FX 74-130 WP1 (fx74130wp1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 74-130 WP1 (fx74130wp1-il) Reynolds number: 1,000,000 Max Cl/Cd: 152.61 at α=4.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx74130wp1-il-1000000.txt Download as CSV file: xf-fx74130wp1-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.250 -0.0841 0.08328 0.08076 -0.1097 0.8182 0.0097
-11.000 -0.0811 0.07981 0.07728 -0.1109 0.8170 0.0099
-10.750 -0.0789 0.07606 0.07354 -0.1123 0.8163 0.0099
-10.500 -0.0758 0.07277 0.07026 -0.1133 0.8155 0.0101
-10.250 -0.0743 0.06909 0.06658 -0.1146 0.8147 0.0102
-10.000 -0.0740 0.06514 0.06264 -0.1161 0.8138 0.0102
-9.750 -0.0738 0.06137 0.05889 -0.1175 0.8128 0.0103
-9.500 -0.0743 0.05755 0.05508 -0.1189 0.8118 0.0104
-9.250 -0.0772 0.05334 0.05089 -0.1207 0.8107 0.0106
-9.000 -0.0827 0.04874 0.04631 -0.1230 0.8094 0.0106
-8.750 -0.0995 0.04221 0.03979 -0.1286 0.8079 0.0104
-8.500 -0.1228 0.03683 0.03435 -0.1314 0.8062 0.0103
-8.250 -0.1442 0.03350 0.03097 -0.1303 0.8044 0.0103
-8.000 -0.1542 0.03048 0.02785 -0.1290 0.8025 0.0104
-7.750 -0.1572 0.02736 0.02465 -0.1279 0.8015 0.0105
-7.500 -0.1563 0.02437 0.02155 -0.1268 0.8002 0.0107
-7.250 -0.1527 0.02131 0.01835 -0.1255 0.7987 0.0109
-7.000 -0.1456 0.01847 0.01536 -0.1244 0.7972 0.0112
-6.750 -0.1364 0.01566 0.01235 -0.1231 0.7957 0.0115
-6.500 -0.1242 0.01295 0.00941 -0.1218 0.7943 0.0123
-6.250 -0.1017 0.01190 0.00810 -0.1207 0.7931 0.0135
-6.000 -0.1045 0.01699 0.01187 -0.1231 0.7944 0.0099
-5.750 -0.0813 0.01539 0.01006 -0.1225 0.7932 0.0100
-5.500 -0.0560 0.01472 0.00932 -0.1226 0.7921 0.0107
-5.250 -0.0307 0.01365 0.00811 -0.1223 0.7911 0.0107
-5.000 -0.0050 0.01283 0.00718 -0.1221 0.7899 0.0108
-4.750 0.0203 0.01218 0.00644 -0.1218 0.7885 0.0109
-4.500 0.0460 0.01166 0.00590 -0.1217 0.7875 0.0114
-4.250 0.0718 0.01121 0.00543 -0.1216 0.7864 0.0119
-4.000 0.0971 0.01066 0.00482 -0.1213 0.7850 0.0122
-3.750 0.1230 0.01020 0.00432 -0.1211 0.7836 0.0125
-3.500 0.1496 0.00986 0.00395 -0.1212 0.7822 0.0133
-3.250 0.1761 0.00941 0.00343 -0.1211 0.7809 0.0151
-3.000 0.2037 0.00920 0.00320 -0.1213 0.7796 0.0175
-2.750 0.2315 0.00897 0.00295 -0.1216 0.7784 0.0219
-2.500 0.2593 0.00870 0.00276 -0.1219 0.7772 0.0457
-2.250 0.2861 0.00821 0.00263 -0.1223 0.7758 0.1586
-2.000 0.3120 0.00744 0.00254 -0.1229 0.7742 0.3829
-1.750 0.3390 0.00636 0.00240 -0.1239 0.7730 0.6754
-1.500 0.3663 0.00638 0.00264 -0.1238 0.7716 0.7667
-1.250 0.3946 0.00650 0.00275 -0.1240 0.7701 0.7841
-1.000 0.4222 0.00668 0.00293 -0.1238 0.7685 0.7990
-0.750 0.4498 0.00683 0.00308 -0.1237 0.7669 0.8096
-0.500 0.4772 0.00698 0.00323 -0.1236 0.7653 0.8184
-0.250 0.5046 0.00705 0.00329 -0.1235 0.7639 0.8241
0.000 0.5322 0.00715 0.00338 -0.1234 0.7626 0.8292
0.250 0.5612 0.00726 0.00346 -0.1238 0.7611 0.8337
0.500 0.5884 0.00729 0.00351 -0.1238 0.7595 0.8369
0.750 0.6153 0.00730 0.00355 -0.1238 0.7577 0.8395
1.000 0.6431 0.00730 0.00356 -0.1239 0.7555 0.8416
1.250 0.6717 0.00726 0.00352 -0.1243 0.7531 0.8432
1.500 0.7010 0.00721 0.00346 -0.1248 0.7506 0.8445
1.750 0.7305 0.00717 0.00339 -0.1254 0.7484 0.8455
2.000 0.7597 0.00717 0.00338 -0.1260 0.7458 0.8465
2.250 0.7876 0.00711 0.00336 -0.1263 0.7423 0.8474
2.500 0.8163 0.00704 0.00330 -0.1267 0.7384 0.8482
2.750 0.8451 0.00695 0.00321 -0.1271 0.7347 0.8489
3.000 0.8728 0.00688 0.00316 -0.1273 0.7303 0.8499
