GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 703 AIRFOIL (goe703-il) Reynolds number: 1,000,000 Max Cl/Cd: 65.6 at α=8° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe703-il-1000000-n5.txt Download as CSV file: xf-goe703-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 703 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
------ -------- --------- --------- -------- -------- --------
-19.750 -1.0820 0.07641 0.07232 -0.0745 1.0000 0.0246
-19.500 -1.1005 0.07061 0.06639 -0.0771 1.0000 0.0247
-19.250 -1.1142 0.06556 0.06123 -0.0793 1.0000 0.0247
-19.000 -1.1278 0.06069 0.05625 -0.0813 1.0000 0.0247
-18.750 -1.1387 0.05638 0.05183 -0.0828 1.0000 0.0248
-18.500 -1.1471 0.05255 0.04790 -0.0838 1.0000 0.0248
-18.250 -1.1524 0.04926 0.04452 -0.0845 1.0000 0.0249
-18.000 -1.1554 0.04638 0.04156 -0.0847 1.0000 0.0251
-17.750 -1.1578 0.04374 0.03884 -0.0846 1.0000 0.0251
-17.500 -1.1584 0.04141 0.03643 -0.0842 1.0000 0.0252
-17.250 -1.1584 0.03926 0.03422 -0.0836 1.0000 0.0253
-17.000 -1.1560 0.03744 0.03233 -0.0827 1.0000 0.0254
-16.750 -1.1548 0.03564 0.03046 -0.0815 1.0000 0.0255
-16.500 -1.1522 0.03405 0.02881 -0.0802 1.0000 0.0256
-16.250 -1.1486 0.03262 0.02731 -0.0787 1.0000 0.0257
-16.000 -1.1438 0.03135 0.02599 -0.0770 1.0000 0.0258
-15.750 -1.1387 0.03017 0.02476 -0.0752 1.0000 0.0259
-15.500 -1.1340 0.02905 0.02358 -0.0732 1.0000 0.0259
-15.250 -1.1281 0.02805 0.02253 -0.0712 1.0000 0.0260
-15.000 -1.1054 0.02698 0.02141 -0.0722 0.9991 0.0261
-14.750 -1.0836 0.02579 0.02018 -0.0732 0.9976 0.0263
-14.500 -1.0642 0.02466 0.01901 -0.0736 0.9951 0.0266
-14.250 -1.0510 0.02372 0.01803 -0.0724 0.9902 0.0267
-14.000 -1.0340 0.02284 0.01712 -0.0718 0.9855 0.0269
-13.750 -1.0178 0.02205 0.01630 -0.0710 0.9780 0.0272
-13.500 -0.9985 0.02133 0.01555 -0.0705 0.9661 0.0274
-13.250 -0.9677 0.02055 0.01473 -0.0723 0.9538 0.0276
-13.000 -0.9264 0.01978 0.01393 -0.0762 0.9411 0.0279
-12.750 -0.8784 0.01907 0.01315 -0.0815 0.9245 0.0285
-12.500 -0.8311 0.01844 0.01242 -0.0865 0.9035 0.0288
-12.250 -0.7855 0.01791 0.01178 -0.0911 0.8822 0.0292
-12.000 -0.7473 0.01743 0.01120 -0.0942 0.8666 0.0295
-11.750 -0.7165 0.01703 0.01071 -0.0957 0.8514 0.0297
-11.250 -0.6679 0.01621 0.00975 -0.0958 0.8245 0.0305
-11.000 -0.6458 0.01585 0.00933 -0.0953 0.8136 0.0310
-10.750 -0.6242 0.01553 0.00897 -0.0947 0.8037 0.0314
-10.500 -0.6030 0.01523 0.00861 -0.0938 0.7937 0.0319
-10.250 -0.5823 0.01493 0.00827 -0.0929 0.7834 0.0324
-10.000 -0.5621 0.01467 0.00795 -0.0918 0.7727 0.0328
-9.750 -0.5420 0.01442 0.00765 -0.0906 0.7602 0.0332
-9.500 -0.5218 0.01419 0.00736 -0.0894 0.7484 0.0337
-9.250 -0.5026 0.01394 0.00706 -0.0880 0.7350 0.0346
-9.000 -0.4829 0.01371 0.00679 -0.0866 0.7211 0.0353
-8.750 -0.4639 0.01350 0.00652 -0.0851 0.7052 0.0363
-8.500 -0.4449 0.01333 0.00628 -0.0836 0.6891 0.0371
