GOE 390 AIRFOIL (goe390-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 390 AIRFOIL (goe390-il) Reynolds number: 1,000,000 Max Cl/Cd: 98.88 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe390-il-1000000-n5.txt Download as CSV file: xf-goe390-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 390 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.750 -0.4837 0.10952 0.10672 -0.0876 0.9139 0.0263
-17.500 -0.5182 0.10057 0.09759 -0.0924 0.8981 0.0265
-17.250 -0.5423 0.09358 0.09041 -0.0962 0.8768 0.0266
-17.000 -0.5629 0.08717 0.08382 -0.0999 0.8577 0.0267
-16.750 -0.5851 0.08060 0.07709 -0.1040 0.8431 0.0267
-16.500 -0.6161 0.07304 0.06937 -0.1090 0.8325 0.0268
-16.250 -0.6582 0.06426 0.06041 -0.1150 0.8225 0.0268
-16.000 -0.7211 0.05261 0.04855 -0.1234 0.8142 0.0268
-15.750 -0.7859 0.03909 0.03472 -0.1348 0.8055 0.0267
-15.500 -0.8045 0.03111 0.02646 -0.1442 0.7971 0.0268
-15.250 -0.8048 0.02744 0.02263 -0.1486 0.7909 0.0268
-15.000 -0.7985 0.02554 0.02061 -0.1496 0.7842 0.0269
-14.750 -0.7887 0.02429 0.01925 -0.1493 0.7776 0.0270
-14.500 -0.7780 0.02338 0.01825 -0.1482 0.7725 0.0271
-14.250 -0.7614 0.02256 0.01734 -0.1477 0.7669 0.0272
-14.000 -0.7446 0.02171 0.01641 -0.1471 0.7605 0.0273
-13.750 -0.7278 0.02087 0.01547 -0.1465 0.7539 0.0275
-13.500 -0.7085 0.02011 0.01465 -0.1459 0.7489 0.0277
-13.250 -0.6879 0.01943 0.01391 -0.1454 0.7431 0.0278
-13.000 -0.6664 0.01884 0.01325 -0.1449 0.7369 0.0280
-12.750 -0.6440 0.01831 0.01264 -0.1445 0.7313 0.0282
-12.500 -0.6206 0.01779 0.01208 -0.1441 0.7258 0.0284
-12.250 -0.5969 0.01733 0.01156 -0.1437 0.7193 0.0286
-12.000 -0.5730 0.01691 0.01107 -0.1432 0.7128 0.0288
-11.750 -0.5482 0.01649 0.01060 -0.1429 0.7071 0.0290
-11.500 -0.5233 0.01611 0.01016 -0.1425 0.7000 0.0292
-11.250 -0.4984 0.01577 0.00974 -0.1421 0.6924 0.0294
-11.000 -0.4728 0.01542 0.00934 -0.1418 0.6862 0.0296
-10.750 -0.4472 0.01510 0.00896 -0.1415 0.6785 0.0299
-10.500 -0.4218 0.01482 0.00860 -0.1411 0.6704 0.0301
-10.250 -0.3956 0.01453 0.00825 -0.1408 0.6630 0.0303
-10.000 -0.3697 0.01428 0.00793 -0.1404 0.6549 0.0306
-9.750 -0.3433 0.01403 0.00762 -0.1401 0.6480 0.0308
-9.500 -0.3172 0.01374 0.00727 -0.1398 0.6409 0.0311
-9.250 -0.2913 0.01347 0.00695 -0.1394 0.6339 0.0315
-9.000 -0.2647 0.01322 0.00666 -0.1392 0.6287 0.0319
-8.750 -0.2376 0.01297 0.00639 -0.1390 0.6242 0.0323
-8.500 -0.2105 0.01276 0.00614 -0.1387 0.6194 0.0328
-8.250 -0.1835 0.01257 0.00591 -0.1385 0.6144 0.0333
-8.000 -0.1564 0.01239 0.00569 -0.1382 0.6100 0.0338
-7.750 -0.1285 0.01220 0.00547 -0.1381 0.6072 0.0343
-7.500 -0.1008 0.01201 0.00526 -0.1380 0.6037 0.0349
-7.250 -0.0733 0.01181 0.00505 -0.1379 0.5997 0.0359
