GOE 604 AIRFOIL (goe604-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 604 AIRFOIL (goe604-il) Reynolds number: 200,000 Max Cl/Cd: 61.19 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe604-il-200000-n5.txt Download as CSV file: xf-goe604-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 604 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 -0.6124 0.05568 0.05112 -0.0872 1.0000 0.0330
-13.250 -0.6406 0.04988 0.04518 -0.0908 1.0000 0.0331
-13.000 -0.6666 0.04571 0.04088 -0.0922 0.9998 0.0332
-12.750 -0.6598 0.04183 0.03682 -0.0975 0.9872 0.0336
-12.500 -0.6509 0.03903 0.03383 -0.1010 0.9749 0.0343
-12.250 -0.6408 0.03647 0.03103 -0.1033 0.9624 0.0350
-12.000 -0.6295 0.03418 0.02845 -0.1046 0.9489 0.0358
-11.750 -0.6157 0.03208 0.02600 -0.1053 0.9345 0.0366
-11.500 -0.5902 0.03073 0.02460 -0.1065 0.9214 0.0372
-11.250 -0.5668 0.02971 0.02352 -0.1069 0.9052 0.0380
-11.000 -0.5455 0.02863 0.02230 -0.1069 0.8870 0.0389
-10.750 -0.5261 0.02756 0.02102 -0.1064 0.8659 0.0399
-10.500 -0.5076 0.02650 0.01971 -0.1054 0.8425 0.0408
-10.250 -0.4891 0.02555 0.01847 -0.1043 0.8174 0.0417
-10.000 -0.4693 0.02479 0.01763 -0.1032 0.7928 0.0425
-9.750 -0.4503 0.02416 0.01687 -0.1019 0.7689 0.0434
-9.500 -0.4314 0.02357 0.01610 -0.1006 0.7466 0.0444
-9.250 -0.4124 0.02296 0.01528 -0.0991 0.7264 0.0455
-9.000 -0.3930 0.02237 0.01447 -0.0977 0.7087 0.0465
-8.750 -0.3731 0.02179 0.01372 -0.0964 0.6935 0.0475
-8.500 -0.3530 0.02126 0.01313 -0.0951 0.6802 0.0486
-8.250 -0.3322 0.02080 0.01256 -0.0939 0.6678 0.0498
-8.000 -0.3109 0.02033 0.01197 -0.0928 0.6565 0.0511
-7.750 -0.2893 0.01990 0.01138 -0.0916 0.6467 0.0524
-7.500 -0.2673 0.01944 0.01082 -0.0906 0.6371 0.0537
-7.000 -0.2234 0.01862 0.00988 -0.0885 0.6201 0.0571
-6.750 -0.2005 0.01828 0.00942 -0.0875 0.6123 0.0591
-6.500 -0.1778 0.01790 0.00897 -0.0865 0.6051 0.0611
-6.250 -0.1549 0.01754 0.00856 -0.0856 0.5973 0.0634
-5.750 -0.1080 0.01691 0.00779 -0.0838 0.5831 0.0701
-5.500 -0.0842 0.01662 0.00743 -0.0829 0.5760 0.0747
-5.250 -0.0605 0.01633 0.00709 -0.0821 0.5700 0.0804
-5.000 -0.0363 0.01602 0.00681 -0.0813 0.5635 0.0892
-4.750 -0.0122 0.01575 0.00660 -0.0806 0.5575 0.1051
-4.500 0.0127 0.01559 0.00646 -0.0799 0.5522 0.1269
-4.250 0.0385 0.01547 0.00634 -0.0794 0.5462 0.1439
-4.000 0.0639 0.01537 0.00621 -0.0788 0.5403 0.1567
-3.750 0.0895 0.01531 0.00606 -0.0782 0.5352 0.1678
-3.500 0.1151 0.01520 0.00596 -0.0776 0.5299 0.1786
-3.250 0.1405 0.01510 0.00586 -0.0771 0.5243 0.1888
-3.000 0.1661 0.01504 0.00574 -0.0765 0.5190 0.1995
-2.750 0.1912 0.01495 0.00566 -0.0759 0.5140 0.2112
-2.500 0.2166 0.01486 0.00560 -0.0753 0.5082 0.2250
-2.250 0.2417 0.01478 0.00555 -0.0747 0.5029 0.2418
-2.000 0.2666 0.01473 0.00549 -0.0740 0.4985 0.2612
-1.750 0.2919 0.01464 0.00547 -0.0734 0.4933 0.2796
-1.500 0.3171 0.01457 0.00543 -0.0728 0.4879 0.2970
-1.250 0.3419 0.01453 0.00537 -0.0721 0.4828 0.3160
-1.000 0.3666 0.01448 0.00535 -0.0714 0.4779 0.3373
-0.750 0.3913 0.01442 0.00535 -0.0707 0.4721 0.3610
-0.250 0.4390 0.01430 0.00533 -0.0691 0.4622 0.4226
0.000 0.4625 0.01419 0.00539 -0.0682 0.4570 0.4640
0.250 0.4849 0.01406 0.00543 -0.0670 0.4518 0.5169
0.500 0.5059 0.01391 0.00547 -0.0656 0.4473 0.5877
0.750 0.5265 0.01371 0.00558 -0.0639 0.4427 0.6782
1.000 0.5528 0.01356 0.00576 -0.0632 0.4373 0.7850
1.250 0.6081 0.01368 0.00600 -0.0683 0.4311 0.8865
1.500 0.6609 0.01389 0.00616 -0.0733 0.4250 0.9334
1.750 0.7065 0.01409 0.00631 -0.0769 0.4188 0.9594
