GOE 683 AIRFOIL (goe683-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 683 AIRFOIL (goe683-il) Reynolds number: 500,000 Max Cl/Cd: 85.75 at α=8° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe683-il-500000.txt Download as CSV file: xf-goe683-il-500000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 683 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9670 0.08817 0.08409 -0.0697 1.0000 0.0448
-19.500 -0.9735 0.08398 0.07985 -0.0719 1.0000 0.0451
-19.250 -0.9777 0.08014 0.07596 -0.0740 1.0000 0.0456
-19.000 -0.9865 0.07573 0.07145 -0.0763 1.0000 0.0459
-18.750 -0.9938 0.07158 0.06723 -0.0786 1.0000 0.0463
-18.500 -1.0025 0.06736 0.06290 -0.0807 1.0000 0.0467
-18.250 -1.0105 0.06336 0.05879 -0.0826 1.0000 0.0471
-18.000 -1.0190 0.05942 0.05473 -0.0844 1.0000 0.0476
-17.750 -1.0259 0.05584 0.05102 -0.0858 1.0000 0.0480
-17.500 -1.0315 0.05253 0.04758 -0.0870 1.0000 0.0484
-17.250 -1.0358 0.04952 0.04444 -0.0877 1.0000 0.0487
-17.000 -1.0409 0.04663 0.04140 -0.0883 1.0000 0.0491
-16.750 -1.0382 0.04454 0.03929 -0.0880 1.0000 0.0497
-16.500 -1.0341 0.04267 0.03739 -0.0877 1.0000 0.0501
-16.250 -1.0301 0.04093 0.03564 -0.0873 1.0000 0.0507
-16.000 -1.0265 0.03924 0.03390 -0.0868 1.0000 0.0512
-15.750 -1.0230 0.03763 0.03224 -0.0860 1.0000 0.0517
-15.500 -1.0199 0.03611 0.03065 -0.0849 1.0000 0.0523
-15.250 -1.0163 0.03470 0.02917 -0.0836 1.0000 0.0528
-15.000 -1.0130 0.03335 0.02773 -0.0820 1.0000 0.0534
-14.750 -1.0098 0.03219 0.02648 -0.0801 1.0000 0.0540
-14.500 -1.0055 0.03109 0.02529 -0.0780 1.0000 0.0545
-14.250 -1.0009 0.02997 0.02409 -0.0758 1.0000 0.0551
-14.000 -0.9936 0.02893 0.02307 -0.0738 1.0000 0.0558
-13.750 -0.9868 0.02812 0.02225 -0.0714 1.0000 0.0564
-13.500 -0.9803 0.02737 0.02150 -0.0689 1.0000 0.0570
-13.250 -0.9742 0.02669 0.02079 -0.0661 1.0000 0.0576
-13.000 -0.9696 0.02607 0.02015 -0.0630 1.0000 0.0583
-12.750 -0.9486 0.02533 0.01934 -0.0629 0.9984 0.0593
-12.500 -0.9164 0.02442 0.01835 -0.0649 0.9889 0.0604
-12.250 -0.8896 0.02345 0.01732 -0.0658 0.9740 0.0615
-12.000 -0.8589 0.02244 0.01633 -0.0674 0.9574 0.0628
-11.750 -0.8184 0.02162 0.01550 -0.0708 0.9430 0.0641
-11.500 -0.7683 0.02079 0.01460 -0.0762 0.9297 0.0658
-11.250 -0.7067 0.02007 0.01373 -0.0838 0.9156 0.0676
-11.000 -0.6482 0.01886 0.01249 -0.0913 0.8971 0.0698
-10.750 -0.6011 0.01823 0.01175 -0.0960 0.8751 0.0717
-10.500 -0.5707 0.01781 0.01119 -0.0972 0.8548 0.0734
-10.250 -0.5487 0.01749 0.01073 -0.0965 0.8367 0.0746
-10.000 -0.5320 0.01704 0.01019 -0.0947 0.8211 0.0760
-9.750 -0.5185 0.01651 0.00961 -0.0925 0.8068 0.0774
-9.500 -0.5023 0.01616 0.00918 -0.0905 0.7939 0.0791
-9.250 -0.4873 0.01582 0.00879 -0.0882 0.7806 0.0806
-9.000 -0.4708 0.01554 0.00842 -0.0862 0.7689 0.0820
-8.750 -0.4532 0.01532 0.00810 -0.0842 0.7571 0.0834
-8.500 -0.4412 0.01484 0.00760 -0.0814 0.7462 0.0854
