WORTMANN FX 05-188 AIRFOIL (fx05188-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 05-188 AIRFOIL (fx05188-il) Reynolds number: 1,000,000 Max Cl/Cd: 126.87 at α=5.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx05188-il-1000000.txt Download as CSV file: xf-fx05188-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-16.500 -0.5840 0.10069 0.09860 -0.0776 0.9546 0.0177
-16.250 -0.5973 0.08979 0.08752 -0.0884 0.9422 0.0179
-16.000 -0.6039 0.08054 0.07805 -0.0973 0.9262 0.0164
-15.750 -0.6244 0.06995 0.06711 -0.1079 0.9049 0.0164
-15.500 -0.6424 0.06110 0.05792 -0.1166 0.8888 0.0161
-15.250 -0.6500 0.05506 0.05157 -0.1227 0.8750 0.0162
-15.000 -0.6599 0.04990 0.04612 -0.1265 0.8637 0.0161
-14.750 -0.6657 0.04602 0.04201 -0.1287 0.8552 0.0161
-14.500 -0.6704 0.04253 0.03827 -0.1302 0.8475 0.0161
-14.250 -0.6705 0.03977 0.03531 -0.1310 0.8409 0.0160
-14.000 -0.6686 0.03728 0.03264 -0.1312 0.8349 0.0160
-13.750 -0.6615 0.03543 0.03061 -0.1316 0.8288 0.0162
-13.500 -0.6542 0.03376 0.02881 -0.1314 0.8236 0.0164
-13.250 -0.6455 0.03227 0.02718 -0.1312 0.8181 0.0165
-13.000 -0.6367 0.03134 0.02612 -0.1310 0.8123 0.0169
-12.750 -0.6257 0.03004 0.02470 -0.1305 0.8075 0.0169
-12.500 -0.6111 0.02869 0.02324 -0.1300 0.8026 0.0169
-12.250 -0.5985 0.02772 0.02216 -0.1294 0.7975 0.0170
-12.000 -0.5926 0.02711 0.02143 -0.1285 0.7922 0.0172
-11.750 -0.5745 0.02597 0.02020 -0.1279 0.7882 0.0173
-11.500 -0.5468 0.02460 0.01874 -0.1278 0.7847 0.0174
-11.250 -0.5252 0.02377 0.01785 -0.1274 0.7811 0.0176
-11.000 -0.5047 0.02297 0.01702 -0.1269 0.7774 0.0179
-10.750 -0.4865 0.02224 0.01628 -0.1262 0.7741 0.0181
-10.500 -0.4688 0.02158 0.01559 -0.1255 0.7704 0.0182
-10.250 -0.4517 0.02091 0.01489 -0.1248 0.7668 0.0184
-10.000 -0.4344 0.02033 0.01426 -0.1241 0.7633 0.0186
-9.750 -0.4178 0.01969 0.01359 -0.1232 0.7601 0.0188
-9.500 -0.4009 0.01910 0.01299 -0.1224 0.7569 0.0192
-9.250 -0.3846 0.01850 0.01235 -0.1215 0.7539 0.0194
-9.000 -0.3688 0.01791 0.01172 -0.1204 0.7509 0.0195
-8.750 -0.3528 0.01734 0.01112 -0.1194 0.7481 0.0198
-8.500 -0.3371 0.01678 0.01051 -0.1183 0.7454 0.0202
-8.250 -0.3205 0.01628 0.01000 -0.1173 0.7434 0.0205
-8.000 -0.3038 0.01579 0.00950 -0.1163 0.7410 0.0207
-7.750 -0.2864 0.01537 0.00904 -0.1152 0.7387 0.0210
-7.500 -0.2759 0.01467 0.00830 -0.1133 0.7364 0.0214
-7.250 -0.2678 0.01395 0.00755 -0.1109 0.7339 0.0218
-7.000 -0.2581 0.01350 0.00705 -0.1085 0.7312 0.0220
-6.750 -0.2452 0.01306 0.00659 -0.1068 0.7291 0.0225
-6.500 -0.2272 0.01263 0.00614 -0.1060 0.7274 0.0231
-6.250 -0.2065 0.01226 0.00577 -0.1055 0.7256 0.0236
