WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 62-K-131 AIRFOIL (fx62k131-il) Reynolds number: 200,000 Max Cl/Cd: 84.07 at α=5.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx62k131-il-200000-n5.txt Download as CSV file: xf-fx62k131-il-200000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 62-K-131 AIRFOIL
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.500 -0.0965 0.08876 0.08524 -0.0945 0.9293 0.0223
-10.250 -0.0943 0.08423 0.08070 -0.0981 0.9250 0.0248
-10.000 -0.0914 0.07974 0.07620 -0.1023 0.9210 0.0257
-9.500 -0.1924 0.08886 0.08527 -0.0934 0.9375 0.0189
-9.250 -0.1799 0.08534 0.08172 -0.0968 0.9318 0.0207
-9.000 -0.1701 0.08087 0.07724 -0.1013 0.9248 0.0223
-8.000 -0.1623 0.05525 0.05134 -0.1275 0.8930 0.0155
-7.750 -0.1626 0.05097 0.04693 -0.1317 0.8852 0.0148
-7.500 -0.1569 0.04639 0.04209 -0.1354 0.8798 0.0140
-7.250 -0.1497 0.04188 0.03731 -0.1375 0.8741 0.0130
-7.000 -0.1386 0.03496 0.02972 -0.1394 0.8690 0.0112
-6.750 -0.1157 0.03165 0.02592 -0.1406 0.8658 0.0108
-6.500 -0.0941 0.02918 0.02309 -0.1412 0.8617 0.0107
-6.250 -0.0703 0.02672 0.02024 -0.1420 0.8581 0.0106
-6.000 -0.0445 0.02418 0.01729 -0.1428 0.8551 0.0107
-5.750 -0.0174 0.02188 0.01465 -0.1434 0.8526 0.0110
-5.500 0.0084 0.02033 0.01286 -0.1436 0.8496 0.0115
-5.250 0.0334 0.01922 0.01163 -0.1434 0.8462 0.0121
-5.000 0.0601 0.01849 0.01079 -0.1436 0.8431 0.0138
-4.750 0.0881 0.01785 0.01002 -0.1438 0.8404 0.0159
-4.500 0.1164 0.01698 0.00903 -0.1441 0.8381 0.0167
-4.250 0.1434 0.01581 0.00783 -0.1447 0.8350 0.0183
-4.000 0.1725 0.01519 0.00713 -0.1456 0.8316 0.0209
-3.750 0.2030 0.01481 0.00665 -0.1466 0.8285 0.0259
-3.500 0.2368 0.01419 0.00594 -0.1484 0.8259 0.0357
-3.250 0.2773 0.01299 0.00535 -0.1527 0.8238 0.1950
-3.000 0.3200 0.01165 0.00553 -0.1576 0.8209 0.5969
-2.750 0.3410 0.01207 0.00609 -0.1555 0.8167 0.6753
-2.500 0.3654 0.01245 0.00640 -0.1542 0.8131 0.7024
-2.250 0.3909 0.01263 0.00648 -0.1533 0.8103 0.7105
-2.000 0.4206 0.01270 0.00642 -0.1540 0.8068 0.7179
-1.750 0.4455 0.01282 0.00649 -0.1534 0.8029 0.7221
-1.500 0.4749 0.01289 0.00646 -0.1539 0.7997 0.7281
-1.250 0.5043 0.01294 0.00643 -0.1543 0.7969 0.7334
-1.000 0.5305 0.01305 0.00648 -0.1540 0.7937 0.7376
-0.750 0.5591 0.01313 0.00652 -0.1545 0.7895 0.7434
-0.500 0.5866 0.01320 0.00656 -0.1545 0.7859 0.7476
-0.250 0.6141 0.01327 0.00658 -0.1544 0.7829 0.7515
0.000 0.6429 0.01334 0.00663 -0.1548 0.7792 0.7567
0.250 0.6708 0.01341 0.00670 -0.1552 0.7746 0.7609
0.500 0.6973 0.01346 0.00674 -0.1549 0.7708 0.7637
0.750 0.7266 0.01348 0.00674 -0.1553 0.7678 0.7671
1.000 0.7541 0.01357 0.00686 -0.1556 0.7625 0.7714
1.250 0.7830 0.01360 0.00690 -0.1561 0.7580 0.7749
1.500 0.8109 0.01360 0.00690 -0.1561 0.7544 0.7772
1.750 0.8356 0.01369 0.00707 -0.1557 0.7482 0.7801
2.000 0.8644 0.01368 0.00707 -0.1561 0.7426 0.7836
2.250 0.8950 0.01369 0.00709 -0.1570 0.7362 0.7876
2.500 0.9203 0.01370 0.00716 -0.1565 0.7294 0.7897
2.750 0.9464 0.01372 0.00726 -0.1563 0.7233 0.7923
3.000 0.9725 0.01377 0.00738 -0.1561 0.7162 0.7952
