GOE 460 AIRFOIL (goe460-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 460 AIRFOIL (goe460-il) Reynolds number: 1,000,000 Max Cl/Cd: 66.6 at α=10.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe460-il-1000000.txt Download as CSV file: xf-goe460-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1869 0.07772 0.07323 -0.0559 1.0000 0.0443
-19.500 -1.1887 0.07458 0.07001 -0.0567 1.0000 0.0448
-19.250 -1.1966 0.07074 0.06610 -0.0577 1.0000 0.0454
-19.000 -1.2069 0.06669 0.06198 -0.0586 1.0000 0.0461
-18.750 -1.2141 0.06310 0.05833 -0.0593 1.0000 0.0467
-18.500 -1.2189 0.05986 0.05503 -0.0598 1.0000 0.0475
-18.250 -1.2222 0.05683 0.05194 -0.0601 1.0000 0.0483
-18.000 -1.2221 0.05423 0.04928 -0.0603 1.0000 0.0491
-17.750 -1.2219 0.05171 0.04669 -0.0604 1.0000 0.0497
-17.500 -1.2198 0.04943 0.04433 -0.0604 1.0000 0.0502
-17.250 -1.2241 0.04657 0.04143 -0.0603 1.0000 0.0514
-17.000 -1.2264 0.04399 0.03880 -0.0600 1.0000 0.0525
-16.750 -1.2267 0.04169 0.03646 -0.0595 1.0000 0.0535
-16.500 -1.2252 0.03963 0.03434 -0.0589 1.0000 0.0546
-16.250 -1.2218 0.03779 0.03245 -0.0583 1.0000 0.0557
-16.000 -1.2206 0.03584 0.03046 -0.0574 1.0000 0.0572
-15.750 -1.2211 0.03387 0.02846 -0.0562 1.0000 0.0589
-15.500 -1.2196 0.03215 0.02670 -0.0549 1.0000 0.0607
-15.250 -1.2166 0.03063 0.02515 -0.0535 1.0000 0.0627
-15.000 -1.2166 0.02899 0.02351 -0.0517 1.0000 0.0660
-14.750 -1.2152 0.02756 0.02209 -0.0498 1.0000 0.0700
-14.500 -1.2147 0.02621 0.02077 -0.0475 1.0000 0.0757
-14.250 -1.2134 0.02501 0.01960 -0.0451 1.0000 0.0824
-14.000 -1.2103 0.02403 0.01863 -0.0426 1.0000 0.0875
-13.750 -1.2057 0.02323 0.01783 -0.0401 1.0000 0.0926
-13.500 -1.2022 0.02247 0.01705 -0.0373 1.0000 0.0956
-13.250 -1.2013 0.02167 0.01625 -0.0340 1.0000 0.0985
-13.000 -1.1988 0.02104 0.01560 -0.0308 1.0000 0.1012
-12.750 -1.1743 0.02045 0.01498 -0.0315 0.9991 0.1043
-12.500 -1.1498 0.01957 0.01411 -0.0326 0.9975 0.1082
-12.250 -1.1221 0.01887 0.01340 -0.0340 0.9955 0.1116
-12.000 -1.0915 0.01834 0.01284 -0.0357 0.9936 0.1143
-11.750 -1.0644 0.01759 0.01210 -0.0370 0.9916 0.1184
-11.500 -1.0418 0.01688 0.01139 -0.0373 0.9882 0.1219
-11.250 -1.0147 0.01631 0.01082 -0.0382 0.9854 0.1253
-11.000 -0.9877 0.01562 0.01016 -0.0393 0.9829 0.1315
-10.750 -0.9589 0.01500 0.00957 -0.0406 0.9809 0.1387
-10.500 -0.9317 0.01427 0.00894 -0.0417 0.9792 0.1531
-10.250 -0.9106 0.01368 0.00844 -0.0413 0.9746 0.1679
-10.000 -0.8825 0.01328 0.00807 -0.0420 0.9711 0.1784
-9.750 -0.8532 0.01283 0.00767 -0.0430 0.9682 0.1882
-9.500 -0.8184 0.01257 0.00739 -0.0449 0.9661 0.1931
-9.250 -0.7829 0.01214 0.00699 -0.0471 0.9641 0.1998
-9.000 -0.7568 0.01185 0.00671 -0.0472 0.9572 0.2044
-8.750 -0.7183 0.01164 0.00647 -0.0498 0.9537 0.2088
-8.500 -0.6792 0.01126 0.00611 -0.0527 0.9502 0.2147
