GOE 702 AIRFOIL (goe702-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 702 AIRFOIL (goe702-il) Reynolds number: 1,000,000 Max Cl/Cd: 117.23 at α=7.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe702-il-1000000.txt Download as CSV file: xf-goe702-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 702 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
------ -------- --------- --------- -------- -------- --------
-18.000 -0.8446 0.10190 0.09935 -0.0387 1.0000 0.0335
-17.750 -0.8780 0.09315 0.09049 -0.0442 1.0000 0.0340
-17.500 -0.8966 0.08676 0.08403 -0.0483 1.0000 0.0342
-17.250 -0.9124 0.08092 0.07813 -0.0520 1.0000 0.0344
-17.000 -0.9292 0.07496 0.07211 -0.0560 1.0000 0.0346
-16.750 -0.9516 0.06854 0.06561 -0.0605 1.0000 0.0348
-16.500 -0.9780 0.06173 0.05871 -0.0654 1.0000 0.0349
-16.250 -1.0074 0.05456 0.05143 -0.0709 1.0000 0.0350
-16.000 -1.0264 0.04665 0.04338 -0.0796 0.9478 0.0351
-15.750 -1.0051 0.03809 0.03450 -0.0965 0.9068 0.0354
-15.500 -1.0399 0.03017 0.02621 -0.1036 0.8699 0.0354
-15.250 -1.0528 0.02801 0.02387 -0.1020 0.8507 0.0356
-15.000 -1.0587 0.02660 0.02233 -0.0992 0.8343 0.0358
-14.750 -1.0591 0.02558 0.02120 -0.0961 0.8189 0.0360
-14.500 -1.0557 0.02470 0.02019 -0.0933 0.8040 0.0363
-14.000 -1.0313 0.02312 0.01837 -0.0897 0.7763 0.0368
-13.750 -1.0156 0.02244 0.01757 -0.0883 0.7647 0.0371
-13.500 -0.9983 0.02180 0.01682 -0.0869 0.7545 0.0374
-13.250 -0.9786 0.02129 0.01620 -0.0858 0.7457 0.0376
-13.000 -0.9654 0.02024 0.01507 -0.0841 0.7378 0.0382
-12.750 -0.9474 0.01955 0.01430 -0.0828 0.7302 0.0387
-12.500 -0.9265 0.01898 0.01369 -0.0818 0.7242 0.0392
-12.250 -0.9045 0.01849 0.01314 -0.0809 0.7178 0.0396
-12.000 -0.8821 0.01805 0.01261 -0.0800 0.7107 0.0401
-11.750 -0.8589 0.01760 0.01211 -0.0792 0.7048 0.0406
-11.500 -0.8353 0.01717 0.01161 -0.0785 0.6989 0.0411
-11.250 -0.8112 0.01679 0.01115 -0.0777 0.6931 0.0416
-11.000 -0.7866 0.01646 0.01072 -0.0770 0.6873 0.0420
-10.750 -0.7627 0.01597 0.01018 -0.0763 0.6837 0.0425
-10.500 -0.7401 0.01536 0.00954 -0.0754 0.6793 0.0433
-10.250 -0.7152 0.01498 0.00912 -0.0748 0.6743 0.0440
-10.000 -0.6897 0.01470 0.00878 -0.0742 0.6687 0.0448
-9.750 -0.6636 0.01439 0.00844 -0.0737 0.6647 0.0455
-9.500 -0.6372 0.01409 0.00809 -0.0732 0.6608 0.0463
-9.250 -0.6106 0.01384 0.00778 -0.0727 0.6568 0.0469
-9.000 -0.5854 0.01343 0.00731 -0.0721 0.6526 0.0478
-8.750 -0.5599 0.01308 0.00692 -0.0715 0.6479 0.0489
-8.500 -0.5330 0.01279 0.00663 -0.0710 0.6449 0.0498
-8.250 -0.5058 0.01254 0.00635 -0.0707 0.6417 0.0509
-8.000 -0.4784 0.01232 0.00609 -0.0703 0.6380 0.0519
-7.750 -0.4515 0.01206 0.00578 -0.0698 0.6340 0.0530
-7.500 -0.4250 0.01176 0.00545 -0.0694 0.6296 0.0546