-7.000 -0.0460 0.01165 0.00487 -0.1377 0.5953 0.0369
-6.750 -0.0187 0.01152 0.00470 -0.1374 0.5906 0.0380
-6.500 0.0093 0.01136 0.00453 -0.1373 0.5874 0.0392
-6.250 0.0374 0.01120 0.00437 -0.1373 0.5842 0.0409
-6.000 0.0654 0.01107 0.00423 -0.1372 0.5804 0.0427
-5.750 0.0931 0.01094 0.00410 -0.1370 0.5764 0.0451
-5.500 0.1207 0.01085 0.00399 -0.1369 0.5721 0.0476
-5.250 0.1486 0.01075 0.00390 -0.1367 0.5682 0.0505
-5.000 0.1771 0.01066 0.00381 -0.1367 0.5641 0.0532
-4.750 0.2052 0.01059 0.00374 -0.1366 0.5590 0.0558
-4.500 0.2329 0.01054 0.00366 -0.1365 0.5538 0.0579
-4.250 0.2605 0.01051 0.00361 -0.1363 0.5492 0.0601
-4.000 0.2891 0.01045 0.00355 -0.1363 0.5450 0.0620
-3.750 0.3171 0.01040 0.00349 -0.1362 0.5396 0.0639
-3.500 0.3445 0.01038 0.00344 -0.1360 0.5335 0.0657
-3.250 0.3721 0.01036 0.00340 -0.1359 0.5277 0.0674
-3.000 0.3998 0.01034 0.00335 -0.1357 0.5203 0.0687
-2.750 0.4261 0.01034 0.00331 -0.1353 0.5116 0.0702
-2.500 0.4536 0.01032 0.00328 -0.1352 0.5039 0.0717
-2.250 0.4799 0.01035 0.00326 -0.1348 0.4947 0.0731
-2.000 0.5068 0.01038 0.00325 -0.1346 0.4865 0.0744
-1.750 0.5326 0.01040 0.00323 -0.1341 0.4769 0.0767
-1.500 0.5587 0.01043 0.00323 -0.1337 0.4682 0.0790
-1.250 0.5842 0.01051 0.00325 -0.1332 0.4584 0.0809
-1.000 0.6100 0.01053 0.00326 -0.1328 0.4506 0.0835
-0.750 0.6357 0.01057 0.00328 -0.1324 0.4433 0.0863
-0.500 0.6608 0.01064 0.00332 -0.1319 0.4366 0.0902
-0.250 0.6870 0.01063 0.00334 -0.1316 0.4316 0.1003
0.000 0.7123 0.01064 0.00343 -0.1311 0.4257 0.1294
0.250 0.7369 0.01074 0.00352 -0.1305 0.4196 0.1385
0.500 0.7627 0.01081 0.00358 -0.1301 0.4156 0.1445
0.750 0.7885 0.01086 0.00365 -0.1297 0.4118 0.1500
1.000 0.8128 0.01095 0.00372 -0.1291 0.4075 0.1539
1.250 0.8354 0.01106 0.00381 -0.1281 0.4030 0.1565
1.500 0.8577 0.01117 0.00391 -0.1270 0.3988 0.1603
1.750 0.8823 0.01122 0.00398 -0.1265 0.3962 0.1645
2.000 0.9067 0.01131 0.00408 -0.1259 0.3929 0.1691
2.250 0.9306 0.01143 0.00420 -0.1252 0.3892 0.1744
2.500 0.9543 0.01158 0.00435 -0.1245 0.3851 0.1820
2.750 0.9776 0.01176 0.00454 -0.1239 0.3806 0.1919
3.000 1.0032 0.01183 0.00468 -0.1236 0.3778 0.2153
3.250 1.0282 0.01190 0.00486 -0.1233 0.3745 0.2565
3.500 1.0526 0.01201 0.00505 -0.1229 0.3712 0.2932
3.750 1.0765 0.01213 0.00526 -0.1225 0.3679 0.3345
4.000 1.0997 0.01222 0.00552 -0.1220 0.3643 0.4156
4.250 1.1234 0.01227 0.00580 -0.1216 0.3612 0.5123
4.500 1.1481 0.01235 0.00603 -0.1213 0.3589 0.5697
4.750 1.1724 0.01244 0.00626 -0.1210 0.3562 0.6238
5.250 1.2143 0.01228 0.00691 -0.1189 0.3497 1.0000
5.500 1.2352 0.01262 0.00721 -0.1180 0.3459 1.0000
5.750 1.2573 0.01292 0.00750 -0.1173 0.3432 1.0000
