GOE 498 AIRFOIL (goe498-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: GOE 498 AIRFOIL (goe498-il) Reynolds number: 1,000,000 Max Cl/Cd: 123.83 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-goe498-il-1000000.txt Download as CSV file: xf-goe498-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: GOE 498 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
------ -------- --------- --------- -------- -------- --------
-19.000 -0.7437 0.11358 0.11101 -0.0695 1.0000 0.0305
-18.750 -0.7648 0.10667 0.10402 -0.0733 1.0000 0.0308
-18.500 -0.7819 0.10065 0.09792 -0.0765 1.0000 0.0310
-18.250 -0.7986 0.09482 0.09201 -0.0797 1.0000 0.0313
-18.000 -0.8150 0.08921 0.08633 -0.0826 1.0000 0.0315
-17.750 -0.8311 0.08379 0.08083 -0.0854 1.0000 0.0318
-17.500 -0.8465 0.07863 0.07558 -0.0880 1.0000 0.0320
-17.250 -0.8593 0.07411 0.07100 -0.0901 1.0000 0.0322
-17.000 -0.8736 0.06954 0.06635 -0.0922 1.0000 0.0324
-16.750 -0.8882 0.06520 0.06194 -0.0939 1.0000 0.0325
-16.500 -0.9056 0.06088 0.05754 -0.0954 1.0000 0.0327
-16.250 -0.9252 0.05701 0.05361 -0.0961 1.0000 0.0327
-16.000 -0.9375 0.05281 0.04933 -0.0987 0.9995 0.0329
-15.750 -0.9389 0.04775 0.04420 -0.1049 0.9975 0.0333
-15.500 -0.9364 0.04284 0.03922 -0.1115 0.9948 0.0336
-15.250 -0.9305 0.03821 0.03452 -0.1181 0.9919 0.0339
-15.000 -0.9247 0.03382 0.03003 -0.1241 0.9869 0.0343
-14.750 -0.9096 0.02995 0.02607 -0.1308 0.9834 0.0346
-14.500 -0.8945 0.02603 0.02204 -0.1381 0.9787 0.0350
-14.250 -0.8716 0.02316 0.01903 -0.1442 0.9732 0.0355
-14.000 -0.8434 0.02177 0.01756 -0.1471 0.9710 0.0360
-13.750 -0.8129 0.02066 0.01637 -0.1497 0.9694 0.0365
-13.500 -0.7800 0.01984 0.01546 -0.1521 0.9683 0.0369
-13.250 -0.7603 0.01859 0.01415 -0.1529 0.9625 0.0376
-13.000 -0.7321 0.01768 0.01321 -0.1543 0.9589 0.0383
-12.750 -0.7004 0.01697 0.01246 -0.1560 0.9563 0.0390
-12.500 -0.6669 0.01633 0.01177 -0.1579 0.9539 0.0397
-12.250 -0.6443 0.01585 0.01124 -0.1574 0.9476 0.0403
-12.000 -0.6154 0.01540 0.01072 -0.1580 0.9429 0.0410
-11.750 -0.5843 0.01484 0.01009 -0.1592 0.9387 0.0418
-11.500 -0.5635 0.01425 0.00947 -0.1584 0.9316 0.0427
-11.250 -0.5365 0.01382 0.00901 -0.1585 0.9257 0.0436
-11.000 -0.5084 0.01347 0.00860 -0.1588 0.9202 0.0445
-10.750 -0.4847 0.01316 0.00824 -0.1580 0.9139 0.0453
-10.500 -0.4575 0.01289 0.00790 -0.1579 0.9080 0.0461
-10.250 -0.4321 0.01242 0.00739 -0.1577 0.9022 0.0475
-10.000 -0.4079 0.01213 0.00710 -0.1570 0.8958 0.0487
-9.750 -0.3810 0.01190 0.00682 -0.1568 0.8895 0.0500
-9.500 -0.3537 0.01170 0.00655 -0.1566 0.8836 0.0512
-9.250 -0.3294 0.01134 0.00618 -0.1559 0.8767 0.0527
-9.000 -0.3027 0.01110 0.00591 -0.1556 0.8695 0.0542
-8.750 -0.2761 0.01092 0.00569 -0.1552 0.8624 0.0558
-8.500 -0.2493 0.01077 0.00549 -0.1548 0.8540 0.0571