-8.250 -0.4257 0.01318 0.00605 -0.0820 0.6724 0.0381
-8.000 -0.4063 0.01298 0.00582 -0.0806 0.6598 0.0398
-7.750 -0.3866 0.01280 0.00560 -0.0791 0.6496 0.0416
-7.500 -0.3666 0.01263 0.00540 -0.0777 0.6400 0.0433
-7.250 -0.3472 0.01245 0.00519 -0.0761 0.6315 0.0459
-7.000 -0.3269 0.01229 0.00501 -0.0748 0.6237 0.0481
-6.750 -0.3076 0.01211 0.00482 -0.0732 0.6161 0.0515
-6.500 -0.2873 0.01193 0.00464 -0.0718 0.6105 0.0553
-6.250 -0.2670 0.01174 0.00446 -0.0703 0.6051 0.0604
-6.000 -0.2477 0.01154 0.00428 -0.0688 0.5993 0.0681
-5.500 -0.2102 0.01110 0.00394 -0.0653 0.5890 0.0932
-5.250 -0.1912 0.01088 0.00379 -0.0636 0.5842 0.1087
-5.000 -0.1715 0.01073 0.00366 -0.0620 0.5790 0.1195
-4.750 -0.1519 0.01060 0.00355 -0.0604 0.5739 0.1294
-4.500 -0.1313 0.01045 0.00344 -0.0590 0.5697 0.1389
-4.250 -0.1099 0.01034 0.00334 -0.0576 0.5656 0.1464
-4.000 -0.0898 0.01022 0.00325 -0.0561 0.5604 0.1554
-3.750 -0.0697 0.01014 0.00316 -0.0545 0.5552 0.1628
-3.500 -0.0496 0.01003 0.00308 -0.0529 0.5507 0.1725
-3.250 -0.0294 0.00990 0.00300 -0.0513 0.5462 0.1844
-3.000 -0.0099 0.00976 0.00292 -0.0496 0.5413 0.2006
-2.750 0.0089 0.00965 0.00285 -0.0478 0.5364 0.2177
-2.500 0.0276 0.00953 0.00278 -0.0459 0.5319 0.2356
-2.250 0.0472 0.00940 0.00272 -0.0442 0.5282 0.2537
-2.000 0.0662 0.00928 0.00266 -0.0423 0.5235 0.2721
-1.750 0.0855 0.00921 0.00261 -0.0405 0.5186 0.2857
-1.500 0.1039 0.00913 0.00257 -0.0385 0.5145 0.3009
-1.250 0.1228 0.00903 0.00252 -0.0366 0.5111 0.3195
-1.000 0.1407 0.00890 0.00247 -0.0345 0.5072 0.3429
-0.750 0.1556 0.00873 0.00241 -0.0318 0.5029 0.3767
-0.500 0.1647 0.00849 0.00235 -0.0279 0.4982 0.4314
-0.250 0.1718 0.00828 0.00230 -0.0236 0.4940 0.4840
0.000 0.1803 0.00806 0.00225 -0.0194 0.4910 0.5316
0.250 0.1833 0.00785 0.00222 -0.0141 0.4874 0.5807
0.500 0.1805 0.00767 0.00220 -0.0074 0.4834 0.6273
0.750 0.1753 0.00749 0.00218 -0.0001 0.4790 0.6751
1.000 0.1725 0.00731 0.00216 0.0067 0.4747 0.7225
1.250 0.1758 0.00716 0.00217 0.0122 0.4704 0.7667
1.500 0.1846 0.00708 0.00221 0.0164 0.4661 0.7986
1.750 0.1980 0.00710 0.00226 0.0197 0.4593 0.8193
2.000 0.2165 0.00713 0.00231 0.0218 0.4545 0.8332
2.250 0.2349 0.00717 0.00236 0.0239 0.4484 0.8451
2.500 0.2548 0.00726 0.00246 0.0257 0.4403 0.8580
2.750 0.2753 0.00733 0.00254 0.0273 0.4348 0.8688
3.000 0.2932 0.00741 0.00263 0.0295 0.4292 0.8805
3.250 0.3191 0.00754 0.00276 0.0299 0.4231 0.8892
3.500 0.3372 0.00763 0.00284 0.0320 0.4171 0.8962
3.750 0.3531 0.00772 0.00291 0.0345 0.4092 0.9019
4.000 0.3828 0.00790 0.00306 0.0340 0.4006 0.9058
4.250 0.4059 0.00802 0.00318 0.0349 0.3930 0.9106
4.500 0.4119 0.00813 0.00325 0.0396 0.3866 0.9176
5.000 0.4731 0.00854 0.00360 0.0379 0.3656 0.9239
5.250 0.4957 0.00873 0.00374 0.0387 0.3543 0.9267
5.500 0.5128 0.00892 0.00389 0.0407 0.3441 0.9307
