 0.7798 0.0407
-6.000 -0.4643 0.01003 0.00363 -0.0419 0.7691 0.0427
-5.750 -0.4364 0.00987 0.00342 -0.0419 0.7599 0.0454
-5.500 -0.4085 0.00968 0.00320 -0.0420 0.7511 0.0492
-5.250 -0.3803 0.00953 0.00301 -0.0422 0.7438 0.0527
-5.000 -0.3521 0.00936 0.00283 -0.0423 0.7365 0.0584
-4.750 -0.3242 0.00914 0.00263 -0.0425 0.7301 0.0698
-4.500 -0.2964 0.00887 0.00248 -0.0426 0.7237 0.0977
-4.250 -0.2677 0.00879 0.00237 -0.0428 0.7177 0.1044
-4.000 -0.2391 0.00866 0.00225 -0.0430 0.7128 0.1123
-3.750 -0.2102 0.00858 0.00215 -0.0433 0.7078 0.1167
-3.500 -0.1814 0.00851 0.00206 -0.0435 0.7020 0.1212
-3.250 -0.1526 0.00841 0.00196 -0.0437 0.6958 0.1272
-3.000 -0.1238 0.00835 0.00187 -0.0440 0.6888 0.1322
-2.750 -0.0950 0.00828 0.00179 -0.0442 0.6829 0.1383
-2.500 -0.0660 0.00819 0.00171 -0.0445 0.6771 0.1452
-2.250 -0.0372 0.00810 0.00163 -0.0447 0.6716 0.1554
-2.000 -0.0085 0.00795 0.00155 -0.0449 0.6668 0.1752
-1.750 0.0192 0.00756 0.00142 -0.0452 0.6610 0.2544
-1.500 0.0473 0.00732 0.00135 -0.0454 0.6550 0.3080
-1.250 0.0759 0.00715 0.00130 -0.0457 0.6492 0.3481
-1.000 0.1047 0.00702 0.00127 -0.0460 0.6429 0.3803
-0.750 0.1334 0.00693 0.00124 -0.0462 0.6377 0.4087
-0.500 0.1624 0.00683 0.00123 -0.0465 0.6326 0.4349
-0.250 0.1913 0.00676 0.00122 -0.0468 0.6266 0.4597
0.000 0.2202 0.00670 0.00122 -0.0470 0.6209 0.4843
0.250 0.2493 0.00664 0.00123 -0.0473 0.6143 0.5079
0.750 0.3071 0.00662 0.00125 -0.0478 0.5964 0.5422
1.000 0.3355 0.00667 0.00127 -0.0480 0.5758 0.5584
1.250 0.3637 0.00673 0.00130 -0.0481 0.5490 0.5763
1.500 0.3917 0.00684 0.00135 -0.0482 0.5198 0.5917
1.750 0.4187 0.00706 0.00143 -0.0482 0.4734 0.6080
2.000 0.4455 0.00730 0.00156 -0.0482 0.4321 0.6249
2.500 0.5004 0.00756 0.00178 -0.0483 0.3868 0.6697
2.750 0.5278 0.00764 0.00189 -0.0483 0.3684 0.6988
3.000 0.5553 0.00771 0.00201 -0.0483 0.3529 0.7294
3.250 0.5826 0.00777 0.00213 -0.0483 0.3385 0.7609
3.500 0.6093 0.00782 0.00226 -0.0482 0.3239 0.8024
3.750 0.6346 0.00788 0.00241 -0.0477 0.3051 0.8509
4.000 0.6585 0.00801 0.00258 -0.0468 0.2829 0.8970
4.250 0.6816 0.00823 0.00277 -0.0458 0.2553 0.9343
4.500 0.7088 0.00846 0.00294 -0.0458 0.2333 0.9620
4.750 0.7395 0.00878 0.00315 -0.0466 0.2080 0.9804
5.000 0.7711 0.00909 0.00336 -0.0477 0.1858 0.9930
5.250 0.8019 0.00938 0.00357 -0.0487 0.1695 1.0000
5.500 0.8273 0.00963 0.00377 -0.0484 0.1562 1.0000
5.750 0.8527 0.00991 0.00399 -0.0481 0.1425 1.0000
6.000 0.8773 0.01027 0.00425 -0.0477 0.1236 1.0000
6.250 0.9013 0.01067 0.00454 -0.0472 0.1019 1.0000
6.500 0.9255 0.01106 0.00485 -0.0468 0.0875 1.0000
6.750 0.9504 0.01138 0.00513 -0.0464 0.0792 1.0000