-7.250 -0.3975 0.01155 0.00522 -0.0690 0.6259 0.0561
-7.000 -0.3695 0.01135 0.00500 -0.0687 0.6226 0.0574
-6.750 -0.3419 0.01112 0.00474 -0.0684 0.6188 0.0590
-6.500 -0.3146 0.01086 0.00448 -0.0680 0.6146 0.0610
-6.250 -0.2869 0.01071 0.00429 -0.0677 0.6097 0.0629
-6.000 -0.2587 0.01055 0.00410 -0.0674 0.6057 0.0647
-5.750 -0.2309 0.01030 0.00388 -0.0672 0.6016 0.0677
-5.500 -0.2026 0.01016 0.00372 -0.0669 0.5970 0.0705
-5.250 -0.1747 0.00999 0.00355 -0.0666 0.5920 0.0739
-5.000 -0.1464 0.00987 0.00342 -0.0664 0.5871 0.0776
-4.750 -0.1179 0.00971 0.00328 -0.0662 0.5817 0.0816
-4.500 -0.0894 0.00961 0.00317 -0.0660 0.5754 0.0859
-4.250 -0.0612 0.00952 0.00306 -0.0658 0.5690 0.0904
-4.000 -0.0323 0.00943 0.00299 -0.0656 0.5627 0.0947
-3.750 -0.0040 0.00935 0.00288 -0.0654 0.5547 0.0986
-3.500 0.0245 0.00927 0.00280 -0.0652 0.5465 0.1026
-3.250 0.0530 0.00925 0.00273 -0.0650 0.5352 0.1056
-3.000 0.0811 0.00917 0.00262 -0.0648 0.5228 0.1097
-2.750 0.1091 0.00913 0.00255 -0.0646 0.5081 0.1132
-2.500 0.1370 0.00916 0.00251 -0.0643 0.4915 0.1163
-2.250 0.1646 0.00918 0.00245 -0.0640 0.4750 0.1196
-2.000 0.1919 0.00919 0.00241 -0.0637 0.4599 0.1237
-1.750 0.2197 0.00921 0.00239 -0.0635 0.4480 0.1274
-1.500 0.2476 0.00925 0.00237 -0.0632 0.4379 0.1303
-1.250 0.2751 0.00923 0.00234 -0.0630 0.4293 0.1362
-1.000 0.3028 0.00925 0.00234 -0.0627 0.4221 0.1416
-0.750 0.3308 0.00922 0.00232 -0.0625 0.4166 0.1491
-0.500 0.3584 0.00922 0.00232 -0.0623 0.4109 0.1588
-0.250 0.3854 0.00919 0.00234 -0.0620 0.4051 0.1785
0.000 0.4130 0.00908 0.00235 -0.0617 0.4015 0.2117
0.250 0.4405 0.00904 0.00239 -0.0615 0.3971 0.2418
0.500 0.4680 0.00907 0.00245 -0.0613 0.3923 0.2616
0.750 0.4951 0.00914 0.00253 -0.0610 0.3871 0.2769
1.000 0.5235 0.00914 0.00257 -0.0608 0.3847 0.2893
1.250 0.5516 0.00916 0.00261 -0.0607 0.3816 0.3012
1.500 0.5793 0.00920 0.00267 -0.0605 0.3781 0.3132
1.750 0.6068 0.00928 0.00274 -0.0603 0.3744 0.3227
2.000 0.6334 0.00938 0.00284 -0.0599 0.3698 0.3346
2.250 0.6615 0.00940 0.00290 -0.0598 0.3674 0.3453
2.500 0.6893 0.00941 0.00296 -0.0596 0.3647 0.3585
2.750 0.7168 0.00945 0.00303 -0.0594 0.3617 0.3727
3.000 0.7438 0.00951 0.00311 -0.0592 0.3586 0.3898
3.250 0.7702 0.00958 0.00322 -0.0588 0.3552 0.4104
3.500 0.7960 0.00968 0.00336 -0.0584 0.3513 0.4366
3.750 0.8226 0.00961 0.00345 -0.0581 0.3497 0.4843
4.000 0.8721 0.00863 0.00372 -0.0626 0.3469 0.9695
4.250 0.9224 0.00879 0.00385 -0.0672 0.3435 0.9886
4.500 0.9706 0.00897 0.00398 -0.0714 0.3398 0.9969
4.750 1.0141 0.00919 0.00413 -0.0747 0.3358 1.0000
5.000 1.0377 0.00934 0.00427 -0.0738 0.3334 1.0000
5.250 1.0621 0.00943 0.00438 -0.0731 0.3318 1.0000
5.500 1.0863 0.00954 0.00449 -0.0723 0.3296 1.0000
5.750 1.1101 0.00967 0.00461 -0.0715 0.3271 1.0000
