GOE 683 AIRFOIL (goe683-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 683 AIRFOIL (goe683-il) Reynolds number: 500,000 Max Cl/Cd: 70.85 at α=8.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe683-il-500000-n5.txt Download as CSV file: xf-goe683-il-500000-n5.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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9573 0.09230 0.08799 -0.0630 1.0000 0.0389
-19.500 -0.9678 0.08755 0.08319 -0.0654 1.0000 0.0393
-19.250 -0.9785 0.08287 0.07845 -0.0677 1.0000 0.0395
-19.000 -0.9904 0.07800 0.07352 -0.0701 1.0000 0.0399
-18.750 -1.0022 0.07321 0.06864 -0.0724 1.0000 0.0402
-18.500 -1.0134 0.06860 0.06395 -0.0746 1.0000 0.0404
-18.250 -1.0237 0.06416 0.05942 -0.0766 1.0000 0.0408
-18.000 -1.0329 0.05996 0.05512 -0.0785 1.0000 0.0411
-17.750 -1.0397 0.05610 0.05117 -0.0801 1.0000 0.0415
-17.500 -1.0449 0.05254 0.04751 -0.0815 1.0000 0.0420
-17.250 -1.0510 0.04904 0.04391 -0.0826 1.0000 0.0421
-17.000 -1.0531 0.04606 0.04083 -0.0835 1.0000 0.0426
-16.750 -1.0543 0.04332 0.03799 -0.0840 1.0000 0.0430
-16.500 -1.0548 0.04080 0.03538 -0.0843 1.0000 0.0434
-16.250 -1.0541 0.03854 0.03302 -0.0842 1.0000 0.0437
-16.000 -1.0550 0.03630 0.03072 -0.0838 1.0000 0.0441
-15.750 -1.0551 0.03431 0.02868 -0.0830 1.0000 0.0445
-15.500 -1.0523 0.03269 0.02702 -0.0819 1.0000 0.0449
-15.250 -1.0492 0.03122 0.02549 -0.0806 1.0000 0.0453
-15.000 -1.0447 0.02995 0.02418 -0.0790 1.0000 0.0458
-14.750 -1.0396 0.02883 0.02300 -0.0772 1.0000 0.0463
-14.500 -1.0332 0.02786 0.02198 -0.0752 1.0000 0.0470
-14.250 -1.0272 0.02694 0.02101 -0.0730 1.0000 0.0475
-13.750 -0.9951 0.02499 0.01893 -0.0717 0.9882 0.0488
-13.500 -0.9759 0.02400 0.01790 -0.0716 0.9644 0.0494
-13.250 -0.9343 0.02299 0.01685 -0.0759 0.9382 0.0503
-13.000 -0.8810 0.02206 0.01586 -0.0824 0.9196 0.0515
-12.750 -0.8217 0.02123 0.01491 -0.0899 0.9025 0.0529
-12.500 -0.7647 0.02051 0.01404 -0.0969 0.8811 0.0542
-12.250 -0.7256 0.01990 0.01328 -0.1003 0.8582 0.0554
-11.750 -0.6797 0.01897 0.01215 -0.1003 0.8209 0.0572
-11.500 -0.6610 0.01860 0.01169 -0.0991 0.8055 0.0582
-11.250 -0.6436 0.01826 0.01124 -0.0976 0.7900 0.0590
-11.000 -0.6267 0.01794 0.01081 -0.0960 0.7756 0.0599
-10.750 -0.6099 0.01765 0.01041 -0.0942 0.7614 0.0608
-10.500 -0.5946 0.01728 0.00998 -0.0922 0.7487 0.0617
-10.250 -0.5800 0.01693 0.00956 -0.0901 0.7368 0.0626
-10.000 -0.5636 0.01663 0.00921 -0.0881 0.7249 0.0638
-9.750 -0.5467 0.01636 0.00887 -0.0863 0.7135 0.0648
-9.500 -0.5297 0.01611 0.00854 -0.0843 0.7019 0.0658
-9.250 -0.5118 0.01588 0.00824 -0.0825 0.6924 0.0670
-9.000 -0.4941 0.01566 0.00794 -0.0807 0.6821 0.0678
-8.750 -0.4776 0.01536 0.00760 -0.0786 0.6735 0.0691
-8.500 -0.4608 0.01509 0.00728 -0.0766 0.6634 0.0705
-8.250 -0.4428 0.01485 0.00700 -0.0748 0.6556 0.0717
