GOE 16K AIRFOIL (goe16k-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 16K AIRFOIL (goe16k-il) Reynolds number: 1,000,000 Max Cl/Cd: 80.17 at α=3.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe16k-il-1000000.txt Download as CSV file: xf-goe16k-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 16K 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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.7470 0.07578 0.07252 -0.1670 0.9560 0.0246
-19.500 -0.7731 0.06890 0.06550 -0.1713 0.9557 0.0245
-19.250 -0.7902 0.06312 0.05960 -0.1752 0.9553 0.0246
-19.000 -0.8113 0.06001 0.05641 -0.1728 0.9499 0.0251
-18.750 -0.8385 0.05357 0.04983 -0.1762 0.9482 0.0250
-18.500 -0.8378 0.04998 0.04614 -0.1788 0.9472 0.0254
-18.250 -0.8530 0.04454 0.04057 -0.1825 0.9462 0.0261
-18.000 -0.8509 0.04129 0.03725 -0.1850 0.9455 0.0267
-17.750 -0.8490 0.03827 0.03413 -0.1870 0.9449 0.0269
-17.500 -0.8381 0.03626 0.03205 -0.1886 0.9444 0.0281
-17.250 -0.8285 0.03430 0.03001 -0.1899 0.9439 0.0284
-17.000 -0.8470 0.03252 0.02814 -0.1852 0.9375 0.0285
-16.750 -0.8365 0.03120 0.02673 -0.1850 0.9358 0.0290
-16.500 -0.8325 0.02939 0.02483 -0.1844 0.9346 0.0292
-16.250 -0.8218 0.02806 0.02344 -0.1842 0.9336 0.0301
-16.000 -0.8082 0.02691 0.02228 -0.1840 0.9329 0.0311
-15.750 -0.7889 0.02615 0.02147 -0.1843 0.9323 0.0319
-15.500 -0.7683 0.02545 0.02073 -0.1846 0.9317 0.0326
-15.250 -0.7739 0.02471 0.01992 -0.1798 0.9258 0.0330
-15.000 -0.7590 0.02404 0.01917 -0.1787 0.9236 0.0336
-14.750 -0.7447 0.02318 0.01824 -0.1779 0.9220 0.0343
-14.500 -0.7312 0.02224 0.01727 -0.1769 0.9207 0.0351
-14.250 -0.7106 0.02150 0.01649 -0.1770 0.9198 0.0358
-14.000 -0.6851 0.02097 0.01592 -0.1778 0.9189 0.0366
-13.750 -0.6611 0.02027 0.01516 -0.1785 0.9180 0.0372
-13.500 -0.6520 0.02030 0.01516 -0.1752 0.9117 0.0382
-13.250 -0.6303 0.01986 0.01465 -0.1749 0.9093 0.0388
-13.000 -0.6071 0.01921 0.01390 -0.1752 0.9076 0.0392
-12.750 -0.5861 0.01831 0.01294 -0.1755 0.9060 0.0400
-12.500 -0.5555 0.01781 0.01243 -0.1772 0.9048 0.0411
-12.250 -0.5369 0.01766 0.01226 -0.1760 0.9010 0.0421
-12.000 -0.5245 0.01738 0.01193 -0.1735 0.8965 0.0427
-11.750 -0.4982 0.01699 0.01148 -0.1742 0.8944 0.0436
-11.500 -0.4697 0.01656 0.01098 -0.1752 0.8924 0.0442
-11.250 -0.4363 0.01637 0.01072 -0.1771 0.8907 0.0448
-11.000 -0.4155 0.01585 0.01014 -0.1766 0.8881 0.0453
-10.750 -0.4177 0.01546 0.00973 -0.1710 0.8831 0.0466
-10.500 -0.3991 0.01515 0.00939 -0.1697 0.8802 0.0474
-10.250 -0.3742 0.01483 0.00904 -0.1699 0.8781 0.0482
-10.000 -0.3435 0.01464 0.00881 -0.1711 0.8763 0.0494
-9.750 -0.3123 0.01429 0.00840 -0.1726 0.8746 0.0501
-9.500 -0.3052 0.01411 0.00818 -0.1686 0.8715 0.0505
-9.250 -0.2922 0.01404 0.00808 -0.1658 0.8687 0.0512
-9.000 -0.2750 0.01391 0.00792 -0.1639 0.8662 0.0516
-8.750 -0.2592 0.01344 0.00740 -0.1620 0.8640 0.0524
-8.500 -0.2363 0.01307 0.00700 -0.1616 0.8621 0.0538
