GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 703 AIRFOIL (goe703-il) Reynolds number: 500,000 Max Cl/Cd: 57.38 at α=7.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe703-il-500000-n5.txt Download as CSV file: xf-goe703-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9179 0.09801 0.09355 -0.0667 1.0000 0.0285
-19.500 -0.9296 0.09287 0.08830 -0.0692 1.0000 0.0286
-19.250 -0.9406 0.08790 0.08322 -0.0716 1.0000 0.0287
-19.000 -0.9507 0.08312 0.07834 -0.0738 1.0000 0.0288
-18.750 -0.9597 0.07856 0.07368 -0.0759 1.0000 0.0289
-18.500 -0.9690 0.07405 0.06906 -0.0779 1.0000 0.0290
-18.250 -0.9772 0.06979 0.06470 -0.0797 1.0000 0.0291
-18.000 -0.9840 0.06577 0.06056 -0.0813 1.0000 0.0292
-17.750 -0.9895 0.06206 0.05676 -0.0826 1.0000 0.0293
-17.500 -0.9946 0.05855 0.05314 -0.0836 1.0000 0.0294
-17.250 -0.9983 0.05534 0.04983 -0.0844 1.0000 0.0295
-17.000 -1.0009 0.05236 0.04676 -0.0849 1.0000 0.0296
-16.750 -1.0028 0.04963 0.04393 -0.0851 1.0000 0.0297
-16.500 -1.0037 0.04713 0.04134 -0.0850 1.0000 0.0297
-16.250 -1.0043 0.04478 0.03892 -0.0846 1.0000 0.0298
-16.000 -1.0070 0.04242 0.03649 -0.0839 1.0000 0.0300
-15.750 -1.0075 0.04035 0.03437 -0.0829 1.0000 0.0302
-15.500 -1.0069 0.03851 0.03247 -0.0818 1.0000 0.0302
-15.250 -1.0063 0.03678 0.03069 -0.0803 1.0000 0.0304
-15.000 -1.0047 0.03522 0.02908 -0.0787 1.0000 0.0306
-14.750 -1.0020 0.03384 0.02765 -0.0769 1.0000 0.0308
-14.500 -0.9987 0.03259 0.02636 -0.0749 1.0000 0.0310
-14.250 -0.9946 0.03147 0.02520 -0.0728 1.0000 0.0312
-14.000 -0.9911 0.03039 0.02407 -0.0705 1.0000 0.0313
-13.750 -0.9821 0.02936 0.02299 -0.0690 0.9996 0.0316
-13.250 -0.9366 0.02711 0.02065 -0.0709 0.9928 0.0323
-12.250 -0.8590 0.02349 0.01682 -0.0703 0.9573 0.0335
-12.000 -0.8311 0.02262 0.01590 -0.0716 0.9467 0.0339
-11.750 -0.7979 0.02167 0.01492 -0.0741 0.9362 0.0343
-11.500 -0.7586 0.02079 0.01399 -0.0778 0.9252 0.0349
-11.250 -0.7111 0.01998 0.01314 -0.0829 0.9141 0.0356
-11.000 -0.6601 0.01924 0.01232 -0.0888 0.9021 0.0365
-10.750 -0.6157 0.01861 0.01160 -0.0932 0.8875 0.0372
-10.500 -0.5778 0.01811 0.01098 -0.0962 0.8711 0.0380
-10.250 -0.5493 0.01762 0.01041 -0.0972 0.8561 0.0388
-10.000 -0.5261 0.01721 0.00993 -0.0969 0.8403 0.0396
-9.750 -0.5052 0.01685 0.00951 -0.0961 0.8280 0.0404
-9.250 -0.4656 0.01626 0.00878 -0.0938 0.8046 0.0428
-9.000 -0.4474 0.01594 0.00840 -0.0924 0.7929 0.0439
-8.750 -0.4294 0.01564 0.00806 -0.0908 0.7805 0.0457
-8.500 -0.4107 0.01539 0.00775 -0.0892 0.7690 0.0471
-8.250 -0.3928 0.01512 0.00744 -0.0876 0.7568 0.0488
-8.000 -0.3749 0.01485 0.00713 -0.0858 0.7448 0.0513
-7.750 -0.3573 0.01462 0.00685 -0.0840 0.7317 0.0541
-7.500 -0.3399 0.01438 0.00656 -0.0821 0.7166 0.0579