-8.000 -0.4241 0.01463 0.00673 -0.0730 0.6479 0.0730
-7.750 -0.4054 0.01445 0.00648 -0.0712 0.6407 0.0745
-7.500 -0.3853 0.01427 0.00625 -0.0697 0.6339 0.0756
-7.250 -0.3669 0.01402 0.00597 -0.0679 0.6266 0.0775
-7.000 -0.3483 0.01381 0.00572 -0.0661 0.6192 0.0793
-6.750 -0.3281 0.01360 0.00549 -0.0646 0.6133 0.0811
-6.500 -0.3077 0.01343 0.00528 -0.0630 0.6069 0.0834
-6.250 -0.2880 0.01325 0.00507 -0.0614 0.6008 0.0862
-6.000 -0.2677 0.01303 0.00486 -0.0599 0.5950 0.0903
-5.750 -0.2477 0.01280 0.00466 -0.0583 0.5884 0.0974
-5.500 -0.2291 0.01252 0.00448 -0.0566 0.5819 0.1203
-5.250 -0.2079 0.01235 0.00436 -0.0552 0.5759 0.1377
-5.000 -0.1864 0.01221 0.00424 -0.0539 0.5698 0.1490
-4.750 -0.1649 0.01211 0.00412 -0.0525 0.5635 0.1553
-4.500 -0.1430 0.01200 0.00402 -0.0512 0.5577 0.1625
-4.250 -0.1208 0.01190 0.00391 -0.0500 0.5504 0.1698
-4.000 -0.0995 0.01181 0.00381 -0.0486 0.5435 0.1772
-3.750 -0.0771 0.01174 0.00373 -0.0474 0.5372 0.1830
-3.500 -0.0551 0.01164 0.00364 -0.0462 0.5306 0.1897
-3.250 -0.0335 0.01159 0.00356 -0.0448 0.5239 0.1960
-3.000 -0.0111 0.01151 0.00349 -0.0436 0.5174 0.2032
-2.750 0.0107 0.01144 0.00343 -0.0423 0.5101 0.2128
-2.500 0.0318 0.01140 0.00337 -0.0408 0.5033 0.2216
-2.250 0.0542 0.01132 0.00332 -0.0397 0.4965 0.2326
-2.000 0.0756 0.01125 0.00328 -0.0383 0.4899 0.2459
-1.750 0.0968 0.01122 0.00325 -0.0369 0.4839 0.2585
-1.500 0.1190 0.01116 0.00322 -0.0356 0.4778 0.2730
-1.250 0.1402 0.01110 0.00320 -0.0342 0.4713 0.2875
-1.000 0.1609 0.01108 0.00318 -0.0327 0.4653 0.3019
-0.750 0.1827 0.01101 0.00317 -0.0314 0.4599 0.3198
-0.500 0.2034 0.01093 0.00316 -0.0299 0.4546 0.3438
-0.250 0.2228 0.01087 0.00317 -0.0282 0.4491 0.3711
0.000 0.2416 0.01072 0.00318 -0.0263 0.4447 0.4155
0.250 0.2593 0.01057 0.00319 -0.0242 0.4398 0.4611
0.500 0.2754 0.01046 0.00321 -0.0218 0.4350 0.5043
0.750 0.2890 0.01035 0.00324 -0.0188 0.4309 0.5490
1.000 0.3020 0.01023 0.00328 -0.0156 0.4273 0.5930
1.250 0.3142 0.01009 0.00331 -0.0122 0.4237 0.6394
1.500 0.3255 0.00995 0.00334 -0.0086 0.4193 0.6880
1.750 0.3466 0.00975 0.00341 -0.0072 0.4151 0.7576
2.000 0.5048 0.01050 0.00444 -0.0347 0.4056 0.8548
2.250 0.5415 0.01086 0.00479 -0.0363 0.3992 0.8755
2.500 0.5673 0.01116 0.00506 -0.0357 0.3947 0.8892
2.750 0.5899 0.01140 0.00528 -0.0344 0.3912 0.9001
3.000 0.6072 0.01158 0.00546 -0.0321 0.3876 0.9116
3.250 0.6382 0.01190 0.00576 -0.0326 0.3828 0.9190
3.500 0.6571 0.01214 0.00597 -0.0306 0.3787 0.9270
3.750 0.6919 0.01245 0.00624 -0.0321 0.3740 0.9304
4.000 0.7195 0.01266 0.00646 -0.0320 0.3709 0.9354
4.250 0.7380 0.01285 0.00665 -0.0300 0.3676 0.9412
4.500 0.7750 0.01310 0.00688 -0.0320 0.3629 0.9433
4.750 0.8048 0.01334 0.00708 -0.0325 0.3583 0.9459
5.000 0.8309 0.01358 0.00731 -0.0322 0.3549 0.9506
5.250 0.8555 0.01381 0.00755 -0.0316 0.3514 0.9554