7.000 0.9754 0.01169 0.00540 -0.0461 0.0730 1.0000
7.250 1.0009 0.01193 0.00566 -0.0458 0.0688 1.0000
7.500 1.0251 0.01229 0.00598 -0.0454 0.0607 1.0000
7.750 1.0471 0.01283 0.00638 -0.0446 0.0410 1.0000
8.000 1.0696 0.01331 0.00680 -0.0440 0.0323 1.0000
8.250 1.0927 0.01373 0.00721 -0.0434 0.0284 1.0000
8.500 1.1163 0.01408 0.00758 -0.0428 0.0261 1.0000
8.750 1.1396 0.01444 0.00796 -0.0423 0.0244 1.0000
9.000 1.1618 0.01487 0.00839 -0.0416 0.0223 1.0000
9.250 1.1841 0.01527 0.00881 -0.0409 0.0206 1.0000
9.500 1.2064 0.01566 0.00922 -0.0402 0.0190 1.0000
9.750 1.2273 0.01612 0.00968 -0.0393 0.0170 1.0000
10.000 1.2479 0.01658 0.01016 -0.0383 0.0156 1.0000
10.250 1.2678 0.01704 0.01064 -0.0373 0.0143 1.0000
10.500 1.2862 0.01757 0.01117 -0.0361 0.0129 1.0000
10.750 1.3025 0.01809 0.01171 -0.0344 0.0119 1.0000
11.000 1.3184 0.01862 0.01229 -0.0327 0.0112 1.0000
11.250 1.3337 0.01923 0.01293 -0.0311 0.0104 1.0000
11.500 1.3481 0.01992 0.01364 -0.0294 0.0097 1.0000
11.750 1.3623 0.02066 0.01442 -0.0279 0.0091 1.0000
12.000 1.3771 0.02137 0.01519 -0.0265 0.0088 1.0000
12.250 1.3913 0.02216 0.01603 -0.0251 0.0084 1.0000
12.500 1.4046 0.02303 0.01695 -0.0237 0.0080 1.0000
12.750 1.4172 0.02398 0.01795 -0.0224 0.0077 1.0000
13.000 1.4287 0.02503 0.01905 -0.0211 0.0073 1.0000
13.250 1.4391 0.02621 0.02028 -0.0197 0.0070 1.0000
13.500 1.4486 0.02749 0.02163 -0.0184 0.0067 1.0000
13.750 1.4592 0.02871 0.02292 -0.0174 0.0066 1.0000
14.000 1.4691 0.03004 0.02431 -0.0163 0.0064 1.0000
14.250 1.4780 0.03148 0.02583 -0.0154 0.0062 1.0000
14.500 1.4861 0.03303 0.02746 -0.0145 0.0060 1.0000
14.750 1.4931 0.03473 0.02922 -0.0137 0.0058 1.0000
15.000 1.4991 0.03658 0.03115 -0.0130 0.0056 1.0000
15.250 1.5037 0.03859 0.03323 -0.0123 0.0055 1.0000
15.500 1.5069 0.04079 0.03551 -0.0118 0.0054 1.0000
15.750 1.5088 0.04319 0.03799 -0.0113 0.0052 1.0000
16.000 1.5088 0.04583 0.04072 -0.0110 0.0051 1.0000
16.250 1.5066 0.04883 0.04381 -0.0108 0.0050 1.0000
16.500 1.5033 0.05208 0.04716 -0.0108 0.0049 1.0000
16.750 1.5016 0.05525 0.05043 -0.0110 0.0048 1.0000
17.000 1.4985 0.05866 0.05395 -0.0115 0.0048 1.0000
17.250 1.4940 0.06241 0.05782 -0.0121 0.0047 1.0000
17.500 1.4879 0.06649 0.06201 -0.0130 0.0047 1.0000
17.750 1.4800 0.07098 0.06661 -0.0142 0.0046 1.0000
18.000 1.4701 0.07590 0.07165 -0.0157 0.0046 1.0000
18.250 1.4585 0.08124 0.07711 -0.0175 0.0046 1.0000
18.500 1.4453 0.08700 0.08300 -0.0197 0.0045 1.0000
18.750 1.4303 0.09314 0.08926 -0.0221 0.0045 1.0000
19.000 1.4132 0.09971 0.09596 -0.0248 0.0045 1.0000
19.250 1.3946 0.10667 0.10306 -0.0277 0.0044 1.0000
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