-8.250 -0.4263 0.01449 0.00722 -0.0790 0.7357 0.0877
-8.000 -0.4095 0.01422 0.00689 -0.0769 0.7253 0.0898
-7.750 -0.3919 0.01399 0.00658 -0.0749 0.7151 0.0919
-7.500 -0.3759 0.01367 0.00625 -0.0726 0.7060 0.0950
-7.250 -0.3584 0.01339 0.00596 -0.0706 0.6970 0.0991
-7.000 -0.3399 0.01314 0.00570 -0.0687 0.6888 0.1045
-6.750 -0.3216 0.01287 0.00547 -0.0669 0.6802 0.1141
-6.500 -0.3027 0.01264 0.00528 -0.0651 0.6723 0.1327
-6.250 -0.2824 0.01242 0.00513 -0.0636 0.6646 0.1507
-6.000 -0.2616 0.01229 0.00499 -0.0621 0.6568 0.1642
-5.750 -0.2411 0.01215 0.00486 -0.0606 0.6500 0.1747
-5.500 -0.2196 0.01202 0.00473 -0.0593 0.6428 0.1831
-5.250 -0.1986 0.01192 0.00460 -0.0578 0.6356 0.1917
-5.000 -0.1768 0.01183 0.00449 -0.0565 0.6288 0.1984
-4.750 -0.1557 0.01169 0.00438 -0.0550 0.6215 0.2067
-4.500 -0.1334 0.01165 0.00427 -0.0538 0.6146 0.2128
-4.250 -0.1123 0.01151 0.00417 -0.0524 0.6083 0.2215
-4.000 -0.0898 0.01143 0.00408 -0.0512 0.6015 0.2300
-3.750 -0.0689 0.01132 0.00397 -0.0497 0.5946 0.2401
-3.250 -0.0253 0.01111 0.00381 -0.0471 0.5807 0.2619
-3.000 -0.0041 0.01104 0.00372 -0.0456 0.5738 0.2750
-2.750 0.0179 0.01093 0.00366 -0.0443 0.5673 0.2903
-2.500 0.0393 0.01082 0.00358 -0.0429 0.5601 0.3073
-2.250 0.0596 0.01073 0.00351 -0.0414 0.5532 0.3267
-2.000 0.0801 0.01055 0.00345 -0.0398 0.5462 0.3521
-1.750 0.0992 0.01039 0.00339 -0.0380 0.5390 0.3826
-1.500 0.1167 0.01025 0.00335 -0.0358 0.5326 0.4225
-1.250 0.1329 0.01003 0.00333 -0.0334 0.5261 0.4727
-1.000 0.1473 0.00985 0.00329 -0.0305 0.5196 0.5176
-0.750 0.1592 0.00970 0.00327 -0.0271 0.5133 0.5642
-0.500 0.1693 0.00947 0.00327 -0.0232 0.5074 0.6195
-0.250 0.1785 0.00925 0.00327 -0.0191 0.5014 0.6820
0.000 0.2195 0.00902 0.00340 -0.0218 0.4946 0.7770
0.250 0.3453 0.00981 0.00437 -0.0419 0.4841 0.8482
0.500 0.3808 0.01023 0.00472 -0.0431 0.4777 0.8670
0.750 0.4058 0.01049 0.00497 -0.0422 0.4726 0.8817
1.000 0.4252 0.01072 0.00518 -0.0401 0.4674 0.8948
1.250 0.4577 0.01111 0.00550 -0.0408 0.4616 0.9020
1.500 0.4812 0.01142 0.00575 -0.0396 0.4565 0.9110
1.750 0.5213 0.01174 0.00606 -0.0419 0.4514 0.9149
2.000 0.5378 0.01199 0.00628 -0.0394 0.4468 0.9248
2.250 0.5837 0.01240 0.00660 -0.0429 0.4411 0.9273
2.500 0.6275 0.01276 0.00694 -0.0460 0.4359 0.9313
2.750 0.6522 0.01307 0.00725 -0.0452 0.4308 0.9401
3.000 0.6967 0.01332 0.00742 -0.0485 0.4249 0.9421
3.250 0.7394 0.01360 0.00764 -0.0516 0.4193 0.9454
3.500 0.7625 0.01390 0.00797 -0.0505 0.4151 0.9538
3.750 0.8108 0.01399 0.00803 -0.0547 0.4102 0.9558
4.000 0.8540 0.01414 0.00812 -0.0579 0.4056 0.9590
4.250 0.8852 0.01437 0.00831 -0.0588 0.4012 0.9639
4.500 0.9133 0.01447 0.00845 -0.0589 0.3977 0.9684
4.750 0.9511 0.01444 0.00842 -0.0611 0.3931 0.9705
5.000 0.9862 0.01451 0.00845 -0.0628 0.3887 0.9738
5.250 1.0151 0.01486 0.00875 -0.0632 0.3836 0.9807