-8.250 -0.2233 0.01047 0.00516 -0.1544 0.8458 0.0591
-8.000 -0.1969 0.01030 0.00498 -0.1540 0.8357 0.0609
-7.750 -0.1701 0.01019 0.00480 -0.1536 0.8251 0.0626
-7.500 -0.1441 0.01000 0.00454 -0.1530 0.8124 0.0644
-7.250 -0.1181 0.00980 0.00432 -0.1525 0.7997 0.0664
-7.000 -0.0918 0.00970 0.00415 -0.1520 0.7869 0.0682
-6.500 -0.0395 0.00945 0.00376 -0.1509 0.7621 0.0719
-6.250 -0.0135 0.00933 0.00358 -0.1504 0.7512 0.0742
-6.000 0.0134 0.00923 0.00344 -0.1500 0.7419 0.0762
-5.750 0.0402 0.00919 0.00332 -0.1496 0.7332 0.0777
-5.500 0.0672 0.00898 0.00310 -0.1493 0.7258 0.0806
-5.250 0.0938 0.00888 0.00295 -0.1488 0.7177 0.0832
-5.000 0.1213 0.00880 0.00283 -0.1486 0.7109 0.0856
-4.750 0.1485 0.00865 0.00267 -0.1483 0.7038 0.0893
-4.500 0.1750 0.00857 0.00255 -0.1478 0.6956 0.0935
-4.250 0.2024 0.00841 0.00242 -0.1475 0.6882 0.1006
-4.000 0.2288 0.00826 0.00231 -0.1471 0.6794 0.1183
-3.750 0.2558 0.00813 0.00225 -0.1468 0.6718 0.1414
-3.500 0.2833 0.00805 0.00219 -0.1465 0.6645 0.1545
-3.250 0.3101 0.00800 0.00213 -0.1461 0.6574 0.1656
-3.000 0.3380 0.00794 0.00208 -0.1459 0.6512 0.1745
-2.750 0.3653 0.00789 0.00203 -0.1456 0.6434 0.1834
-2.500 0.3919 0.00786 0.00200 -0.1451 0.6351 0.1938
-2.250 0.4195 0.00779 0.00196 -0.1449 0.6272 0.2071
-2.000 0.4461 0.00777 0.00194 -0.1444 0.6189 0.2221
-1.750 0.4735 0.00773 0.00193 -0.1441 0.6111 0.2391
-1.500 0.5002 0.00773 0.00194 -0.1437 0.6022 0.2554
-1.250 0.5271 0.00772 0.00195 -0.1433 0.5942 0.2709
-1.000 0.5540 0.00773 0.00196 -0.1429 0.5855 0.2837
-0.750 0.5804 0.00778 0.00198 -0.1424 0.5767 0.2939
-0.500 0.6075 0.00778 0.00201 -0.1420 0.5686 0.3052
0.000 0.6607 0.00786 0.00207 -0.1411 0.5526 0.3263
0.250 0.6867 0.00794 0.00211 -0.1406 0.5440 0.3344
0.500 0.7134 0.00797 0.00216 -0.1401 0.5366 0.3450
0.750 0.7398 0.00803 0.00221 -0.1397 0.5288 0.3549
1.000 0.7654 0.00809 0.00227 -0.1391 0.5212 0.3675
1.250 0.7922 0.00813 0.00233 -0.1387 0.5141 0.3795
1.500 0.8175 0.00820 0.00240 -0.1380 0.5062 0.3940
1.750 0.8437 0.00824 0.00247 -0.1375 0.4990 0.4094
2.000 0.8692 0.00831 0.00255 -0.1369 0.4906 0.4254
2.250 0.8942 0.00839 0.00264 -0.1362 0.4824 0.4434
2.500 0.9193 0.00846 0.00274 -0.1355 0.4725 0.4639
2.750 0.9437 0.00855 0.00285 -0.1347 0.4638 0.4880
3.000 0.9684 0.00863 0.00297 -0.1340 0.4544 0.5110
3.250 0.9923 0.00874 0.00309 -0.1331 0.4450 0.5317
3.500 1.0160 0.00886 0.00322 -0.1321 0.4345 0.5534
3.750 1.0395 0.00898 0.00335 -0.1312 0.4252 0.5742
4.000 1.0615 0.00912 0.00349 -0.1299 0.4143 0.5938
4.250 1.0835 0.00924 0.00362 -0.1287 0.4046 0.6117
4.500 1.1031 0.00940 0.00379 -0.1270 0.3939 0.6336
4.750 1.1246 0.00951 0.00394 -0.1256 0.3842 0.6574
5.000 1.1439 0.00966 0.00414 -0.1239 0.3741 0.6939
5.250 1.1595 0.00957 0.00438 -0.1213 0.3647 0.8248
