GOE 683 AIRFOIL (goe683-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 683 AIRFOIL (goe683-il) Reynolds number: 1,000,000 Max Cl/Cd: 98.24 at α=10° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe683-il-1000000.txt Download as CSV file: xf-goe683-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -1.1053 0.07278 0.06900 -0.0721 1.0000 0.0375
-19.500 -1.1189 0.06792 0.06404 -0.0743 1.0000 0.0378
-19.250 -1.1294 0.06347 0.05950 -0.0764 1.0000 0.0381
-19.000 -1.1406 0.05904 0.05498 -0.0783 1.0000 0.0384
-18.750 -1.1492 0.05501 0.05084 -0.0800 1.0000 0.0386
-18.500 -1.1573 0.05115 0.04688 -0.0815 1.0000 0.0388
-18.250 -1.1588 0.04809 0.04372 -0.0825 1.0000 0.0391
-18.000 -1.1683 0.04433 0.03987 -0.0836 1.0000 0.0395
-17.750 -1.1774 0.04081 0.03628 -0.0843 1.0000 0.0399
-17.500 -1.1822 0.03793 0.03333 -0.0845 1.0000 0.0402
-17.250 -1.1828 0.03561 0.03095 -0.0843 1.0000 0.0407
-17.000 -1.1816 0.03360 0.02888 -0.0838 1.0000 0.0410
-16.750 -1.1768 0.03201 0.02725 -0.0830 1.0000 0.0415
-16.500 -1.1727 0.03049 0.02567 -0.0820 1.0000 0.0419
-16.250 -1.1674 0.02917 0.02429 -0.0807 1.0000 0.0424
-16.000 -1.1618 0.02796 0.02303 -0.0791 1.0000 0.0428
-15.750 -1.1540 0.02696 0.02198 -0.0775 1.0000 0.0432
-15.500 -1.1465 0.02602 0.02097 -0.0757 1.0000 0.0437
-15.250 -1.1378 0.02520 0.02009 -0.0738 1.0000 0.0440
-15.000 -1.1395 0.02393 0.01879 -0.0707 1.0000 0.0447
-14.750 -1.1341 0.02308 0.01792 -0.0681 1.0000 0.0452
-14.500 -1.1267 0.02238 0.01720 -0.0655 1.0000 0.0458
-14.250 -1.1183 0.02178 0.01657 -0.0629 1.0000 0.0464
-14.000 -1.1098 0.02124 0.01601 -0.0602 1.0000 0.0469
-13.750 -1.0813 0.02073 0.01547 -0.0611 0.9990 0.0478
-13.500 -1.0448 0.02010 0.01480 -0.0637 0.9961 0.0486
-13.250 -1.0198 0.01953 0.01420 -0.0636 0.9818 0.0491
-13.000 -0.9947 0.01850 0.01314 -0.0644 0.9583 0.0503
-12.750 -0.9446 0.01782 0.01245 -0.0697 0.9402 0.0516
-12.500 -0.8845 0.01726 0.01182 -0.0769 0.9182 0.0529
-12.250 -0.8223 0.01684 0.01128 -0.0844 0.8949 0.0543
-12.000 -0.7700 0.01627 0.01057 -0.0903 0.8709 0.0556
-11.750 -0.7372 0.01583 0.01004 -0.0921 0.8485 0.0569
-11.500 -0.7104 0.01554 0.00967 -0.0924 0.8307 0.0580
-11.250 -0.6864 0.01530 0.00933 -0.0920 0.8148 0.0591
-11.000 -0.6652 0.01505 0.00903 -0.0910 0.8027 0.0599
-10.750 -0.6439 0.01484 0.00873 -0.0900 0.7897 0.0606
-10.500 -0.6265 0.01450 0.00832 -0.0883 0.7775 0.0618
-10.250 -0.6098 0.01415 0.00793 -0.0864 0.7655 0.0631
-10.000 -0.5909 0.01394 0.00765 -0.0848 0.7530 0.0643
-9.750 -0.5719 0.01370 0.00738 -0.0832 0.7416 0.0652
-9.500 -0.5526 0.01352 0.00713 -0.0816 0.7302 0.0662
-9.250 -0.5329 0.01334 0.00688 -0.0801 0.7181 0.0672
-9.000 -0.5126 0.01319 0.00666 -0.0786 0.7072 0.0680
-8.750 -0.4972 0.01285 0.00627 -0.0763 0.6959 0.0695
-8.500 -0.4787 0.01261 0.00600 -0.0745 0.6861 0.0711
-8.250 -0.4595 0.01242 0.00577 -0.0728 0.6765 0.0725