5.500 0.8924 0.01400 0.00774 -0.0336 0.3470 0.9571
5.750 0.9237 0.01420 0.00792 -0.0346 0.3430 0.9593
6.000 0.9501 0.01443 0.00813 -0.0345 0.3385 0.9625
6.250 0.9605 0.01467 0.00840 -0.0310 0.3358 0.9677
6.500 0.9896 0.01478 0.00851 -0.0316 0.3311 0.9686
6.750 1.0145 0.01493 0.00864 -0.0313 0.3259 0.9698
7.000 1.0354 0.01509 0.00879 -0.0303 0.3219 0.9712
7.250 1.0570 0.01520 0.00893 -0.0293 0.3183 0.9728
7.500 1.0766 0.01537 0.00911 -0.0280 0.3140 0.9751
7.750 1.0892 0.01559 0.00934 -0.0253 0.3102 0.9778
8.000 1.0963 0.01590 0.00964 -0.0216 0.3066 0.9806
8.250 1.1204 0.01604 0.00980 -0.0213 0.3033 0.9814
8.500 1.1447 0.01621 0.01000 -0.0212 0.2993 0.9825
8.750 1.1654 0.01645 0.01026 -0.0204 0.2950 0.9838
9.000 1.1826 0.01677 0.01057 -0.0190 0.2909 0.9853
9.250 1.2001 0.01707 0.01090 -0.0177 0.2865 0.9867
9.500 1.2167 0.01741 0.01126 -0.0163 0.2819 0.9882
9.750 1.2279 0.01796 0.01180 -0.0142 0.2748 0.9902
10.000 1.2412 0.01848 0.01234 -0.0124 0.2705 0.9920
10.250 1.2587 0.01892 0.01280 -0.0115 0.2653 0.9929
10.500 1.2742 0.01951 0.01340 -0.0106 0.2596 0.9940
10.750 1.2897 0.02013 0.01403 -0.0097 0.2546 0.9951
11.000 1.3057 0.02073 0.01467 -0.0089 0.2495 0.9962
11.250 1.3174 0.02161 0.01556 -0.0078 0.2430 0.9974
11.500 1.3318 0.02248 0.01644 -0.0072 0.2359 0.9986
11.750 1.3442 0.02357 0.01752 -0.0066 0.2280 0.9996
12.000 1.3503 0.02472 0.01869 -0.0049 0.2205 1.0000
12.250 1.3506 0.02601 0.01998 -0.0023 0.2132 1.0000
12.500 1.3499 0.02744 0.02143 0.0002 0.2056 1.0000
12.750 1.3468 0.02912 0.02309 0.0026 0.1968 1.0000
13.000 1.3433 0.03091 0.02489 0.0049 0.1867 1.0000
13.250 1.3342 0.03322 0.02717 0.0073 0.1740 1.0000
13.500 1.3236 0.03577 0.02970 0.0095 0.1615 1.0000
13.750 1.3093 0.03876 0.03265 0.0116 0.1491 1.0000
14.000 1.2971 0.04174 0.03563 0.0134 0.1406 1.0000
14.250 1.2880 0.04459 0.03849 0.0148 0.1346 1.0000
14.500 1.2814 0.04729 0.04123 0.0160 0.1311 1.0000
14.750 1.2762 0.04997 0.04395 0.0170 0.1278 1.0000
15.000 1.2706 0.05276 0.04678 0.0178 0.1247 1.0000
15.250 1.2645 0.05565 0.04972 0.0186 0.1222 1.0000
15.500 1.2575 0.05872 0.05282 0.0192 0.1196 1.0000
15.750 1.2525 0.06166 0.05581 0.0197 0.1174 1.0000
16.000 1.2509 0.06428 0.05851 0.0201 0.1157 1.0000
16.250 1.2488 0.06697 0.06125 0.0205 0.1139 1.0000
16.500 1.2427 0.07016 0.06448 0.0207 0.1113 1.0000
16.750 1.2374 0.07331 0.06767 0.0209 0.1094 1.0000
17.000 1.2336 0.07633 0.07073 0.0210 0.1080 1.0000
17.250 1.2276 0.07964 0.07409 0.0210 0.1063 1.0000
17.500 1.2303 0.08192 0.07644 0.0211 0.1051 1.0000
17.750 1.2307 0.08452 0.07911 0.0210 0.1034 1.0000
18.000 1.2304 0.08722 0.08186 0.0210 0.1017 1.0000
18.250 1.2295 0.09000 0.08469 0.0208 0.0999 1.0000
18.500 1.2273 0.09298 0.08772 0.0206 0.0985 1.0000
18.750 1.2254 0.09592 0.09069 0.0203 0.0971 1.0000
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