GOE 601 AIRFOIL (goe601-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 601 AIRFOIL (goe601-il) Reynolds number: 500,000 Max Cl/Cd: 68.97 at α=6.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe601-il-500000-n5.txt Download as CSV file: xf-goe601-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 601 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.8259 0.12018 0.11673 -0.0565 1.0000 0.0206
-19.500 -0.8440 0.11333 0.10977 -0.0600 1.0000 0.0207
-19.250 -0.8577 0.10725 0.10360 -0.0632 1.0000 0.0210
-19.000 -0.8722 0.10123 0.09749 -0.0663 1.0000 0.0213
-18.750 -0.8858 0.09556 0.09172 -0.0691 1.0000 0.0215
-18.500 -0.8980 0.09020 0.08624 -0.0718 1.0000 0.0217
-18.250 -0.9092 0.08513 0.08108 -0.0742 1.0000 0.0219
-18.000 -0.9196 0.08026 0.07611 -0.0765 1.0000 0.0221
-17.750 -0.9292 0.07564 0.07137 -0.0786 1.0000 0.0224
-17.500 -0.9376 0.07129 0.06691 -0.0805 1.0000 0.0226
-17.250 -0.9456 0.06721 0.06273 -0.0822 1.0000 0.0227
-17.000 -0.9524 0.06335 0.05876 -0.0837 1.0000 0.0230
-16.750 -0.9593 0.05971 0.05502 -0.0849 1.0000 0.0232
-16.500 -0.9672 0.05616 0.05142 -0.0859 1.0000 0.0235
-16.250 -0.9732 0.05299 0.04818 -0.0866 1.0000 0.0236
-16.000 -0.9798 0.04989 0.04502 -0.0871 1.0000 0.0238
-15.750 -0.9837 0.04715 0.04222 -0.0874 1.0000 0.0241
-15.500 -0.9883 0.04449 0.03948 -0.0874 1.0000 0.0242
-15.250 -0.9912 0.04211 0.03704 -0.0872 1.0000 0.0245
-15.000 -0.9939 0.03990 0.03476 -0.0868 1.0000 0.0248
-14.750 -0.9969 0.03783 0.03262 -0.0860 1.0000 0.0251
-14.500 -1.0004 0.03589 0.03060 -0.0848 1.0000 0.0254
-14.250 -0.9896 0.03395 0.02858 -0.0861 0.9990 0.0259
-14.000 -0.9730 0.03210 0.02663 -0.0881 0.9969 0.0264
-13.750 -0.9557 0.03047 0.02489 -0.0898 0.9942 0.0268
-13.500 -0.9397 0.02901 0.02332 -0.0909 0.9913 0.0271
-13.250 -0.9269 0.02730 0.02155 -0.0919 0.9879 0.0276
-13.000 -0.9097 0.02584 0.02005 -0.0932 0.9849 0.0282
-12.750 -0.8885 0.02463 0.01877 -0.0947 0.9826 0.0287
-12.500 -0.8730 0.02361 0.01770 -0.0945 0.9778 0.0291
-12.250 -0.8527 0.02266 0.01668 -0.0951 0.9743 0.0296
-12.000 -0.8286 0.02179 0.01574 -0.0961 0.9716 0.0303
-11.750 -0.8066 0.02101 0.01489 -0.0965 0.9678 0.0309
-11.500 -0.7848 0.02031 0.01412 -0.0966 0.9627 0.0314
-11.250 -0.7572 0.01959 0.01332 -0.0978 0.9595 0.0319
-11.000 -0.7332 0.01865 0.01236 -0.0986 0.9557 0.0328
-10.750 -0.7166 0.01802 0.01168 -0.0973 0.9474 0.0334
-10.500 -0.6893 0.01736 0.01098 -0.0982 0.9426 0.0341
-10.250 -0.6747 0.01690 0.01046 -0.0961 0.9318 0.0346
-10.000 -0.6542 0.01642 0.00993 -0.0952 0.9230 0.0353
-9.750 -0.6327 0.01598 0.00941 -0.0945 0.9123 0.0360
-9.500 -0.6118 0.01558 0.00895 -0.0935 0.8990 0.0367
-9.250 -0.5898 0.01511 0.00840 -0.0928 0.8855 0.0374
-9.000 -0.5679 0.01466 0.00788 -0.0920 0.8727 0.0384
-8.750 -0.5458 0.01429 0.00742 -0.0912 0.8609 0.0394
