GOE 601 AIRFOIL (goe601-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 601 AIRFOIL (goe601-il) Reynolds number: 1,000,000 Max Cl/Cd: 82.42 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe601-il-1000000-n5.txt Download as CSV file: xf-goe601-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0232 0.08908 0.08569 -0.0717 1.0000 0.0166
-19.500 -1.0430 0.08287 0.07937 -0.0747 1.0000 0.0167
-19.250 -1.0595 0.07724 0.07365 -0.0775 1.0000 0.0169
-19.000 -1.0777 0.07147 0.06777 -0.0802 1.0000 0.0169
-18.750 -1.0885 0.06689 0.06312 -0.0823 1.0000 0.0173
-18.500 -1.1005 0.06229 0.05843 -0.0843 1.0000 0.0174
-18.250 -1.1106 0.05813 0.05419 -0.0859 1.0000 0.0176
-18.000 -1.1200 0.05425 0.05022 -0.0873 1.0000 0.0178
-17.750 -1.1299 0.05051 0.04638 -0.0884 1.0000 0.0178
-17.500 -1.1342 0.04755 0.04336 -0.0890 1.0000 0.0183
-17.250 -1.1408 0.04443 0.04016 -0.0896 1.0000 0.0184
-17.000 -1.1437 0.04181 0.03747 -0.0898 1.0000 0.0187
-16.750 -1.1482 0.03914 0.03472 -0.0899 1.0000 0.0189
-16.500 -1.1512 0.03678 0.03228 -0.0895 1.0000 0.0191
-16.250 -1.1526 0.03472 0.03015 -0.0890 1.0000 0.0193
-16.000 -1.1409 0.03252 0.02788 -0.0909 0.9992 0.0197
-15.750 -1.1284 0.03049 0.02579 -0.0927 0.9981 0.0201
-15.500 -1.1135 0.02872 0.02396 -0.0943 0.9964 0.0204
-15.250 -1.0985 0.02719 0.02238 -0.0954 0.9931 0.0208
-15.000 -1.0842 0.02585 0.02099 -0.0960 0.9907 0.0212
-14.750 -1.0675 0.02465 0.01974 -0.0968 0.9882 0.0216
-14.500 -1.0497 0.02352 0.01855 -0.0975 0.9860 0.0219
-14.250 -1.0293 0.02250 0.01747 -0.0985 0.9839 0.0224
-14.000 -1.0074 0.02161 0.01652 -0.0995 0.9820 0.0227
-13.750 -0.9910 0.02077 0.01561 -0.0992 0.9776 0.0229
-13.500 -0.9702 0.01996 0.01476 -0.0996 0.9745 0.0233
-13.250 -0.9474 0.01910 0.01386 -0.1005 0.9722 0.0239
-13.000 -0.9200 0.01840 0.01313 -0.1019 0.9705 0.0244
-12.750 -0.8970 0.01778 0.01248 -0.1023 0.9665 0.0248
-12.500 -0.8692 0.01725 0.01191 -0.1034 0.9630 0.0254
-12.250 -0.8394 0.01670 0.01131 -0.1048 0.9596 0.0260
-12.000 -0.8087 0.01617 0.01073 -0.1064 0.9565 0.0264
-11.750 -0.7892 0.01573 0.01024 -0.1056 0.9493 0.0267
-11.500 -0.7613 0.01532 0.00978 -0.1063 0.9433 0.0271
-11.250 -0.7447 0.01489 0.00929 -0.1047 0.9335 0.0274
-11.000 -0.7275 0.01443 0.00877 -0.1032 0.9225 0.0279
-10.750 -0.7115 0.01404 0.00833 -0.1013 0.9055 0.0285
-10.500 -0.6945 0.01375 0.00793 -0.0995 0.8793 0.0291
-10.250 -0.6787 0.01353 0.00758 -0.0974 0.8544 0.0296
-10.000 -0.6619 0.01331 0.00726 -0.0954 0.8389 0.0299
-9.750 -0.6438 0.01309 0.00696 -0.0937 0.8282 0.0304
-9.500 -0.6247 0.01288 0.00667 -0.0922 0.8195 0.0308
-9.250 -0.6048 0.01266 0.00639 -0.0908 0.8127 0.0312
-9.000 -0.5835 0.01246 0.00614 -0.0897 0.8070 0.0317
-8.750 -0.5632 0.01221 0.00584 -0.0884 0.8014 0.0323
-8.500 -0.5423 0.01197 0.00556 -0.0872 0.7966 0.0330
-8.250 -0.5204 0.01172 0.00530 -0.0862 0.7923 0.0338
