GOE 625 AIRFOIL (goe625-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 625 AIRFOIL (goe625-il) Reynolds number: 1,000,000 Max Cl/Cd: 101.41 at α=7° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe625-il-1000000.txt Download as CSV file: xf-goe625-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 625 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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.8062 0.08434 0.08151 -0.0931 1.0000 0.0373
-18.000 -0.8871 0.07048 0.06747 -0.1020 1.0000 0.0374
-17.750 -1.0531 0.04508 0.04164 -0.1187 1.0000 0.0369
-17.500 -1.0866 0.03545 0.03174 -0.1285 0.9968 0.0370
-17.250 -1.0781 0.03121 0.02735 -0.1347 0.9930 0.0375
-17.000 -1.0664 0.02861 0.02462 -0.1379 0.9852 0.0380
-16.750 -1.0518 0.02679 0.02268 -0.1397 0.9763 0.0384
-16.500 -1.0502 0.02484 0.02064 -0.1393 0.9616 0.0391
-16.250 -1.0465 0.02356 0.01926 -0.1376 0.9476 0.0397
-16.000 -1.0395 0.02260 0.01821 -0.1356 0.9352 0.0403
-15.750 -1.0302 0.02184 0.01737 -0.1335 0.9248 0.0409
-15.250 -0.9990 0.02060 0.01595 -0.1308 0.9092 0.0423
-15.000 -0.9806 0.02003 0.01528 -0.1297 0.9020 0.0430
-14.750 -0.9632 0.01934 0.01455 -0.1286 0.8949 0.0441
-14.500 -0.9423 0.01884 0.01402 -0.1278 0.8878 0.0451
-14.250 -0.9202 0.01843 0.01354 -0.1271 0.8810 0.0462
-14.000 -0.8967 0.01805 0.01308 -0.1265 0.8751 0.0473
-13.750 -0.8744 0.01756 0.01255 -0.1258 0.8690 0.0484
-13.500 -0.8506 0.01720 0.01216 -0.1253 0.8627 0.0496
-13.250 -0.8254 0.01693 0.01184 -0.1249 0.8569 0.0508
-13.000 -0.7995 0.01665 0.01152 -0.1246 0.8515 0.0520
-12.750 -0.7742 0.01635 0.01114 -0.1242 0.8459 0.0531
-12.500 -0.7491 0.01607 0.01083 -0.1238 0.8399 0.0543
-12.250 -0.7218 0.01588 0.01065 -0.1236 0.8352 0.0555
-12.000 -0.6945 0.01572 0.01045 -0.1235 0.8295 0.0567
-11.750 -0.6673 0.01558 0.01022 -0.1232 0.8233 0.0577
-11.500 -0.6411 0.01531 0.00988 -0.1230 0.8172 0.0587
-11.250 -0.6151 0.01500 0.00957 -0.1227 0.8108 0.0598
-11.000 -0.5877 0.01486 0.00939 -0.1225 0.8047 0.0608
-10.750 -0.5601 0.01472 0.00921 -0.1224 0.7997 0.0618
-10.500 -0.5320 0.01456 0.00902 -0.1223 0.7951 0.0628
-10.250 -0.5039 0.01444 0.00883 -0.1223 0.7898 0.0637
-10.000 -0.4756 0.01438 0.00868 -0.1222 0.7845 0.0643
-9.750 -0.4505 0.01387 0.00817 -0.1219 0.7795 0.0657
-9.500 -0.4227 0.01367 0.00796 -0.1218 0.7740 0.0666
-9.250 -0.3949 0.01350 0.00777 -0.1217 0.7679 0.0674
-9.000 -0.3672 0.01336 0.00756 -0.1216 0.7619 0.0684
-8.750 -0.3389 0.01318 0.00736 -0.1216 0.7564 0.0693
-8.500 -0.3105 0.01305 0.00717 -0.1216 0.7503 0.0701
-8.250 -0.2821 0.01299 0.00702 -0.1216 0.7439 0.0707
-8.000 -0.2557 0.01252 0.00654 -0.1214 0.7383 0.0719
-7.750 -0.2283 0.01224 0.00625 -0.1213 0.7314 0.0729
-7.500 -0.2007 0.01207 0.00604 -0.1211 0.7243 0.0737
-7.250 -0.1722 0.01190 0.00585 -0.1212 0.7176 0.0747
