WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il) Reynolds number: 1,000,000 Max Cl/Cd: 112.63 at α=4.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx05191-il-1000000-n5.txt Download as CSV file: xf-fx05191-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-191 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.750 -0.8280 0.08299 0.07932 -0.1100 0.8752 0.0116
-19.500 -0.8325 0.07806 0.07425 -0.1136 0.8702 0.0117
-19.250 -0.8373 0.07340 0.06946 -0.1168 0.8663 0.0117
-19.000 -0.8380 0.06941 0.06535 -0.1195 0.8626 0.0118
-18.750 -0.8398 0.06538 0.06120 -0.1223 0.8590 0.0119
-18.250 -0.8351 0.05886 0.05445 -0.1266 0.8532 0.0121
-18.000 -0.8317 0.05594 0.05144 -0.1283 0.8507 0.0122
-17.750 -0.8276 0.05318 0.04858 -0.1299 0.8483 0.0123
-17.500 -0.8233 0.05051 0.04581 -0.1314 0.8462 0.0124
-17.250 -0.8159 0.04821 0.04341 -0.1328 0.8440 0.0126
-17.000 -0.8052 0.04633 0.04145 -0.1340 0.8420 0.0127
-16.500 -0.7905 0.04213 0.03707 -0.1360 0.8385 0.0128
-16.250 -0.7813 0.04036 0.03522 -0.1366 0.8371 0.0130
-16.000 -0.7684 0.03896 0.03375 -0.1373 0.8357 0.0131
-15.750 -0.7588 0.03732 0.03204 -0.1378 0.8341 0.0132
-15.500 -0.7467 0.03592 0.03057 -0.1382 0.8326 0.0133
-15.250 -0.7389 0.03422 0.02880 -0.1384 0.8311 0.0134
-15.000 -0.7304 0.03262 0.02714 -0.1385 0.8296 0.0137
-14.750 -0.7193 0.03128 0.02574 -0.1386 0.8281 0.0137
-14.500 -0.7071 0.03006 0.02447 -0.1387 0.8266 0.0139
-14.250 -0.6946 0.02890 0.02324 -0.1387 0.8249 0.0141
-13.750 -0.6657 0.02697 0.02123 -0.1386 0.8221 0.0145
-13.500 -0.6514 0.02605 0.02028 -0.1383 0.8211 0.0147
-13.250 -0.6378 0.02513 0.01931 -0.1379 0.8199 0.0148
-13.000 -0.6224 0.02435 0.01850 -0.1376 0.8188 0.0150
-12.750 -0.6064 0.02363 0.01775 -0.1373 0.8176 0.0152
-12.500 -0.5922 0.02283 0.01690 -0.1367 0.8164 0.0154
-12.250 -0.5774 0.02209 0.01612 -0.1361 0.8152 0.0156
-12.000 -0.5612 0.02144 0.01544 -0.1356 0.8140 0.0159
-11.750 -0.5441 0.02086 0.01482 -0.1351 0.8128 0.0161
-11.500 -0.5282 0.02023 0.01415 -0.1345 0.8114 0.0163
-11.250 -0.5117 0.01966 0.01353 -0.1338 0.8097 0.0165
-11.000 -0.4952 0.01910 0.01292 -0.1331 0.8076 0.0166
-10.750 -0.4811 0.01844 0.01223 -0.1321 0.8056 0.0169
-10.500 -0.4663 0.01783 0.01160 -0.1311 0.8042 0.0171
-10.250 -0.4516 0.01724 0.01099 -0.1300 0.8026 0.0176
-10.000 -0.4351 0.01674 0.01048 -0.1290 0.8010 0.0178
-9.750 -0.4184 0.01626 0.00999 -0.1281 0.7993 0.0182
-9.500 -0.4012 0.01583 0.00954 -0.1271 0.7973 0.0186
-9.250 -0.3843 0.01539 0.00907 -0.1261 0.7952 0.0189
-9.000 -0.3669 0.01498 0.00863 -0.1251 0.7934 0.0192
-8.750 -0.3493 0.01460 0.00821 -0.1241 0.7913 0.0197
-8.500 -0.3310 0.01424 0.00783 -0.1232 0.7896 0.0200
-8.250 -0.3128 0.01388 0.00746 -0.1221 0.7883 0.0203
-8.000 -0.2960 0.01349 0.00707 -0.1209 0.7865 0.0211