-8.000 -0.4981 0.01150 0.00505 -0.0852 0.7880 0.0346
-7.750 -0.4754 0.01131 0.00483 -0.0843 0.7837 0.0354
-7.500 -0.4523 0.01113 0.00461 -0.0834 0.7798 0.0364
-7.250 -0.4285 0.01094 0.00440 -0.0827 0.7764 0.0374
-7.000 -0.4051 0.01072 0.00418 -0.0819 0.7725 0.0392
-6.750 -0.3816 0.01053 0.00397 -0.0811 0.7685 0.0415
-6.500 -0.3583 0.01033 0.00377 -0.0803 0.7647 0.0454
-6.250 -0.3353 0.01008 0.00355 -0.0795 0.7613 0.0537
-6.000 -0.3130 0.00975 0.00335 -0.0785 0.7579 0.0749
-5.750 -0.2883 0.00959 0.00323 -0.0779 0.7542 0.0853
-5.500 -0.2631 0.00946 0.00311 -0.0774 0.7504 0.0920
-5.250 -0.2373 0.00939 0.00301 -0.0770 0.7468 0.0951
-5.000 -0.2121 0.00925 0.00289 -0.0765 0.7430 0.1001
-4.750 -0.1865 0.00913 0.00277 -0.0761 0.7380 0.1035
-4.500 -0.1609 0.00906 0.00266 -0.0756 0.7322 0.1059
-4.250 -0.1353 0.00900 0.00257 -0.0751 0.7266 0.1077
-4.000 -0.1092 0.00889 0.00247 -0.0747 0.7222 0.1105
-3.750 -0.0835 0.00879 0.00236 -0.0743 0.7172 0.1135
-3.500 -0.0584 0.00871 0.00226 -0.0737 0.7116 0.1168
-3.250 -0.0324 0.00862 0.00217 -0.0733 0.7060 0.1207
-3.000 -0.0069 0.00851 0.00208 -0.0728 0.7003 0.1273
-2.750 0.0178 0.00841 0.00198 -0.0722 0.6945 0.1365
-2.500 0.0384 0.00796 0.00181 -0.0709 0.6889 0.2099
-2.250 0.0623 0.00778 0.00173 -0.0701 0.6820 0.2427
-2.000 0.0869 0.00768 0.00168 -0.0695 0.6753 0.2637
-1.750 0.1115 0.00756 0.00162 -0.0688 0.6671 0.2861
-1.500 0.1361 0.00749 0.00158 -0.0681 0.6595 0.3025
-1.250 0.1617 0.00743 0.00154 -0.0677 0.6516 0.3159
-1.000 0.1859 0.00738 0.00151 -0.0669 0.6431 0.3323
-0.750 0.2101 0.00728 0.00148 -0.0661 0.6331 0.3561
-0.500 0.2330 0.00718 0.00146 -0.0651 0.6228 0.3903
-0.250 0.2556 0.00713 0.00147 -0.0640 0.6101 0.4252
0.000 0.2794 0.00713 0.00149 -0.0632 0.5964 0.4454
0.250 0.3034 0.00717 0.00151 -0.0623 0.5826 0.4576
0.500 0.3266 0.00725 0.00154 -0.0613 0.5654 0.4694
0.750 0.3488 0.00733 0.00158 -0.0601 0.5464 0.4799
1.000 0.3715 0.00745 0.00163 -0.0590 0.5280 0.4870
1.250 0.3935 0.00754 0.00168 -0.0578 0.5098 0.4946
1.500 0.4152 0.00768 0.00175 -0.0566 0.4880 0.5011
1.750 0.4349 0.00788 0.00184 -0.0549 0.4595 0.5064
2.000 0.4519 0.00814 0.00196 -0.0527 0.4209 0.5128
2.250 0.4661 0.00850 0.00213 -0.0500 0.3742 0.5199
2.500 0.4832 0.00872 0.00226 -0.0479 0.3470 0.5270
2.750 0.5004 0.00888 0.00236 -0.0457 0.3291 0.5362
3.000 0.5169 0.00904 0.00248 -0.0434 0.3114 0.5466
3.250 0.5357 0.00913 0.00258 -0.0416 0.3009 0.5621
3.500 0.5532 0.00922 0.00271 -0.0395 0.2911 0.5872
3.750 0.5713 0.00923 0.00285 -0.0376 0.2842 0.6283
4.000 0.5902 0.00928 0.00298 -0.0358 0.2786 0.6603
4.250 0.6083 0.00937 0.00313 -0.0338 0.2722 0.6876
4.500 0.6271 0.00941 0.00327 -0.0320 0.2672 0.7205
4.750 0.6439 0.00948 0.00343 -0.0298 0.2596 0.7542
5.000 0.6593 0.00952 0.00360 -0.0273 0.2539 0.7976
5.250 0.6755 0.00952 0.00376 -0.0248 0.2486 0.8491
5.500 0.7022 0.00959 0.00399 -0.0248 0.2418 0.9065