-8.250 -0.6471 0.01097 0.00582 -0.0541 0.9431 0.2190
-8.000 -0.6119 0.01073 0.00556 -0.0560 0.9352 0.2227
-7.750 -0.5790 0.01055 0.00534 -0.0574 0.9262 0.2259
-7.500 -0.5510 0.01026 0.00504 -0.0578 0.9151 0.2311
-7.250 -0.5291 0.01003 0.00480 -0.0569 0.9021 0.2363
-7.000 -0.5047 0.00986 0.00459 -0.0565 0.8901 0.2406
-6.750 -0.4825 0.00970 0.00438 -0.0555 0.8777 0.2455
-6.500 -0.4649 0.00951 0.00418 -0.0536 0.8654 0.2510
-6.250 -0.4456 0.00936 0.00399 -0.0520 0.8544 0.2571
-6.000 -0.4277 0.00920 0.00382 -0.0502 0.8436 0.2642
-5.750 -0.4109 0.00901 0.00364 -0.0481 0.8338 0.2747
-5.500 -0.3953 0.00881 0.00347 -0.0457 0.8235 0.2869
-5.250 -0.3795 0.00862 0.00330 -0.0434 0.8141 0.3024
-5.000 -0.3646 0.00842 0.00315 -0.0408 0.8030 0.3205
-4.750 -0.3495 0.00824 0.00300 -0.0383 0.7923 0.3388
-4.500 -0.3336 0.00809 0.00288 -0.0358 0.7804 0.3557
-4.250 -0.3160 0.00796 0.00277 -0.0337 0.7700 0.3707
-4.000 -0.2993 0.00786 0.00267 -0.0314 0.7582 0.3843
-3.750 -0.2823 0.00774 0.00258 -0.0291 0.7460 0.3963
-3.500 -0.2642 0.00769 0.00250 -0.0271 0.7328 0.4074
-3.250 -0.2490 0.00763 0.00244 -0.0244 0.7163 0.4190
-2.750 -0.2178 0.00762 0.00235 -0.0191 0.6813 0.4379
-2.500 -0.2010 0.00762 0.00232 -0.0167 0.6647 0.4472
-2.250 -0.1830 0.00760 0.00228 -0.0146 0.6503 0.4580
-2.000 -0.1643 0.00760 0.00226 -0.0127 0.6373 0.4678
-1.750 -0.1447 0.00760 0.00224 -0.0109 0.6246 0.4781
-1.500 -0.1246 0.00758 0.00222 -0.0092 0.6133 0.4878
-1.250 -0.1045 0.00759 0.00221 -0.0076 0.6026 0.4989
-1.000 -0.0841 0.00755 0.00219 -0.0059 0.5921 0.5102
-0.500 -0.0428 0.00753 0.00218 -0.0028 0.5712 0.5324
-0.250 -0.0218 0.00756 0.00218 -0.0013 0.5611 0.5425
0.000 0.0000 0.00753 0.00218 0.0000 0.5525 0.5525
0.250 0.0217 0.00756 0.00218 0.0013 0.5425 0.5612
0.500 0.0429 0.00753 0.00218 0.0028 0.5332 0.5712
1.000 0.0843 0.00755 0.00219 0.0059 0.5106 0.5920
1.250 0.1045 0.00759 0.00221 0.0076 0.4988 0.6025
1.500 0.1246 0.00758 0.00222 0.0092 0.4880 0.6133
1.750 0.1449 0.00760 0.00224 0.0108 0.4782 0.6239
2.000 0.1642 0.00761 0.00226 0.0127 0.4674 0.6372
2.250 0.1829 0.00760 0.00228 0.0146 0.4577 0.6504
2.500 0.2010 0.00762 0.00232 0.0167 0.4471 0.6645
2.750 0.2181 0.00762 0.00235 0.0191 0.4380 0.6809
3.000 0.2330 0.00763 0.00239 0.0218 0.4282 0.6986
3.250 0.2490 0.00764 0.00244 0.0244 0.4190 0.7163
3.500 0.2644 0.00769 0.00250 0.0270 0.4075 0.7323
3.750 0.2824 0.00774 0.00258 0.0291 0.3964 0.7460
4.000 0.2994 0.00786 0.00267 0.0314 0.3843 0.7581
4.250 0.3161 0.00796 0.00277 0.0337 0.3705 0.7698
4.500 0.3334 0.00810 0.00288 0.0359 0.3551 0.7806
4.750 0.3495 0.00824 0.00300 0.0383 0.3389 0.7924
5.000 0.3644 0.00841 0.00315 0.0408 0.3207 0.8041
5.250 0.3794 0.00862 0.00330 0.0434 0.3022 0.8145
5.500 0.3953 0.00881 0.00347 0.0457 0.2870 0.8240
5.750 0.4109 0.00901 0.00364 0.0481 0.2743 0.8338
