WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il) Reynolds number: 500,000 Max Cl/Cd: 97.84 at α=5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx05188-il-500000-n5.txt Download as CSV file: xf-fx05188-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-188 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-17.250 -0.6802 0.09838 0.09509 -0.0743 1.0000 0.0137
-17.000 -0.7046 0.08939 0.08594 -0.0787 0.9821 0.0137
-16.750 -0.7156 0.08031 0.07660 -0.0878 0.9481 0.0138
-16.500 -0.7217 0.07192 0.06793 -0.0969 0.9350 0.0138
-16.250 -0.7154 0.06564 0.06145 -0.1049 0.9234 0.0141
-16.000 -0.7043 0.05967 0.05518 -0.1135 0.9084 0.0141
-15.750 -0.6894 0.05542 0.05069 -0.1199 0.8905 0.0142
-15.500 -0.6808 0.05184 0.04687 -0.1239 0.8750 0.0142
-15.000 -0.6665 0.04673 0.04141 -0.1278 0.8540 0.0144
-14.500 -0.6532 0.04249 0.03689 -0.1296 0.8395 0.0147
-14.250 -0.6459 0.04061 0.03487 -0.1300 0.8330 0.0147
-13.750 -0.6281 0.03739 0.03140 -0.1304 0.8225 0.0150
-13.500 -0.6182 0.03597 0.02987 -0.1303 0.8175 0.0151
-13.250 -0.6071 0.03467 0.02845 -0.1302 0.8129 0.0153
-13.000 -0.5952 0.03346 0.02713 -0.1300 0.8086 0.0155
-12.750 -0.5826 0.03230 0.02589 -0.1296 0.8043 0.0156
-12.500 -0.5691 0.03121 0.02470 -0.1291 0.7998 0.0157
-12.250 -0.5550 0.03021 0.02360 -0.1287 0.7958 0.0158
-12.000 -0.5405 0.02928 0.02259 -0.1283 0.7920 0.0161
-11.750 -0.5256 0.02838 0.02162 -0.1277 0.7877 0.0163
-11.500 -0.5104 0.02752 0.02068 -0.1271 0.7833 0.0164
-11.250 -0.4949 0.02673 0.01982 -0.1265 0.7793 0.0166
-11.000 -0.4790 0.02598 0.01899 -0.1259 0.7756 0.0168
-10.750 -0.4631 0.02523 0.01818 -0.1253 0.7719 0.0170
-10.500 -0.4470 0.02455 0.01744 -0.1246 0.7682 0.0171
-10.250 -0.4322 0.02377 0.01661 -0.1237 0.7647 0.0174
-10.000 -0.4183 0.02298 0.01579 -0.1228 0.7614 0.0177
-9.750 -0.4040 0.02223 0.01502 -0.1219 0.7580 0.0180
-9.500 -0.3890 0.02156 0.01433 -0.1210 0.7547 0.0183
-9.250 -0.3743 0.02090 0.01364 -0.1200 0.7513 0.0185
-9.000 -0.3598 0.02025 0.01295 -0.1189 0.7480 0.0187
-8.750 -0.3450 0.01964 0.01229 -0.1178 0.7450 0.0190
-8.500 -0.3303 0.01902 0.01165 -0.1167 0.7420 0.0194
-8.250 -0.3155 0.01844 0.01104 -0.1155 0.7391 0.0196
-8.000 -0.3008 0.01787 0.01043 -0.1143 0.7363 0.0198
-7.750 -0.2857 0.01735 0.00986 -0.1131 0.7336 0.0203
-7.500 -0.2703 0.01685 0.00932 -0.1118 0.7312 0.0207
-7.250 -0.2550 0.01637 0.00880 -0.1105 0.7290 0.0210
-7.000 -0.2414 0.01586 0.00827 -0.1089 0.7267 0.0212
-6.750 -0.2311 0.01534 0.00774 -0.1067 0.7241 0.0218
-6.500 -0.2197 0.01493 0.00732 -0.1047 0.7217 0.0225
-6.250 -0.2022 0.01455 0.00691 -0.1037 0.7195 0.0232