-6.000 -0.1845 0.01195 0.00544 -0.1050 0.7236 0.0243
-5.750 -0.1613 0.01168 0.00514 -0.1047 0.7216 0.0249
-5.500 -0.1371 0.01144 0.00488 -0.1046 0.7195 0.0255
-5.250 -0.1132 0.01113 0.00454 -0.1044 0.7175 0.0269
-5.000 -0.0877 0.01091 0.00429 -0.1045 0.7154 0.0288
-4.750 -0.0611 0.01073 0.00410 -0.1047 0.7131 0.0313
-4.500 -0.0361 0.01038 0.00384 -0.1047 0.7118 0.0459
-4.250 -0.0151 0.00938 0.00334 -0.1049 0.7100 0.1616
-4.000 0.0091 0.00791 0.00268 -0.1064 0.7079 0.3670
-3.750 0.0393 0.00725 0.00239 -0.1080 0.7058 0.4680
-3.500 0.0700 0.00699 0.00228 -0.1090 0.7038 0.5199
-3.250 0.1005 0.00685 0.00222 -0.1099 0.7018 0.5524
-3.000 0.1311 0.00677 0.00220 -0.1108 0.6997 0.5790
-2.750 0.1618 0.00679 0.00224 -0.1116 0.6971 0.5977
-2.500 0.1919 0.00680 0.00228 -0.1122 0.6952 0.6114
-2.250 0.2218 0.00681 0.00229 -0.1128 0.6933 0.6225
-2.000 0.2515 0.00685 0.00235 -0.1133 0.6911 0.6329
-1.750 0.2815 0.00688 0.00236 -0.1139 0.6888 0.6390
-1.500 0.3113 0.00694 0.00242 -0.1144 0.6865 0.6446
-1.250 0.3413 0.00700 0.00244 -0.1149 0.6842 0.6500
-1.000 0.3714 0.00706 0.00245 -0.1156 0.6815 0.6535
-0.750 0.4010 0.00713 0.00252 -0.1161 0.6784 0.6565
-0.500 0.4300 0.00713 0.00254 -0.1164 0.6757 0.6597
-0.250 0.4593 0.00714 0.00255 -0.1168 0.6724 0.6631
0.000 0.4888 0.00716 0.00255 -0.1173 0.6690 0.6664
0.250 0.5184 0.00719 0.00255 -0.1178 0.6659 0.6693
0.500 0.5476 0.00726 0.00260 -0.1183 0.6625 0.6722
0.750 0.5764 0.00726 0.00266 -0.1186 0.6597 0.6750
1.000 0.6054 0.00729 0.00270 -0.1189 0.6562 0.6781
1.250 0.6346 0.00732 0.00274 -0.1194 0.6528 0.6812
1.500 0.6640 0.00737 0.00276 -0.1198 0.6494 0.6836
1.750 0.6930 0.00740 0.00277 -0.1203 0.6458 0.6859
2.000 0.7218 0.00738 0.00280 -0.1206 0.6420 0.6880
2.250 0.7503 0.00738 0.00283 -0.1209 0.6371 0.6900
2.500 0.7782 0.00742 0.00285 -0.1211 0.6316 0.6920
2.750 0.8067 0.00744 0.00291 -0.1214 0.6258 0.6942
3.000 0.8348 0.00749 0.00295 -0.1216 0.6197 0.6964
3.250 0.8628 0.00756 0.00301 -0.1218 0.6144 0.6983
3.500 0.8913 0.00762 0.00308 -0.1222 0.6085 0.6999
3.750 0.9182 0.00771 0.00313 -0.1222 0.6007 0.7013
4.000 0.9450 0.00774 0.00316 -0.1222 0.5899 0.7035
4.250 0.9709 0.00784 0.00325 -0.1220 0.5792 0.7052
4.750 1.0215 0.00811 0.00349 -0.1214 0.5558 0.7087
5.000 1.0466 0.00826 0.00362 -0.1211 0.5439 0.7105
5.250 1.0708 0.00844 0.00377 -0.1206 0.5301 0.7122
5.500 1.0945 0.00864 0.00393 -0.1200 0.5166 0.7137
5.750 1.1177 0.00885 0.00411 -0.1194 0.5020 0.7151
6.000 1.1400 0.00909 0.00430 -0.1186 0.4843 0.7164
6.250 1.1579 0.00947 0.00457 -0.1170 0.4556 0.7175
6.750 1.1791 0.01048 0.00528 -0.1111 0.3897 0.7211
7.000 1.1860 0.01103 0.00571 -0.1074 0.3602 0.7227
