GOE 798 AIRFOIL (goe798-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 798 AIRFOIL (goe798-il) Reynolds number: 1,000,000 Max Cl/Cd: 119.99 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe798-il-1000000.txt Download as CSV file: xf-goe798-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.250 -0.6650 0.09501 0.09228 -0.1070 0.9943 0.0390
-18.000 -0.7077 0.08398 0.08107 -0.1150 0.9931 0.0393
-17.750 -0.7449 0.07441 0.07135 -0.1222 0.9910 0.0395
-17.500 -0.7835 0.06534 0.06212 -0.1289 0.9859 0.0397
-17.250 -0.8169 0.05668 0.05330 -0.1358 0.9808 0.0399
-17.000 -0.8463 0.04894 0.04539 -0.1415 0.9731 0.0400
-16.750 -0.8666 0.04234 0.03861 -0.1466 0.9648 0.0401
-16.500 -0.8780 0.03723 0.03333 -0.1508 0.9560 0.0402
-16.250 -0.8827 0.03353 0.02946 -0.1534 0.9478 0.0403
-16.000 -0.8819 0.03084 0.02664 -0.1551 0.9398 0.0405
-15.750 -0.8901 0.02795 0.02361 -0.1555 0.9313 0.0408
-15.500 -0.8912 0.02597 0.02153 -0.1551 0.9237 0.0411
-15.250 -0.8877 0.02458 0.02005 -0.1538 0.9162 0.0414
-15.000 -0.8793 0.02353 0.01893 -0.1525 0.9096 0.0417
-14.750 -0.8687 0.02268 0.01802 -0.1509 0.9023 0.0421
-14.500 -0.8572 0.02198 0.01723 -0.1492 0.8952 0.0424
-14.250 -0.8459 0.02139 0.01658 -0.1472 0.8875 0.0428
-14.000 -0.8297 0.02080 0.01590 -0.1459 0.8798 0.0432
-13.750 -0.8117 0.02022 0.01525 -0.1448 0.8725 0.0436
-13.500 -0.7926 0.01969 0.01463 -0.1438 0.8639 0.0440
-13.250 -0.7724 0.01920 0.01405 -0.1429 0.8556 0.0444
-13.000 -0.7511 0.01876 0.01352 -0.1422 0.8455 0.0447
-12.750 -0.7289 0.01838 0.01303 -0.1415 0.8351 0.0450
-12.500 -0.7127 0.01758 0.01215 -0.1401 0.8221 0.0456
-12.250 -0.6922 0.01704 0.01154 -0.1392 0.8090 0.0462
-12.000 -0.6701 0.01664 0.01105 -0.1385 0.7961 0.0467
-11.500 -0.6233 0.01595 0.01020 -0.1373 0.7738 0.0478
-11.250 -0.5993 0.01567 0.00982 -0.1368 0.7642 0.0485
-11.000 -0.5741 0.01538 0.00947 -0.1364 0.7570 0.0491
-10.750 -0.5485 0.01515 0.00915 -0.1361 0.7500 0.0496
-10.500 -0.5255 0.01473 0.00864 -0.1354 0.7430 0.0504
-10.250 -0.5011 0.01430 0.00820 -0.1350 0.7382 0.0512
-10.000 -0.4757 0.01399 0.00785 -0.1347 0.7328 0.0520
-9.750 -0.4500 0.01374 0.00754 -0.1344 0.7276 0.0528
-9.500 -0.4237 0.01352 0.00725 -0.1341 0.7227 0.0536
-9.250 -0.3966 0.01328 0.00698 -0.1340 0.7195 0.0544
-9.000 -0.3701 0.01299 0.00666 -0.1339 0.7158 0.0553
-8.750 -0.3443 0.01267 0.00632 -0.1336 0.7120 0.0567
-8.500 -0.3177 0.01245 0.00606 -0.1334 0.7081 0.0580
-8.250 -0.2906 0.01229 0.00584 -0.1333 0.7034 0.0593
-8.000 -0.2630 0.01206 0.00560 -0.1332 0.7009 0.0607
-7.750 -0.2359 0.01178 0.00534 -0.1332 0.6980 0.0627
-7.500 -0.2082 0.01159 0.00513 -0.1331 0.6950 0.0648
-7.250 -0.1806 0.01140 0.00494 -0.1331 0.6919 0.0674
-7.000 -0.1528 0.01126 0.00480 -0.1331 0.6887 0.0709
