GOE 685 AIRFOIL (goe685-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 685 AIRFOIL (goe685-il) Reynolds number: 1,000,000 Max Cl/Cd: 96.32 at α=7° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe685-il-1000000-n5.txt Download as CSV file: xf-goe685-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 685 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
------ -------- --------- --------- -------- -------- --------
-19.250 -0.7735 0.14032 0.13797 -0.0295 1.0000 0.0185
-19.000 -0.7798 0.13522 0.13285 -0.0323 1.0000 0.0189
-18.750 -0.7871 0.12997 0.12757 -0.0352 1.0000 0.0192
-18.500 -0.7952 0.12463 0.12218 -0.0381 1.0000 0.0195
-18.250 -0.8023 0.11960 0.11711 -0.0409 1.0000 0.0197
-18.000 -0.8089 0.11471 0.11217 -0.0435 1.0000 0.0200
-17.750 -0.8173 0.10956 0.10697 -0.0464 1.0000 0.0202
-17.500 -0.8230 0.10501 0.10236 -0.0489 1.0000 0.0204
-17.250 -0.8313 0.10000 0.09730 -0.0516 1.0000 0.0207
-17.000 -0.8362 0.09572 0.09297 -0.0540 1.0000 0.0209
-16.750 -0.8448 0.09084 0.08803 -0.0567 1.0000 0.0211
-16.500 -0.8505 0.08654 0.08367 -0.0591 1.0000 0.0213
-16.250 -0.8579 0.08204 0.07912 -0.0616 1.0000 0.0214
-16.000 -0.8648 0.07765 0.07466 -0.0641 1.0000 0.0216
-15.750 -0.8737 0.07309 0.07005 -0.0666 1.0000 0.0218
-15.500 -0.8819 0.06878 0.06567 -0.0691 1.0000 0.0219
-15.250 -0.8933 0.06412 0.06095 -0.0718 1.0000 0.0220
-15.000 -0.9095 0.05920 0.05597 -0.0746 1.0000 0.0220
-14.750 -0.9336 0.05366 0.05037 -0.0779 1.0000 0.0220
-14.500 -0.9756 0.04664 0.04327 -0.0818 1.0000 0.0220
-14.250 -1.0624 0.02934 0.02564 -0.0991 0.9922 0.0217
-14.000 -1.0396 0.02643 0.02256 -0.1029 0.9877 0.0219
-13.750 -1.0159 0.02418 0.02019 -0.1060 0.9836 0.0223
-13.500 -0.9907 0.02260 0.01851 -0.1080 0.9794 0.0227
-13.250 -0.9628 0.02143 0.01727 -0.1098 0.9754 0.0230
-13.000 -0.9330 0.02049 0.01627 -0.1116 0.9720 0.0235
-12.750 -0.9034 0.01969 0.01540 -0.1130 0.9688 0.0239
-12.500 -0.8765 0.01892 0.01456 -0.1138 0.9635 0.0242
-12.250 -0.8477 0.01826 0.01383 -0.1148 0.9588 0.0246
-12.000 -0.8202 0.01763 0.01313 -0.1154 0.9538 0.0250
-11.750 -0.7952 0.01704 0.01246 -0.1154 0.9474 0.0253
-11.500 -0.7692 0.01650 0.01184 -0.1155 0.9416 0.0256
-11.250 -0.7443 0.01606 0.01132 -0.1153 0.9358 0.0259
-11.000 -0.7194 0.01563 0.01082 -0.1150 0.9297 0.0261
-10.500 -0.6726 0.01440 0.00944 -0.1142 0.9180 0.0270
-10.250 -0.6482 0.01393 0.00891 -0.1138 0.9121 0.0274
-10.000 -0.6229 0.01353 0.00844 -0.1134 0.9066 0.0278
-9.750 -0.5976 0.01316 0.00803 -0.1131 0.9011 0.0282
-9.500 -0.5721 0.01281 0.00762 -0.1127 0.8951 0.0286
-9.250 -0.5463 0.01248 0.00722 -0.1123 0.8890 0.0290
-9.000 -0.5205 0.01216 0.00684 -0.1119 0.8817 0.0294
-8.750 -0.4947 0.01187 0.00647 -0.1115 0.8726 0.0298
-8.500 -0.4685 0.01159 0.00613 -0.1111 0.8633 0.0301
-8.250 -0.4425 0.01134 0.00580 -0.1107 0.8524 0.0304
