GOE 798 AIRFOIL (goe798-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: GOE 798 AIRFOIL (goe798-il) Reynolds number: 500,000 Max Cl/Cd: 83.79 at α=4.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-goe798-il-500000-n5.txt Download as CSV file: xf-goe798-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: GOE 798 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
------ -------- --------- --------- -------- -------- --------
-16.750 -0.5638 0.08575 0.08202 -0.1168 0.9559 0.0406
-16.500 -0.6254 0.07353 0.06955 -0.1243 0.9499 0.0409
-16.250 -0.6736 0.06376 0.05958 -0.1304 0.9420 0.0411
-16.000 -0.7158 0.05472 0.05032 -0.1362 0.9340 0.0412
-15.750 -0.7469 0.04660 0.04198 -0.1422 0.9251 0.0413
-15.500 -0.7659 0.04003 0.03521 -0.1478 0.9166 0.0415
-15.250 -0.7760 0.03521 0.03022 -0.1520 0.9071 0.0417
-15.000 -0.7801 0.03203 0.02688 -0.1540 0.8985 0.0419
-14.750 -0.7797 0.02979 0.02453 -0.1546 0.8893 0.0421
-14.500 -0.7763 0.02815 0.02277 -0.1541 0.8809 0.0424
-14.250 -0.7698 0.02685 0.02137 -0.1532 0.8717 0.0427
-14.000 -0.7618 0.02579 0.02018 -0.1518 0.8627 0.0430
-13.750 -0.7526 0.02487 0.01917 -0.1502 0.8522 0.0433
-13.500 -0.7441 0.02415 0.01833 -0.1480 0.8416 0.0437
-13.250 -0.7301 0.02344 0.01750 -0.1466 0.8298 0.0441
-13.000 -0.7141 0.02278 0.01673 -0.1454 0.8186 0.0445
-12.750 -0.6966 0.02219 0.01600 -0.1443 0.8070 0.0450
-12.500 -0.6778 0.02163 0.01532 -0.1433 0.7958 0.0455
-12.250 -0.6580 0.02114 0.01468 -0.1424 0.7855 0.0459
-12.000 -0.6400 0.02050 0.01397 -0.1413 0.7754 0.0464
-11.750 -0.6204 0.01997 0.01335 -0.1404 0.7666 0.0469
-11.500 -0.5993 0.01948 0.01279 -0.1396 0.7582 0.0474
-11.000 -0.5548 0.01864 0.01177 -0.1383 0.7444 0.0486
-10.750 -0.5316 0.01824 0.01130 -0.1377 0.7386 0.0492
-10.500 -0.5080 0.01788 0.01084 -0.1372 0.7332 0.0499
-10.250 -0.4839 0.01755 0.01041 -0.1367 0.7285 0.0505
-10.000 -0.4596 0.01716 0.00997 -0.1363 0.7244 0.0512
-9.750 -0.4356 0.01675 0.00954 -0.1359 0.7199 0.0521
-9.500 -0.4110 0.01641 0.00916 -0.1355 0.7154 0.0530
-9.250 -0.3859 0.01612 0.00879 -0.1351 0.7111 0.0539
-9.000 -0.3603 0.01583 0.00845 -0.1348 0.7074 0.0549
-8.750 -0.3342 0.01555 0.00812 -0.1346 0.7042 0.0558
-8.500 -0.3083 0.01525 0.00779 -0.1343 0.7008 0.0568
-8.250 -0.2823 0.01496 0.00749 -0.1341 0.6975 0.0581
-8.000 -0.2559 0.01472 0.00720 -0.1339 0.6942 0.0596
-7.750 -0.2294 0.01450 0.00693 -0.1337 0.6910 0.0612
-7.500 -0.2027 0.01429 0.00670 -0.1336 0.6878 0.0633
-7.250 -0.1755 0.01407 0.00649 -0.1335 0.6850 0.0658
-7.000 -0.1481 0.01389 0.00631 -0.1335 0.6819 0.0686
-6.750 -0.1204 0.01375 0.00619 -0.1335 0.6790 0.0720
-6.500 -0.0924 0.01365 0.00609 -0.1335 0.6761 0.0756