5.500 1.0613 0.01460 0.00854 -0.0672 0.3795 0.9837
5.750 1.0986 0.01455 0.00850 -0.0694 0.3754 0.9876
6.000 1.1332 0.01464 0.00856 -0.0711 0.3708 0.9929
6.250 1.1715 0.01454 0.00840 -0.0736 0.3661 0.9961
6.500 1.2139 0.01428 0.00821 -0.0769 0.3620 1.0000
6.750 1.2316 0.01440 0.00836 -0.0751 0.3584 1.0000
7.000 1.2482 0.01456 0.00852 -0.0732 0.3547 1.0000
7.250 1.2636 0.01477 0.00871 -0.0710 0.3511 1.0000
7.500 1.2791 0.01499 0.00893 -0.0689 0.3475 1.0000
7.750 1.2952 0.01511 0.00911 -0.0668 0.3435 1.0000
8.000 1.3103 0.01528 0.00930 -0.0646 0.3399 1.0000
8.250 1.3233 0.01549 0.00951 -0.0620 0.3360 1.0000
8.500 1.3344 0.01577 0.00977 -0.0591 0.3325 1.0000
8.750 1.3468 0.01598 0.01002 -0.0563 0.3295 1.0000
9.000 1.3553 0.01613 0.01024 -0.0528 0.3260 1.0000
9.250 1.3594 0.01632 0.01046 -0.0485 0.3222 1.0000
9.500 1.3633 0.01657 0.01072 -0.0443 0.3186 1.0000
9.750 1.3656 0.01694 0.01106 -0.0399 0.3148 1.0000
10.000 1.3735 0.01719 0.01139 -0.0365 0.3115 1.0000
10.250 1.3811 0.01748 0.01174 -0.0332 0.3078 1.0000
10.500 1.3860 0.01788 0.01215 -0.0296 0.3035 1.0000
10.750 1.3884 0.01841 0.01268 -0.0258 0.2993 1.0000
11.000 1.3951 0.01889 0.01320 -0.0227 0.2958 1.0000
11.250 1.4027 0.01936 0.01374 -0.0199 0.2915 1.0000
11.500 1.4068 0.02000 0.01439 -0.0168 0.2866 1.0000
11.750 1.4094 0.02078 0.01517 -0.0136 0.2825 1.0000
12.000 1.4166 0.02144 0.01589 -0.0111 0.2784 1.0000
12.250 1.4230 0.02218 0.01668 -0.0087 0.2737 1.0000
12.500 1.4266 0.02309 0.01761 -0.0060 0.2691 1.0000
12.750 1.4287 0.02415 0.01868 -0.0034 0.2643 1.0000
13.000 1.4357 0.02501 0.01961 -0.0014 0.2594 1.0000
13.250 1.4371 0.02623 0.02085 0.0010 0.2535 1.0000
13.500 1.4374 0.02760 0.02224 0.0033 0.2465 1.0000
13.750 1.4398 0.02891 0.02358 0.0053 0.2404 1.0000
14.000 1.4348 0.03078 0.02544 0.0077 0.2316 1.0000
14.250 1.4342 0.03244 0.02714 0.0095 0.2241 1.0000
14.500 1.4270 0.03468 0.02937 0.0116 0.2140 1.0000
14.750 1.4163 0.03732 0.03200 0.0135 0.2041 1.0000
15.000 1.4079 0.03992 0.03460 0.0152 0.1927 1.0000
15.250 1.3946 0.04306 0.03772 0.0167 0.1803 1.0000
15.500 1.3761 0.04681 0.04145 0.0182 0.1673 1.0000
15.750 1.3598 0.05054 0.04516 0.0193 0.1582 1.0000
16.000 1.3441 0.05432 0.04894 0.0202 0.1512 1.0000
16.250 1.3324 0.05780 0.05244 0.0209 0.1457 1.0000
16.500 1.3201 0.06145 0.05610 0.0215 0.1410 1.0000
16.750 1.3097 0.06496 0.05964 0.0219 0.1381 1.0000
17.000 1.3046 0.06797 0.06270 0.0222 0.1350 1.0000
17.250 1.2986 0.07110 0.06587 0.0224 0.1320 1.0000
17.500 1.2914 0.07441 0.06921 0.0226 0.1295 1.0000
17.750 1.2828 0.07792 0.07272 0.0226 0.1268 1.0000
18.000 1.2815 0.08057 0.07542 0.0227 0.1248 1.0000
18.250 1.2810 0.08324 0.07817 0.0227 0.1226 1.0000
18.500 1.2782 0.08618 0.08116 0.0226 0.1203 1.0000
18.750 1.2732 0.08939 0.08438 0.0224 0.1176 1.0000
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