-8.000 -0.4164 0.01109 0.00547 -0.1103 0.8397 0.0308
-7.750 -0.3908 0.01078 0.00509 -0.1098 0.8244 0.0316
-7.500 -0.3652 0.01055 0.00477 -0.1092 0.8052 0.0324
-7.250 -0.3396 0.01037 0.00448 -0.1087 0.7843 0.0331
-7.000 -0.3136 0.01020 0.00422 -0.1082 0.7661 0.0339
-6.750 -0.2873 0.01005 0.00398 -0.1077 0.7507 0.0346
-6.500 -0.2606 0.00991 0.00376 -0.1073 0.7377 0.0354
-6.250 -0.2338 0.00975 0.00354 -0.1070 0.7261 0.0365
-6.000 -0.2071 0.00959 0.00332 -0.1067 0.7149 0.0383
-5.750 -0.1801 0.00944 0.00313 -0.1063 0.7043 0.0405
-5.500 -0.1529 0.00928 0.00293 -0.1061 0.6957 0.0438
-5.250 -0.1259 0.00908 0.00273 -0.1058 0.6870 0.0504
-5.000 -0.0990 0.00884 0.00252 -0.1055 0.6790 0.0634
-4.750 -0.0723 0.00859 0.00230 -0.1052 0.6696 0.0807
-4.500 -0.0455 0.00836 0.00212 -0.1050 0.6606 0.0998
-4.250 -0.0184 0.00821 0.00200 -0.1047 0.6511 0.1171
-4.000 0.0093 0.00811 0.00191 -0.1045 0.6425 0.1272
-3.750 0.0366 0.00809 0.00184 -0.1042 0.6296 0.1340
-3.250 0.0910 0.00803 0.00170 -0.1036 0.5994 0.1468
-3.000 0.1184 0.00801 0.00165 -0.1033 0.5861 0.1533
-2.750 0.1456 0.00799 0.00160 -0.1030 0.5721 0.1603
-2.500 0.1728 0.00802 0.00156 -0.1027 0.5555 0.1654
-2.250 0.1995 0.00804 0.00153 -0.1023 0.5358 0.1727
-2.000 0.2262 0.00809 0.00151 -0.1019 0.5161 0.1791
-1.750 0.2529 0.00813 0.00150 -0.1016 0.4978 0.1859
-1.500 0.2799 0.00818 0.00150 -0.1012 0.4818 0.1926
-1.250 0.3070 0.00821 0.00150 -0.1009 0.4686 0.1998
-1.000 0.3341 0.00826 0.00151 -0.1006 0.4571 0.2072
-0.750 0.3612 0.00831 0.00153 -0.1003 0.4458 0.2136
-0.500 0.3885 0.00835 0.00155 -0.1000 0.4350 0.2206
-0.250 0.4155 0.00843 0.00158 -0.0997 0.4241 0.2262
0.000 0.4427 0.00847 0.00162 -0.0994 0.4152 0.2323
0.250 0.4701 0.00852 0.00165 -0.0991 0.4090 0.2385
0.500 0.4977 0.00856 0.00168 -0.0989 0.4032 0.2430
0.750 0.5249 0.00861 0.00173 -0.0986 0.3971 0.2488
1.000 0.5522 0.00866 0.00178 -0.0984 0.3915 0.2544
1.250 0.5797 0.00871 0.00182 -0.0981 0.3861 0.2593
1.500 0.6068 0.00877 0.00188 -0.0978 0.3796 0.2650
1.750 0.6339 0.00884 0.00195 -0.0975 0.3741 0.2699
2.000 0.6609 0.00891 0.00201 -0.0972 0.3656 0.2742
2.250 0.6876 0.00901 0.00208 -0.0969 0.3584 0.2778
2.500 0.7148 0.00906 0.00215 -0.0966 0.3529 0.2827
2.750 0.7414 0.00916 0.00223 -0.0962 0.3451 0.2877
3.000 0.7678 0.00927 0.00232 -0.0958 0.3349 0.2924
3.250 0.7938 0.00940 0.00242 -0.0954 0.3246 0.2974
3.500 0.8201 0.00950 0.00252 -0.0950 0.3149 0.3025
3.750 0.8460 0.00964 0.00263 -0.0945 0.3057 0.3070
4.250 0.8962 0.01000 0.00292 -0.0933 0.2775 0.3202
4.500 0.9178 0.01041 0.00317 -0.0922 0.2409 0.3279
4.750 0.9337 0.01122 0.00366 -0.0902 0.1784 0.3351
5.000 0.9575 0.01146 0.00387 -0.0894 0.1685 0.3428
5.250 0.9812 0.01170 0.00410 -0.0886 0.1598 0.3510
5.500 1.0061 0.01184 0.00427 -0.0880 0.1568 0.3602
5.750 1.0304 0.01201 0.00447 -0.0872 0.1526 0.3711