-7.750 -0.2791 0.01311 0.00669 -0.1197 0.7847 0.0218
-7.500 -0.2617 0.01275 0.00634 -0.1184 0.7826 0.0226
-7.250 -0.2442 0.01243 0.00600 -0.1172 0.7804 0.0234
-7.000 -0.2266 0.01212 0.00568 -0.1159 0.7784 0.0242
-6.750 -0.2097 0.01185 0.00538 -0.1144 0.7764 0.0250
-6.500 -0.1958 0.01159 0.00512 -0.1124 0.7741 0.0264
-6.250 -0.1802 0.01135 0.00488 -0.1107 0.7722 0.0282
-6.000 -0.1606 0.01110 0.00464 -0.1097 0.7700 0.0305
-5.750 -0.1400 0.01084 0.00441 -0.1090 0.7676 0.0346
-5.500 -0.1187 0.01059 0.00419 -0.1083 0.7650 0.0413
-5.250 -0.0965 0.01035 0.00397 -0.1077 0.7623 0.0499
-5.000 -0.0738 0.01011 0.00377 -0.1073 0.7597 0.0610
-4.750 -0.0507 0.00986 0.00357 -0.1069 0.7573 0.0751
-4.250 -0.0051 0.00916 0.00314 -0.1062 0.7510 0.1408
-4.000 0.0170 0.00866 0.00286 -0.1059 0.7473 0.2012
-3.750 0.0385 0.00791 0.00249 -0.1058 0.7436 0.3062
-3.500 0.0640 0.00725 0.00220 -0.1064 0.7400 0.4041
-3.250 0.0926 0.00683 0.00203 -0.1074 0.7355 0.4743
-3.000 0.1218 0.00659 0.00192 -0.1082 0.7303 0.5184
-2.750 0.1513 0.00643 0.00184 -0.1089 0.7251 0.5504
-2.500 0.1810 0.00634 0.00179 -0.1096 0.7186 0.5700
-2.250 0.2097 0.00629 0.00173 -0.1101 0.7119 0.5801
-2.000 0.2388 0.00628 0.00170 -0.1106 0.7036 0.5868
-1.750 0.2669 0.00628 0.00166 -0.1109 0.6941 0.5931
-1.500 0.2949 0.00630 0.00164 -0.1112 0.6834 0.5998
-1.250 0.3228 0.00633 0.00163 -0.1114 0.6738 0.6062
-1.000 0.3505 0.00637 0.00163 -0.1117 0.6649 0.6130
-0.750 0.3787 0.00641 0.00165 -0.1120 0.6565 0.6196
-0.500 0.4062 0.00647 0.00167 -0.1122 0.6486 0.6260
-0.250 0.4346 0.00651 0.00170 -0.1126 0.6414 0.6332
0.000 0.4621 0.00658 0.00174 -0.1128 0.6346 0.6396
0.250 0.4908 0.00662 0.00179 -0.1132 0.6293 0.6462
0.500 0.5191 0.00667 0.00183 -0.1136 0.6235 0.6532
0.750 0.5465 0.00675 0.00190 -0.1138 0.6176 0.6597
1.000 0.5751 0.00679 0.00196 -0.1142 0.6124 0.6665
1.250 0.6031 0.00686 0.00202 -0.1145 0.6069 0.6722
1.500 0.6305 0.00694 0.00210 -0.1147 0.6018 0.6783
1.750 0.6586 0.00700 0.00218 -0.1150 0.5972 0.6847
2.000 0.6865 0.00707 0.00225 -0.1153 0.5920 0.6898
2.250 0.7134 0.00717 0.00235 -0.1154 0.5866 0.6950
2.500 0.7403 0.00726 0.00244 -0.1154 0.5806 0.6999
2.750 0.7667 0.00736 0.00253 -0.1154 0.5728 0.7043
3.000 0.7921 0.00749 0.00266 -0.1152 0.5663 0.7087
3.250 0.8190 0.00758 0.00276 -0.1153 0.5601 0.7130
3.750 0.8682 0.00785 0.00299 -0.1146 0.5424 0.7201
4.000 0.8912 0.00801 0.00314 -0.1138 0.5343 0.7231
4.250 0.9157 0.00813 0.00328 -0.1135 0.5262 0.7265
4.500 0.9356 0.00831 0.00343 -0.1121 0.5162 0.7301
4.750 0.9537 0.00852 0.00359 -0.1105 0.5029 0.7334
5.000 0.9715 0.00878 0.00379 -0.1088 0.4872 0.7360
5.250 0.9870 0.00910 0.00406 -0.1067 0.4689 0.7384
5.500 1.0029 0.00944 0.00435 -0.1047 0.4507 0.7411
5.750 1.0191 0.00978 0.00466 -0.1029 0.4343 0.7440