6.000 1.2802 0.01319 0.00777 -0.1168 0.3409 1.0000
6.250 1.3022 0.01350 0.00807 -0.1162 0.3378 1.0000
6.500 1.3234 0.01386 0.00841 -0.1155 0.3341 1.0000
6.750 1.3429 0.01430 0.00882 -0.1146 0.3302 1.0000
7.000 1.3622 0.01476 0.00927 -0.1136 0.3267 1.0000
7.250 1.3842 0.01511 0.00962 -0.1131 0.3243 1.0000
7.500 1.4047 0.01553 0.01004 -0.1124 0.3209 1.0000
7.750 1.4240 0.01602 0.01052 -0.1116 0.3169 1.0000
8.000 1.4414 0.01662 0.01109 -0.1106 0.3125 1.0000
8.250 1.4596 0.01720 0.01166 -0.1098 0.3090 1.0000
8.500 1.4795 0.01769 0.01217 -0.1091 0.3058 1.0000
8.750 1.4975 0.01830 0.01278 -0.1083 0.3020 1.0000
9.000 1.5138 0.01902 0.01348 -0.1073 0.2976 1.0000
9.250 1.5287 0.01983 0.01428 -0.1063 0.2932 1.0000
9.500 1.5464 0.02050 0.01496 -0.1055 0.2894 1.0000
9.750 1.5618 0.02131 0.01576 -0.1046 0.2845 1.0000
10.000 1.5743 0.02233 0.01676 -0.1034 0.2795 1.0000
10.250 1.5897 0.02317 0.01761 -0.1025 0.2758 1.0000
10.500 1.6042 0.02408 0.01854 -0.1016 0.2718 1.0000
10.750 1.6174 0.02510 0.01955 -0.1006 0.2672 1.0000
11.000 1.6272 0.02638 0.02082 -0.0994 0.2626 1.0000
11.250 1.6417 0.02734 0.02180 -0.0986 0.2592 1.0000
11.500 1.6540 0.02847 0.02294 -0.0976 0.2549 1.0000
11.750 1.6626 0.02988 0.02435 -0.0964 0.2500 1.0000
12.000 1.6722 0.03125 0.02571 -0.0954 0.2459 1.0000
12.250 1.6835 0.03252 0.02701 -0.0945 0.2422 1.0000
12.500 1.6937 0.03387 0.02838 -0.0936 0.2384 1.0000
12.750 1.7000 0.03559 0.03010 -0.0924 0.2344 1.0000
13.000 1.7088 0.03708 0.03161 -0.0915 0.2311 1.0000
13.250 1.7184 0.03857 0.03314 -0.0907 0.2284 1.0000
13.500 1.7276 0.04009 0.03467 -0.0899 0.2252 1.0000
13.750 1.7333 0.04196 0.03656 -0.0890 0.2219 1.0000
14.000 1.7380 0.04390 0.03852 -0.0880 0.2184 1.0000
14.250 1.7447 0.04570 0.04036 -0.0872 0.2159 1.0000
14.500 1.7530 0.04736 0.04206 -0.0866 0.2132 1.0000
14.750 1.7584 0.04931 0.04404 -0.0858 0.2102 1.0000
15.000 1.7610 0.05155 0.04629 -0.0850 0.2069 1.0000
15.250 1.7613 0.05401 0.04878 -0.0840 0.2035 1.0000
15.500 1.7676 0.05592 0.05074 -0.0835 0.2014 1.0000
15.750 1.7740 0.05780 0.05265 -0.0829 0.1988 1.0000
16.000 1.7751 0.06028 0.05516 -0.0822 0.1959 1.0000
16.250 1.7750 0.06285 0.05775 -0.0815 0.1924 1.0000
16.500 1.7712 0.06587 0.06080 -0.0807 0.1891 1.0000
16.750 1.7767 0.06790 0.06288 -0.0803 0.1865 1.0000
17.000 1.7768 0.07053 0.06555 -0.0798 0.1833 1.0000
17.250 1.7756 0.07333 0.06838 -0.0793 0.1803 1.0000
17.500 1.7706 0.07657 0.07166 -0.0788 0.1774 1.0000
17.750 1.7709 0.07924 0.07438 -0.0785 0.1751 1.0000
18.000 1.7727 0.08175 0.07693 -0.0783 0.1725 1.0000
18.250 1.7699 0.08481 0.08003 -0.0780 0.1695 1.0000
18.500 1.7648 0.08814 0.08340 -0.0778 0.1665 1.0000
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