-8.250 -0.2085 0.01274 0.00664 -0.1622 0.8605 0.0549
-8.000 -0.1746 0.01257 0.00645 -0.1641 0.8591 0.0564
-7.750 -0.1602 0.01240 0.00626 -0.1616 0.8573 0.0567
-7.500 -0.1527 0.01227 0.00610 -0.1574 0.8551 0.0573
-7.250 -0.1368 0.01217 0.00598 -0.1551 0.8533 0.0583
-7.000 -0.1176 0.01205 0.00584 -0.1536 0.8515 0.0589
-6.750 -0.0966 0.01192 0.00568 -0.1525 0.8500 0.0592
-6.500 -0.0761 0.01165 0.00538 -0.1512 0.8485 0.0612
-6.250 -0.0523 0.01145 0.00518 -0.1508 0.8473 0.0629
-6.000 -0.0247 0.01129 0.00501 -0.1512 0.8461 0.0644
-5.750 0.0056 0.01113 0.00483 -0.1521 0.8451 0.0663
-5.500 0.0381 0.01101 0.00468 -0.1536 0.8441 0.0677
-5.250 0.0730 0.01084 0.00451 -0.1557 0.8431 0.0705
-5.000 0.0896 0.01075 0.00445 -0.1535 0.8419 0.0742
-4.750 0.0937 0.01072 0.00444 -0.1483 0.8401 0.0766
-4.500 0.1062 0.01063 0.00439 -0.1452 0.8385 0.0846
-4.250 0.1231 0.01037 0.00430 -0.1431 0.8370 0.1195
-4.000 0.1428 0.01005 0.00425 -0.1418 0.8357 0.1807
-3.750 0.1649 0.00994 0.00422 -0.1410 0.8346 0.2050
-3.500 0.1887 0.00982 0.00419 -0.1404 0.8335 0.2300
-3.250 0.2138 0.00973 0.00416 -0.1401 0.8325 0.2486
-3.000 0.2396 0.00963 0.00414 -0.1401 0.8316 0.2697
-2.750 0.2665 0.00954 0.00412 -0.1402 0.8307 0.2932
-2.500 0.2936 0.00946 0.00412 -0.1404 0.8298 0.3200
-2.250 0.3217 0.00937 0.00413 -0.1409 0.8289 0.3462
-2.000 0.3539 0.00931 0.00414 -0.1423 0.8278 0.3711
-1.750 0.3891 0.00926 0.00417 -0.1445 0.8267 0.3975
-1.500 0.3697 0.00937 0.00433 -0.1337 0.8237 0.4069
-1.250 0.3700 0.00938 0.00442 -0.1276 0.8207 0.4259
-1.000 0.3852 0.00934 0.00446 -0.1250 0.8189 0.4519
-0.750 0.4071 0.00914 0.00439 -0.1240 0.8167 0.4950
-0.500 0.4227 0.00878 0.00435 -0.1216 0.8151 0.5912
-0.250 0.5146 0.00872 0.00531 -0.1364 0.8156 0.8733
0.000 0.5581 0.00899 0.00558 -0.1400 0.8145 0.8895
0.250 0.5878 0.00925 0.00583 -0.1404 0.8130 0.9033
0.500 0.6260 0.00945 0.00600 -0.1429 0.8112 0.9091
0.750 0.6496 0.00967 0.00623 -0.1421 0.8098 0.9153
1.000 0.6710 0.01007 0.00665 -0.1406 0.8084 0.9183
1.250 0.6592 0.01044 0.00706 -0.1316 0.8055 0.9279
1.500 0.6948 0.01072 0.00734 -0.1336 0.8041 0.9292
1.750 0.7304 0.01090 0.00753 -0.1355 0.8020 0.9307
2.000 0.7721 0.01106 0.00768 -0.1387 0.8000 0.9327
2.250 0.8118 0.01106 0.00766 -0.1415 0.7972 0.9345
2.500 0.8536 0.01107 0.00765 -0.1450 0.7947 0.9364
2.750 0.8596 0.01149 0.00811 -0.1401 0.7912 0.9420
3.000 0.8786 0.01170 0.00835 -0.1381 0.7865 0.9440
3.250 0.9060 0.01174 0.00839 -0.1382 0.7825 0.9458
3.500 0.9380 0.01170 0.00831 -0.1393 0.7769 0.9477
3.750 0.9286 0.01220 0.00886 -0.1311 0.7704 0.9537
4.000 0.9585 0.01224 0.00888 -0.1317 0.7625 0.9552
4.250 0.9671 0.01261 0.00929 -0.1277 0.7560 0.9581
4.500 0.9712 0.01309 0.00980 -0.1227 0.7515 0.9639
4.750 0.9982 0.01316 0.00986 -0.1228 0.7430 0.9650
5.000 1.0198 0.01341 0.01015 -0.1219 0.7345 0.9668
5.250 1.0389 0.01373 0.01047 -0.1203 0.7232 0.9699
5.500 1.0536 0.01436 0.01108 -0.1179 0.7035 0.9758
