GOE 386 AIRFOIL (goe386-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 386 AIRFOIL (goe386-il) Reynolds number: 1,000,000 Max Cl/Cd: 94.02 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe386-il-1000000-n5.txt Download as CSV file: xf-goe386-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 386 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
------ -------- --------- --------- -------- -------- --------
-19.000 -0.9069 0.08445 0.08112 -0.0841 1.0000 0.0381
-18.750 -0.9308 0.07783 0.07442 -0.0881 1.0000 0.0383
-18.500 -0.9618 0.07063 0.06711 -0.0926 1.0000 0.0385
-18.250 -0.9975 0.06293 0.05929 -0.0973 1.0000 0.0386
-18.000 -1.0346 0.05503 0.05124 -0.1023 1.0000 0.0387
-17.750 -1.0674 0.04746 0.04353 -0.1073 1.0000 0.0389
-17.500 -1.0822 0.04093 0.03685 -0.1133 0.9916 0.0390
-17.000 -1.0811 0.03209 0.02773 -0.1227 0.9607 0.0395
-16.750 -1.0786 0.02938 0.02489 -0.1244 0.9431 0.0397
-16.500 -1.0744 0.02736 0.02273 -0.1250 0.9280 0.0399
-16.250 -1.0672 0.02577 0.02103 -0.1250 0.9157 0.0401
-16.000 -1.0580 0.02451 0.01965 -0.1246 0.9052 0.0403
-15.750 -1.0470 0.02346 0.01850 -0.1239 0.8946 0.0406
-15.500 -1.0346 0.02258 0.01752 -0.1229 0.8849 0.0408
-15.250 -1.0204 0.02182 0.01667 -0.1218 0.8754 0.0410
-15.000 -1.0069 0.02110 0.01586 -0.1205 0.8674 0.0412
-14.750 -0.9935 0.02045 0.01517 -0.1189 0.8604 0.0416
-14.500 -0.9761 0.01989 0.01457 -0.1178 0.8522 0.0419
-14.250 -0.9564 0.01940 0.01401 -0.1169 0.8445 0.0423
-14.000 -0.9353 0.01894 0.01351 -0.1161 0.8360 0.0426
-13.750 -0.9140 0.01852 0.01302 -0.1153 0.8259 0.0430
-13.500 -0.8918 0.01810 0.01254 -0.1146 0.8149 0.0434
-13.250 -0.8695 0.01773 0.01208 -0.1138 0.8007 0.0437
-13.000 -0.8469 0.01739 0.01164 -0.1130 0.7820 0.0441
-12.750 -0.8241 0.01708 0.01122 -0.1123 0.7583 0.0445
-12.500 -0.8013 0.01682 0.01081 -0.1115 0.7285 0.0448
-12.250 -0.7784 0.01660 0.01043 -0.1107 0.6960 0.0451
-12.000 -0.7552 0.01637 0.01006 -0.1099 0.6676 0.0454
-11.750 -0.7318 0.01609 0.00968 -0.1092 0.6474 0.0459
-11.500 -0.7073 0.01584 0.00936 -0.1087 0.6327 0.0463
-11.250 -0.6822 0.01560 0.00906 -0.1082 0.6207 0.0467
-11.000 -0.6566 0.01537 0.00878 -0.1077 0.6117 0.0472
-10.750 -0.6306 0.01515 0.00852 -0.1074 0.6037 0.0478
-10.500 -0.6047 0.01495 0.00826 -0.1070 0.5960 0.0483
-10.250 -0.5783 0.01473 0.00799 -0.1066 0.5904 0.0488
-10.000 -0.5518 0.01451 0.00773 -0.1063 0.5846 0.0492
-9.750 -0.5253 0.01432 0.00747 -0.1059 0.5784 0.0496
-9.250 -0.4723 0.01387 0.00696 -0.1053 0.5685 0.0506
-9.000 -0.4452 0.01367 0.00675 -0.1050 0.5645 0.0512
-8.750 -0.4179 0.01349 0.00655 -0.1048 0.5604 0.0517
-8.500 -0.3906 0.01333 0.00636 -0.1046 0.5562 0.0523
-8.250 -0.3633 0.01320 0.00618 -0.1043 0.5519 0.0530
-8.000 -0.3356 0.01304 0.00600 -0.1041 0.5488 0.0536
-7.750 -0.3077 0.01288 0.00582 -0.1040 0.5462 0.0542
