FX 74-130 WP1 (fx74130wp1-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 74-130 WP1 (fx74130wp1-il) Reynolds number: 500,000 Max Cl/Cd: 115.85 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx74130wp1-il-500000-n5.txt Download as CSV file: xf-fx74130wp1-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 74-130 WP1
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
------ -------- --------- --------- -------- -------- --------
-10.250 -0.1271 0.08430 0.08083 -0.1184 0.8158 0.0107
-10.000 -0.1291 0.07931 0.07587 -0.1206 0.8145 0.0090
-9.750 -0.1279 0.07587 0.07244 -0.1222 0.8130 0.0088
-9.500 -0.1300 0.07175 0.06837 -0.1241 0.8114 0.0084
-9.250 -0.1340 0.06728 0.06392 -0.1266 0.8097 0.0082
-9.000 -0.1415 0.06220 0.05889 -0.1304 0.8077 0.0080
-8.750 -0.1563 0.05690 0.05356 -0.1340 0.8056 0.0077
-8.500 -0.1760 0.05282 0.04942 -0.1338 0.8036 0.0075
-8.000 -0.2246 0.03816 0.03425 -0.1300 0.7993 0.0067
-7.750 -0.2312 0.03230 0.02802 -0.1273 0.7975 0.0066
-7.500 -0.2263 0.02864 0.02404 -0.1254 0.7960 0.0068
-7.250 -0.2160 0.02553 0.02058 -0.1238 0.7945 0.0069
-7.000 -0.1983 0.02389 0.01870 -0.1230 0.7931 0.0072
-6.750 -0.1806 0.02171 0.01619 -0.1220 0.7918 0.0073
-6.500 -0.1599 0.02002 0.01422 -0.1213 0.7906 0.0076
-6.250 -0.1374 0.01855 0.01245 -0.1207 0.7896 0.0079
-6.000 -0.1137 0.01727 0.01093 -0.1203 0.7886 0.0081
-5.750 -0.0895 0.01632 0.00982 -0.1199 0.7875 0.0085
-5.500 -0.0642 0.01576 0.00914 -0.1197 0.7863 0.0091
-5.250 -0.0392 0.01505 0.00831 -0.1194 0.7849 0.0093
-5.000 -0.0145 0.01431 0.00746 -0.1191 0.7835 0.0094
-4.750 0.0097 0.01352 0.00659 -0.1187 0.7820 0.0096
-4.500 0.0337 0.01278 0.00580 -0.1183 0.7806 0.0101
-4.250 0.0591 0.01233 0.00531 -0.1182 0.7793 0.0106
-4.000 0.0851 0.01197 0.00491 -0.1181 0.7781 0.0114
-3.750 0.1115 0.01164 0.00453 -0.1181 0.7770 0.0124
-3.500 0.1384 0.01137 0.00421 -0.1182 0.7759 0.0134
-3.250 0.1652 0.01107 0.00387 -0.1183 0.7748 0.0153
-3.000 0.1921 0.01090 0.00370 -0.1184 0.7735 0.0185
-2.750 0.2185 0.01068 0.00349 -0.1184 0.7719 0.0241
-2.500 0.2451 0.01046 0.00333 -0.1185 0.7702 0.0396
-2.250 0.2716 0.01016 0.00320 -0.1187 0.7687 0.0881
-2.000 0.2979 0.00975 0.00308 -0.1190 0.7672 0.1790
-1.750 0.3232 0.00882 0.00293 -0.1196 0.7657 0.4213
-1.500 0.3461 0.00795 0.00316 -0.1192 0.7642 0.7329
-1.250 0.3743 0.00813 0.00331 -0.1192 0.7629 0.7766
-1.000 0.4014 0.00834 0.00350 -0.1189 0.7616 0.7968
-0.750 0.4283 0.00853 0.00366 -0.1186 0.7604 0.8098
-0.500 0.4547 0.00868 0.00380 -0.1183 0.7588 0.8184
-0.250 0.4809 0.00876 0.00389 -0.1181 0.7569 0.8234
0.000 0.5075 0.00882 0.00396 -0.1179 0.7550 0.8272
0.250 0.5355 0.00885 0.00397 -0.1182 0.7531 0.8300
0.500 0.5643 0.00886 0.00395 -0.1186 0.7513 0.8320
0.750 0.5936 0.00887 0.00393 -0.1192 0.7498 0.8336
1.000 0.6229 0.00887 0.00391 -0.1198 0.7484 0.8347
1.250 0.6516 0.00886 0.00389 -0.1202 0.7470 0.8356
1.500 0.6791 0.00889 0.00395 -0.1204 0.7451 0.8366
1.750 0.7060 0.00891 0.00401 -0.1205 0.7425 0.8375
2.000 0.7335 0.00891 0.00403 -0.1207 0.7393 0.8385
2.250 0.7617 0.00887 0.00400 -0.1210 0.7362 0.8394
2.500 0.7906 0.00883 0.00397 -0.1215 0.7337 0.8401
2.750 0.8178 0.00884 0.00402 -0.1216 0.7301 0.8410
3.000 0.8446 0.00883 0.00405 -0.1216 0.7252 0.8420