3.250 1.0012 0.01379 0.00745 -0.1565 0.7098 0.7984
3.500 1.0303 0.01384 0.00759 -0.1571 0.7017 0.8019
3.750 1.0548 0.01389 0.00773 -0.1565 0.6936 0.8040
4.000 1.0811 0.01391 0.00781 -0.1562 0.6855 0.8064
4.250 1.1061 0.01400 0.00801 -0.1558 0.6755 0.8093
4.500 1.1330 0.01407 0.00816 -0.1559 0.6650 0.8125
4.750 1.1602 0.01412 0.00830 -0.1559 0.6503 0.8157
5.000 1.1819 0.01416 0.00832 -0.1546 0.6262 0.8177
5.250 1.2025 0.01431 0.00841 -0.1530 0.5954 0.8202
5.500 1.2240 0.01456 0.00862 -0.1519 0.5693 0.8231
5.750 1.2450 0.01493 0.00893 -0.1507 0.5411 0.8262
6.000 1.2630 0.01550 0.00937 -0.1492 0.5014 0.8292
6.250 1.2718 0.01623 0.00991 -0.1458 0.4506 0.8316
6.500 1.2766 0.01715 0.01058 -0.1418 0.3976 0.8345
6.750 1.2775 0.01821 0.01140 -0.1374 0.3468 0.8378
7.000 1.2783 0.01964 0.01251 -0.1334 0.2864 0.8412
7.250 1.2770 0.02129 0.01381 -0.1294 0.2220 0.8442
7.500 1.2752 0.02299 0.01519 -0.1255 0.1642 0.8469
7.750 1.2788 0.02453 0.01654 -0.1226 0.1243 0.8497
8.000 1.2851 0.02602 0.01789 -0.1202 0.0932 0.8526
8.250 1.2898 0.02775 0.01943 -0.1179 0.0604 0.8555
8.500 1.2950 0.02939 0.02095 -0.1156 0.0381 0.8581
8.750 1.2988 0.03110 0.02261 -0.1131 0.0221 0.8606
9.000 1.3052 0.03270 0.02425 -0.1110 0.0141 0.8631
9.250 1.3136 0.03423 0.02590 -0.1091 0.0101 0.8658
9.500 1.3194 0.03606 0.02781 -0.1072 0.0081 0.8686
9.750 1.3275 0.03773 0.02964 -0.1055 0.0071 0.8712
10.000 1.3332 0.03946 0.03154 -0.1035 0.0065 0.8736
10.250 1.3388 0.04129 0.03352 -0.1017 0.0060 0.8760
10.500 1.3438 0.04323 0.03561 -0.1000 0.0058 0.8787
10.750 1.3475 0.04537 0.03790 -0.0983 0.0055 0.8815
11.000 1.3492 0.04780 0.04047 -0.0966 0.0052 0.8841
11.250 1.3483 0.05036 0.04319 -0.0947 0.0051 0.8864
11.500 1.3466 0.05308 0.04606 -0.0928 0.0050 0.8887
11.750 1.3478 0.05563 0.04877 -0.0912 0.0049 0.8911
12.000 1.3488 0.05828 0.05163 -0.0898 0.0048 0.8938
12.250 1.3505 0.06099 0.05451 -0.0884 0.0047 0.8966
12.500 1.3522 0.06367 0.05737 -0.0871 0.0046 0.8992
12.750 1.3536 0.06635 0.06025 -0.0859 0.0044 0.9018
13.000 1.3546 0.06919 0.06328 -0.0849 0.0042 0.9046
13.250 1.3553 0.07218 0.06646 -0.0842 0.0040 0.9075
13.500 1.3550 0.07542 0.06988 -0.0837 0.0038 0.9105
13.750 1.3537 0.07865 0.07329 -0.0835 0.0035 0.9139
14.000 1.3503 0.08219 0.07701 -0.0832 0.0034 0.9176
14.250 1.3460 0.08610 0.08109 -0.0834 0.0033 0.9215
14.750 1.3327 0.09480 0.09018 -0.0841 0.0031 0.9298
15.000 1.3235 0.09979 0.09539 -0.0850 0.0031 0.9346
15.250 1.3134 0.10491 0.10072 -0.0861 0.0031 0.9408
15.500 1.3019 0.11035 0.10639 -0.0875 0.0030 0.9500
15.750 1.2879 0.11590 0.11215 -0.0892 0.0030 0.9996
16.000 1.2776 0.12255 0.11903 -0.0926 0.0030 0.9999
16.250 1.2665 0.12952 0.12621 -0.0965 0.0030 0.9999
16.500 1.2532 0.13729 0.13420 -0.1011 0.0030 0.9999
16.750 1.2429 0.14479 0.14190 -0.1059 0.0030 0.9999
17.000 1.2299 0.15352 0.15083 -0.1117 0.0030 0.9999
17.250 1.2179 0.16244 0.15994 -0.1179 0.0030 0.9999
17.500 1.2040 0.17297 0.17068 -0.1253 0.0031 0.9999
17.750 1.1790 0.18889 0.18684 -0.1359 0.0033 0.9999
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