-6.250 -0.0644 0.01358 0.00599 -0.1335 0.6733 0.0797
-6.000 -0.0362 0.01354 0.00592 -0.1336 0.6705 0.0829
-5.750 -0.0079 0.01351 0.00584 -0.1336 0.6676 0.0862
-5.500 0.0204 0.01342 0.00574 -0.1337 0.6651 0.0887
-5.250 0.0487 0.01335 0.00567 -0.1338 0.6625 0.0907
-5.000 0.0770 0.01329 0.00560 -0.1339 0.6598 0.0928
-4.750 0.1053 0.01323 0.00551 -0.1339 0.6571 0.0949
-4.500 0.1334 0.01319 0.00541 -0.1339 0.6538 0.0966
-4.250 0.1606 0.01308 0.00528 -0.1338 0.6502 0.0983
-4.000 0.1883 0.01302 0.00520 -0.1338 0.6467 0.0999
-3.750 0.2162 0.01292 0.00512 -0.1338 0.6434 0.1015
-3.500 0.2440 0.01284 0.00503 -0.1338 0.6399 0.1030
-3.250 0.2717 0.01279 0.00494 -0.1338 0.6362 0.1044
-3.000 0.2995 0.01276 0.00485 -0.1337 0.6328 0.1055
-2.750 0.3263 0.01263 0.00471 -0.1336 0.6296 0.1070
-2.500 0.3536 0.01253 0.00463 -0.1335 0.6263 0.1086
-2.250 0.3811 0.01244 0.00457 -0.1335 0.6224 0.1103
-2.000 0.4083 0.01238 0.00450 -0.1334 0.6184 0.1120
-1.750 0.4354 0.01233 0.00443 -0.1332 0.6146 0.1133
-1.500 0.4623 0.01231 0.00437 -0.1330 0.6107 0.1147
-1.250 0.4894 0.01228 0.00433 -0.1329 0.6067 0.1158
-1.000 0.5160 0.01217 0.00425 -0.1327 0.6023 0.1175
-0.750 0.5425 0.01211 0.00420 -0.1325 0.5981 0.1189
-0.500 0.5688 0.01207 0.00415 -0.1322 0.5941 0.1201
-0.250 0.5949 0.01206 0.00412 -0.1319 0.5903 0.1212
0.000 0.6217 0.01202 0.00411 -0.1317 0.5864 0.1225
0.250 0.6482 0.01200 0.00410 -0.1315 0.5821 0.1239
0.500 0.6741 0.01200 0.00409 -0.1312 0.5779 0.1253
0.750 0.6995 0.01203 0.00409 -0.1307 0.5736 0.1268
1.000 0.7251 0.01203 0.00411 -0.1303 0.5696 0.1291
1.250 0.7508 0.01202 0.00414 -0.1300 0.5650 0.1323
1.500 0.7755 0.01204 0.00417 -0.1294 0.5598 0.1364
1.750 0.7989 0.01208 0.00422 -0.1286 0.5546 0.1431
2.000 0.8231 0.01207 0.00428 -0.1280 0.5496 0.1587
2.250 0.8463 0.01203 0.00437 -0.1272 0.5434 0.1952
2.500 0.8657 0.01204 0.00446 -0.1257 0.5369 0.2297
2.750 0.8858 0.01205 0.00456 -0.1243 0.5302 0.2637
3.000 0.9045 0.01209 0.00469 -0.1226 0.5217 0.3009
3.250 0.9237 0.01214 0.00486 -0.1212 0.5131 0.3566
3.500 0.9432 0.01212 0.00510 -0.1199 0.5028 0.4617
3.750 0.9620 0.01199 0.00540 -0.1185 0.4928 0.6211
4.000 0.9763 0.01190 0.00576 -0.1161 0.4815 0.7846
4.250 1.0105 0.01206 0.00624 -0.1174 0.4676 0.9947
4.500 1.0263 0.01244 0.00654 -0.1154 0.4546 1.0000
4.750 1.0383 0.01289 0.00691 -0.1127 0.4413 1.0000
5.250 1.0644 0.01390 0.00777 -0.1080 0.4146 1.0000
5.500 1.0771 0.01449 0.00828 -0.1058 0.4023 1.0000
5.750 1.0890 0.01515 0.00886 -0.1035 0.3904 1.0000
6.000 1.1040 0.01574 0.00939 -0.1017 0.3800 1.0000
6.250 1.1170 0.01644 0.01003 -0.0997 0.3709 1.0000
6.500 1.1327 0.01705 0.01060 -0.0982 0.3629 1.0000