-8.000 -0.4396 0.01226 0.00555 -0.0712 0.6679 0.0736
-7.750 -0.4190 0.01211 0.00536 -0.0697 0.6592 0.0747
-7.500 -0.3994 0.01195 0.00513 -0.0680 0.6510 0.0762
-7.250 -0.3800 0.01168 0.00486 -0.0664 0.6439 0.0785
-7.000 -0.3598 0.01151 0.00466 -0.0648 0.6365 0.0803
-6.750 -0.3390 0.01136 0.00447 -0.0633 0.6300 0.0821
-6.500 -0.3174 0.01121 0.00429 -0.0620 0.6238 0.0841
-6.250 -0.2974 0.01100 0.00408 -0.0603 0.6170 0.0876
-6.000 -0.2771 0.01083 0.00389 -0.0588 0.6105 0.0918
-5.750 -0.2565 0.01057 0.00370 -0.0573 0.6046 0.1018
-5.500 -0.2377 0.01025 0.00353 -0.0555 0.5985 0.1348
-5.250 -0.2167 0.01014 0.00343 -0.0541 0.5919 0.1489
-5.000 -0.1940 0.00998 0.00333 -0.0530 0.5868 0.1592
-4.750 -0.1712 0.00989 0.00323 -0.0518 0.5807 0.1669
-4.500 -0.1496 0.00981 0.00315 -0.0504 0.5737 0.1747
-4.250 -0.1258 0.00974 0.00307 -0.0495 0.5676 0.1792
-4.000 -0.1031 0.00963 0.00298 -0.0483 0.5613 0.1873
-3.750 -0.0809 0.00958 0.00291 -0.0471 0.5544 0.1941
-3.500 -0.0576 0.00948 0.00284 -0.0460 0.5485 0.2022
-3.250 -0.0345 0.00941 0.00278 -0.0450 0.5414 0.2103
-3.000 -0.0128 0.00935 0.00271 -0.0436 0.5338 0.2206
-2.750 0.0109 0.00928 0.00266 -0.0426 0.5271 0.2306
-2.500 0.0332 0.00920 0.00261 -0.0414 0.5197 0.2442
-2.250 0.0554 0.00914 0.00257 -0.0402 0.5125 0.2575
-2.000 0.0785 0.00906 0.00253 -0.0391 0.5053 0.2734
-1.750 0.1003 0.00901 0.00250 -0.0378 0.4978 0.2903
-1.500 0.1229 0.00895 0.00247 -0.0366 0.4909 0.3075
-1.250 0.1451 0.00887 0.00244 -0.0354 0.4841 0.3277
-1.000 0.1657 0.00881 0.00243 -0.0338 0.4768 0.3518
-0.750 0.1877 0.00867 0.00241 -0.0326 0.4713 0.3867
-0.500 0.2078 0.00854 0.00240 -0.0310 0.4650 0.4301
-0.250 0.2258 0.00843 0.00241 -0.0289 0.4586 0.4753
0.000 0.2446 0.00828 0.00241 -0.0270 0.4541 0.5191
0.250 0.2605 0.00812 0.00242 -0.0244 0.4493 0.5664
0.500 0.2700 0.00795 0.00242 -0.0204 0.4444 0.6243
0.750 0.2762 0.00782 0.00244 -0.0157 0.4390 0.6785
1.000 0.2813 0.00756 0.00244 -0.0107 0.4361 0.7418
1.250 0.3859 0.00771 0.00303 -0.0271 0.4285 0.8729
1.500 0.4255 0.00806 0.00334 -0.0294 0.4215 0.8908
1.750 0.4610 0.00832 0.00360 -0.0308 0.4180 0.8997
2.000 0.4774 0.00842 0.00369 -0.0282 0.4137 0.9105
2.250 0.5080 0.00871 0.00394 -0.0286 0.4084 0.9147
2.500 0.5155 0.00886 0.00407 -0.0241 0.4042 0.9250
2.750 0.5534 0.00914 0.00433 -0.0261 0.3997 0.9266
3.000 0.5930 0.00943 0.00460 -0.0285 0.3959 0.9288
3.250 0.6297 0.00974 0.00487 -0.0302 0.3918 0.9320
3.500 0.6365 0.00990 0.00502 -0.0257 0.3883 0.9400
3.750 0.6840 0.01030 0.00537 -0.0297 0.3834 0.9412
4.000 0.7277 0.01053 0.00561 -0.0330 0.3799 0.9426
4.250 0.7676 0.01077 0.00583 -0.0355 0.3758 0.9442
4.500 0.8031 0.01101 0.00603 -0.0371 0.3713 0.9465
4.750 0.8107 0.01131 0.00631 -0.0328 0.3673 0.9541
5.000 0.8528 0.01146 0.00646 -0.0359 0.3639 0.9549
5.250 0.8924 0.01158 0.00657 -0.0384 0.3595 0.9558