7.250 1.1882 0.01181 0.00631 -0.1031 0.3233 0.7242
7.500 1.1826 0.01290 0.00717 -0.0978 0.2757 0.7258
7.750 1.1758 0.01416 0.00820 -0.0926 0.2315 0.7274
8.000 1.1704 0.01552 0.00937 -0.0882 0.1922 0.7291
8.250 1.1692 0.01687 0.01055 -0.0846 0.1598 0.7308
8.500 1.1698 0.01825 0.01178 -0.0815 0.1301 0.7323
8.750 1.1692 0.01979 0.01315 -0.0785 0.0996 0.7337
9.000 1.1759 0.02101 0.01429 -0.0764 0.0849 0.7348
9.250 1.1864 0.02201 0.01528 -0.0749 0.0761 0.7369
9.500 1.1976 0.02300 0.01627 -0.0735 0.0681 0.7386
9.750 1.2071 0.02413 0.01738 -0.0719 0.0586 0.7400
10.000 1.2124 0.02558 0.01873 -0.0701 0.0434 0.7414
10.250 1.2181 0.02703 0.02013 -0.0683 0.0334 0.7427
10.500 1.2285 0.02823 0.02133 -0.0671 0.0302 0.7439
10.750 1.2391 0.02945 0.02257 -0.0660 0.0286 0.7450
11.000 1.2487 0.03076 0.02391 -0.0648 0.0270 0.7461
11.250 1.2598 0.03200 0.02519 -0.0638 0.0262 0.7473
11.500 1.2719 0.03320 0.02644 -0.0630 0.0256 0.7485
11.750 1.2830 0.03451 0.02779 -0.0621 0.0250 0.7498
12.000 1.2938 0.03587 0.02919 -0.0613 0.0243 0.7508
12.250 1.3033 0.03737 0.03072 -0.0604 0.0237 0.7518
12.500 1.3117 0.03898 0.03238 -0.0596 0.0230 0.7533
12.750 1.3167 0.04096 0.03443 -0.0586 0.0222 0.7546
13.000 1.3260 0.04258 0.03612 -0.0579 0.0219 0.7560
13.250 1.3362 0.04416 0.03776 -0.0573 0.0217 0.7574
13.500 1.3455 0.04585 0.03951 -0.0568 0.0214 0.7588
13.750 1.3551 0.04755 0.04127 -0.0563 0.0211 0.7602
14.000 1.3628 0.04948 0.04327 -0.0558 0.0207 0.7617
14.250 1.3711 0.05138 0.04523 -0.0554 0.0204 0.7632
14.500 1.3784 0.05344 0.04735 -0.0551 0.0201 0.7648
14.750 1.3856 0.05553 0.04949 -0.0548 0.0197 0.7664
15.000 1.3911 0.05787 0.05188 -0.0545 0.0194 0.7679
15.250 1.3961 0.06029 0.05437 -0.0544 0.0191 0.7698
15.500 1.3970 0.06325 0.05740 -0.0542 0.0186 0.7716
15.750 1.3944 0.06669 0.06094 -0.0541 0.0183 0.7731
16.000 1.3982 0.06942 0.06375 -0.0541 0.0181 0.7750
16.250 1.4057 0.07177 0.06617 -0.0544 0.0179 0.7770
16.500 1.4125 0.07422 0.06869 -0.0546 0.0178 0.7792
16.750 1.4181 0.07688 0.07143 -0.0550 0.0176 0.7813
17.000 1.4239 0.07952 0.07413 -0.0553 0.0174 0.7834
17.250 1.4283 0.08239 0.07709 -0.0558 0.0171 0.7856
17.500 1.4331 0.08521 0.08000 -0.0564 0.0169 0.7879
17.750 1.4371 0.08822 0.08309 -0.0570 0.0167 0.7904
18.000 1.4418 0.09113 0.08608 -0.0577 0.0164 0.7930
18.250 1.4453 0.09427 0.08928 -0.0585 0.0162 0.7957
18.500 1.4488 0.09740 0.09247 -0.0594 0.0160 0.7984
18.750 1.4512 0.10073 0.09587 -0.0604 0.0158 0.8009
19.000 1.4532 0.10412 0.09934 -0.0615 0.0156 0.8037
19.250 1.4544 0.10766 0.10296 -0.0627 0.0154 0.8066
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