-8.500 -0.5239 0.01397 0.00702 -0.0903 0.8502 0.0405
-8.250 -0.5025 0.01370 0.00667 -0.0892 0.8412 0.0419
-8.000 -0.4808 0.01343 0.00632 -0.0882 0.8335 0.0435
-7.750 -0.4599 0.01313 0.00599 -0.0871 0.8267 0.0458
-7.500 -0.4382 0.01287 0.00569 -0.0860 0.8203 0.0487
-7.250 -0.4165 0.01258 0.00538 -0.0850 0.8149 0.0542
-7.000 -0.3957 0.01226 0.00513 -0.0838 0.8097 0.0660
-6.750 -0.3733 0.01202 0.00494 -0.0830 0.8046 0.0820
-6.500 -0.3490 0.01187 0.00478 -0.0823 0.8000 0.0909
-6.250 -0.3242 0.01174 0.00462 -0.0818 0.7960 0.0960
-6.000 -0.3006 0.01156 0.00445 -0.0810 0.7915 0.1012
-5.750 -0.2759 0.01144 0.00429 -0.0804 0.7871 0.1050
-5.500 -0.2503 0.01136 0.00415 -0.0800 0.7831 0.1078
-5.250 -0.2262 0.01118 0.00395 -0.0794 0.7793 0.1124
-5.000 -0.2020 0.01101 0.00379 -0.0787 0.7753 0.1165
-4.750 -0.1772 0.01088 0.00365 -0.0781 0.7712 0.1202
-4.500 -0.1522 0.01075 0.00349 -0.0776 0.7671 0.1247
-4.250 -0.1272 0.01060 0.00333 -0.0770 0.7634 0.1302
-4.000 -0.1029 0.01043 0.00319 -0.0764 0.7592 0.1389
-3.750 -0.0807 0.01013 0.00302 -0.0754 0.7536 0.1647
-3.500 -0.0596 0.00976 0.00285 -0.0742 0.7479 0.2221
-3.250 -0.0363 0.00954 0.00274 -0.0734 0.7427 0.2596
-3.000 -0.0122 0.00936 0.00265 -0.0727 0.7373 0.2838
-2.750 0.0125 0.00923 0.00256 -0.0720 0.7322 0.3034
-2.500 0.0373 0.00911 0.00247 -0.0714 0.7271 0.3212
-2.250 0.0617 0.00898 0.00240 -0.0707 0.7210 0.3384
-2.000 0.0861 0.00884 0.00234 -0.0700 0.7158 0.3614
-1.750 0.1100 0.00870 0.00229 -0.0692 0.7107 0.3945
-1.500 0.1341 0.00859 0.00228 -0.0684 0.7042 0.4236
-1.250 0.1589 0.00854 0.00226 -0.0677 0.6973 0.4449
-1.000 0.1843 0.00851 0.00224 -0.0672 0.6913 0.4612
-0.750 0.2098 0.00848 0.00223 -0.0666 0.6844 0.4736
-0.500 0.2348 0.00848 0.00220 -0.0660 0.6768 0.4842
-0.250 0.2598 0.00845 0.00219 -0.0653 0.6681 0.4938
0.000 0.2848 0.00846 0.00218 -0.0646 0.6607 0.5042
0.250 0.3093 0.00844 0.00218 -0.0639 0.6512 0.5143
0.500 0.3333 0.00846 0.00217 -0.0630 0.6398 0.5223
0.750 0.3565 0.00848 0.00217 -0.0620 0.6279 0.5298
1.000 0.3803 0.00850 0.00219 -0.0611 0.6159 0.5387
1.250 0.4034 0.00852 0.00221 -0.0601 0.6044 0.5479
1.500 0.4258 0.00857 0.00224 -0.0589 0.5907 0.5583
1.750 0.4468 0.00861 0.00228 -0.0575 0.5752 0.5706
2.000 0.4671 0.00867 0.00234 -0.0559 0.5585 0.5860
2.250 0.4862 0.00871 0.00241 -0.0540 0.5414 0.6112
2.500 0.5034 0.00875 0.00251 -0.0518 0.5214 0.6434
2.750 0.5189 0.00885 0.00262 -0.0492 0.4980 0.6741
3.000 0.5322 0.00901 0.00275 -0.0462 0.4692 0.7010
3.250 0.5399 0.00922 0.00290 -0.0421 0.4324 0.7289
3.500 0.5469 0.00947 0.00310 -0.0378 0.3951 0.7602
3.750 0.5559 0.00972 0.00335 -0.0340 0.3652 0.7977
4.000 0.5691 0.00995 0.00363 -0.0311 0.3434 0.8436
4.250 0.5953 0.01025 0.00397 -0.0310 0.3228 0.8933
4.500 0.6424 0.01066 0.00436 -0.0355 0.3065 0.9268
4.750 0.6915 0.01103 0.00469 -0.0405 0.2936 0.9459