6.750 1.1459 0.01779 0.01129 -0.0964 0.3555 1.0000
7.000 1.1626 0.01840 0.01188 -0.0951 0.3500 1.0000
7.250 1.1794 0.01902 0.01249 -0.0939 0.3449 1.0000
7.500 1.1943 0.01975 0.01320 -0.0925 0.3403 1.0000
7.750 1.2085 0.02055 0.01397 -0.0911 0.3359 1.0000
8.000 1.2267 0.02114 0.01457 -0.0902 0.3328 1.0000
8.250 1.2437 0.02181 0.01525 -0.0892 0.3295 1.0000
8.500 1.2600 0.02254 0.01598 -0.0881 0.3260 1.0000
8.750 1.2745 0.02339 0.01682 -0.0869 0.3224 1.0000
9.000 1.2884 0.02430 0.01772 -0.0857 0.3189 1.0000
9.250 1.3043 0.02511 0.01854 -0.0847 0.3163 1.0000
9.500 1.3220 0.02582 0.01929 -0.0840 0.3143 1.0000
9.750 1.3392 0.02657 0.02006 -0.0832 0.3120 1.0000
10.000 1.3551 0.02742 0.02093 -0.0824 0.3093 1.0000
10.250 1.3701 0.02834 0.02186 -0.0814 0.3065 1.0000
10.500 1.3840 0.02935 0.02287 -0.0805 0.3036 1.0000
10.750 1.3960 0.03052 0.02403 -0.0793 0.3002 1.0000
11.000 1.4120 0.03140 0.02495 -0.0786 0.2976 1.0000
11.250 1.4283 0.03228 0.02588 -0.0780 0.2954 1.0000
11.500 1.4440 0.03321 0.02685 -0.0773 0.2930 1.0000
11.750 1.4587 0.03421 0.02787 -0.0766 0.2900 1.0000
12.000 1.4714 0.03539 0.02907 -0.0757 0.2869 1.0000
12.250 1.4831 0.03665 0.03033 -0.0748 0.2838 1.0000
12.500 1.4959 0.03782 0.03152 -0.0740 0.2810 1.0000
12.750 1.5112 0.03884 0.03260 -0.0734 0.2785 1.0000
13.000 1.5254 0.03992 0.03373 -0.0728 0.2756 1.0000
13.250 1.5386 0.04109 0.03493 -0.0721 0.2723 1.0000
13.500 1.5488 0.04252 0.03638 -0.0712 0.2686 1.0000
13.750 1.5574 0.04410 0.03796 -0.0703 0.2649 1.0000
14.000 1.5718 0.04520 0.03913 -0.0698 0.2612 1.0000
14.250 1.5826 0.04664 0.04061 -0.0691 0.2564 1.0000
14.500 1.5902 0.04836 0.04234 -0.0683 0.2515 1.0000
14.750 1.5997 0.04991 0.04391 -0.0675 0.2469 1.0000
15.000 1.6080 0.05159 0.04564 -0.0668 0.2404 1.0000
15.250 1.6115 0.05375 0.04779 -0.0658 0.2331 1.0000
15.500 1.6162 0.05581 0.04987 -0.0650 0.2236 1.0000
15.750 1.6163 0.05834 0.05237 -0.0640 0.2131 1.0000
16.000 1.6127 0.06127 0.05527 -0.0629 0.2020 1.0000
16.500 1.6053 0.06722 0.06119 -0.0608 0.1842 1.0000
16.750 1.6013 0.07028 0.06424 -0.0599 0.1776 1.0000
17.000 1.6005 0.07306 0.06705 -0.0593 0.1724 1.0000
17.250 1.5965 0.07618 0.07017 -0.0585 0.1670 1.0000
17.500 1.5946 0.07913 0.07315 -0.0580 0.1627 1.0000
17.750 1.5955 0.08179 0.07584 -0.0576 0.1585 1.0000
18.000 1.5916 0.08503 0.07912 -0.0571 0.1549 1.0000
18.250 1.5894 0.08810 0.08222 -0.0568 0.1518 1.0000
18.500 1.5928 0.09056 0.08474 -0.0567 0.1496 1.0000
18.750 1.5955 0.09308 0.08732 -0.0566 0.1469 1.0000
19.000 1.5944 0.09608 0.09037 -0.0565 0.1442 1.0000
19.250 1.5920 0.09925 0.09359 -0.0565 0.1416 1.0000
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