5.750 0.5233 0.00905 0.00400 0.0442 0.3368 0.9353
6.000 0.5542 0.00928 0.00419 0.0431 0.3274 0.9367
6.250 0.5847 0.00951 0.00439 0.0421 0.3183 0.9380
6.500 0.6151 0.00976 0.00461 0.0411 0.3094 0.9395
6.750 0.6432 0.01004 0.00485 0.0405 0.2990 0.9412
7.000 0.6692 0.01031 0.00508 0.0404 0.2890 0.9433
7.250 0.6909 0.01060 0.00533 0.0411 0.2802 0.9459
7.500 0.6995 0.01080 0.00552 0.0447 0.2734 0.9511
7.750 0.7297 0.01116 0.00584 0.0434 0.2629 0.9521
8.000 0.7577 0.01155 0.00618 0.0426 0.2504 0.9531
8.250 0.7833 0.01196 0.00655 0.0422 0.2385 0.9544
8.500 0.8052 0.01247 0.00699 0.0424 0.2244 0.9560
8.750 0.8235 0.01309 0.00754 0.0431 0.2070 0.9581
9.000 0.8363 0.01389 0.00823 0.0446 0.1865 0.9611
9.250 0.8412 0.01454 0.00883 0.0479 0.1734 0.9661
9.500 0.8604 0.01536 0.00957 0.0480 0.1589 0.9670
9.750 0.8812 0.01604 0.01023 0.0479 0.1504 0.9680
10.000 0.9016 0.01676 0.01092 0.0478 0.1436 0.9691
10.250 0.9227 0.01746 0.01161 0.0477 0.1380 0.9702
10.500 0.9421 0.01822 0.01235 0.0477 0.1330 0.9715
10.750 0.9613 0.01892 0.01306 0.0478 0.1294 0.9730
11.000 0.9795 0.01963 0.01378 0.0481 0.1263 0.9747
11.250 0.9938 0.02043 0.01458 0.0490 0.1235 0.9771
11.500 1.0039 0.02126 0.01542 0.0507 0.1209 0.9800
11.750 1.0249 0.02207 0.01625 0.0501 0.1187 0.9807
12.000 1.0452 0.02292 0.01712 0.0496 0.1161 0.9814
12.250 1.0633 0.02389 0.01810 0.0493 0.1134 0.9822
12.500 1.0793 0.02500 0.01921 0.0491 0.1103 0.9832
12.750 1.0962 0.02603 0.02027 0.0488 0.1084 0.9841
13.000 1.1133 0.02703 0.02131 0.0486 0.1063 0.9852
13.250 1.1293 0.02813 0.02243 0.0484 0.1039 0.9864
13.500 1.1425 0.02946 0.02378 0.0484 0.1011 0.9878
13.750 1.1539 0.03089 0.02521 0.0485 0.0983 0.9892
14.000 1.1671 0.03211 0.02647 0.0486 0.0953 0.9904
14.250 1.1749 0.03373 0.02809 0.0490 0.0903 0.9916
14.500 1.1769 0.03593 0.03024 0.0495 0.0774 0.9927
14.750 1.1749 0.03880 0.03303 0.0494 0.0647 0.9938
15.000 1.1774 0.04133 0.03556 0.0490 0.0591 0.9948
15.250 1.1859 0.04328 0.03755 0.0486 0.0575 0.9957
15.500 1.1912 0.04555 0.03984 0.0482 0.0555 0.9965
15.750 1.1973 0.04774 0.04206 0.0478 0.0538 0.9972
16.000 1.2050 0.04985 0.04422 0.0473 0.0529 0.9978
16.250 1.2128 0.05192 0.04634 0.0468 0.0518 0.9983
16.500 1.2185 0.05429 0.04875 0.0462 0.0509 0.9988
16.750 1.2264 0.05649 0.05100 0.0454 0.0503 0.9992
17.000 1.2310 0.05909 0.05364 0.0446 0.0494 0.9996
17.250 1.2345 0.06177 0.05637 0.0439 0.0485 0.9999
17.500 1.2342 0.06427 0.05892 0.0440 0.0478 1.0000
17.750 1.2357 0.06640 0.06109 0.0445 0.0470 1.0000
18.000 1.2355 0.06875 0.06350 0.0449 0.0469 1.0000
18.250 1.2359 0.07106 0.06586 0.0452 0.0462 1.0000
18.500 1.2346 0.07362 0.06848 0.0454 0.0456 1.0000
18.750 1.2333 0.07619 0.07110 0.0455 0.0449 1.0000
19.000 1.2310 0.07894 0.07390 0.0456 0.0444 1.0000
19.250 1.2285 0.08175 0.07676 0.0455 0.0439 1.0000
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