GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 703 AIRFOIL (goe703-il) Reynolds number: 200,000 Max Cl/Cd: 49.14 at α=8.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe703-il-200000-n5.txt Download as CSV file: xf-goe703-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.7644 0.10082 0.09523 -0.0696 1.0000 0.0381
-17.750 -0.8266 0.08382 0.07775 -0.0795 1.0000 0.0382
-17.500 -0.8376 0.07911 0.07293 -0.0817 1.0000 0.0383
-17.250 -0.8483 0.07458 0.06828 -0.0837 1.0000 0.0384
-17.000 -0.8565 0.07060 0.06420 -0.0852 1.0000 0.0386
-16.750 -0.8632 0.06698 0.06049 -0.0863 1.0000 0.0388
-16.500 -0.8686 0.06368 0.05710 -0.0871 1.0000 0.0389
-16.250 -0.8735 0.06060 0.05392 -0.0876 1.0000 0.0392
-16.000 -0.8783 0.05766 0.05088 -0.0878 1.0000 0.0394
-15.750 -0.8820 0.05502 0.04815 -0.0877 1.0000 0.0396
-15.500 -0.8849 0.05256 0.04558 -0.0872 1.0000 0.0398
-15.250 -0.8871 0.05030 0.04322 -0.0865 1.0000 0.0401
-15.000 -0.8885 0.04823 0.04106 -0.0855 1.0000 0.0404
-14.750 -0.8890 0.04632 0.03905 -0.0843 1.0000 0.0406
-14.500 -0.8889 0.04454 0.03717 -0.0828 1.0000 0.0410
-14.250 -0.8871 0.04294 0.03548 -0.0812 1.0000 0.0412
-14.000 -0.8854 0.04144 0.03389 -0.0794 1.0000 0.0415
-13.750 -0.8830 0.04003 0.03239 -0.0774 1.0000 0.0418
-13.500 -0.8801 0.03874 0.03100 -0.0753 1.0000 0.0421
-13.250 -0.8767 0.03757 0.02975 -0.0730 1.0000 0.0424
-13.000 -0.8731 0.03649 0.02859 -0.0706 1.0000 0.0427
-12.750 -0.8698 0.03546 0.02755 -0.0680 1.0000 0.0431
-12.500 -0.8673 0.03455 0.02665 -0.0651 1.0000 0.0433
-12.250 -0.8529 0.03346 0.02555 -0.0645 0.9982 0.0438
-12.000 -0.8271 0.03218 0.02425 -0.0659 0.9919 0.0444
-11.750 -0.8040 0.03102 0.02305 -0.0667 0.9852 0.0450
-11.500 -0.7811 0.02995 0.02192 -0.0673 0.9777 0.0458
-11.250 -0.7590 0.02896 0.02087 -0.0676 0.9683 0.0468
-11.000 -0.7373 0.02804 0.01985 -0.0677 0.9577 0.0476
-10.750 -0.7138 0.02700 0.01881 -0.0683 0.9491 0.0485
-10.500 -0.6890 0.02607 0.01786 -0.0689 0.9396 0.0494
-10.250 -0.6609 0.02516 0.01692 -0.0702 0.9312 0.0507
-10.000 -0.6296 0.02427 0.01596 -0.0719 0.9227 0.0520
-9.750 -0.5937 0.02339 0.01500 -0.0746 0.9150 0.0536
-9.500 -0.5593 0.02248 0.01408 -0.0771 0.9049 0.0553
-9.250 -0.5220 0.02168 0.01321 -0.0799 0.8954 0.0578
-9.000 -0.4874 0.02093 0.01241 -0.0822 0.8838 0.0604
-8.750 -0.4542 0.02025 0.01168 -0.0841 0.8718 0.0644
-8.500 -0.4218 0.01962 0.01101 -0.0857 0.8592 0.0685
-8.250 -0.3973 0.01913 0.01048 -0.0856 0.8456 0.0737
-8.000 -0.3724 0.01864 0.00996 -0.0856 0.8338 0.0812
-7.750 -0.3520 0.01821 0.00955 -0.0846 0.8210 0.0907
-7.500 -0.3321 0.01782 0.00918 -0.0834 0.8088 0.1034
-7.250 -0.3118 0.01749 0.00884 -0.0823 0.7965 0.1181
-7.000 -0.2938 0.01721 0.00857 -0.0806 0.7843 0.1314
