WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il) Reynolds number: 1,000,000 Max Cl/Cd: 117.94 at α=4° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx05188-il-1000000-n5.txt Download as CSV file: xf-fx05188-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.500 -0.7928 0.11624 0.11361 -0.0596 1.0000 0.0108
-19.250 -0.8252 0.10537 0.10253 -0.0662 0.9998 0.0109
-18.750 -0.8536 0.09030 0.08718 -0.0759 0.9547 0.0109
-18.500 -0.8607 0.08173 0.07838 -0.0847 0.9383 0.0111
-18.250 -0.8528 0.07525 0.07162 -0.0929 0.9102 0.0110
-18.000 -0.8465 0.07005 0.06617 -0.0990 0.8820 0.0112
-17.750 -0.8421 0.06564 0.06157 -0.1034 0.8668 0.0112
-17.500 -0.8358 0.06174 0.05752 -0.1074 0.8571 0.0113
-17.250 -0.8287 0.05840 0.05405 -0.1105 0.8487 0.0114
-17.000 -0.8233 0.05524 0.05076 -0.1130 0.8422 0.0114
-16.750 -0.8155 0.05260 0.04803 -0.1151 0.8365 0.0115
-16.500 -0.8075 0.05002 0.04533 -0.1170 0.8311 0.0116
-16.250 -0.7963 0.04788 0.04311 -0.1188 0.8264 0.0117
-16.000 -0.7919 0.04534 0.04046 -0.1200 0.8224 0.0117
-15.750 -0.7821 0.04334 0.03837 -0.1212 0.8178 0.0118
-15.500 -0.7721 0.04139 0.03632 -0.1223 0.8133 0.0118
-15.250 -0.7604 0.03970 0.03455 -0.1233 0.8093 0.0119
-15.000 -0.7492 0.03811 0.03290 -0.1239 0.8052 0.0120
-14.750 -0.7392 0.03645 0.03115 -0.1244 0.8008 0.0121
-14.500 -0.7257 0.03511 0.02973 -0.1250 0.7966 0.0122
-14.250 -0.7141 0.03370 0.02824 -0.1253 0.7926 0.0123
-14.000 -0.7020 0.03239 0.02687 -0.1254 0.7886 0.0124
-13.750 -0.6886 0.03122 0.02564 -0.1255 0.7838 0.0125
-13.500 -0.6755 0.03009 0.02442 -0.1255 0.7791 0.0126
-13.250 -0.6618 0.02903 0.02330 -0.1254 0.7748 0.0127
-13.000 -0.6478 0.02804 0.02225 -0.1253 0.7696 0.0128
-12.750 -0.6343 0.02706 0.02120 -0.1250 0.7644 0.0129
-12.500 -0.6211 0.02609 0.02016 -0.1245 0.7598 0.0130
-12.250 -0.6068 0.02520 0.01922 -0.1242 0.7548 0.0131
-12.000 -0.5911 0.02445 0.01841 -0.1238 0.7494 0.0133
-11.750 -0.5763 0.02366 0.01755 -0.1233 0.7450 0.0134
-11.500 -0.5615 0.02288 0.01671 -0.1227 0.7413 0.0135
-11.250 -0.5461 0.02215 0.01593 -0.1222 0.7379 0.0136
-11.000 -0.5301 0.02148 0.01522 -0.1216 0.7346 0.0137
-10.500 -0.4985 0.02019 0.01382 -0.1203 0.7288 0.0138
-10.250 -0.4875 0.01928 0.01288 -0.1191 0.7263 0.0141
-10.000 -0.4724 0.01863 0.01220 -0.1182 0.7237 0.0142
-9.750 -0.4574 0.01800 0.01154 -0.1173 0.7209 0.0145
-9.500 -0.4407 0.01749 0.01100 -0.1164 0.7179 0.0148
-9.250 -0.4244 0.01698 0.01046 -0.1155 0.7152 0.0150
-9.000 -0.4077 0.01650 0.00995 -0.1146 0.7129 0.0152
-8.750 -0.3907 0.01601 0.00945 -0.1137 0.7113 0.0154
-8.500 -0.3740 0.01553 0.00895 -0.1126 0.7096 0.0157
-8.250 -0.3577 0.01506 0.00846 -0.1115 0.7078 0.0159
-8.000 -0.3418 0.01459 0.00798 -0.1103 0.7059 0.0160
-7.750 -0.3257 0.01418 0.00754 -0.1090 0.7040 0.0164