-7.000 -0.1441 0.01176 0.00567 -0.1211 0.7095 0.0757
-6.750 -0.1158 0.01163 0.00549 -0.1211 0.7017 0.0766
-6.500 -0.0873 0.01154 0.00535 -0.1211 0.6923 0.0775
-6.250 -0.0590 0.01148 0.00523 -0.1211 0.6826 0.0781
-6.000 -0.0329 0.01111 0.00481 -0.1208 0.6709 0.0796
-5.750 -0.0055 0.01093 0.00459 -0.1206 0.6586 0.0806
-5.500 0.0218 0.01082 0.00443 -0.1205 0.6446 0.0816
-5.250 0.0488 0.01075 0.00428 -0.1202 0.6286 0.0825
-5.000 0.0758 0.01070 0.00414 -0.1200 0.6104 0.0833
-4.750 0.1024 0.01067 0.00402 -0.1197 0.5900 0.0842
-4.500 0.1289 0.01069 0.00393 -0.1193 0.5677 0.0850
-4.250 0.1551 0.01075 0.00386 -0.1189 0.5450 0.0857
-4.000 0.1808 0.01072 0.00373 -0.1185 0.5246 0.0868
-3.750 0.2069 0.01070 0.00363 -0.1181 0.5074 0.0883
-3.500 0.2333 0.01070 0.00357 -0.1178 0.4934 0.0897
-3.250 0.2600 0.01072 0.00352 -0.1175 0.4817 0.0910
-3.000 0.2874 0.01071 0.00347 -0.1174 0.4732 0.0925
-2.750 0.3145 0.01073 0.00344 -0.1172 0.4653 0.0940
-2.500 0.3415 0.01072 0.00339 -0.1170 0.4584 0.0966
-2.250 0.3692 0.01067 0.00336 -0.1170 0.4536 0.0999
-2.000 0.3966 0.01067 0.00334 -0.1168 0.4487 0.1037
-1.750 0.4233 0.01067 0.00335 -0.1166 0.4439 0.1123
-1.500 0.4504 0.01066 0.00338 -0.1165 0.4400 0.1265
-1.250 0.4785 0.01063 0.00341 -0.1165 0.4375 0.1396
-1.000 0.5063 0.01064 0.00345 -0.1165 0.4347 0.1492
-0.750 0.5337 0.01067 0.00349 -0.1164 0.4318 0.1565
-0.500 0.5607 0.01072 0.00354 -0.1162 0.4288 0.1629
-0.250 0.5872 0.01082 0.00361 -0.1160 0.4255 0.1665
0.000 0.6132 0.01090 0.00368 -0.1157 0.4219 0.1731
0.250 0.6411 0.01090 0.00371 -0.1157 0.4204 0.1785
0.500 0.6689 0.01093 0.00375 -0.1157 0.4184 0.1825
0.750 0.6962 0.01094 0.00379 -0.1156 0.4161 0.1892
1.000 0.7229 0.01098 0.00384 -0.1154 0.4135 0.1965
1.250 0.7491 0.01104 0.00391 -0.1152 0.4108 0.2040
1.500 0.7744 0.01112 0.00400 -0.1148 0.4075 0.2157
1.750 0.7986 0.01123 0.00413 -0.1142 0.4038 0.2331
2.000 0.8254 0.01115 0.00420 -0.1141 0.4024 0.2757
2.250 0.8515 0.01091 0.00431 -0.1141 0.4008 0.3976
2.500 0.8771 0.01062 0.00443 -0.1140 0.3988 0.5450
2.750 0.9015 0.01031 0.00460 -0.1135 0.3967 0.7103
3.000 0.9219 0.01009 0.00479 -0.1120 0.3947 0.8479
3.250 0.9377 0.01008 0.00497 -0.1092 0.3927 0.9422
3.500 0.9741 0.01027 0.00516 -0.1111 0.3901 0.9917
3.750 1.0024 0.01048 0.00533 -0.1115 0.3874 1.0000
4.000 1.0228 0.01069 0.00550 -0.1102 0.3851 1.0000
4.250 1.0466 0.01079 0.00561 -0.1095 0.3841 1.0000
4.500 1.0706 0.01091 0.00573 -0.1089 0.3828 1.0000
4.750 1.0947 0.01105 0.00586 -0.1084 0.3813 1.0000
5.000 1.1188 0.01120 0.00601 -0.1079 0.3794 1.0000
5.250 1.1428 0.01136 0.00616 -0.1073 0.3773 1.0000
5.500 1.1661 0.01155 0.00634 -0.1067 0.3750 1.0000
5.750 1.1888 0.01178 0.00655 -0.1061 0.3727 1.0000
6.000 1.2107 0.01206 0.00679 -0.1053 0.3700 1.0000