-6.750 -0.2739 0.01695 0.00829 -0.0792 0.7730 0.1443
-6.500 -0.2567 0.01670 0.00805 -0.0773 0.7610 0.1557
-6.250 -0.2380 0.01647 0.00780 -0.0757 0.7497 0.1667
-6.000 -0.2196 0.01626 0.00757 -0.0739 0.7378 0.1779
-5.750 -0.2012 0.01607 0.00735 -0.0722 0.7266 0.1895
-5.500 -0.1833 0.01586 0.00714 -0.0703 0.7159 0.2012
-5.250 -0.1654 0.01566 0.00694 -0.0685 0.7060 0.2138
-4.750 -0.1295 0.01529 0.00657 -0.0647 0.6872 0.2429
-4.500 -0.1128 0.01508 0.00639 -0.0626 0.6784 0.2611
-4.250 -0.0959 0.01487 0.00621 -0.0605 0.6709 0.2794
-4.000 -0.0797 0.01466 0.00604 -0.0583 0.6632 0.2974
-3.750 -0.0629 0.01447 0.00585 -0.0562 0.6562 0.3148
-3.500 -0.0476 0.01425 0.00569 -0.0537 0.6495 0.3353
-3.250 -0.0344 0.01400 0.00554 -0.0509 0.6428 0.3613
-3.000 -0.0241 0.01371 0.00537 -0.0474 0.6368 0.3975
-2.750 -0.0177 0.01337 0.00523 -0.0432 0.6315 0.4503
-2.500 -0.0145 0.01301 0.00516 -0.0381 0.6255 0.5147
-2.250 -0.0056 0.01269 0.00515 -0.0341 0.6198 0.5872
-2.000 0.0365 0.01260 0.00538 -0.0367 0.6144 0.6740
-1.750 0.1028 0.01306 0.00601 -0.0439 0.6079 0.7300
-1.500 0.1445 0.01345 0.00640 -0.0461 0.6016 0.7562
-1.250 0.1742 0.01371 0.00660 -0.0461 0.5959 0.7741
-1.000 0.2027 0.01397 0.00681 -0.0459 0.5908 0.7877
-0.750 0.2322 0.01424 0.00707 -0.0458 0.5848 0.7981
-0.500 0.2486 0.01433 0.00712 -0.0433 0.5794 0.8115
-0.250 0.2820 0.01472 0.00744 -0.0440 0.5743 0.8196
0.000 0.3012 0.01494 0.00762 -0.0419 0.5694 0.8315
0.250 0.3337 0.01535 0.00803 -0.0424 0.5636 0.8382
0.500 0.3502 0.01550 0.00815 -0.0398 0.5584 0.8487
0.750 0.3892 0.01593 0.00849 -0.0417 0.5535 0.8524
1.000 0.4171 0.01619 0.00874 -0.0414 0.5484 0.8589
1.250 0.4364 0.01634 0.00890 -0.0396 0.5430 0.8671
1.500 0.4759 0.01670 0.00921 -0.0416 0.5373 0.8705
1.750 0.5073 0.01697 0.00940 -0.0421 0.5325 0.8761
2.000 0.5203 0.01704 0.00951 -0.0391 0.5273 0.8843
2.250 0.5537 0.01720 0.00967 -0.0402 0.5214 0.8864
2.500 0.5838 0.01733 0.00974 -0.0407 0.5159 0.8889
2.750 0.6100 0.01744 0.00984 -0.0404 0.5106 0.8925
3.000 0.6136 0.01745 0.00987 -0.0356 0.5055 0.9010
3.250 0.6458 0.01757 0.00998 -0.0366 0.4998 0.9026
3.500 0.6761 0.01769 0.01004 -0.0372 0.4942 0.9045
3.750 0.7027 0.01780 0.01019 -0.0370 0.4866 0.9072
4.000 0.7251 0.01789 0.01026 -0.0360 0.4794 0.9109
4.250 0.7280 0.01795 0.01029 -0.0311 0.4740 0.9183
4.500 0.7571 0.01806 0.01043 -0.0316 0.4655 0.9200
4.750 0.7835 0.01817 0.01049 -0.0315 0.4577 0.9220
5.000 0.8081 0.01829 0.01064 -0.0310 0.4496 0.9246
5.250 0.8278 0.01842 0.01075 -0.0296 0.4415 0.9283
5.750 0.8548 0.01866 0.01099 -0.0243 0.4259 0.9368
6.000 0.8796 0.01882 0.01113 -0.0240 0.4170 0.9390
6.250 0.9000 0.01898 0.01129 -0.0228 0.4074 0.9418
