FX S 03-182 AIRFOIL (fxs03182-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
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Airfoil: FX S 03-182 AIRFOIL (fxs03182-il) Reynolds number: 1,000,000 Max Cl/Cd: 110.82 at α=3.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fxs03182-il-1000000.txt Download as CSV file: xf-fxs03182-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: FX S 03-182 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
------ -------- --------- --------- -------- -------- --------
-15.000 -0.1403 0.12095 0.11886 -0.0960 0.8668 0.0123
-14.750 -0.1382 0.11777 0.11562 -0.0975 0.8545 0.0130
-14.500 -0.3149 0.12690 0.12523 -0.0730 0.9609 0.0107
-10.500 -0.4656 0.02266 0.01717 -0.1245 0.7623 0.0058
-10.250 -0.4504 0.02207 0.01649 -0.1235 0.7552 0.0057
-10.000 -0.4380 0.02081 0.01516 -0.1218 0.7494 0.0050
-9.750 -0.4248 0.01996 0.01421 -0.1205 0.7433 0.0048
-9.500 -0.4122 0.01917 0.01331 -0.1190 0.7377 0.0047
-9.250 -0.4005 0.01828 0.01233 -0.1174 0.7325 0.0045
-9.000 -0.3871 0.01761 0.01158 -0.1160 0.7273 0.0044
-8.750 -0.3747 0.01691 0.01080 -0.1143 0.7227 0.0043
-8.500 -0.3618 0.01625 0.01008 -0.1128 0.7182 0.0043
-8.250 -0.3506 0.01557 0.00934 -0.1110 0.7137 0.0042
-8.000 -0.3414 0.01494 0.00864 -0.1087 0.7094 0.0042
-7.750 -0.3344 0.01440 0.00806 -0.1060 0.7057 0.0043
-7.500 -0.3209 0.01384 0.00744 -0.1044 0.7018 0.0043
-7.250 -0.3033 0.01342 0.00696 -0.1033 0.6981 0.0043
-7.000 -0.2844 0.01304 0.00651 -0.1024 0.6945 0.0043
-6.750 -0.2646 0.01258 0.00601 -0.1016 0.6917 0.0046
-6.500 -0.2422 0.01225 0.00564 -0.1011 0.6888 0.0046
-6.250 -0.2199 0.01189 0.00522 -0.1006 0.6859 0.0050
-6.000 -0.1960 0.01162 0.00488 -0.1004 0.6832 0.0052
-5.750 -0.1717 0.01137 0.00454 -0.1002 0.6803 0.0058
-5.500 -0.1459 0.01113 0.00428 -0.1002 0.6783 0.0064
-5.250 -0.1211 0.01079 0.00398 -0.1002 0.6760 0.0101
-5.000 -0.0939 0.01067 0.00384 -0.1005 0.6738 0.0147
-4.750 -0.0671 0.01050 0.00368 -0.1007 0.6716 0.0182
-4.500 -0.0399 0.01038 0.00353 -0.1010 0.6695 0.0207
-4.250 -0.0125 0.01028 0.00340 -0.1013 0.6673 0.0228
-4.000 0.0150 0.01013 0.00326 -0.1016 0.6653 0.0269
-3.750 0.0426 0.00992 0.00310 -0.1020 0.6635 0.0372
-3.500 0.0706 0.00978 0.00298 -0.1024 0.6617 0.0461
-3.250 0.0977 0.00937 0.00277 -0.1030 0.6599 0.1040
-3.000 0.1237 0.00804 0.00223 -0.1045 0.6581 0.3247
-2.750 0.1536 0.00700 0.00187 -0.1064 0.6565 0.5198
-2.500 0.1835 0.00699 0.00191 -0.1071 0.6549 0.5526
-2.250 0.2133 0.00704 0.00194 -0.1077 0.6532 0.5681
-2.000 0.2434 0.00714 0.00202 -0.1084 0.6513 0.5820
-1.750 0.2730 0.00717 0.00206 -0.1090 0.6502 0.5896
-1.500 0.3028 0.00721 0.00209 -0.1096 0.6489 0.5949
-1.250 0.3323 0.00724 0.00213 -0.1101 0.6474 0.6000
-1.000 0.3620 0.00729 0.00218 -0.1107 0.6458 0.6046
-0.750 0.3918 0.00736 0.00221 -0.1113 0.6443 0.6088
-0.500 0.4211 0.00740 0.00229 -0.1118 0.6429 0.6148
-0.250 0.4505 0.00749 0.00237 -0.1123 0.6407 0.6209
0.000 0.4800 0.00760 0.00241 -0.1129 0.6373 0.6241
0.250 0.5081 0.00752 0.00237 -0.1131 0.6334 0.6257
0.500 0.5369 0.00751 0.00238 -0.1135 0.6304 0.6279
0.750 0.5658 0.00754 0.00242 -0.1139 0.6276 0.6310
1.000 0.5948 0.00761 0.00247 -0.1144 0.6252 0.6342
1.250 0.6238 0.00768 0.00252 -0.1149 0.6219 0.6362
1.500 0.6517 0.00763 0.00249 -0.1151 0.6162 0.6371
1.750 0.6792 0.00767 0.00247 -0.1152 0.6088 0.6380