-7.250 -0.3225 0.01413 0.00629 -0.0803 0.7025 0.0628
-7.000 -0.3053 0.01390 0.00603 -0.0783 0.6895 0.0691
-6.750 -0.2883 0.01365 0.00578 -0.0764 0.6775 0.0793
-6.500 -0.2712 0.01338 0.00555 -0.0745 0.6671 0.0928
-6.250 -0.2538 0.01317 0.00534 -0.0725 0.6570 0.1066
-6.000 -0.2353 0.01298 0.00517 -0.0708 0.6480 0.1191
-5.750 -0.2166 0.01280 0.00500 -0.0691 0.6393 0.1301
-5.500 -0.1976 0.01265 0.00485 -0.0674 0.6324 0.1397
-5.250 -0.1778 0.01249 0.00471 -0.0659 0.6260 0.1490
-5.000 -0.1583 0.01237 0.00457 -0.0643 0.6192 0.1581
-4.750 -0.1396 0.01224 0.00444 -0.0625 0.6131 0.1681
-4.500 -0.1193 0.01210 0.00433 -0.0610 0.6077 0.1777
-4.250 -0.0994 0.01197 0.00421 -0.0595 0.6020 0.1878
-4.000 -0.0804 0.01184 0.00411 -0.0577 0.5965 0.2000
-3.750 -0.0616 0.01170 0.00401 -0.0560 0.5917 0.2157
-3.500 -0.0425 0.01154 0.00392 -0.0542 0.5868 0.2333
-3.250 -0.0244 0.01137 0.00382 -0.0523 0.5818 0.2538
-3.000 -0.0064 0.01124 0.00373 -0.0504 0.5767 0.2720
-2.750 0.0120 0.01113 0.00364 -0.0484 0.5719 0.2890
-2.500 0.0309 0.01098 0.00356 -0.0466 0.5669 0.3071
-2.250 0.0484 0.01083 0.00347 -0.0445 0.5623 0.3265
-2.000 0.0640 0.01067 0.00338 -0.0420 0.5572 0.3508
-1.500 0.0837 0.01012 0.00318 -0.0347 0.5486 0.4457
-1.250 0.0862 0.00977 0.00308 -0.0294 0.5446 0.5080
-1.000 0.0873 0.00950 0.00301 -0.0238 0.5403 0.5608
-0.750 0.0859 0.00928 0.00296 -0.0175 0.5361 0.6128
-0.500 0.0827 0.00909 0.00296 -0.0107 0.5323 0.6640
-0.250 0.0882 0.00889 0.00301 -0.0057 0.5287 0.7204
0.000 0.1096 0.00882 0.00309 -0.0041 0.5244 0.7612
0.250 0.1355 0.00885 0.00318 -0.0036 0.5198 0.7893
0.500 0.1610 0.00893 0.00327 -0.0029 0.5151 0.8089
0.750 0.1903 0.00902 0.00338 -0.0031 0.5105 0.8258
1.000 0.2252 0.00913 0.00352 -0.0045 0.5057 0.8374
1.250 0.2407 0.00921 0.00359 -0.0017 0.5012 0.8491
1.500 0.2733 0.00938 0.00374 -0.0026 0.4963 0.8579
1.750 0.2872 0.00946 0.00382 0.0005 0.4918 0.8674
2.000 0.3257 0.00965 0.00401 -0.0016 0.4864 0.8734
2.750 0.4012 0.01015 0.00445 0.0004 0.4681 0.8910
3.000 0.3897 0.01015 0.00445 0.0090 0.4625 0.9013
3.250 0.4315 0.01044 0.00469 0.0059 0.4550 0.9033
3.500 0.4717 0.01067 0.00492 0.0033 0.4481 0.9050
3.750 0.5015 0.01088 0.00510 0.0028 0.4412 0.9073
4.000 0.5216 0.01101 0.00521 0.0044 0.4349 0.9106
4.250 0.5094 0.01094 0.00514 0.0130 0.4290 0.9192
4.500 0.5399 0.01114 0.00530 0.0122 0.4214 0.9203
4.750 0.5702 0.01129 0.00545 0.0115 0.4141 0.9214
5.000 0.5959 0.01150 0.00561 0.0117 0.4051 0.9229
5.250 0.6205 0.01169 0.00578 0.0122 0.3961 0.9249
5.500 0.6395 0.01188 0.00594 0.0138 0.3875 0.9279
5.750 0.6332 0.01190 0.00595 0.0208 0.3814 0.9357
6.000 0.6618 0.01216 0.00618 0.0202 0.3706 0.9367