-6.750 -0.1247 0.01118 0.00472 -0.1331 0.6848 0.0751
-6.500 -0.0957 0.01111 0.00466 -0.1333 0.6821 0.0796
-6.250 -0.0664 0.01107 0.00465 -0.1335 0.6797 0.0836
-6.000 -0.0369 0.01105 0.00461 -0.1338 0.6771 0.0868
-5.750 -0.0078 0.01100 0.00459 -0.1340 0.6745 0.0895
-5.500 0.0215 0.01102 0.00459 -0.1342 0.6715 0.0920
-5.250 0.0507 0.01108 0.00459 -0.1344 0.6677 0.0939
-5.000 0.0788 0.01100 0.00449 -0.1344 0.6633 0.0961
-4.750 0.1077 0.01092 0.00444 -0.1346 0.6609 0.0980
-4.500 0.1367 0.01087 0.00440 -0.1348 0.6581 0.0997
-4.250 0.1657 0.01084 0.00435 -0.1350 0.6552 0.1013
-4.000 0.1946 0.01083 0.00431 -0.1352 0.6519 0.1025
-3.750 0.2224 0.01072 0.00417 -0.1351 0.6484 0.1041
-3.500 0.2501 0.01063 0.00406 -0.1352 0.6441 0.1059
-3.250 0.2786 0.01053 0.00398 -0.1353 0.6420 0.1074
-3.000 0.3072 0.01044 0.00391 -0.1354 0.6393 0.1087
-2.750 0.3358 0.01037 0.00384 -0.1356 0.6364 0.1100
-2.500 0.3642 0.01032 0.00377 -0.1357 0.6331 0.1113
-2.250 0.3923 0.01030 0.00372 -0.1357 0.6294 0.1123
-2.000 0.4201 0.01031 0.00367 -0.1357 0.6247 0.1131
-1.750 0.4475 0.01011 0.00351 -0.1357 0.6220 0.1152
-1.500 0.4756 0.01000 0.00343 -0.1357 0.6187 0.1170
-1.250 0.5037 0.00994 0.00338 -0.1358 0.6155 0.1186
-1.000 0.5316 0.00991 0.00334 -0.1358 0.6123 0.1201
-0.750 0.5591 0.00990 0.00330 -0.1358 0.6089 0.1216
-0.500 0.5868 0.00990 0.00328 -0.1358 0.6052 0.1225
-0.250 0.6151 0.00985 0.00325 -0.1359 0.6027 0.1233
0.000 0.6430 0.00978 0.00319 -0.1359 0.5996 0.1250
0.250 0.6705 0.00972 0.00315 -0.1359 0.5961 0.1271
0.500 0.6975 0.00970 0.00313 -0.1357 0.5923 0.1291
0.750 0.7238 0.00972 0.00313 -0.1355 0.5881 0.1313
1.000 0.7513 0.00971 0.00313 -0.1355 0.5847 0.1336
1.250 0.7788 0.00968 0.00313 -0.1354 0.5807 0.1369
1.500 0.8051 0.00965 0.00314 -0.1352 0.5761 0.1442
1.750 0.8300 0.00963 0.00317 -0.1347 0.5712 0.1640
2.000 0.8550 0.00952 0.00324 -0.1343 0.5668 0.2240
2.250 0.8811 0.00940 0.00330 -0.1341 0.5623 0.2808
2.500 0.9056 0.00928 0.00337 -0.1336 0.5569 0.3519
2.750 0.9272 0.00909 0.00348 -0.1326 0.5510 0.4784
3.000 0.9498 0.00875 0.00362 -0.1319 0.5459 0.6474
3.250 0.9677 0.00843 0.00377 -0.1299 0.5396 0.8084
3.500 0.9859 0.00844 0.00408 -0.1275 0.5323 0.9591
3.750 1.0260 0.00864 0.00426 -0.1303 0.5244 0.9862
4.250 1.1027 0.00919 0.00468 -0.1354 0.5012 1.0000
4.500 1.1073 0.00938 0.00481 -0.1308 0.4894 1.0000
4.750 1.1136 0.00967 0.00502 -0.1266 0.4752 1.0000
5.000 1.1230 0.01004 0.00530 -0.1231 0.4588 1.0000
5.250 1.1344 0.01048 0.00564 -0.1202 0.4411 1.0000
5.500 1.1458 0.01099 0.00605 -0.1174 0.4229 1.0000
5.750 1.1578 0.01155 0.00651 -0.1149 0.4056 1.0000
6.000 1.1717 0.01208 0.00697 -0.1127 0.3909 1.0000
6.250 1.1874 0.01259 0.00742 -0.1109 0.3794 1.0000
6.500 1.2012 0.01320 0.00795 -0.1089 0.3691 1.0000
