GOE 460 AIRFOIL (goe460-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 460 AIRFOIL (goe460-il) Reynolds number: 1,000,000 Max Cl/Cd: 57.48 at α=10.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe460-il-1000000-n5.txt Download as CSV file: xf-goe460-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 460 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 -1.2033 0.07561 0.07092 -0.0563 1.0000 0.0374
-19.500 -1.2068 0.07231 0.06756 -0.0571 1.0000 0.0382
-19.250 -1.2103 0.06903 0.06420 -0.0579 1.0000 0.0385
-19.000 -1.2121 0.06599 0.06110 -0.0586 1.0000 0.0390
-18.750 -1.2136 0.06306 0.05810 -0.0591 1.0000 0.0395
-18.500 -1.2177 0.05990 0.05488 -0.0596 1.0000 0.0402
-18.250 -1.2200 0.05698 0.05191 -0.0599 1.0000 0.0406
-18.000 -1.2219 0.05416 0.04903 -0.0602 1.0000 0.0413
-17.750 -1.2224 0.05156 0.04638 -0.0603 1.0000 0.0422
-17.500 -1.2205 0.04928 0.04403 -0.0602 1.0000 0.0426
-17.250 -1.2181 0.04708 0.04179 -0.0601 1.0000 0.0436
-17.000 -1.2149 0.04500 0.03965 -0.0599 1.0000 0.0440
-16.750 -1.2124 0.04292 0.03752 -0.0595 1.0000 0.0448
-16.500 -1.2108 0.04083 0.03539 -0.0590 1.0000 0.0457
-16.250 -1.2079 0.03893 0.03344 -0.0584 1.0000 0.0463
-16.000 -1.2051 0.03707 0.03155 -0.0576 1.0000 0.0475
-15.750 -1.2007 0.03543 0.02986 -0.0568 1.0000 0.0485
-15.500 -1.1953 0.03394 0.02833 -0.0558 1.0000 0.0492
-15.250 -1.1904 0.03249 0.02684 -0.0546 1.0000 0.0504
-15.000 -1.1871 0.03100 0.02531 -0.0532 1.0000 0.0515
-14.750 -1.1841 0.02957 0.02386 -0.0516 1.0000 0.0529
-14.500 -1.1798 0.02833 0.02259 -0.0499 1.0000 0.0541
-14.250 -1.1751 0.02722 0.02145 -0.0480 1.0000 0.0554
-14.000 -1.1719 0.02613 0.02033 -0.0458 1.0000 0.0570
-13.750 -1.1591 0.02492 0.01911 -0.0454 0.9995 0.0594
-13.500 -1.1406 0.02377 0.01796 -0.0460 0.9985 0.0626
-13.250 -1.1243 0.02249 0.01672 -0.0464 0.9970 0.0699
-13.000 -1.1077 0.02132 0.01563 -0.0466 0.9947 0.0793
-12.500 -1.0701 0.01966 0.01399 -0.0465 0.9878 0.0903
-12.250 -1.0464 0.01902 0.01334 -0.0470 0.9847 0.0936
-12.000 -1.0210 0.01843 0.01272 -0.0478 0.9819 0.0960
-11.750 -0.9962 0.01774 0.01204 -0.0486 0.9795 0.0991
-11.500 -0.9761 0.01713 0.01143 -0.0482 0.9744 0.1017
-11.250 -0.9515 0.01661 0.01089 -0.0486 0.9700 0.1038
-11.000 -0.9225 0.01614 0.01039 -0.0498 0.9667 0.1056
-10.750 -0.8945 0.01564 0.00987 -0.0509 0.9618 0.1079
-10.500 -0.8672 0.01510 0.00933 -0.0518 0.9558 0.1111
-10.250 -0.8353 0.01460 0.00883 -0.0536 0.9517 0.1146
-10.000 -0.8005 0.01417 0.00840 -0.0559 0.9477 0.1172
-9.750 -0.7678 0.01370 0.00793 -0.0579 0.9411 0.1217
-9.500 -0.7314 0.01315 0.00742 -0.0607 0.9348 0.1305
-9.250 -0.7014 0.01260 0.00692 -0.0622 0.9252 0.1432
-9.000 -0.6713 0.01204 0.00645 -0.0638 0.9136 0.1637
-8.750 -0.6434 0.01171 0.00612 -0.0645 0.8986 0.1740
-8.500 -0.6177 0.01148 0.00585 -0.0645 0.8818 0.1814
