WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=50,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 75-193 (fx75193-il) Reynolds number: 50,000 Max Cl/Cd: 11.67 at α=14.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx75193-il-50000-n5.txt Download as CSV file: xf-fx75193-il-50000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 75-193
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.050 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.000 -0.1954 0.11991 0.11253 -0.1148 0.9335 0.0461
-12.750 -0.1964 0.11454 0.10717 -0.1180 0.9320 0.0460
-12.250 -0.2418 0.09740 0.09004 -0.1264 0.9280 0.0429
-12.000 -0.2648 0.09303 0.08568 -0.1266 0.9247 0.0426
-11.750 -0.2865 0.08846 0.08108 -0.1276 0.9215 0.0422
-11.500 -0.3111 0.08353 0.07607 -0.1291 0.9183 0.0417
-11.250 -0.3358 0.07892 0.07132 -0.1304 0.9154 0.0413
-11.000 -0.3589 0.07493 0.06716 -0.1310 0.9130 0.0410
-10.750 -0.3900 0.07309 0.06523 -0.1270 0.9087 0.0404
-10.500 -0.4216 0.07179 0.06386 -0.1222 0.9036 0.0403
-10.250 -0.4458 0.06988 0.06181 -0.1190 0.8995 0.0404
-10.000 -0.4643 0.06772 0.05944 -0.1166 0.8959 0.0403
-9.750 -0.4791 0.06575 0.05723 -0.1142 0.8928 0.0406
-9.500 -0.5175 0.06592 0.05740 -0.1055 0.8868 0.0402
-9.250 -0.5337 0.06445 0.05576 -0.1012 0.8823 0.0405
-9.000 -0.5400 0.06246 0.05349 -0.0985 0.8787 0.0412
-8.750 -0.5391 0.06017 0.05082 -0.0967 0.8759 0.0420
-8.500 -0.5385 0.05813 0.04835 -0.0942 0.8732 0.0429
-8.250 -0.5484 0.05736 0.04754 -0.0893 0.8686 0.0435
-8.000 -0.5421 0.05609 0.04614 -0.0868 0.8648 0.0443
-7.750 -0.5275 0.05457 0.04438 -0.0854 0.8617 0.0456
-7.500 -0.5045 0.05295 0.04240 -0.0847 0.8595 0.0476
-7.250 -0.4774 0.05188 0.04128 -0.0846 0.8576 0.0503
-7.000 -0.4446 0.05097 0.04024 -0.0850 0.8559 0.0554
-6.750 -0.4408 0.05063 0.03980 -0.0811 0.8516 0.0591
-6.500 -0.4315 0.05018 0.03930 -0.0780 0.8474 0.0652
-6.250 -0.4165 0.04963 0.03876 -0.0758 0.8441 0.0726
-6.000 -0.4024 0.04905 0.03814 -0.0741 0.8411 0.0839
-5.750 -0.3868 0.04842 0.03757 -0.0732 0.8383 0.1022
-5.500 -0.3865 0.04790 0.03716 -0.0699 0.8340 0.1155
-5.250 -0.3906 0.04741 0.03673 -0.0657 0.8288 0.1270
-5.000 -0.3845 0.04674 0.03611 -0.0630 0.8249 0.1425
-4.750 -0.3749 0.04577 0.03534 -0.0613 0.8215 0.1653
-4.500 -0.3631 0.04438 0.03438 -0.0604 0.8187 0.2162
-4.250 -0.3748 0.04332 0.03378 -0.0558 0.8127 0.2723
-4.000 -0.3782 0.04412 0.03610 -0.0473 0.8084 0.4468
-3.750 -0.3572 0.04664 0.03865 -0.0424 0.8048 0.5663
-3.500 -0.3332 0.04792 0.03959 -0.0414 0.8016 0.6220
-3.250 -0.3327 0.04857 0.04006 -0.0376 0.7958 0.6506
-3.000 -0.3250 0.04963 0.04093 -0.0339 0.7911 0.6799
-2.750 -0.3124 0.05112 0.04227 -0.0291 0.7874 0.7107
-2.500 -0.2907 0.05270 0.04371 -0.0241 0.7845 0.7373
-2.250 -0.2885 0.05310 0.04401 -0.0192 0.7791 0.7548
-2.000 -0.2801 0.05324 0.04401 -0.0158 0.7742 0.7686
-1.750 -0.2657 0.05313 0.04369 -0.0145 0.7704 0.7799
-1.500 -0.2378 0.05318 0.04352 -0.0145 0.7675 0.7861
-1.250 -0.2360 0.05300 0.04322 -0.0113 0.7616 0.7938
-1.000 -0.2242 0.05280 0.04286 -0.0099 0.7565 0.7999
-0.750 -0.2002 0.05276 0.04264 -0.0099 0.7530 0.8043
-0.500 -0.1809 0.05272 0.04241 -0.0095 0.7491 0.8097
-0.250 -0.1774 0.05256 0.04215 -0.0072 0.7427 0.8157
0.000 -0.1552 0.05254 0.04199 -0.0070 0.7387 0.8192