6.000 1.1333 0.00983 0.00475 -0.0706 0.3245 1.0000
6.250 1.1559 0.01001 0.00491 -0.0696 0.3218 1.0000
6.500 1.1775 0.01025 0.00513 -0.0685 0.3186 1.0000
6.750 1.2003 0.01043 0.00530 -0.0676 0.3165 1.0000
7.000 1.2242 0.01055 0.00544 -0.0668 0.3148 1.0000
7.250 1.2477 0.01068 0.00559 -0.0660 0.3127 1.0000
7.500 1.2707 0.01084 0.00576 -0.0651 0.3105 1.0000
7.750 1.2930 0.01103 0.00594 -0.0642 0.3082 1.0000
8.000 1.3146 0.01124 0.00615 -0.0631 0.3057 1.0000
8.250 1.3344 0.01154 0.00641 -0.0618 0.3024 1.0000
8.500 1.3554 0.01177 0.00666 -0.0607 0.3002 1.0000
8.750 1.3781 0.01192 0.00684 -0.0598 0.2985 1.0000
9.000 1.4005 0.01207 0.00702 -0.0589 0.2958 1.0000
9.250 1.4212 0.01227 0.00722 -0.0578 0.2925 1.0000
9.500 1.4397 0.01255 0.00749 -0.0564 0.2894 1.0000
9.750 1.4532 0.01292 0.00784 -0.0541 0.2860 1.0000
10.000 1.4681 0.01318 0.00813 -0.0520 0.2837 1.0000
10.250 1.4861 0.01340 0.00839 -0.0505 0.2816 1.0000
10.500 1.5032 0.01369 0.00871 -0.0490 0.2792 1.0000
10.750 1.5193 0.01407 0.00912 -0.0475 0.2768 1.0000
11.000 1.5343 0.01457 0.00962 -0.0462 0.2739 1.0000
11.250 1.5474 0.01523 0.01028 -0.0447 0.2704 1.0000
11.500 1.5651 0.01571 0.01080 -0.0438 0.2675 1.0000
11.750 1.5839 0.01616 0.01128 -0.0431 0.2653 1.0000
12.000 1.6013 0.01669 0.01185 -0.0423 0.2624 1.0000
12.250 1.6164 0.01740 0.01257 -0.0414 0.2587 1.0000
12.500 1.6278 0.01835 0.01351 -0.0403 0.2544 1.0000
12.750 1.6456 0.01894 0.01415 -0.0397 0.2519 1.0000
13.000 1.6625 0.01960 0.01485 -0.0391 0.2490 1.0000
13.250 1.6772 0.02041 0.01569 -0.0384 0.2456 1.0000
13.500 1.6889 0.02146 0.01675 -0.0376 0.2419 1.0000
13.750 1.6999 0.02259 0.01790 -0.0368 0.2378 1.0000
14.000 1.7152 0.02341 0.01877 -0.0363 0.2342 1.0000
14.250 1.7250 0.02466 0.02003 -0.0355 0.2288 1.0000
14.500 1.7311 0.02622 0.02159 -0.0346 0.2238 1.0000
14.750 1.7432 0.02731 0.02272 -0.0341 0.2188 1.0000
15.000 1.7480 0.02899 0.02440 -0.0332 0.2129 1.0000
15.250 1.7523 0.03075 0.02618 -0.0325 0.2063 1.0000
15.500 1.7558 0.03257 0.02802 -0.0317 0.2002 1.0000
15.750 1.7545 0.03488 0.03032 -0.0309 0.1917 1.0000
16.000 1.7507 0.03750 0.03294 -0.0302 0.1842 1.0000
16.250 1.7464 0.04023 0.03567 -0.0295 0.1755 1.0000
16.500 1.7350 0.04371 0.03915 -0.0289 0.1658 1.0000
16.750 1.7207 0.04759 0.04302 -0.0284 0.1567 1.0000
17.000 1.7052 0.05174 0.04717 -0.0281 0.1466 1.0000
17.250 1.6883 0.05615 0.05159 -0.0280 0.1375 1.0000
17.500 1.6663 0.06128 0.05673 -0.0281 0.1282 1.0000
17.750 1.6404 0.06705 0.06252 -0.0285 0.1196 1.0000
18.000 1.6125 0.07320 0.06870 -0.0291 0.1111 1.0000
18.250 1.5857 0.07938 0.07490 -0.0299 0.1028 1.0000
18.500 1.5652 0.08488 0.08045 -0.0307 0.0978 1.0000
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