5.750 0.7645 0.00988 0.00431 -0.0327 0.2305 0.9427
6.000 0.8250 0.01025 0.00462 -0.0402 0.2176 0.9586
6.250 0.8685 0.01060 0.00490 -0.0440 0.2051 0.9705
6.500 0.9008 0.01093 0.00518 -0.0454 0.1931 0.9811
6.750 0.9286 0.01130 0.00547 -0.0459 0.1788 0.9895
7.000 0.9488 0.01181 0.00587 -0.0449 0.1585 0.9992
7.250 0.9596 0.01246 0.00634 -0.0422 0.1288 1.0000
7.500 0.9433 0.01394 0.00740 -0.0348 0.0571 1.0000
7.750 0.9507 0.01466 0.00800 -0.0315 0.0352 1.0000
8.000 0.9660 0.01507 0.00839 -0.0295 0.0319 1.0000
8.250 0.9825 0.01545 0.00878 -0.0278 0.0305 1.0000
8.500 0.9989 0.01586 0.00919 -0.0262 0.0294 1.0000
8.750 1.0152 0.01629 0.00963 -0.0245 0.0284 1.0000
9.000 1.0314 0.01675 0.01009 -0.0229 0.0276 1.0000
9.250 1.0479 0.01722 0.01058 -0.0214 0.0270 1.0000
9.500 1.0648 0.01768 0.01106 -0.0201 0.0266 1.0000
9.750 1.0813 0.01818 0.01157 -0.0187 0.0261 1.0000
10.000 1.0976 0.01871 0.01212 -0.0173 0.0257 1.0000
10.250 1.1134 0.01928 0.01272 -0.0160 0.0251 1.0000
10.500 1.1289 0.01990 0.01335 -0.0146 0.0247 1.0000
10.750 1.1440 0.02054 0.01402 -0.0133 0.0243 1.0000
11.000 1.1586 0.02125 0.01474 -0.0120 0.0239 1.0000
11.250 1.1722 0.02203 0.01556 -0.0106 0.0235 1.0000
11.500 1.1851 0.02288 0.01644 -0.0092 0.0231 1.0000
11.750 1.1986 0.02371 0.01730 -0.0080 0.0228 1.0000
12.000 1.2129 0.02450 0.01813 -0.0068 0.0227 1.0000
12.250 1.2267 0.02534 0.01901 -0.0057 0.0224 1.0000
12.500 1.2398 0.02624 0.01995 -0.0046 0.0222 1.0000
12.750 1.2527 0.02718 0.02092 -0.0036 0.0219 1.0000
13.000 1.2653 0.02815 0.02193 -0.0025 0.0215 1.0000
13.250 1.2766 0.02924 0.02307 -0.0015 0.0213 1.0000
13.500 1.2885 0.03030 0.02416 -0.0005 0.0209 1.0000
13.750 1.2990 0.03150 0.02540 0.0005 0.0206 1.0000
14.000 1.3089 0.03277 0.02671 0.0015 0.0204 1.0000
14.250 1.3177 0.03415 0.02814 0.0024 0.0201 1.0000
14.500 1.3251 0.03568 0.02972 0.0034 0.0199 1.0000
14.750 1.3315 0.03735 0.03144 0.0043 0.0196 1.0000
15.000 1.3346 0.03935 0.03350 0.0052 0.0192 1.0000
15.250 1.3408 0.04112 0.03533 0.0059 0.0191 1.0000
15.500 1.3484 0.04281 0.03708 0.0064 0.0189 1.0000
15.750 1.3548 0.04466 0.03899 0.0069 0.0188 1.0000
16.000 1.3611 0.04656 0.04096 0.0073 0.0186 1.0000
16.250 1.3666 0.04859 0.04305 0.0076 0.0183 1.0000
16.500 1.3712 0.05075 0.04528 0.0079 0.0180 1.0000
16.750 1.3740 0.05315 0.04775 0.0080 0.0179 1.0000
17.000 1.3763 0.05567 0.05034 0.0081 0.0177 1.0000
17.250 1.3773 0.05841 0.05315 0.0080 0.0175 1.0000
17.500 1.3780 0.06123 0.05604 0.0078 0.0173 1.0000
17.750 1.3782 0.06416 0.05904 0.0075 0.0171 1.0000
18.000 1.3751 0.06756 0.06252 0.0071 0.0170 1.0000
18.250 1.3724 0.07099 0.06603 0.0065 0.0168 1.0000
18.500 1.3684 0.07466 0.06978 0.0058 0.0166 1.0000
18.750 1.3627 0.07860 0.07380 0.0048 0.0164 1.0000
19.000 1.3564 0.08270 0.07797 0.0038 0.0161 1.0000
19.250 1.3445 0.08771 0.08309 0.0023 0.0162 1.0000
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