6.000 1.0333 0.01022 0.00501 -0.1008 0.4136 0.7468
6.250 1.0391 0.01095 0.00557 -0.0973 0.3779 0.7494
6.500 1.0395 0.01195 0.00633 -0.0931 0.3320 0.7518
6.750 1.0394 0.01305 0.00722 -0.0890 0.2855 0.7542
7.000 1.0365 0.01438 0.00828 -0.0847 0.2323 0.7566
7.250 1.0399 0.01551 0.00923 -0.0815 0.1930 0.7590
7.500 1.0461 0.01657 0.01013 -0.0789 0.1612 0.7614
7.750 1.0528 0.01765 0.01106 -0.0764 0.1314 0.7639
8.000 1.0601 0.01874 0.01201 -0.0741 0.1037 0.7663
8.250 1.0711 0.01967 0.01286 -0.0724 0.0879 0.7682
8.500 1.0862 0.02037 0.01356 -0.0712 0.0809 0.7702
8.750 1.1004 0.02113 0.01432 -0.0699 0.0752 0.7720
9.000 1.1166 0.02181 0.01501 -0.0688 0.0709 0.7737
9.250 1.1321 0.02253 0.01575 -0.0678 0.0673 0.7754
9.500 1.1463 0.02334 0.01656 -0.0666 0.0635 0.7770
9.750 1.1626 0.02406 0.01729 -0.0657 0.0609 0.7786
10.000 1.1784 0.02481 0.01806 -0.0648 0.0583 0.7802
10.250 1.1924 0.02568 0.01895 -0.0638 0.0549 0.7816
10.500 1.2068 0.02657 0.01983 -0.0628 0.0516 0.7830
10.750 1.2214 0.02745 0.02073 -0.0619 0.0485 0.7841
11.000 1.2338 0.02850 0.02177 -0.0608 0.0443 0.7855
11.250 1.2476 0.02946 0.02276 -0.0599 0.0410 0.7868
11.500 1.2588 0.03063 0.02392 -0.0588 0.0372 0.7881
11.750 1.2714 0.03173 0.02505 -0.0578 0.0340 0.7894
12.000 1.2820 0.03301 0.02632 -0.0568 0.0307 0.7905
12.250 1.2941 0.03421 0.02755 -0.0559 0.0285 0.7918
12.500 1.3059 0.03546 0.02883 -0.0551 0.0270 0.7931
12.750 1.3165 0.03685 0.03024 -0.0542 0.0252 0.7942
13.000 1.3286 0.03813 0.03156 -0.0535 0.0241 0.7953
13.250 1.3395 0.03956 0.03302 -0.0528 0.0231 0.7963
13.500 1.3502 0.04103 0.03452 -0.0522 0.0221 0.7974
13.750 1.3597 0.04265 0.03616 -0.0515 0.0210 0.7985
14.000 1.3712 0.04411 0.03767 -0.0510 0.0204 0.7994
14.250 1.3815 0.04571 0.03932 -0.0505 0.0197 0.8002
14.500 1.3915 0.04736 0.04102 -0.0501 0.0189 0.8011
14.750 1.4004 0.04916 0.04286 -0.0496 0.0182 0.8021
15.000 1.4089 0.05103 0.04477 -0.0492 0.0175 0.8030
15.250 1.4179 0.05287 0.04667 -0.0489 0.0170 0.8039
15.500 1.4274 0.05468 0.04855 -0.0487 0.0166 0.8048
15.750 1.4360 0.05661 0.05054 -0.0485 0.0161 0.8058
16.000 1.4443 0.05862 0.05260 -0.0483 0.0155 0.8069
16.250 1.4516 0.06076 0.05479 -0.0482 0.0148 0.8079
16.500 1.4583 0.06300 0.05708 -0.0482 0.0143 0.8089
16.750 1.4649 0.06528 0.05941 -0.0482 0.0138 0.8098
17.000 1.4723 0.06750 0.06170 -0.0483 0.0134 0.8106
17.250 1.4791 0.06982 0.06409 -0.0484 0.0129 0.8115
17.500 1.4851 0.07228 0.06660 -0.0486 0.0124 0.8123
17.750 1.4907 0.07480 0.06918 -0.0489 0.0120 0.8131
18.000 1.4952 0.07752 0.07195 -0.0492 0.0115 0.8138
18.250 1.4993 0.08028 0.07477 -0.0496 0.0111 0.8145
18.500 1.5038 0.08306 0.07762 -0.0501 0.0108 0.8152
18.750 1.5086 0.08579 0.08042 -0.0506 0.0105 0.8158
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