-6.000 -0.1828 0.01420 0.00653 -0.1030 0.7173 0.0241
-5.750 -0.1616 0.01390 0.00617 -0.1025 0.7151 0.0250
-5.500 -0.1394 0.01362 0.00584 -0.1021 0.7130 0.0259
-5.250 -0.1171 0.01331 0.00554 -0.1017 0.7112 0.0274
-5.000 -0.0937 0.01304 0.00528 -0.1015 0.7093 0.0298
-4.750 -0.0702 0.01275 0.00501 -0.1013 0.7071 0.0355
-4.500 -0.0479 0.01229 0.00469 -0.1011 0.7049 0.0672
-4.250 -0.0266 0.01161 0.00430 -0.1010 0.7026 0.1352
-4.000 -0.0062 0.01038 0.00367 -0.1016 0.7004 0.2846
-3.750 0.0207 0.00929 0.00316 -0.1032 0.6984 0.4342
-3.500 0.0508 0.00892 0.00302 -0.1045 0.6965 0.5084
-3.250 0.0804 0.00876 0.00298 -0.1052 0.6947 0.5433
-3.000 0.1098 0.00866 0.00298 -0.1058 0.6925 0.5716
-2.750 0.1392 0.00863 0.00300 -0.1063 0.6901 0.5887
-2.500 0.1686 0.00865 0.00305 -0.1067 0.6877 0.6040
-2.250 0.1980 0.00870 0.00310 -0.1072 0.6854 0.6150
-2.000 0.2279 0.00874 0.00310 -0.1077 0.6832 0.6231
-1.750 0.2574 0.00880 0.00314 -0.1082 0.6811 0.6282
-1.500 0.2874 0.00886 0.00314 -0.1088 0.6790 0.6333
-1.250 0.3168 0.00887 0.00314 -0.1094 0.6765 0.6381
-1.000 0.3456 0.00890 0.00319 -0.1097 0.6736 0.6416
-0.750 0.3749 0.00893 0.00321 -0.1102 0.6708 0.6454
-0.500 0.4045 0.00896 0.00321 -0.1107 0.6682 0.6499
-0.250 0.4340 0.00901 0.00323 -0.1112 0.6657 0.6542
0.000 0.4631 0.00908 0.00328 -0.1116 0.6631 0.6577
0.250 0.4918 0.00912 0.00334 -0.1119 0.6596 0.6617
0.500 0.5207 0.00914 0.00336 -0.1124 0.6552 0.6656
0.750 0.5498 0.00915 0.00334 -0.1128 0.6507 0.6687
1.000 0.5781 0.00918 0.00336 -0.1130 0.6467 0.6707
1.250 0.6065 0.00920 0.00343 -0.1133 0.6424 0.6728
1.500 0.6349 0.00924 0.00348 -0.1136 0.6383 0.6751
1.750 0.6634 0.00927 0.00352 -0.1139 0.6343 0.6776
2.000 0.6919 0.00932 0.00355 -0.1143 0.6304 0.6803
2.250 0.7206 0.00936 0.00360 -0.1147 0.6257 0.6828
2.500 0.7491 0.00940 0.00365 -0.1150 0.6210 0.6848
2.750 0.7767 0.00944 0.00370 -0.1151 0.6169 0.6865
3.000 0.8044 0.00949 0.00378 -0.1153 0.6123 0.6882
3.250 0.8316 0.00955 0.00387 -0.1154 0.6063 0.6900
3.500 0.8579 0.00963 0.00393 -0.1152 0.5986 0.6921
3.750 0.8843 0.00971 0.00402 -0.1151 0.5899 0.6942
4.000 0.9107 0.00982 0.00412 -0.1151 0.5836 0.6963
4.250 0.9379 0.00991 0.00423 -0.1152 0.5774 0.6982
4.500 0.9641 0.01004 0.00434 -0.1151 0.5707 0.6998
4.750 0.9893 0.01017 0.00447 -0.1149 0.5606 0.7013
5.000 1.0117 0.01034 0.00462 -0.1140 0.5462 0.7030
5.250 1.0321 0.01056 0.00481 -0.1128 0.5269 0.7046
5.500 1.0508 0.01084 0.00502 -0.1113 0.5060 0.7063
5.750 1.0679 0.01117 0.00528 -0.1095 0.4842 0.7080
6.000 1.0839 0.01151 0.00556 -0.1075 0.4600 0.7096
6.250 1.0938 0.01193 0.00588 -0.1044 0.4354 0.7114
6.500 1.1008 0.01247 0.00630 -0.1009 0.4084 0.7133