5.500 1.1912 0.00962 0.00461 -0.1222 0.3550 1.0000
5.750 1.2111 0.00988 0.00481 -0.1207 0.3452 1.0000
6.000 1.2312 0.01013 0.00502 -0.1192 0.3355 1.0000
6.250 1.2509 0.01040 0.00524 -0.1176 0.3271 1.0000
6.500 1.2707 0.01066 0.00547 -0.1161 0.3183 1.0000
6.750 1.2892 0.01098 0.00573 -0.1144 0.3086 1.0000
7.000 1.3090 0.01125 0.00597 -0.1130 0.2995 1.0000
7.250 1.3256 0.01163 0.00629 -0.1110 0.2876 1.0000
7.500 1.3421 0.01204 0.00662 -0.1091 0.2731 1.0000
7.750 1.3583 0.01246 0.00697 -0.1072 0.2585 1.0000
8.000 1.3714 0.01301 0.00741 -0.1048 0.2392 1.0000
8.250 1.3784 0.01384 0.00806 -0.1015 0.2088 1.0000
8.500 1.3868 0.01463 0.00873 -0.0986 0.1882 1.0000
8.750 1.3984 0.01531 0.00934 -0.0962 0.1776 1.0000
9.000 1.4131 0.01585 0.00987 -0.0943 0.1726 1.0000
9.250 1.4264 0.01648 0.01048 -0.0923 0.1674 1.0000
9.500 1.4422 0.01701 0.01102 -0.0907 0.1642 1.0000
9.750 1.4582 0.01754 0.01156 -0.0892 0.1618 1.0000
10.000 1.4735 0.01812 0.01215 -0.0876 0.1592 1.0000
10.250 1.4866 0.01882 0.01286 -0.0858 0.1561 1.0000
10.500 1.4994 0.01957 0.01361 -0.0840 0.1528 1.0000
10.750 1.5141 0.02022 0.01429 -0.0825 0.1506 1.0000
11.000 1.5306 0.02080 0.01491 -0.0813 0.1489 1.0000
11.250 1.5455 0.02148 0.01562 -0.0799 0.1464 1.0000
11.500 1.5581 0.02232 0.01646 -0.0784 0.1433 1.0000
11.750 1.5689 0.02329 0.01745 -0.0767 0.1398 1.0000
12.000 1.5823 0.02412 0.01831 -0.0753 0.1370 1.0000
12.250 1.5975 0.02486 0.01909 -0.0742 0.1339 1.0000
12.500 1.6083 0.02592 0.02014 -0.0728 0.1286 1.0000
12.750 1.6191 0.02701 0.02124 -0.0714 0.1230 1.0000
13.000 1.6267 0.02837 0.02255 -0.0699 0.1124 1.0000
13.250 1.6220 0.03070 0.02473 -0.0677 0.0907 1.0000
13.500 1.6162 0.03327 0.02724 -0.0656 0.0792 1.0000
13.750 1.6162 0.03547 0.02944 -0.0641 0.0732 1.0000
14.000 1.6166 0.03772 0.03170 -0.0627 0.0689 1.0000
14.250 1.6199 0.03979 0.03381 -0.0617 0.0653 1.0000
14.500 1.6197 0.04223 0.03626 -0.0606 0.0619 1.0000
14.750 1.6239 0.04429 0.03837 -0.0597 0.0589 1.0000
15.000 1.6247 0.04675 0.04085 -0.0589 0.0563 1.0000
15.250 1.6272 0.04912 0.04327 -0.0583 0.0538 1.0000
15.500 1.6287 0.05162 0.04581 -0.0577 0.0518 1.0000
15.750 1.6274 0.05447 0.04869 -0.0572 0.0495 1.0000
16.000 1.6300 0.05697 0.05125 -0.0568 0.0481 1.0000
16.250 1.6306 0.05976 0.05408 -0.0566 0.0466 1.0000
16.500 1.6291 0.06283 0.05719 -0.0564 0.0451 1.0000
16.750 1.6265 0.06609 0.06051 -0.0563 0.0439 1.0000
17.000 1.6275 0.06900 0.06350 -0.0564 0.0430 1.0000
17.250 1.6278 0.07202 0.06659 -0.0565 0.0421 1.0000
17.500 1.6257 0.07541 0.07003 -0.0568 0.0412 1.0000
17.750 1.6217 0.07911 0.07380 -0.0572 0.0404 1.0000
18.000 1.6162 0.08307 0.07782 -0.0578 0.0396 1.0000
18.250 1.6104 0.08715 0.08197 -0.0585 0.0389 1.0000
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