-7.500 -0.2798 0.01273 0.00564 -0.1038 0.5434 0.0546
-7.250 -0.2524 0.01254 0.00544 -0.1036 0.5403 0.0552
-7.000 -0.2247 0.01240 0.00528 -0.1034 0.5369 0.0558
-6.750 -0.1970 0.01228 0.00514 -0.1032 0.5329 0.0565
-6.500 -0.1693 0.01218 0.00501 -0.1030 0.5283 0.0572
-6.250 -0.1408 0.01206 0.00488 -0.1029 0.5254 0.0579
-6.000 -0.1125 0.01194 0.00475 -0.1028 0.5220 0.0587
-5.750 -0.0843 0.01184 0.00462 -0.1027 0.5185 0.0593
-5.500 -0.0563 0.01174 0.00449 -0.1026 0.5152 0.0598
-5.250 -0.0284 0.01161 0.00434 -0.1024 0.5125 0.0606
-5.000 -0.0005 0.01152 0.00424 -0.1023 0.5092 0.0613
-4.750 0.0278 0.01143 0.00414 -0.1022 0.5064 0.0621
-4.500 0.0565 0.01133 0.00405 -0.1022 0.5038 0.0629
-4.250 0.0850 0.01125 0.00396 -0.1021 0.5013 0.0638
-4.000 0.1135 0.01117 0.00387 -0.1021 0.4990 0.0645
-3.750 0.1420 0.01111 0.00379 -0.1020 0.4964 0.0651
-3.500 0.1699 0.01101 0.00368 -0.1019 0.4930 0.0659
-3.250 0.1977 0.01096 0.00360 -0.1017 0.4887 0.0668
-3.000 0.2261 0.01089 0.00354 -0.1016 0.4860 0.0678
-2.750 0.2548 0.01082 0.00347 -0.1016 0.4833 0.0688
-2.500 0.2834 0.01076 0.00341 -0.1016 0.4799 0.0697
-2.250 0.3117 0.01072 0.00336 -0.1015 0.4764 0.0705
-2.000 0.3399 0.01067 0.00330 -0.1014 0.4733 0.0713
-1.750 0.3677 0.01062 0.00324 -0.1013 0.4701 0.0725
-1.500 0.3959 0.01058 0.00320 -0.1012 0.4672 0.0738
-1.250 0.4245 0.01053 0.00316 -0.1012 0.4645 0.0750
-1.000 0.4529 0.01050 0.00313 -0.1012 0.4606 0.0761
-0.750 0.4810 0.01049 0.00310 -0.1011 0.4560 0.0771
-0.500 0.5085 0.01047 0.00307 -0.1010 0.4516 0.0788
-0.250 0.5364 0.01044 0.00305 -0.1009 0.4479 0.0807
0.000 0.5646 0.01042 0.00303 -0.1008 0.4437 0.0827
0.250 0.5923 0.01041 0.00302 -0.1007 0.4381 0.0857
0.750 0.6460 0.01026 0.00302 -0.1003 0.4257 0.1430
1.000 0.6725 0.01030 0.00307 -0.1000 0.4158 0.1568
1.250 0.6988 0.01037 0.00313 -0.0996 0.4036 0.1680
1.500 0.7236 0.01052 0.00322 -0.0991 0.3859 0.1766
1.750 0.7473 0.01074 0.00335 -0.0983 0.3666 0.1837
2.000 0.7713 0.01093 0.00349 -0.0976 0.3511 0.1927
2.250 0.7956 0.01111 0.00364 -0.0970 0.3394 0.2021
2.500 0.8198 0.01127 0.00379 -0.0963 0.3295 0.2158
2.750 0.8448 0.01138 0.00392 -0.0958 0.3229 0.2320
3.000 0.8696 0.01148 0.00405 -0.0953 0.3170 0.2519
3.250 0.8936 0.01161 0.00422 -0.0947 0.3110 0.2780
3.500 0.9185 0.01165 0.00436 -0.0942 0.3070 0.3153
3.750 0.9428 0.01169 0.00452 -0.0936 0.3031 0.3609
4.000 0.9655 0.01176 0.00468 -0.0928 0.2992 0.4051
4.250 0.9872 0.01183 0.00487 -0.0918 0.2954 0.4549
4.500 1.0092 0.01188 0.00507 -0.0908 0.2919 0.5190
4.750 1.0338 0.01183 0.00527 -0.0904 0.2901 0.6101
5.000 1.0579 0.01178 0.00550 -0.0899 0.2878 0.7128
5.250 1.0799 0.01174 0.00576 -0.0889 0.2850 0.8197
5.500 1.0967 0.01176 0.00605 -0.0865 0.2821 0.9244
5.750 1.1282 0.01200 0.00631 -0.0875 0.2784 1.0000