6.250 0.6886 0.01243 0.00641 0.0200 0.3602 0.9378
6.500 0.7137 0.01270 0.00666 0.0202 0.3519 0.9391
6.750 0.7379 0.01296 0.00690 0.0205 0.3438 0.9407
7.000 0.7587 0.01327 0.00718 0.0214 0.3342 0.9429
7.250 0.7758 0.01352 0.00742 0.0232 0.3277 0.9465
7.500 0.7805 0.01375 0.00763 0.0274 0.3190 0.9519
7.750 0.8055 0.01412 0.00798 0.0272 0.3101 0.9528
8.000 0.8294 0.01453 0.00836 0.0272 0.2999 0.9539
8.250 0.8533 0.01493 0.00875 0.0272 0.2907 0.9553
8.500 0.8737 0.01543 0.00921 0.0277 0.2805 0.9572
8.750 0.8934 0.01584 0.00961 0.0285 0.2711 0.9595
9.000 0.9036 0.01635 0.01010 0.0309 0.2618 0.9634
9.250 0.9143 0.01692 0.01064 0.0331 0.2498 0.9668
9.500 0.9347 0.01765 0.01132 0.0331 0.2350 0.9680
9.750 0.9527 0.01847 0.01208 0.0333 0.2200 0.9695
10.000 0.9678 0.01938 0.01294 0.0338 0.2052 0.9714
10.250 0.9793 0.02041 0.01391 0.0349 0.1905 0.9738
10.500 0.9888 0.02141 0.01487 0.0363 0.1798 0.9768
10.750 0.9958 0.02249 0.01592 0.0382 0.1711 0.9802
11.000 1.0132 0.02353 0.01695 0.0379 0.1626 0.9813
11.250 1.0282 0.02468 0.01809 0.0379 0.1556 0.9825
11.500 1.0440 0.02575 0.01918 0.0378 0.1503 0.9838
11.750 1.0564 0.02705 0.02047 0.0380 0.1449 0.9854
12.000 1.0709 0.02819 0.02164 0.0380 0.1412 0.9871
12.250 1.0838 0.02946 0.02294 0.0382 0.1371 0.9889
12.500 1.0937 0.03097 0.02445 0.0385 0.1331 0.9908
12.750 1.1046 0.03232 0.02584 0.0389 0.1307 0.9923
13.000 1.1192 0.03365 0.02721 0.0385 0.1278 0.9934
13.250 1.1318 0.03513 0.02872 0.0382 0.1248 0.9947
13.500 1.1426 0.03680 0.03041 0.0379 0.1220 0.9959
13.750 1.1539 0.03850 0.03215 0.0375 0.1193 0.9971
14.000 1.1679 0.04004 0.03373 0.0369 0.1166 0.9982
14.250 1.1801 0.04177 0.03551 0.0363 0.1139 0.9991
14.500 1.1893 0.04375 0.03751 0.0357 0.1105 0.9998
14.750 1.1911 0.04566 0.03945 0.0367 0.1086 1.0000
15.000 1.1944 0.04716 0.04101 0.0380 0.1061 1.0000
15.250 1.1958 0.04890 0.04279 0.0392 0.1038 1.0000
15.500 1.1952 0.05087 0.04479 0.0404 0.1005 1.0000
15.750 1.1944 0.05290 0.04684 0.0415 0.0976 1.0000
16.000 1.1964 0.05472 0.04871 0.0425 0.0935 1.0000
16.250 1.1948 0.05695 0.05096 0.0434 0.0881 1.0000
16.500 1.1899 0.05959 0.05358 0.0442 0.0781 1.0000
16.750 1.1816 0.06264 0.05659 0.0449 0.0699 1.0000
17.000 1.1759 0.06550 0.05945 0.0454 0.0660 1.0000
17.250 1.1697 0.06850 0.06247 0.0458 0.0629 1.0000
17.500 1.1658 0.07129 0.06529 0.0462 0.0611 1.0000
17.750 1.1608 0.07429 0.06834 0.0464 0.0595 1.0000
18.000 1.1582 0.07705 0.07115 0.0465 0.0582 1.0000
18.250 1.1551 0.07993 0.07408 0.0465 0.0572 1.0000
18.500 1.1509 0.08300 0.07721 0.0464 0.0561 1.0000
18.750 1.1460 0.08621 0.08046 0.0463 0.0551 1.0000
19.000 1.1407 0.08951 0.08382 0.0459 0.0545 1.0000
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