2.000 0.7076 0.00762 0.00246 -0.1156 0.6044 0.6394
2.250 0.7354 0.00760 0.00246 -0.1158 0.5983 0.6407
2.500 0.7629 0.00763 0.00248 -0.1160 0.5913 0.6420
2.750 0.7902 0.00765 0.00249 -0.1161 0.5820 0.6433
3.000 0.8176 0.00768 0.00253 -0.1163 0.5716 0.6447
3.250 0.8442 0.00774 0.00257 -0.1163 0.5588 0.6462
3.500 0.8699 0.00785 0.00263 -0.1161 0.5413 0.6475
3.750 0.8905 0.00816 0.00277 -0.1150 0.5005 0.6489
4.000 0.8941 0.00925 0.00337 -0.1108 0.4046 0.6503
4.250 0.8868 0.01071 0.00423 -0.1048 0.2886 0.6516
4.500 0.8812 0.01173 0.00487 -0.0990 0.2114 0.6527
4.750 0.8704 0.01291 0.00569 -0.0924 0.1329 0.6545
5.000 0.8733 0.01376 0.00635 -0.0885 0.0893 0.6562
5.250 0.8845 0.01435 0.00688 -0.0861 0.0668 0.6579
5.500 0.8942 0.01504 0.00750 -0.0836 0.0460 0.6597
5.750 0.9051 0.01574 0.00812 -0.0814 0.0304 0.6616
6.000 0.9223 0.01619 0.00859 -0.0802 0.0267 0.6635
6.250 0.9393 0.01668 0.00909 -0.0791 0.0233 0.6653
6.500 0.9501 0.01749 0.00987 -0.0771 0.0131 0.6669
6.750 0.9649 0.01813 0.01052 -0.0757 0.0117 0.6689
7.000 0.9807 0.01874 0.01116 -0.0746 0.0101 0.6710
7.250 0.9969 0.01936 0.01181 -0.0735 0.0094 0.6732
7.500 1.0137 0.01997 0.01244 -0.0726 0.0091 0.6754
7.750 1.0301 0.02061 0.01311 -0.0717 0.0086 0.6777
8.000 1.0462 0.02130 0.01382 -0.0707 0.0081 0.6801
9.000 1.1033 0.02466 0.01731 -0.0666 0.0028 0.6909
9.250 1.1165 0.02563 0.01832 -0.0655 0.0026 0.6939
9.500 1.1291 0.02667 0.01940 -0.0644 0.0024 0.6966
9.750 1.1424 0.02765 0.02045 -0.0635 0.0024 0.6999
10.000 1.1552 0.02869 0.02156 -0.0625 0.0023 0.7033
10.250 1.1683 0.02975 0.02267 -0.0617 0.0023 0.7069
10.500 1.1808 0.03087 0.02384 -0.0608 0.0022 0.7104
10.750 1.1927 0.03205 0.02509 -0.0599 0.0022 0.7142
11.000 1.2048 0.03325 0.02635 -0.0590 0.0021 0.7183
11.250 1.2160 0.03454 0.02771 -0.0582 0.0021 0.7227
11.500 1.2271 0.03588 0.02911 -0.0574 0.0021 0.7271
11.750 1.2373 0.03731 0.03062 -0.0565 0.0020 0.7319
12.000 1.2471 0.03881 0.03221 -0.0557 0.0020 0.7374
12.250 1.2559 0.04043 0.03391 -0.0549 0.0020 0.7427
12.500 1.2665 0.04192 0.03549 -0.0543 0.0019 0.7487
12.750 1.2759 0.04356 0.03720 -0.0536 0.0019 0.7550
13.000 1.2846 0.04529 0.03902 -0.0530 0.0018 0.7615
13.250 1.2933 0.04706 0.04088 -0.0524 0.0018 0.7687
13.500 1.3007 0.04899 0.04291 -0.0518 0.0018 0.7761
13.750 1.3076 0.05102 0.04503 -0.0513 0.0018 0.7843
14.000 1.3133 0.05322 0.04735 -0.0508 0.0017 0.7930
14.250 1.3179 0.05559 0.04982 -0.0504 0.0017 0.8021
14.500 1.3225 0.05801 0.05236 -0.0500 0.0017 0.8123
14.750 1.3277 0.06040 0.05488 -0.0498 0.0017 0.8237
15.000 1.3297 0.06322 0.05783 -0.0495 0.0016 0.8364
15.250 1.3328 0.06593 0.06068 -0.0494 0.0016 0.8517
15.500 1.3349 0.06876 0.06365 -0.0492 0.0016 0.8716
15.750 1.3335 0.07160 0.06671 -0.0485 0.0016 0.9105
16.000 1.3309 0.07426 0.06954 -0.0476 0.0016 1.0000
16.250 1.3312 0.07769 0.07306 -0.0480 0.0017 1.0000
16.500 1.3310 0.08125 0.07673 -0.0485 0.0017 1.0000
16.750 1.3301 0.08496 0.08054 -0.0491 0.0017 1.0000
17.000 1.3279 0.08897 0.08466 -0.0499 0.0017 1.0000
17.250 1.3249 0.09317 0.08897 -0.0509 0.0017 1.0000
17.500 1.3226 0.09735 0.09326 -0.0520 0.0017 1.0000
17.750 1.3180 0.10195 0.09798 -0.0534 0.0018 1.0000
18.000 1.3129 0.10672 0.10288 -0.0549 0.0018 1.0000
18.250 1.3072 0.11168 0.10796 -0.0567 0.0018 1.0000
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