3.250 0.8728 0.00876 0.00400 -0.1219 0.7204 0.8428
3.500 0.8992 0.00874 0.00404 -0.1219 0.7137 0.8436
3.750 0.9266 0.00868 0.00398 -0.1220 0.7064 0.8443
4.000 0.9525 0.00867 0.00401 -0.1218 0.6962 0.8451
4.250 0.9782 0.00865 0.00400 -0.1215 0.6828 0.8460
4.500 1.0026 0.00869 0.00398 -0.1210 0.6647 0.8470
4.750 1.0241 0.00884 0.00404 -0.1199 0.6370 0.8478
5.000 1.0383 0.00922 0.00420 -0.1173 0.5842 0.8487
5.250 1.0330 0.01018 0.00471 -0.1110 0.4990 0.8499
5.500 1.0239 0.01114 0.00534 -0.1042 0.4336 0.8514
5.750 1.0181 0.01211 0.00606 -0.0983 0.3787 0.8529
6.000 1.0168 0.01310 0.00683 -0.0936 0.3292 0.8546
6.250 1.0166 0.01419 0.00769 -0.0894 0.2796 0.8563
6.500 1.0205 0.01525 0.00854 -0.0861 0.2343 0.8576
6.750 1.0244 0.01640 0.00945 -0.0830 0.1857 0.8588
7.000 1.0321 0.01744 0.01030 -0.0805 0.1471 0.8599
7.250 1.0420 0.01840 0.01111 -0.0784 0.1156 0.8610
7.500 1.0527 0.01935 0.01195 -0.0765 0.0880 0.8620
8.000 1.0769 0.02115 0.01357 -0.0731 0.0487 0.8638
8.250 1.0908 0.02196 0.01435 -0.0716 0.0387 0.8647
8.500 1.1058 0.02270 0.01511 -0.0704 0.0321 0.8656
8.750 1.1207 0.02348 0.01591 -0.0691 0.0277 0.8667
9.000 1.1358 0.02425 0.01673 -0.0679 0.0245 0.8679
9.250 1.1496 0.02514 0.01764 -0.0666 0.0216 0.8692
9.500 1.1644 0.02596 0.01853 -0.0654 0.0202 0.8703
9.750 1.1798 0.02677 0.01940 -0.0644 0.0188 0.8714
10.000 1.1945 0.02763 0.02031 -0.0633 0.0171 0.8725
10.250 1.2072 0.02867 0.02137 -0.0620 0.0155 0.8737
10.500 1.2205 0.02967 0.02246 -0.0609 0.0143 0.8748
10.750 1.2355 0.03056 0.02342 -0.0599 0.0133 0.8760
11.250 1.2619 0.03261 0.02562 -0.0578 0.0115 0.8783
11.500 1.2731 0.03382 0.02688 -0.0565 0.0106 0.8796
11.750 1.2837 0.03512 0.02826 -0.0553 0.0098 0.8811
12.000 1.2966 0.03623 0.02947 -0.0544 0.0092 0.8826
12.250 1.3094 0.03736 0.03068 -0.0535 0.0083 0.8843
12.500 1.3213 0.03861 0.03200 -0.0525 0.0076 0.8861
12.750 1.3309 0.04010 0.03356 -0.0515 0.0070 0.8880
13.000 1.3397 0.04170 0.03527 -0.0504 0.0066 0.8899
13.250 1.3490 0.04327 0.03695 -0.0494 0.0063 0.8919
13.500 1.3576 0.04491 0.03872 -0.0485 0.0059 0.8944
13.750 1.3662 0.04658 0.04049 -0.0476 0.0055 0.8974
14.000 1.3735 0.04840 0.04242 -0.0466 0.0053 0.9010
14.500 1.3856 0.05237 0.04662 -0.0449 0.0048 0.9105
14.750 1.3876 0.05484 0.04922 -0.0439 0.0046 0.9175
15.000 1.3878 0.05730 0.05186 -0.0427 0.0045 0.9318
15.250 1.3884 0.05972 0.05445 -0.0417 0.0044 1.0000
15.500 1.3911 0.06250 0.05738 -0.0414 0.0042 1.0000
15.750 1.3926 0.06550 0.06053 -0.0412 0.0041 1.0000
16.000 1.3936 0.06862 0.06380 -0.0411 0.0040 1.0000
16.250 1.3923 0.07214 0.06747 -0.0412 0.0039 1.0000
16.500 1.3902 0.07586 0.07135 -0.0415 0.0038 1.0000
16.750 1.3870 0.07986 0.07551 -0.0421 0.0038 1.0000
17.000 1.3831 0.08409 0.07990 -0.0429 0.0037 1.0000
17.250 1.3775 0.08868 0.08465 -0.0439 0.0036 1.0000
17.500 1.3706 0.09363 0.08977 -0.0453 0.0035 1.0000
17.750 1.3630 0.09888 0.09518 -0.0471 0.0035 1.0000
18.000 1.3544 0.10445 0.10092 -0.0493 0.0034 1.0000
18.250 1.3451 0.11032 0.10696 -0.0518 0.0034 1.0000
18.500 1.3343 0.11665 0.11345 -0.0548 0.0034 1.0000
18.750 1.3226 0.12336 0.12033 -0.0583 0.0033 1.0000
19.000 1.3094 0.13059 0.12773 -0.0623 0.0033 1.0000
19.250 1.2953 0.13827 0.13558 -0.0668 0.0033 1.0000
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