6.000 1.0537 0.01222 0.00469 -0.0864 0.1470 0.3861
6.250 1.0776 0.01237 0.00490 -0.0857 0.1434 0.4083
6.500 1.1017 0.01246 0.00510 -0.0849 0.1410 0.4455
7.000 1.1578 0.01202 0.00576 -0.0856 0.1280 1.0000
7.250 1.1734 0.01268 0.00619 -0.0835 0.0882 1.0000
7.500 1.1905 0.01322 0.00666 -0.0817 0.0745 1.0000
7.750 1.2098 0.01360 0.00702 -0.0801 0.0688 1.0000
8.000 1.2288 0.01394 0.00736 -0.0786 0.0648 1.0000
8.250 1.2464 0.01426 0.00768 -0.0767 0.0606 1.0000
8.500 1.2625 0.01464 0.00805 -0.0746 0.0562 1.0000
8.750 1.2787 0.01503 0.00842 -0.0726 0.0509 1.0000
9.000 1.2940 0.01546 0.00883 -0.0705 0.0454 1.0000
9.250 1.3092 0.01592 0.00926 -0.0684 0.0410 1.0000
9.500 1.3246 0.01638 0.00971 -0.0665 0.0381 1.0000
9.750 1.3397 0.01686 0.01020 -0.0645 0.0357 1.0000
10.000 1.3550 0.01735 0.01070 -0.0627 0.0340 1.0000
10.250 1.3697 0.01789 0.01124 -0.0608 0.0326 1.0000
10.500 1.3833 0.01849 0.01185 -0.0589 0.0311 1.0000
10.750 1.3978 0.01906 0.01246 -0.0571 0.0302 1.0000
11.000 1.4120 0.01967 0.01309 -0.0554 0.0294 1.0000
11.250 1.4254 0.02034 0.01380 -0.0537 0.0286 1.0000
11.500 1.4379 0.02109 0.01457 -0.0519 0.0278 1.0000
11.750 1.4494 0.02193 0.01543 -0.0501 0.0268 1.0000
12.000 1.4599 0.02286 0.01640 -0.0484 0.0260 1.0000
12.250 1.4721 0.02372 0.01730 -0.0469 0.0256 1.0000
12.500 1.4838 0.02464 0.01827 -0.0454 0.0251 1.0000
12.750 1.4946 0.02566 0.01933 -0.0440 0.0245 1.0000
13.000 1.5046 0.02678 0.02050 -0.0426 0.0239 1.0000
13.250 1.5134 0.02804 0.02180 -0.0412 0.0233 1.0000
13.500 1.5213 0.02942 0.02322 -0.0400 0.0228 1.0000
13.750 1.5273 0.03102 0.02486 -0.0387 0.0220 1.0000
14.000 1.5344 0.03259 0.02649 -0.0377 0.0217 1.0000
14.250 1.5427 0.03411 0.02807 -0.0368 0.0212 1.0000
14.500 1.5488 0.03587 0.02990 -0.0360 0.0209 1.0000
14.750 1.5548 0.03770 0.03179 -0.0353 0.0205 1.0000
15.000 1.5599 0.03967 0.03381 -0.0346 0.0199 1.0000
15.250 1.5637 0.04183 0.03603 -0.0341 0.0194 1.0000
15.500 1.5664 0.04416 0.03842 -0.0336 0.0190 1.0000
15.750 1.5672 0.04677 0.04108 -0.0333 0.0186 1.0000
16.000 1.5674 0.04952 0.04390 -0.0331 0.0181 1.0000
16.250 1.5690 0.05217 0.04664 -0.0330 0.0178 1.0000
16.500 1.5692 0.05503 0.04958 -0.0330 0.0175 1.0000
16.750 1.5690 0.05801 0.05263 -0.0331 0.0171 1.0000
17.000 1.5674 0.06125 0.05595 -0.0334 0.0168 1.0000
17.250 1.5660 0.06453 0.05929 -0.0338 0.0162 1.0000
17.500 1.5625 0.06812 0.06296 -0.0343 0.0160 1.0000
17.750 1.5587 0.07182 0.06672 -0.0350 0.0155 1.0000
18.000 1.5538 0.07577 0.07074 -0.0358 0.0151 1.0000
18.250 1.5487 0.07980 0.07485 -0.0368 0.0149 1.0000
18.500 1.5438 0.08383 0.07898 -0.0378 0.0147 1.0000
18.750 1.5389 0.08793 0.08316 -0.0389 0.0144 1.0000
19.000 1.5336 0.09217 0.08749 -0.0402 0.0141 1.0000
19.250 1.5281 0.09650 0.09190 -0.0415 0.0138 1.0000
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