2.000 0.7478 0.01432 0.00643 -0.0797 0.4137 0.9798
2.250 0.7931 0.01454 0.00658 -0.0834 0.4087 0.9947
2.500 0.8265 0.01472 0.00672 -0.0847 0.4037 1.0000
2.750 0.8455 0.01489 0.00682 -0.0831 0.3996 1.0000
3.000 0.8643 0.01508 0.00693 -0.0815 0.3960 1.0000
3.250 0.8838 0.01527 0.00708 -0.0800 0.3919 1.0000
3.500 0.9031 0.01545 0.00724 -0.0785 0.3874 1.0000
3.750 0.9218 0.01565 0.00738 -0.0768 0.3829 1.0000
4.000 0.9403 0.01587 0.00752 -0.0752 0.3789 1.0000
4.250 0.9595 0.01608 0.00772 -0.0737 0.3746 1.0000
4.500 0.9784 0.01629 0.00792 -0.0721 0.3702 1.0000
4.750 0.9971 0.01652 0.00811 -0.0705 0.3665 1.0000
5.000 1.0157 0.01677 0.00831 -0.0689 0.3635 1.0000
5.250 1.0347 0.01704 0.00853 -0.0674 0.3606 1.0000
5.500 1.0537 0.01728 0.00880 -0.0659 0.3574 1.0000
5.750 1.0720 0.01754 0.00907 -0.0643 0.3540 1.0000
6.000 1.0898 0.01781 0.00932 -0.0627 0.3507 1.0000
6.250 1.1075 0.01810 0.00958 -0.0610 0.3479 1.0000
6.500 1.1248 0.01841 0.00984 -0.0593 0.3453 1.0000
6.750 1.1410 0.01870 0.01017 -0.0575 0.3425 1.0000
7.000 1.1563 0.01899 0.01051 -0.0554 0.3393 1.0000
7.250 1.1717 0.01931 0.01085 -0.0535 0.3361 1.0000
7.500 1.1872 0.01965 0.01118 -0.0516 0.3331 1.0000
7.750 1.2030 0.02001 0.01152 -0.0499 0.3304 1.0000
8.000 1.2193 0.02040 0.01190 -0.0483 0.3276 1.0000
8.250 1.2346 0.02080 0.01237 -0.0466 0.3248 1.0000
8.500 1.2503 0.02123 0.01286 -0.0451 0.3222 1.0000
8.750 1.2655 0.02167 0.01335 -0.0435 0.3195 1.0000
9.000 1.2798 0.02215 0.01384 -0.0419 0.3164 1.0000
9.250 1.2943 0.02265 0.01432 -0.0403 0.3134 1.0000
9.500 1.3086 0.02320 0.01489 -0.0388 0.3105 1.0000
9.750 1.3217 0.02380 0.01559 -0.0373 0.3077 1.0000
10.000 1.3343 0.02444 0.01631 -0.0358 0.3047 1.0000
10.250 1.3463 0.02512 0.01704 -0.0343 0.3015 1.0000
10.500 1.3580 0.02584 0.01777 -0.0328 0.2983 1.0000
10.750 1.3711 0.02655 0.01847 -0.0316 0.2955 1.0000
11.000 1.3800 0.02749 0.01955 -0.0301 0.2921 1.0000
11.250 1.3886 0.02850 0.02066 -0.0287 0.2883 1.0000
11.500 1.3971 0.02955 0.02176 -0.0274 0.2846 1.0000
11.750 1.4058 0.03062 0.02285 -0.0262 0.2813 1.0000
12.000 1.4135 0.03184 0.02415 -0.0251 0.2779 1.0000
12.250 1.4186 0.03331 0.02576 -0.0241 0.2737 1.0000
12.500 1.4231 0.03486 0.02738 -0.0231 0.2693 1.0000
12.750 1.4281 0.03641 0.02894 -0.0222 0.2654 1.0000
13.000 1.4301 0.03835 0.03101 -0.0214 0.2608 1.0000
13.250 1.4299 0.04054 0.03330 -0.0208 0.2555 1.0000
13.500 1.4307 0.04268 0.03546 -0.0202 0.2506 1.0000
13.750 1.4278 0.04536 0.03827 -0.0199 0.2447 1.0000
14.000 1.4244 0.04810 0.04107 -0.0195 0.2387 1.0000
14.250 1.4198 0.05107 0.04411 -0.0194 0.2327 1.0000
14.500 1.4127 0.05440 0.04751 -0.0193 0.2259 1.0000
14.750 1.4062 0.05771 0.05087 -0.0193 0.2198 1.0000
15.000 1.3981 0.06131 0.05453 -0.0195 0.2132 1.0000
15.250 1.3918 0.06474 0.05797 -0.0197 0.2081 1.0000
15.500 1.3848 0.06835 0.06165 -0.0200 0.2027 1.0000
15.750 1.3789 0.07182 0.06511 -0.0203 0.1978 1.0000
16.000 1.3745 0.07519 0.06851 -0.0206 0.1935 1.0000
16.250 1.3696 0.07868 0.07206 -0.0211 0.1894 1.0000
16.500 1.3680 0.08171 0.07509 -0.0214 0.1857 1.0000
16.750 1.3685 0.08446 0.07782 -0.0218 0.1824 1.0000
17.000 1.3661 0.08775 0.08121 -0.0223 0.1795 1.0000
17.250 1.3642 0.09099 0.08451 -0.0229 0.1766 1.0000
17.500 1.3657 0.09371 0.08725 -0.0234 0.1736 1.0000
17.750 1.3721 0.09569 0.08920 -0.0237 0.1709 1.0000
18.000 1.3761 0.09807 0.09162 -0.0241 0.1688 1.0000
18.250 1.3735 0.10151 0.09519 -0.0250 0.1667 1.0000
18.500 1.3719 0.10483 0.09861 -0.0259 0.1645 1.0000
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