5.500 0.9275 0.01173 0.00670 -0.0400 0.3545 0.9569
5.750 0.9628 0.01194 0.00687 -0.0417 0.3498 0.9586
6.000 0.9985 0.01209 0.00703 -0.0435 0.3465 0.9610
6.250 1.0120 0.01242 0.00737 -0.0405 0.3436 0.9678
6.500 1.0500 0.01246 0.00741 -0.0428 0.3391 0.9686
6.750 1.0843 0.01257 0.00749 -0.0444 0.3343 0.9696
7.000 1.1180 0.01268 0.00759 -0.0459 0.3300 0.9710
7.250 1.1507 0.01276 0.00768 -0.0471 0.3263 0.9728
7.500 1.1784 0.01291 0.00783 -0.0473 0.3221 0.9753
7.750 1.1846 0.01336 0.00827 -0.0430 0.3180 0.9806
8.000 1.2137 0.01335 0.00825 -0.0437 0.3124 0.9813
8.250 1.2440 0.01335 0.00826 -0.0445 0.3081 0.9822
8.500 1.2710 0.01342 0.00833 -0.0447 0.3035 0.9835
8.750 1.2913 0.01357 0.00845 -0.0436 0.2985 0.9852
9.000 1.3129 0.01365 0.00857 -0.0427 0.2949 0.9869
9.250 1.3314 0.01380 0.00873 -0.0412 0.2901 0.9890
9.500 1.3511 0.01414 0.00905 -0.0400 0.2852 0.9928
9.750 1.3786 0.01420 0.00911 -0.0405 0.2802 0.9941
10.000 1.4039 0.01429 0.00922 -0.0406 0.2748 0.9954
10.250 1.4258 0.01453 0.00943 -0.0402 0.2679 0.9975
10.750 1.4662 0.01502 0.00994 -0.0386 0.2563 1.0000
11.000 1.4679 0.01551 0.01043 -0.0344 0.2512 1.0000
11.250 1.4730 0.01597 0.01090 -0.0309 0.2458 1.0000
11.500 1.4755 0.01656 0.01150 -0.0272 0.2392 1.0000
11.750 1.4756 0.01732 0.01225 -0.0233 0.2321 1.0000
12.000 1.4782 0.01807 0.01300 -0.0200 0.2249 1.0000
12.250 1.4767 0.01907 0.01399 -0.0164 0.2166 1.0000
12.500 1.4738 0.02024 0.01513 -0.0128 0.2064 1.0000
12.750 1.4670 0.02172 0.01657 -0.0091 0.1926 1.0000
13.000 1.4652 0.02305 0.01789 -0.0062 0.1834 1.0000
13.250 1.4462 0.02550 0.02024 -0.0020 0.1633 1.0000
13.500 1.4287 0.02808 0.02275 0.0016 0.1473 1.0000
13.750 1.4147 0.03062 0.02526 0.0046 0.1371 1.0000
14.000 1.4094 0.03270 0.02736 0.0067 0.1324 1.0000
14.250 1.4067 0.03467 0.02936 0.0084 0.1296 1.0000
14.500 1.4003 0.03703 0.03174 0.0102 0.1257 1.0000
14.750 1.4007 0.03891 0.03368 0.0115 0.1238 1.0000
15.000 1.3974 0.04117 0.03598 0.0129 0.1213 1.0000
15.250 1.3955 0.04337 0.03823 0.0140 0.1201 1.0000
15.500 1.3883 0.04611 0.04101 0.0152 0.1174 1.0000
15.750 1.3846 0.04861 0.04356 0.0162 0.1161 1.0000
16.000 1.3800 0.05126 0.04625 0.0170 0.1139 1.0000
16.250 1.3798 0.05355 0.04861 0.0177 0.1131 1.0000
16.500 1.3799 0.05581 0.05093 0.0183 0.1115 1.0000
16.750 1.3780 0.05834 0.05352 0.0188 0.1104 1.0000
17.000 1.3737 0.06118 0.05641 0.0193 0.1088 1.0000
17.250 1.3691 0.06408 0.05936 0.0197 0.1073 1.0000
17.500 1.3602 0.06750 0.06282 0.0200 0.1054 1.0000
17.750 1.3511 0.07101 0.06639 0.0201 0.1037 1.0000
18.000 1.3528 0.07331 0.06875 0.0203 0.1029 1.0000
18.250 1.3540 0.07575 0.07125 0.0204 0.1016 1.0000
18.500 1.3543 0.07823 0.07379 0.0205 0.1000 1.0000
18.750 1.3498 0.08133 0.07694 0.0204 0.0983 1.0000
19.000 1.3463 0.08432 0.07996 0.0203 0.0965 1.0000
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