6.000 1.1490 0.01228 0.00657 -0.0865 0.2752 1.0000
6.250 1.1717 0.01250 0.00679 -0.0857 0.2736 1.0000
6.500 1.1947 0.01273 0.00701 -0.0850 0.2719 1.0000
6.750 1.2171 0.01298 0.00726 -0.0843 0.2699 1.0000
7.000 1.2390 0.01326 0.00753 -0.0835 0.2676 1.0000
7.250 1.2604 0.01357 0.00783 -0.0827 0.2652 1.0000
7.500 1.2811 0.01392 0.00817 -0.0818 0.2628 1.0000
7.750 1.3012 0.01431 0.00855 -0.0809 0.2602 1.0000
8.000 1.3212 0.01471 0.00894 -0.0800 0.2577 1.0000
8.250 1.3429 0.01504 0.00928 -0.0793 0.2564 1.0000
8.500 1.3644 0.01539 0.00964 -0.0787 0.2547 1.0000
8.750 1.3852 0.01578 0.01004 -0.0780 0.2528 1.0000
9.000 1.4050 0.01622 0.01049 -0.0772 0.2507 1.0000
9.250 1.4245 0.01669 0.01096 -0.0764 0.2487 1.0000
9.500 1.4431 0.01721 0.01149 -0.0755 0.2468 1.0000
9.750 1.4607 0.01780 0.01208 -0.0745 0.2447 1.0000
10.000 1.4776 0.01844 0.01272 -0.0735 0.2421 1.0000
10.250 1.4967 0.01898 0.01328 -0.0728 0.2406 1.0000
10.500 1.5156 0.01953 0.01386 -0.0721 0.2388 1.0000
10.750 1.5335 0.02014 0.01449 -0.0714 0.2371 1.0000
11.000 1.5502 0.02084 0.01521 -0.0705 0.2350 1.0000
11.250 1.5660 0.02161 0.01599 -0.0696 0.2324 1.0000
11.500 1.5796 0.02254 0.01693 -0.0686 0.2298 1.0000
11.750 1.5932 0.02349 0.01789 -0.0676 0.2275 1.0000
12.000 1.6079 0.02439 0.01882 -0.0668 0.2260 1.0000
12.250 1.6237 0.02523 0.01970 -0.0661 0.2245 1.0000
12.500 1.6379 0.02621 0.02071 -0.0653 0.2228 1.0000
12.750 1.6518 0.02723 0.02177 -0.0646 0.2207 1.0000
13.000 1.6629 0.02850 0.02305 -0.0638 0.2180 1.0000
13.250 1.6720 0.02994 0.02451 -0.0628 0.2149 1.0000
13.500 1.6807 0.03146 0.02605 -0.0620 0.2118 1.0000
13.750 1.6920 0.03282 0.02745 -0.0613 0.2091 1.0000
14.000 1.7017 0.03432 0.02898 -0.0607 0.2059 1.0000
14.250 1.7081 0.03615 0.03083 -0.0599 0.2024 1.0000
14.500 1.7112 0.03831 0.03301 -0.0591 0.1988 1.0000
14.750 1.7194 0.04003 0.03477 -0.0586 0.1957 1.0000
15.000 1.7251 0.04199 0.03676 -0.0580 0.1918 1.0000
15.250 1.7254 0.04450 0.03929 -0.0573 0.1875 1.0000
15.500 1.7276 0.04684 0.04165 -0.0566 0.1836 1.0000
15.750 1.7297 0.04916 0.04399 -0.0560 0.1787 1.0000
16.000 1.7245 0.05225 0.04710 -0.0553 0.1736 1.0000
16.250 1.7260 0.05469 0.04957 -0.0548 0.1690 1.0000
16.500 1.7213 0.05776 0.05265 -0.0542 0.1635 1.0000
16.750 1.7169 0.06084 0.05575 -0.0537 0.1583 1.0000
17.000 1.7112 0.06406 0.05898 -0.0532 0.1521 1.0000
17.250 1.7039 0.06756 0.06250 -0.0528 0.1465 1.0000
17.500 1.6970 0.07097 0.06591 -0.0525 0.1408 1.0000
17.750 1.6899 0.07451 0.06948 -0.0523 0.1363 1.0000
18.000 1.6843 0.07788 0.07287 -0.0521 0.1318 1.0000
18.250 1.6765 0.08159 0.07662 -0.0520 0.1283 1.0000
18.500 1.6750 0.08456 0.07963 -0.0521 0.1255 1.0000
18.750 1.6684 0.08818 0.08330 -0.0521 0.1229 1.0000
19.000 1.6630 0.09167 0.08682 -0.0523 0.1203 1.0000
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