5.000 0.7357 0.01137 0.00499 -0.0443 0.2829 0.9595
5.250 0.7720 0.01168 0.00526 -0.0465 0.2746 0.9713
5.750 0.8348 0.01223 0.00577 -0.0487 0.2596 0.9901
6.000 0.8637 0.01256 0.00607 -0.0493 0.2516 0.9989
6.250 0.8828 0.01280 0.00628 -0.0478 0.2436 1.0000
6.500 0.8944 0.01304 0.00650 -0.0449 0.2382 1.0000
6.750 0.9092 0.01325 0.00671 -0.0425 0.2319 1.0000
7.000 0.9229 0.01353 0.00696 -0.0400 0.2247 1.0000
7.250 0.9377 0.01381 0.00723 -0.0377 0.2174 1.0000
7.500 0.9512 0.01416 0.00754 -0.0353 0.2073 1.0000
7.750 0.9667 0.01449 0.00785 -0.0333 0.1984 1.0000
8.000 0.9807 0.01489 0.00821 -0.0311 0.1879 1.0000
8.250 0.9937 0.01538 0.00863 -0.0288 0.1733 1.0000
8.500 1.0024 0.01609 0.00919 -0.0260 0.1484 1.0000
8.750 0.9961 0.01762 0.01032 -0.0214 0.0872 1.0000
9.000 0.9938 0.01910 0.01154 -0.0174 0.0450 1.0000
9.250 1.0053 0.01988 0.01228 -0.0154 0.0381 1.0000
9.500 1.0198 0.02051 0.01292 -0.0139 0.0358 1.0000
9.750 1.0340 0.02119 0.01361 -0.0123 0.0343 1.0000
10.000 1.0478 0.02191 0.01435 -0.0108 0.0329 1.0000
10.250 1.0612 0.02267 0.01514 -0.0093 0.0319 1.0000
10.500 1.0755 0.02340 0.01592 -0.0080 0.0314 1.0000
10.750 1.0893 0.02419 0.01674 -0.0067 0.0307 1.0000
11.000 1.1025 0.02502 0.01762 -0.0053 0.0300 1.0000
11.250 1.1151 0.02592 0.01856 -0.0040 0.0293 1.0000
11.500 1.1267 0.02691 0.01959 -0.0027 0.0287 1.0000
11.750 1.1371 0.02802 0.02073 -0.0014 0.0282 1.0000
12.000 1.1464 0.02921 0.02197 0.0000 0.0277 1.0000
12.250 1.1535 0.03061 0.02342 0.0014 0.0272 1.0000
12.500 1.1637 0.03180 0.02467 0.0026 0.0270 1.0000
12.750 1.1738 0.03304 0.02598 0.0036 0.0267 1.0000
13.000 1.1821 0.03443 0.02744 0.0047 0.0264 1.0000
13.250 1.1904 0.03587 0.02894 0.0057 0.0260 1.0000
13.500 1.1971 0.03748 0.03062 0.0066 0.0257 1.0000
13.750 1.2041 0.03912 0.03232 0.0075 0.0253 1.0000
14.000 1.2094 0.04095 0.03421 0.0083 0.0250 1.0000
14.250 1.2147 0.04283 0.03616 0.0090 0.0246 1.0000
14.500 1.2182 0.04494 0.03834 0.0096 0.0243 1.0000
14.750 1.2214 0.04715 0.04062 0.0101 0.0240 1.0000
15.000 1.2219 0.04970 0.04323 0.0105 0.0237 1.0000
15.250 1.2217 0.05240 0.04601 0.0108 0.0235 1.0000
15.500 1.2177 0.05560 0.04927 0.0109 0.0231 1.0000
15.750 1.2166 0.05859 0.05234 0.0109 0.0229 1.0000
16.000 1.2177 0.06140 0.05525 0.0108 0.0227 1.0000
16.250 1.2179 0.06436 0.05830 0.0105 0.0225 1.0000
16.500 1.2172 0.06751 0.06154 0.0101 0.0224 1.0000
16.750 1.2162 0.07077 0.06489 0.0096 0.0222 1.0000
17.000 1.2141 0.07421 0.06843 0.0090 0.0220 1.0000
17.250 1.2123 0.07769 0.07200 0.0082 0.0217 1.0000
17.500 1.2101 0.08125 0.07565 0.0073 0.0214 1.0000
17.750 1.2066 0.08505 0.07954 0.0064 0.0212 1.0000
18.000 1.2040 0.08880 0.08338 0.0053 0.0209 1.0000
18.250 1.2002 0.09274 0.08739 0.0041 0.0207 1.0000
18.500 1.1968 0.09662 0.09135 0.0029 0.0205 1.0000
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