5.750 1.0586 0.01514 0.01168 -0.1135 0.6624 0.9798
6.000 1.0408 0.01666 0.01298 -0.1045 0.6195 0.9855
6.250 1.0216 0.01838 0.01436 -0.0962 0.5490 0.9894
6.500 1.0269 0.01927 0.01517 -0.0924 0.5209 0.9922
6.750 0.9876 0.02176 0.01732 -0.0800 0.4549 0.9934
7.000 0.9737 0.02337 0.01873 -0.0725 0.4179 0.9939
7.250 0.9873 0.02358 0.01888 -0.0707 0.4011 0.9942
7.500 0.9992 0.02403 0.01925 -0.0686 0.3790 0.9947
7.750 1.0130 0.02449 0.01964 -0.0667 0.3593 0.9952
8.000 1.0227 0.02516 0.02019 -0.0643 0.3315 0.9957
8.250 1.0183 0.02652 0.02119 -0.0596 0.2670 0.9965
8.500 1.0299 0.02714 0.02171 -0.0574 0.2435 0.9970
8.750 1.0401 0.02784 0.02230 -0.0551 0.2202 0.9975
9.000 1.0447 0.02883 0.02309 -0.0519 0.1849 0.9980
9.250 1.0537 0.02960 0.02370 -0.0494 0.1600 0.9983
9.500 1.0698 0.03001 0.02415 -0.0480 0.1570 0.9985
9.750 1.0818 0.03063 0.02470 -0.0459 0.1434 0.9987
10.000 1.0929 0.03131 0.02532 -0.0438 0.1307 0.9988
10.250 1.1069 0.03184 0.02585 -0.0421 0.1255 0.9989
10.500 1.1176 0.03254 0.02648 -0.0399 0.1118 0.9990
10.750 1.1289 0.03322 0.02708 -0.0379 0.0996 0.9991
11.000 1.1419 0.03383 0.02768 -0.0361 0.0944 0.9992
11.250 1.1544 0.03447 0.02833 -0.0343 0.0895 0.9992
11.500 1.1655 0.03520 0.02902 -0.0323 0.0816 0.9993
11.750 1.1781 0.03585 0.02966 -0.0305 0.0773 0.9993
12.000 1.1901 0.03655 0.03034 -0.0288 0.0718 0.9993
12.250 1.2027 0.03723 0.03104 -0.0271 0.0691 0.9994
12.500 1.2127 0.03809 0.03187 -0.0251 0.0638 0.9994
12.750 1.2242 0.03885 0.03262 -0.0233 0.0587 0.9994
13.000 1.2354 0.03964 0.03342 -0.0215 0.0557 0.9994
13.250 1.2478 0.04034 0.03414 -0.0200 0.0533 0.9994
13.500 1.2572 0.04129 0.03507 -0.0181 0.0493 0.9994
13.750 1.2679 0.04215 0.03594 -0.0164 0.0455 0.9994
14.000 1.2785 0.04303 0.03684 -0.0146 0.0437 0.9995
14.250 1.2886 0.04394 0.03774 -0.0130 0.0399 0.9995
14.500 1.2965 0.04505 0.03886 -0.0111 0.0376 0.9995
14.750 1.3057 0.04608 0.03992 -0.0093 0.0353 0.9995
15.000 1.3145 0.04715 0.04099 -0.0076 0.0326 0.9995
15.250 1.3220 0.04831 0.04217 -0.0059 0.0306 0.9995
15.500 1.3304 0.04944 0.04333 -0.0043 0.0298 0.9995
15.750 1.3384 0.05062 0.04456 -0.0026 0.0289 0.9995
16.000 1.3429 0.05209 0.04604 -0.0007 0.0270 0.9995
16.250 1.3505 0.05336 0.04736 0.0008 0.0262 0.9995
16.500 1.3578 0.05465 0.04871 0.0023 0.0255 0.9995
16.750 1.3649 0.05601 0.05010 0.0037 0.0246 0.9995
17.000 1.3707 0.05747 0.05160 0.0052 0.0240 0.9995
17.250 1.3695 0.05961 0.05379 0.0071 0.0229 0.9995
17.500 1.3738 0.06127 0.05551 0.0085 0.0226 0.9995
17.750 1.3811 0.06269 0.05700 0.0097 0.0215 0.9995
18.000 1.3848 0.06445 0.05882 0.0109 0.0218 0.9995
18.250 1.3874 0.06635 0.06078 0.0122 0.0210 0.9995
18.500 1.3853 0.06874 0.06318 0.0135 0.0191 0.9994
18.750 1.3903 0.07049 0.06502 0.0145 0.0201 0.9994
19.000 1.3965 0.07212 0.06669 0.0153 0.0186 0.9994
19.250 1.3976 0.07429 0.06891 0.0162 0.0179 0.9994
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