6.500 0.9151 0.01915 0.01145 -0.0206 0.4004 0.9456
6.750 0.9180 0.01931 0.01164 -0.0159 0.3938 0.9516
7.000 0.9403 0.01948 0.01180 -0.0152 0.3863 0.9536
7.250 0.9603 0.01965 0.01200 -0.0141 0.3790 0.9560
7.500 0.9759 0.01987 0.01222 -0.0122 0.3715 0.9593
7.750 0.9837 0.02014 0.01248 -0.0087 0.3653 0.9644
8.000 0.9986 0.02038 0.01276 -0.0068 0.3575 0.9673
8.250 1.0164 0.02069 0.01304 -0.0057 0.3491 0.9696
8.500 1.0329 0.02102 0.01340 -0.0043 0.3389 0.9725
8.750 1.0445 0.02147 0.01383 -0.0021 0.3300 0.9764
9.000 1.0536 0.02194 0.01432 0.0005 0.3207 0.9802
9.250 1.0705 0.02243 0.01481 0.0013 0.3111 0.9822
9.500 1.0855 0.02299 0.01537 0.0024 0.3006 0.9847
9.750 1.1004 0.02362 0.01602 0.0034 0.2910 0.9877
10.000 1.1104 0.02445 0.01684 0.0049 0.2805 0.9910
10.250 1.1228 0.02525 0.01765 0.0060 0.2687 0.9933
10.500 1.1355 0.02614 0.01855 0.0068 0.2580 0.9957
10.750 1.1464 0.02724 0.01963 0.0075 0.2472 0.9982
11.000 1.1576 0.02836 0.02076 0.0082 0.2354 1.0000
11.250 1.1522 0.02953 0.02193 0.0119 0.2269 1.0000
11.500 1.1474 0.03076 0.02316 0.0154 0.2185 1.0000
11.750 1.1422 0.03209 0.02449 0.0187 0.2105 1.0000
12.000 1.1356 0.03361 0.02599 0.0219 0.2022 1.0000
12.250 1.1314 0.03507 0.02745 0.0247 0.1955 1.0000
12.500 1.1259 0.03670 0.02909 0.0275 0.1885 1.0000
12.750 1.1213 0.03837 0.03076 0.0300 0.1825 1.0000
13.000 1.1183 0.04002 0.03243 0.0322 0.1768 1.0000
13.250 1.1137 0.04188 0.03428 0.0344 0.1722 1.0000
13.500 1.1133 0.04348 0.03592 0.0362 0.1683 1.0000
13.750 1.1127 0.04516 0.03763 0.0379 0.1642 1.0000
14.000 1.1096 0.04713 0.03960 0.0396 0.1600 1.0000
14.250 1.1082 0.04901 0.04150 0.0410 0.1563 1.0000
14.500 1.1094 0.05074 0.04328 0.0423 0.1526 1.0000
14.750 1.1088 0.05268 0.04524 0.0436 0.1489 1.0000
15.000 1.1067 0.05479 0.04735 0.0447 0.1455 1.0000
15.250 1.1085 0.05661 0.04921 0.0457 0.1429 1.0000
15.500 1.1107 0.05845 0.05113 0.0466 0.1396 1.0000
15.750 1.1112 0.06050 0.05322 0.0474 0.1365 1.0000
16.000 1.1105 0.06270 0.05543 0.0481 0.1334 1.0000
16.250 1.1112 0.06483 0.05759 0.0487 0.1307 1.0000
16.500 1.1134 0.06687 0.05972 0.0492 0.1275 1.0000
16.750 1.1139 0.06913 0.06202 0.0496 0.1244 1.0000
17.000 1.1122 0.07166 0.06457 0.0499 0.1212 1.0000
17.250 1.1122 0.07405 0.06703 0.0502 0.1180 1.0000
17.500 1.1127 0.07648 0.06954 0.0503 0.1145 1.0000
17.750 1.1106 0.07923 0.07233 0.0503 0.1111 1.0000
18.000 1.1084 0.08203 0.07515 0.0503 0.1079 1.0000
18.250 1.1080 0.08470 0.07794 0.0501 0.1040 1.0000
18.500 1.1039 0.08786 0.08114 0.0498 0.1000 1.0000
18.750 1.1010 0.09094 0.08430 0.0494 0.0959 1.0000
19.000 1.0975 0.09414 0.08755 0.0489 0.0913 1.0000
19.250 1.0930 0.09751 0.09098 0.0483 0.0870 1.0000
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