6.000 0.4276 0.00920 0.00382 0.0501 0.2639 0.8436
6.250 0.4457 0.00936 0.00399 0.0520 0.2569 0.8542
6.500 0.4650 0.00951 0.00418 0.0536 0.2510 0.8656
6.750 0.4825 0.00970 0.00438 0.0555 0.2451 0.8778
7.000 0.5049 0.00986 0.00459 0.0564 0.2410 0.8900
7.250 0.5295 0.01003 0.00480 0.0569 0.2369 0.9020
7.500 0.5515 0.01025 0.00503 0.0577 0.2318 0.9151
7.750 0.5791 0.01055 0.00534 0.0573 0.2259 0.9263
8.000 0.6119 0.01073 0.00556 0.0560 0.2231 0.9352
8.250 0.6474 0.01096 0.00582 0.0540 0.2190 0.9429
8.500 0.6798 0.01126 0.00610 0.0526 0.2147 0.9503
8.750 0.7187 0.01164 0.00647 0.0497 0.2089 0.9537
9.000 0.7572 0.01185 0.00671 0.0472 0.2049 0.9571
9.250 0.7835 0.01214 0.00699 0.0470 0.1997 0.9641
9.500 0.8190 0.01256 0.00738 0.0448 0.1930 0.9660
9.750 0.8538 0.01283 0.00767 0.0429 0.1878 0.9682
10.000 0.8831 0.01329 0.00807 0.0419 0.1781 0.9711
10.250 0.9111 0.01368 0.00843 0.0412 0.1675 0.9746
10.500 0.9323 0.01427 0.00894 0.0416 0.1524 0.9792
10.750 0.9596 0.01500 0.00956 0.0404 0.1382 0.9809
11.000 0.9884 0.01562 0.01015 0.0391 0.1312 0.9829
11.250 1.0156 0.01630 0.01081 0.0380 0.1254 0.9855
11.500 1.0427 0.01686 0.01138 0.0371 0.1219 0.9883
11.750 1.0650 0.01760 0.01210 0.0369 0.1180 0.9917
12.000 1.0930 0.01831 0.01281 0.0355 0.1140 0.9937
12.250 1.1234 0.01885 0.01338 0.0338 0.1114 0.9957
12.500 1.1511 0.01955 0.01408 0.0324 0.1082 0.9976
12.750 1.1755 0.02045 0.01497 0.0312 0.1040 0.9992
13.000 1.1990 0.02101 0.01556 0.0308 0.1014 1.0000
13.250 1.2020 0.02163 0.01620 0.0340 0.0988 1.0000
13.500 1.2023 0.02244 0.01702 0.0373 0.0956 1.0000
13.750 1.2062 0.02318 0.01778 0.0401 0.0924 1.0000
14.000 1.2113 0.02396 0.01857 0.0425 0.0881 1.0000
14.250 1.2143 0.02496 0.01955 0.0450 0.0830 1.0000
14.500 1.2154 0.02617 0.02072 0.0475 0.0754 1.0000
14.750 1.2161 0.02752 0.02204 0.0497 0.0697 1.0000
15.000 1.2178 0.02893 0.02345 0.0516 0.0658 1.0000
15.250 1.2179 0.03056 0.02508 0.0534 0.0626 1.0000
15.500 1.2207 0.03210 0.02665 0.0548 0.0604 1.0000
15.750 1.2224 0.03381 0.02839 0.0560 0.0587 1.0000
16.000 1.2221 0.03578 0.03039 0.0572 0.0571 1.0000
16.250 1.2239 0.03769 0.03234 0.0581 0.0557 1.0000
16.500 1.2275 0.03951 0.03422 0.0587 0.0546 1.0000
16.750 1.2292 0.04157 0.03633 0.0593 0.0534 1.0000
17.000 1.2293 0.04383 0.03864 0.0597 0.0524 1.0000
17.250 1.2267 0.04645 0.04129 0.0600 0.0513 1.0000
17.500 1.2225 0.04931 0.04421 0.0601 0.0503 1.0000
17.750 1.2247 0.05158 0.04655 0.0601 0.0497 1.0000
18.000 1.2252 0.05410 0.04914 0.0600 0.0489 1.0000
18.250 1.2254 0.05668 0.05179 0.0598 0.0482 1.0000
18.500 1.2230 0.05961 0.05477 0.0595 0.0475 1.0000
18.750 1.2178 0.06291 0.05813 0.0589 0.0466 1.0000
19.000 1.2101 0.06658 0.06186 0.0582 0.0460 1.0000
19.250 1.1995 0.07067 0.06602 0.0573 0.0452 1.0000
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