-7.500 -0.3105 0.01379 0.00712 -0.1075 0.7021 0.0166
-7.250 -0.2981 0.01345 0.00675 -0.1054 0.7003 0.0169
-7.000 -0.2821 0.01311 0.00638 -0.1041 0.6983 0.0170
-6.500 -0.2421 0.01238 0.00561 -0.1030 0.6951 0.0177
-6.250 -0.2199 0.01206 0.00528 -0.1026 0.6938 0.0182
-6.000 -0.1965 0.01178 0.00500 -0.1023 0.6924 0.0187
-5.750 -0.1722 0.01153 0.00475 -0.1022 0.6908 0.0193
-5.500 -0.1473 0.01131 0.00452 -0.1022 0.6891 0.0199
-5.250 -0.1217 0.01111 0.00431 -0.1022 0.6873 0.0205
-5.000 -0.0958 0.01092 0.00411 -0.1023 0.6856 0.0213
-4.750 -0.0698 0.01071 0.00390 -0.1024 0.6840 0.0227
-4.500 -0.0432 0.01054 0.00372 -0.1026 0.6823 0.0242
-4.250 -0.0164 0.01038 0.00355 -0.1028 0.6804 0.0269
-4.000 0.0096 0.01004 0.00332 -0.1031 0.6787 0.0525
-3.750 0.0363 0.00968 0.00311 -0.1035 0.6771 0.0864
-3.500 0.0623 0.00895 0.00275 -0.1043 0.6753 0.1838
-3.250 0.0905 0.00776 0.00224 -0.1061 0.6735 0.3600
-3.000 0.1220 0.00708 0.00197 -0.1080 0.6716 0.4726
-2.750 0.1530 0.00685 0.00188 -0.1091 0.6696 0.5157
-2.500 0.1834 0.00675 0.00182 -0.1099 0.6675 0.5389
-2.250 0.2136 0.00669 0.00178 -0.1106 0.6653 0.5561
-2.000 0.2438 0.00663 0.00176 -0.1114 0.6629 0.5763
-1.750 0.2741 0.00658 0.00175 -0.1121 0.6609 0.5883
-1.500 0.3045 0.00655 0.00176 -0.1128 0.6587 0.5996
-1.250 0.3347 0.00655 0.00177 -0.1135 0.6561 0.6091
-1.000 0.3646 0.00655 0.00178 -0.1141 0.6532 0.6151
-0.750 0.3942 0.00657 0.00177 -0.1146 0.6498 0.6206
-0.500 0.4235 0.00660 0.00179 -0.1150 0.6461 0.6256
-0.250 0.4533 0.00661 0.00181 -0.1156 0.6416 0.6309
0.000 0.4828 0.00663 0.00181 -0.1161 0.6364 0.6358
0.250 0.5117 0.00667 0.00183 -0.1165 0.6315 0.6398
0.500 0.5412 0.00670 0.00187 -0.1170 0.6270 0.6440
0.750 0.5705 0.00675 0.00191 -0.1174 0.6220 0.6484
1.000 0.5992 0.00681 0.00193 -0.1178 0.6167 0.6524
1.250 0.6282 0.00685 0.00198 -0.1182 0.6120 0.6553
1.500 0.6570 0.00690 0.00204 -0.1186 0.6069 0.6578
1.750 0.6854 0.00697 0.00210 -0.1189 0.6018 0.6601
2.000 0.7140 0.00704 0.00215 -0.1192 0.5972 0.6623
2.250 0.7425 0.00711 0.00221 -0.1195 0.5908 0.6645
2.500 0.7697 0.00722 0.00228 -0.1196 0.5827 0.6666
2.750 0.7977 0.00732 0.00236 -0.1198 0.5747 0.6683
3.000 0.8245 0.00743 0.00245 -0.1198 0.5674 0.6702
3.250 0.8527 0.00750 0.00254 -0.1201 0.5616 0.6718
3.500 0.8801 0.00760 0.00264 -0.1202 0.5553 0.6734
3.750 0.9069 0.00772 0.00275 -0.1202 0.5474 0.6749
4.000 0.9317 0.00790 0.00289 -0.1199 0.5323 0.6765
4.250 0.9559 0.00811 0.00304 -0.1194 0.5147 0.6781
4.500 0.9797 0.00834 0.00320 -0.1188 0.4966 0.6798
4.750 1.0002 0.00869 0.00343 -0.1177 0.4696 0.6813
5.000 1.0182 0.00913 0.00371 -0.1161 0.4352 0.6827
5.250 1.0325 0.00969 0.00407 -0.1139 0.3967 0.6839
5.500 1.0464 0.01022 0.00445 -0.1116 0.3641 0.6849