6.750 1.1042 0.01322 0.00691 -0.0969 0.3781 0.7152
7.000 1.1073 0.01405 0.00760 -0.0932 0.3477 0.7169
7.250 1.1044 0.01518 0.00854 -0.0888 0.3079 0.7187
7.500 1.0980 0.01660 0.00976 -0.0842 0.2638 0.7205
7.750 1.0941 0.01810 0.01108 -0.0804 0.2252 0.7222
8.000 1.0933 0.01959 0.01241 -0.0772 0.1904 0.7240
8.250 1.0960 0.02098 0.01369 -0.0747 0.1632 0.7259
8.500 1.0992 0.02241 0.01500 -0.0724 0.1367 0.7277
8.750 1.1012 0.02399 0.01643 -0.0700 0.1075 0.7294
9.000 1.1079 0.02533 0.01769 -0.0683 0.0903 0.7310
9.250 1.1169 0.02656 0.01888 -0.0668 0.0799 0.7324
9.500 1.1271 0.02775 0.02006 -0.0656 0.0723 0.7337
10.000 1.1500 0.03003 0.02236 -0.0635 0.0599 0.7359
10.250 1.1605 0.03126 0.02359 -0.0624 0.0518 0.7371
10.500 1.1691 0.03267 0.02498 -0.0612 0.0418 0.7384
10.750 1.1777 0.03412 0.02641 -0.0601 0.0348 0.7398
11.000 1.1866 0.03560 0.02790 -0.0591 0.0309 0.7412
11.250 1.1973 0.03696 0.02930 -0.0583 0.0288 0.7425
11.500 1.2068 0.03846 0.03083 -0.0575 0.0272 0.7437
11.750 1.2175 0.03990 0.03232 -0.0567 0.0260 0.7451
12.000 1.2282 0.04138 0.03386 -0.0561 0.0251 0.7464
12.250 1.2385 0.04292 0.03545 -0.0555 0.0243 0.7478
12.500 1.2483 0.04454 0.03712 -0.0549 0.0236 0.7491
12.750 1.2570 0.04630 0.03892 -0.0544 0.0230 0.7505
13.250 1.2727 0.05009 0.04284 -0.0533 0.0219 0.7531
13.500 1.2821 0.05188 0.04471 -0.0529 0.0216 0.7547
13.750 1.2905 0.05381 0.04672 -0.0526 0.0213 0.7564
14.000 1.2986 0.05580 0.04879 -0.0523 0.0209 0.7581
14.250 1.3061 0.05790 0.05097 -0.0521 0.0204 0.7599
14.500 1.3141 0.06001 0.05315 -0.0520 0.0200 0.7616
14.750 1.3207 0.06230 0.05551 -0.0519 0.0196 0.7634
15.000 1.3269 0.06468 0.05796 -0.0519 0.0192 0.7652
15.250 1.3319 0.06725 0.06059 -0.0520 0.0189 0.7669
15.500 1.3357 0.07000 0.06341 -0.0521 0.0186 0.7686
15.750 1.3381 0.07297 0.06646 -0.0523 0.0183 0.7701
16.000 1.3412 0.07591 0.06949 -0.0525 0.0181 0.7719
16.250 1.3474 0.07850 0.07218 -0.0529 0.0179 0.7739
16.500 1.3523 0.08128 0.07505 -0.0533 0.0177 0.7760
16.750 1.3572 0.08408 0.07795 -0.0538 0.0175 0.7782
17.000 1.3615 0.08704 0.08099 -0.0544 0.0173 0.7804
17.250 1.3660 0.08997 0.08401 -0.0550 0.0170 0.7827
17.500 1.3696 0.09308 0.08720 -0.0558 0.0167 0.7847
17.750 1.3737 0.09612 0.09034 -0.0566 0.0164 0.7868
18.000 1.3766 0.09936 0.09368 -0.0575 0.0162 0.7890
18.250 1.3797 0.10260 0.09701 -0.0585 0.0160 0.7914
18.500 1.3820 0.10598 0.10048 -0.0596 0.0158 0.7938
18.750 1.3843 0.10941 0.10400 -0.0609 0.0156 0.7964
19.000 1.3861 0.11292 0.10758 -0.0622 0.0154 0.7988
19.250 1.3872 0.11655 0.11129 -0.0636 0.0152 0.8010
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