3.250 0.9001 0.00680 0.00313 -0.1274 0.7247 0.8506
3.500 0.9281 0.00675 0.00305 -0.1276 0.7191 0.8511
3.750 0.9546 0.00669 0.00305 -0.1276 0.7104 0.8518
4.000 0.9813 0.00667 0.00303 -0.1275 0.7009 0.8525
4.250 1.0068 0.00667 0.00303 -0.1272 0.6857 0.8533
4.500 1.0310 0.00676 0.00307 -0.1267 0.6670 0.8540
4.750 1.0545 0.00691 0.00316 -0.1260 0.6464 0.8546
5.000 1.0753 0.00715 0.00331 -0.1249 0.6158 0.8554
5.250 1.0893 0.00764 0.00359 -0.1224 0.5626 0.8563
5.500 1.0920 0.00853 0.00411 -0.1177 0.4866 0.8577
5.750 1.0936 0.00942 0.00468 -0.1130 0.4193 0.8590
6.000 1.0903 0.01024 0.00520 -0.1073 0.3605 0.8602
6.250 1.0872 0.01118 0.00586 -0.1019 0.3035 0.8614
6.500 1.0843 0.01223 0.00664 -0.0969 0.2466 0.8624
6.750 1.0853 0.01325 0.00741 -0.0929 0.1980 0.8635
7.000 1.0887 0.01427 0.00823 -0.0894 0.1546 0.8647
7.250 1.0948 0.01525 0.00903 -0.0864 0.1172 0.8660
7.500 1.1024 0.01623 0.00985 -0.0838 0.0849 0.8671
7.750 1.1118 0.01717 0.01066 -0.0816 0.0583 0.8681
8.000 1.1223 0.01810 0.01148 -0.0795 0.0393 0.8690
8.250 1.1361 0.01886 0.01221 -0.0779 0.0309 0.8699
8.500 1.1518 0.01953 0.01291 -0.0766 0.0268 0.8707
8.750 1.1668 0.02026 0.01364 -0.0753 0.0237 0.8716
9.000 1.1802 0.02112 0.01453 -0.0737 0.0208 0.8725
9.250 1.1976 0.02171 0.01517 -0.0728 0.0197 0.8734
9.500 1.2137 0.02240 0.01589 -0.0717 0.0184 0.8742
9.750 1.2284 0.02321 0.01672 -0.0705 0.0169 0.8750
10.000 1.2384 0.02437 0.01795 -0.0687 0.0150 0.8759
10.250 1.2546 0.02509 0.01872 -0.0677 0.0143 0.8766
10.500 1.2717 0.02573 0.01939 -0.0669 0.0133 0.8778
10.750 1.2872 0.02649 0.02019 -0.0659 0.0123 0.8791
11.000 1.3004 0.02743 0.02116 -0.0647 0.0112 0.8804
11.250 1.3082 0.02883 0.02264 -0.0629 0.0100 0.8816
11.500 1.3242 0.02960 0.02347 -0.0620 0.0095 0.8828
11.750 1.3386 0.03050 0.02442 -0.0611 0.0086 0.8840
12.000 1.3524 0.03147 0.02544 -0.0601 0.0081 0.8853
12.250 1.3575 0.03322 0.02725 -0.0583 0.0070 0.8866
12.500 1.3684 0.03450 0.02862 -0.0571 0.0066 0.8879
12.750 1.3811 0.03565 0.02984 -0.0562 0.0063 0.8893
13.000 1.3918 0.03701 0.03128 -0.0551 0.0060 0.8906
13.250 1.4017 0.03843 0.03277 -0.0540 0.0057 0.8924
13.500 1.4124 0.03979 0.03421 -0.0531 0.0054 0.8943
13.750 1.4211 0.04137 0.03586 -0.0521 0.0051 0.8964
14.000 1.4262 0.04337 0.03796 -0.0509 0.0049 0.8986
14.250 1.4178 0.04689 0.04167 -0.0488 0.0045 0.9005
14.500 1.4282 0.04844 0.04331 -0.0482 0.0044 0.9033
14.750 1.4340 0.05053 0.04554 -0.0474 0.0043 0.9064
15.000 1.4403 0.05255 0.04767 -0.0466 0.0042 0.9109
15.250 1.4444 0.05485 0.05012 -0.0459 0.0041 0.9164
15.500 1.4457 0.05736 0.05278 -0.0449 0.0040 0.9267
15.750 1.4431 0.05984 0.05547 -0.0434 0.0039 1.0000
16.000 1.4448 0.06278 0.05852 -0.0432 0.0038 1.0000
16.250 1.4438 0.06615 0.06203 -0.0430 0.0037 1.0000
16.500 1.4427 0.06960 0.06561 -0.0430 0.0037 1.0000
16.750 1.4403 0.07331 0.06945 -0.0433 0.0036 1.0000
17.000 1.4362 0.07740 0.07369 -0.0437 0.0036 1.0000
17.250 1.4306 0.08185 0.07828 -0.0445 0.0035 1.0000
17.500 1.4245 0.08649 0.08307 -0.0455 0.0035 1.0000
17.750 1.4164 0.09161 0.08834 -0.0469 0.0035 1.0000
18.000 1.4072 0.09708 0.09396 -0.0487 0.0034 1.0000
18.250 1.3969 0.10293 0.09997 -0.0509 0.0034 1.0000
18.500 1.3850 0.10929 0.10648 -0.0535 0.0034 1.0000
18.750 1.3717 0.11609 0.11345 -0.0567 0.0034 1.0000
19.000 1.3568 0.12342 0.12095 -0.0605 0.0034 1.0000
19.250 1.3408 0.13126 0.12896 -0.0648 0.0034 1.0000
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