-8.250 -0.5964 0.01127 0.00558 -0.0636 0.8640 0.1867
-8.000 -0.5778 0.01108 0.00534 -0.0621 0.8474 0.1912
-7.750 -0.5588 0.01094 0.00514 -0.0606 0.8335 0.1948
-7.250 -0.5211 0.01066 0.00477 -0.0574 0.8125 0.2015
-7.000 -0.5040 0.01049 0.00457 -0.0555 0.8029 0.2057
-6.750 -0.4851 0.01034 0.00440 -0.0539 0.7943 0.2095
-6.500 -0.4665 0.01022 0.00425 -0.0522 0.7839 0.2127
-6.250 -0.4465 0.01011 0.00411 -0.0507 0.7755 0.2148
-6.000 -0.4278 0.01000 0.00396 -0.0490 0.7650 0.2173
-5.750 -0.4100 0.00986 0.00380 -0.0471 0.7526 0.2218
-5.500 -0.3930 0.00977 0.00365 -0.0449 0.7348 0.2249
-5.250 -0.3755 0.00969 0.00352 -0.0429 0.7187 0.2281
-5.000 -0.3575 0.00963 0.00340 -0.0409 0.7018 0.2309
-4.750 -0.3400 0.00958 0.00328 -0.0388 0.6825 0.2341
-4.500 -0.3239 0.00951 0.00315 -0.0365 0.6649 0.2396
-4.000 -0.2908 0.00937 0.00294 -0.0320 0.6303 0.2532
-3.750 -0.2750 0.00926 0.00283 -0.0295 0.6163 0.2639
-3.500 -0.2594 0.00916 0.00273 -0.0271 0.6050 0.2760
-3.250 -0.2434 0.00902 0.00264 -0.0247 0.5951 0.2922
-3.000 -0.2285 0.00892 0.00257 -0.0221 0.5861 0.3097
-2.750 -0.2128 0.00881 0.00251 -0.0196 0.5773 0.3272
-2.500 -0.1974 0.00877 0.00247 -0.0170 0.5668 0.3417
-2.250 -0.1791 0.00869 0.00243 -0.0150 0.5568 0.3560
-2.000 -0.1606 0.00864 0.00239 -0.0131 0.5468 0.3681
-1.750 -0.1396 0.00859 0.00236 -0.0116 0.5385 0.3787
-1.500 -0.1202 0.00857 0.00233 -0.0099 0.5282 0.3895
-1.250 -0.0995 0.00854 0.00230 -0.0083 0.5160 0.3990
-1.000 -0.0798 0.00853 0.00228 -0.0066 0.5043 0.4108
-0.750 -0.0602 0.00851 0.00226 -0.0049 0.4919 0.4214
-0.500 -0.0391 0.00851 0.00225 -0.0035 0.4804 0.4315
-0.250 -0.0197 0.00851 0.00225 -0.0017 0.4682 0.4420
0.000 0.0002 0.00853 0.00225 0.0000 0.4541 0.4535
0.250 0.0199 0.00851 0.00225 0.0017 0.4423 0.4676
0.500 0.0396 0.00852 0.00226 0.0034 0.4316 0.4782
0.750 0.0603 0.00851 0.00226 0.0049 0.4216 0.4917
1.000 0.0797 0.00853 0.00228 0.0067 0.4103 0.5044
1.250 0.0993 0.00854 0.00230 0.0084 0.3985 0.5164
1.500 0.1202 0.00857 0.00233 0.0099 0.3894 0.5282
1.750 0.1396 0.00859 0.00236 0.0116 0.3785 0.5384
2.000 0.1607 0.00864 0.00239 0.0130 0.3681 0.5466
2.250 0.1792 0.00869 0.00243 0.0150 0.3560 0.5565
2.500 0.1978 0.00876 0.00247 0.0169 0.3424 0.5664
2.750 0.2130 0.00880 0.00251 0.0195 0.3279 0.5773
3.000 0.2285 0.00892 0.00257 0.0221 0.3094 0.5860
3.250 0.2433 0.00903 0.00264 0.0247 0.2918 0.5952
3.500 0.2594 0.00916 0.00273 0.0271 0.2757 0.6053
3.750 0.2751 0.00926 0.00283 0.0295 0.2640 0.6165
4.000 0.2911 0.00938 0.00294 0.0319 0.2530 0.6293
4.250 0.3080 0.00944 0.00304 0.0341 0.2458 0.6461
4.500 0.3240 0.00950 0.00315 0.0365 0.2396 0.6648
4.750 0.3402 0.00958 0.00328 0.0388 0.2342 0.6825
5.000 0.3579 0.00963 0.00339 0.0408 0.2310 0.7004
5.250 0.3757 0.00969 0.00352 0.0428 0.2282 0.7184