5.750 1.0580 0.01071 0.00481 -0.1089 0.3342 0.6864
6.000 1.0632 0.01134 0.00527 -0.1049 0.2958 0.6877
6.250 1.0658 0.01215 0.00589 -0.1008 0.2570 0.6892
6.500 1.0679 0.01301 0.00658 -0.0967 0.2196 0.6907
6.750 1.0662 0.01408 0.00745 -0.0923 0.1797 0.6921
7.000 1.0690 0.01508 0.00832 -0.0889 0.1499 0.6934
7.250 1.0733 0.01612 0.00923 -0.0859 0.1222 0.6947
7.500 1.0766 0.01730 0.01027 -0.0829 0.0940 0.6961
7.750 1.0872 0.01819 0.01111 -0.0811 0.0815 0.6973
8.000 1.1003 0.01898 0.01188 -0.0796 0.0744 0.6987
8.250 1.1143 0.01975 0.01264 -0.0784 0.0680 0.6999
8.750 1.1412 0.02141 0.01429 -0.0758 0.0558 0.7031
9.000 1.1530 0.02236 0.01522 -0.0744 0.0477 0.7048
9.250 1.1605 0.02360 0.01640 -0.0726 0.0346 0.7063
9.500 1.1711 0.02470 0.01747 -0.0712 0.0285 0.7074
9.750 1.1833 0.02571 0.01850 -0.0701 0.0258 0.7084
10.000 1.1966 0.02667 0.01948 -0.0690 0.0244 0.7093
10.250 1.2086 0.02775 0.02058 -0.0680 0.0229 0.7102
10.500 1.2214 0.02879 0.02165 -0.0670 0.0219 0.7113
10.750 1.2347 0.02982 0.02272 -0.0661 0.0213 0.7124
11.000 1.2476 0.03091 0.02383 -0.0652 0.0207 0.7134
11.250 1.2598 0.03206 0.02502 -0.0644 0.0202 0.7142
11.500 1.2720 0.03324 0.02623 -0.0635 0.0197 0.7151
11.750 1.2833 0.03453 0.02755 -0.0627 0.0192 0.7159
12.000 1.2945 0.03585 0.02891 -0.0619 0.0187 0.7166
12.250 1.3044 0.03731 0.03040 -0.0610 0.0182 0.7173
12.750 1.3285 0.03994 0.03313 -0.0598 0.0177 0.7193
13.000 1.3397 0.04137 0.03462 -0.0592 0.0174 0.7204
13.250 1.3511 0.04281 0.03611 -0.0587 0.0171 0.7215
13.500 1.3618 0.04434 0.03770 -0.0582 0.0168 0.7228
13.750 1.3720 0.04594 0.03935 -0.0577 0.0166 0.7242
14.000 1.3821 0.04758 0.04105 -0.0573 0.0163 0.7256
14.250 1.3911 0.04937 0.04289 -0.0568 0.0160 0.7270
14.500 1.4004 0.05115 0.04471 -0.0565 0.0157 0.7283
14.750 1.4082 0.05314 0.04676 -0.0561 0.0155 0.7296
15.000 1.4154 0.05520 0.04887 -0.0558 0.0152 0.7308
15.250 1.4211 0.05749 0.05122 -0.0556 0.0149 0.7321
15.500 1.4277 0.05973 0.05352 -0.0554 0.0147 0.7334
15.750 1.4356 0.06186 0.05573 -0.0553 0.0145 0.7347
16.250 1.4520 0.06615 0.06015 -0.0555 0.0142 0.7382
16.500 1.4591 0.06844 0.06252 -0.0556 0.0140 0.7402
16.750 1.4652 0.07092 0.06508 -0.0558 0.0138 0.7422
17.000 1.4716 0.07338 0.06761 -0.0560 0.0136 0.7444
17.250 1.4769 0.07604 0.07035 -0.0563 0.0135 0.7466
17.500 1.4824 0.07867 0.07305 -0.0567 0.0133 0.7488
17.750 1.4869 0.08150 0.07595 -0.0572 0.0131 0.7510
18.000 1.4917 0.08428 0.07880 -0.0577 0.0130 0.7534
18.250 1.4952 0.08730 0.08191 -0.0583 0.0128 0.7561
18.500 1.4992 0.09028 0.08496 -0.0590 0.0126 0.7591
18.750 1.5016 0.09352 0.08828 -0.0599 0.0124 0.7620
19.000 1.5038 0.09681 0.09164 -0.0608 0.0122 0.7649
19.250 1.5046 0.10035 0.09525 -0.0618 0.0121 0.7675
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