6.250 1.2328 0.01234 0.00706 -0.1046 0.3672 1.0000
6.500 1.2577 0.01250 0.00724 -0.1043 0.3656 1.0000
6.750 1.2823 0.01267 0.00743 -0.1041 0.3633 1.0000
7.000 1.3062 0.01288 0.00764 -0.1037 0.3610 1.0000
7.250 1.3291 0.01313 0.00789 -0.1032 0.3585 1.0000
7.500 1.3512 0.01342 0.00817 -0.1026 0.3557 1.0000
7.750 1.3715 0.01381 0.00853 -0.1018 0.3521 1.0000
8.000 1.3938 0.01411 0.00884 -0.1012 0.3491 1.0000
8.250 1.4180 0.01433 0.00908 -0.1010 0.3459 1.0000
8.500 1.4404 0.01463 0.00939 -0.1006 0.3419 1.0000
8.750 1.4608 0.01503 0.00977 -0.0999 0.3381 1.0000
9.000 1.4794 0.01552 0.01025 -0.0990 0.3338 1.0000
9.250 1.5025 0.01582 0.01057 -0.0987 0.3308 1.0000
9.500 1.5239 0.01620 0.01096 -0.0982 0.3265 1.0000
9.750 1.5429 0.01670 0.01145 -0.0974 0.3212 1.0000
10.000 1.5609 0.01726 0.01200 -0.0965 0.3160 1.0000
10.250 1.5807 0.01773 0.01249 -0.0959 0.3103 1.0000
10.500 1.5965 0.01843 0.01315 -0.0948 0.3030 1.0000
10.750 1.6135 0.01909 0.01380 -0.0939 0.2961 1.0000
11.000 1.6266 0.01997 0.01464 -0.0926 0.2871 1.0000
11.250 1.6400 0.02085 0.01550 -0.0914 0.2780 1.0000
11.500 1.6497 0.02197 0.01656 -0.0898 0.2681 1.0000
11.750 1.6599 0.02309 0.01766 -0.0883 0.2594 1.0000
12.000 1.6707 0.02419 0.01874 -0.0870 0.2526 1.0000
12.250 1.6816 0.02532 0.01987 -0.0857 0.2466 1.0000
12.500 1.6890 0.02670 0.02123 -0.0842 0.2401 1.0000
12.750 1.7013 0.02779 0.02234 -0.0832 0.2356 1.0000
13.000 1.7110 0.02909 0.02364 -0.0820 0.2307 1.0000
13.250 1.7170 0.03071 0.02525 -0.0806 0.2258 1.0000
13.500 1.7294 0.03185 0.02643 -0.0798 0.2230 1.0000
13.750 1.7398 0.03317 0.02778 -0.0789 0.2199 1.0000
14.000 1.7485 0.03465 0.02928 -0.0780 0.2167 1.0000
14.250 1.7537 0.03646 0.03111 -0.0768 0.2132 1.0000
14.500 1.7594 0.03827 0.03294 -0.0758 0.2102 1.0000
14.750 1.7709 0.03960 0.03434 -0.0752 0.2083 1.0000
15.000 1.7796 0.04118 0.03595 -0.0745 0.2057 1.0000
15.250 1.7848 0.04310 0.03791 -0.0736 0.2026 1.0000
15.500 1.7860 0.04544 0.04028 -0.0727 0.1993 1.0000
15.750 1.7863 0.04790 0.04277 -0.0717 0.1962 1.0000
16.000 1.7952 0.04958 0.04452 -0.0713 0.1943 1.0000
16.250 1.8008 0.05157 0.04656 -0.0707 0.1917 1.0000
16.500 1.8024 0.05399 0.04902 -0.0701 0.1887 1.0000
16.750 1.7992 0.05696 0.05203 -0.0693 0.1856 1.0000
17.000 1.7936 0.06023 0.05535 -0.0686 0.1825 1.0000
17.250 1.7989 0.06235 0.05753 -0.0683 0.1800 1.0000
17.500 1.7967 0.06531 0.06055 -0.0679 0.1764 1.0000
17.750 1.7887 0.06894 0.06422 -0.0674 0.1726 1.0000
18.000 1.7781 0.07293 0.06826 -0.0670 0.1689 1.0000
18.250 1.7760 0.07599 0.07137 -0.0668 0.1648 1.0000
18.500 1.7635 0.08024 0.07566 -0.0665 0.1596 1.0000
18.750 1.7503 0.08465 0.08011 -0.0664 0.1552 1.0000
19.000 1.7381 0.08899 0.08450 -0.0664 0.1492 1.0000
19.250 1.7190 0.09421 0.08975 -0.0665 0.1428 1.0000
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