5.500 0.3934 0.00978 0.00365 0.0448 0.2248 0.7335
5.750 0.4109 0.00987 0.00380 0.0469 0.2218 0.7494
6.000 0.4279 0.01000 0.00395 0.0490 0.2176 0.7653
6.250 0.4467 0.01011 0.00410 0.0507 0.2148 0.7752
6.500 0.4665 0.01022 0.00425 0.0522 0.2124 0.7841
6.750 0.4854 0.01034 0.00440 0.0538 0.2097 0.7940
7.000 0.5043 0.01049 0.00457 0.0554 0.2059 0.8029
7.250 0.5208 0.01067 0.00477 0.0574 0.2006 0.8126
7.750 0.5590 0.01094 0.00514 0.0605 0.1948 0.8337
8.000 0.5780 0.01109 0.00534 0.0620 0.1910 0.8472
8.250 0.5966 0.01127 0.00558 0.0635 0.1866 0.8637
8.500 0.6180 0.01148 0.00585 0.0644 0.1819 0.8816
8.750 0.6445 0.01169 0.00611 0.0643 0.1751 0.8990
9.000 0.6723 0.01202 0.00644 0.0636 0.1655 0.9137
9.250 0.7013 0.01264 0.00694 0.0622 0.1410 0.9256
9.500 0.7317 0.01318 0.00743 0.0606 0.1291 0.9349
9.750 0.7683 0.01369 0.00792 0.0578 0.1220 0.9409
10.000 0.8011 0.01417 0.00839 0.0558 0.1171 0.9473
10.250 0.8358 0.01458 0.00882 0.0536 0.1146 0.9516
10.500 0.8679 0.01510 0.00933 0.0517 0.1108 0.9559
10.750 0.8955 0.01563 0.00986 0.0507 0.1078 0.9620
11.000 0.9238 0.01613 0.01038 0.0496 0.1055 0.9668
11.250 0.9526 0.01659 0.01087 0.0485 0.1039 0.9700
11.500 0.9771 0.01712 0.01141 0.0481 0.1016 0.9744
11.750 0.9974 0.01770 0.01200 0.0484 0.0992 0.9794
12.000 1.0222 0.01840 0.01270 0.0476 0.0961 0.9819
12.250 1.0478 0.01900 0.01332 0.0467 0.0937 0.9848
12.500 1.0715 0.01964 0.01397 0.0462 0.0902 0.9879
12.750 1.0904 0.02048 0.01479 0.0463 0.0856 0.9910
13.000 1.1095 0.02128 0.01559 0.0464 0.0796 0.9948
13.500 1.1421 0.02377 0.01795 0.0457 0.0624 0.9986
13.750 1.1609 0.02490 0.01909 0.0451 0.0592 0.9995
14.000 1.1721 0.02610 0.02030 0.0457 0.0568 1.0000
14.250 1.1758 0.02718 0.02140 0.0479 0.0552 1.0000
14.500 1.1806 0.02828 0.02254 0.0498 0.0540 1.0000
14.750 1.1851 0.02951 0.02380 0.0515 0.0529 1.0000
15.000 1.1879 0.03096 0.02527 0.0531 0.0513 1.0000
15.250 1.1913 0.03245 0.02680 0.0545 0.0502 1.0000
15.500 1.1970 0.03385 0.02823 0.0556 0.0491 1.0000
15.750 1.2019 0.03538 0.02980 0.0566 0.0480 1.0000
16.000 1.2062 0.03705 0.03151 0.0575 0.0472 1.0000
16.250 1.2101 0.03881 0.03332 0.0582 0.0463 1.0000
16.500 1.2127 0.04075 0.03531 0.0588 0.0455 1.0000
16.750 1.2139 0.04289 0.03748 0.0593 0.0446 1.0000
17.000 1.2167 0.04495 0.03960 0.0597 0.0442 1.0000
17.250 1.2205 0.04698 0.04168 0.0599 0.0435 1.0000
17.500 1.2232 0.04916 0.04392 0.0600 0.0428 1.0000
17.750 1.2251 0.05146 0.04626 0.0600 0.0420 1.0000
18.000 1.2252 0.05400 0.04887 0.0599 0.0415 1.0000
18.250 1.2235 0.05680 0.05172 0.0596 0.0407 1.0000
18.500 1.2209 0.05977 0.05474 0.0592 0.0401 1.0000
18.750 1.2167 0.06294 0.05797 0.0587 0.0394 1.0000
19.000 1.2154 0.06586 0.06096 0.0582 0.0391 1.0000
19.250 1.2143 0.06882 0.06400 0.0576 0.0386 1.0000
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