0.250 -0.1265 0.05259 0.04187 -0.0080 0.7359 0.8221
0.500 -0.1246 0.05256 0.04178 -0.0056 0.7289 0.8257
0.750 -0.1020 0.05260 0.04167 -0.0059 0.7246 0.8293
1.000 -0.0726 0.05274 0.04165 -0.0074 0.7217 0.8325
1.250 -0.0682 0.05289 0.04176 -0.0053 0.7150 0.8351
1.500 -0.0452 0.05302 0.04180 -0.0057 0.7106 0.8373
1.750 -0.0147 0.05317 0.04182 -0.0069 0.7075 0.8397
2.000 -0.0091 0.05345 0.04206 -0.0052 0.7003 0.8430
2.250 0.0142 0.05371 0.04224 -0.0057 0.6958 0.8459
2.500 0.0453 0.05396 0.04240 -0.0073 0.6926 0.8483
2.750 0.0545 0.05441 0.04280 -0.0063 0.6854 0.8506
3.000 0.0767 0.05467 0.04302 -0.0065 0.6804 0.8529
3.250 0.1067 0.05492 0.04321 -0.0076 0.6771 0.8553
3.500 0.1162 0.05545 0.04373 -0.0065 0.6699 0.8578
3.750 0.1392 0.05586 0.04411 -0.0071 0.6647 0.8599
4.000 0.1699 0.05622 0.04443 -0.0085 0.6613 0.8619
4.500 0.2044 0.05744 0.04564 -0.0087 0.6486 0.8665
4.750 0.2353 0.05774 0.04594 -0.0099 0.6451 0.8685
5.000 0.2445 0.05858 0.04680 -0.0091 0.6373 0.8704
5.250 0.2680 0.05909 0.04733 -0.0097 0.6319 0.8720
5.500 0.3001 0.05937 0.04762 -0.0111 0.6282 0.8738
6.000 0.3329 0.06094 0.04927 -0.0111 0.6142 0.8782
6.250 0.3660 0.06121 0.04958 -0.0126 0.6107 0.8804
6.500 0.3710 0.06257 0.05100 -0.0119 0.6011 0.8823
6.750 0.3984 0.06311 0.05159 -0.0130 0.5959 0.8840
7.000 0.4319 0.06331 0.05186 -0.0144 0.5926 0.8857
7.250 0.4327 0.06493 0.05359 -0.0133 0.5820 0.8876
7.500 0.4607 0.06535 0.05408 -0.0142 0.5771 0.8898
7.750 0.4777 0.06633 0.05514 -0.0144 0.5699 0.8920
8.000 0.4943 0.06735 0.05626 -0.0147 0.5619 0.8942
8.250 0.5266 0.06759 0.05662 -0.0159 0.5578 0.8963
8.500 0.5322 0.06933 0.05845 -0.0156 0.5472 0.8980
8.750 0.5596 0.06985 0.05909 -0.0166 0.5416 0.9002
9.000 0.5935 0.06988 0.05926 -0.0178 0.5382 0.9026
9.250 0.5911 0.07224 0.06174 -0.0171 0.5258 0.9048
9.500 0.6223 0.07244 0.06211 -0.0181 0.5214 0.9075
9.750 0.6259 0.07455 0.06435 -0.0179 0.5102 0.9097
10.000 0.6547 0.07488 0.06483 -0.0188 0.5043 0.9122
10.500 0.6885 0.07723 0.06752 -0.0196 0.4869 0.9173
10.750 0.7241 0.07686 0.06736 -0.0205 0.4831 0.9211
11.000 0.7198 0.07986 0.07050 -0.0203 0.4695 0.9242
11.250 0.7544 0.07957 0.07045 -0.0212 0.4652 0.9289
11.750 0.7890 0.08193 0.07322 -0.0222 0.4469 0.9391
12.000 0.7894 0.08467 0.07612 -0.0225 0.4328 0.9451
12.250 0.8253 0.08338 0.07508 -0.0229 0.4278 0.9685
12.750 0.8368 0.08761 0.07965 -0.0231 0.4014 1.0000
13.000 0.8736 0.08586 0.07817 -0.0231 0.3921 1.0000
13.500 0.9067 0.08639 0.07910 -0.0227 0.3602 1.0000
14.000 0.9572 0.08386 0.07698 -0.0215 0.3214 1.0000
14.250 0.9757 0.08379 0.07704 -0.0211 0.2954 1.0000
14.500 0.9879 0.08467 0.07793 -0.0209 0.2590 1.0000
14.750 0.9979 0.08588 0.07887 -0.0206 0.2117 1.0000
15.000 0.9975 0.08883 0.08143 -0.0207 0.1683 1.0000
15.500 0.9860 0.09706 0.08905 -0.0221 0.1169 1.0000
15.750 0.9820 0.10117 0.09297 -0.0232 0.1015 1.0000
16.000 0.9813 0.10491 0.09658 -0.0243 0.0894 1.0000
16.250 0.9824 0.10849 0.10011 -0.0255 0.0791 1.0000
16.500 0.9859 0.11171 0.10330 -0.0267 0.0713 1.0000
16.750 0.9907 0.11476 0.10635 -0.0278 0.0646 1.0000
17.000 0.9981 0.11741 0.10904 -0.0289 0.0596 1.0000
17.250 1.0064 0.11990 0.11153 -0.0299 0.0553 1.0000
17.500 1.0165 0.12222 0.11398 -0.0308 0.0517 1.0000
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