6.750 1.2198 0.01364 0.00836 -0.1077 0.3620 1.0000
7.000 1.2349 0.01423 0.00891 -0.1059 0.3550 1.0000
7.250 1.2529 0.01473 0.00939 -0.1047 0.3498 1.0000
7.500 1.2721 0.01518 0.00984 -0.1037 0.3457 1.0000
7.750 1.2891 0.01575 0.01040 -0.1025 0.3413 1.0000
8.000 1.3045 0.01641 0.01103 -0.1010 0.3363 1.0000
8.250 1.3217 0.01699 0.01161 -0.0998 0.3326 1.0000
8.500 1.3412 0.01748 0.01211 -0.0990 0.3298 1.0000
8.750 1.3597 0.01803 0.01267 -0.0981 0.3269 1.0000
9.000 1.3761 0.01870 0.01334 -0.0970 0.3240 1.0000
9.250 1.3916 0.01944 0.01407 -0.0957 0.3210 1.0000
9.500 1.4050 0.02030 0.01492 -0.0943 0.3174 1.0000
9.750 1.4224 0.02096 0.01561 -0.0934 0.3152 1.0000
10.000 1.4422 0.02150 0.01618 -0.0928 0.3132 1.0000
10.250 1.4600 0.02217 0.01687 -0.0920 0.3105 1.0000
10.500 1.4761 0.02296 0.01768 -0.0911 0.3079 1.0000
10.750 1.4914 0.02381 0.01853 -0.0901 0.3052 1.0000
11.000 1.5038 0.02487 0.01959 -0.0888 0.3022 1.0000
11.250 1.5157 0.02595 0.02067 -0.0875 0.2988 1.0000
11.500 1.5342 0.02665 0.02142 -0.0870 0.2975 1.0000
11.750 1.5521 0.02739 0.02220 -0.0865 0.2956 1.0000
12.000 1.5693 0.02817 0.02301 -0.0859 0.2933 1.0000
12.250 1.5839 0.02916 0.02403 -0.0850 0.2905 1.0000
12.500 1.5971 0.03025 0.02513 -0.0841 0.2876 1.0000
12.750 1.6079 0.03154 0.02642 -0.0830 0.2844 1.0000
13.000 1.6197 0.03273 0.02763 -0.0820 0.2815 1.0000
13.250 1.6376 0.03350 0.02846 -0.0816 0.2794 1.0000
13.500 1.6528 0.03449 0.02948 -0.0810 0.2765 1.0000
13.750 1.6657 0.03566 0.03068 -0.0802 0.2729 1.0000
14.000 1.6758 0.03704 0.03205 -0.0793 0.2689 1.0000
14.250 1.6843 0.03858 0.03361 -0.0782 0.2650 1.0000
14.500 1.7003 0.03951 0.03460 -0.0778 0.2616 1.0000
14.750 1.7114 0.04084 0.03594 -0.0770 0.2560 1.0000
15.000 1.7149 0.04283 0.03791 -0.0757 0.2493 1.0000
15.250 1.7262 0.04415 0.03925 -0.0750 0.2413 1.0000
15.500 1.7268 0.04643 0.04149 -0.0736 0.2304 1.0000
15.750 1.7246 0.04895 0.04394 -0.0720 0.2149 1.0000
16.000 1.7151 0.05215 0.04705 -0.0701 0.1979 1.0000
16.250 1.7078 0.05521 0.05005 -0.0684 0.1859 1.0000
16.500 1.7033 0.05805 0.05286 -0.0670 0.1773 1.0000
16.750 1.7039 0.06051 0.05533 -0.0660 0.1721 1.0000
17.000 1.7025 0.06315 0.05796 -0.0650 0.1672 1.0000
17.250 1.7043 0.06551 0.06036 -0.0642 0.1635 1.0000
17.500 1.7079 0.06773 0.06262 -0.0635 0.1605 1.0000
17.750 1.7093 0.07016 0.06507 -0.0628 0.1573 1.0000
18.000 1.7058 0.07319 0.06812 -0.0620 0.1539 1.0000
18.250 1.7096 0.07543 0.07040 -0.0615 0.1515 1.0000
18.500 1.7139 0.07764 0.07268 -0.0612 0.1497 1.0000
18.750 1.7170 0.07998 0.07507 -0.0608 0.1474 1.0000
19.000 1.7176 0.08260 0.07772 -0.0604 0.1450 1.0000
19.250 1.7135 0.08581 0.08097 -0.0599 0.1423 1.0000
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