WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 75-141 (fx75141-il) Reynolds number: 500,000 Max Cl/Cd: 103.23 at α=4.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx75141-il-500000-n5.txt Download as CSV file: xf-fx75141-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 75-141
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
------ -------- --------- --------- -------- -------- --------
-15.500 -0.6279 0.08891 0.08553 -0.0791 0.8523 0.0122
-15.250 -0.6819 0.07338 0.06973 -0.0896 0.8482 0.0120
-14.750 -0.7289 0.05493 0.05080 -0.1049 0.8390 0.0119
-14.500 -0.7364 0.04930 0.04498 -0.1101 0.8347 0.0120
-14.250 -0.7396 0.04466 0.04014 -0.1146 0.8308 0.0121
-13.750 -0.7341 0.03783 0.03296 -0.1210 0.8245 0.0125
-13.500 -0.7305 0.03492 0.02988 -0.1234 0.8216 0.0126
-13.250 -0.7211 0.03279 0.02758 -0.1251 0.8187 0.0129
-13.000 -0.7126 0.03068 0.02532 -0.1266 0.8159 0.0130
-12.750 -0.7028 0.02881 0.02330 -0.1277 0.8132 0.0133
-12.500 -0.6922 0.02712 0.02150 -0.1286 0.8109 0.0135
-12.250 -0.6810 0.02570 0.01999 -0.1289 0.8089 0.0137
-12.000 -0.6677 0.02454 0.01877 -0.1291 0.8069 0.0141
-11.750 -0.6554 0.02342 0.01757 -0.1288 0.8049 0.0143
-11.500 -0.6441 0.02245 0.01651 -0.1282 0.8028 0.0146
-11.250 -0.6315 0.02157 0.01554 -0.1274 0.8010 0.0149
-11.000 -0.6147 0.02081 0.01468 -0.1268 0.7993 0.0153
-10.750 -0.5962 0.02014 0.01389 -0.1264 0.7976 0.0157
-10.500 -0.5766 0.01950 0.01314 -0.1259 0.7960 0.0162
-10.250 -0.5577 0.01879 0.01236 -0.1254 0.7944 0.0168
-10.000 -0.5374 0.01818 0.01172 -0.1250 0.7930 0.0174
-9.750 -0.5159 0.01765 0.01115 -0.1246 0.7917 0.0180
-9.500 -0.4936 0.01715 0.01059 -0.1243 0.7903 0.0186
-9.250 -0.4710 0.01665 0.01002 -0.1240 0.7889 0.0193
-9.000 -0.4479 0.01618 0.00948 -0.1237 0.7875 0.0199
-8.750 -0.4249 0.01567 0.00892 -0.1234 0.7859 0.0207
-8.500 -0.4009 0.01525 0.00847 -0.1232 0.7844 0.0217
-8.250 -0.3762 0.01489 0.00806 -0.1230 0.7831 0.0228
-8.000 -0.3510 0.01454 0.00766 -0.1229 0.7819 0.0240
-7.750 -0.3259 0.01416 0.00722 -0.1228 0.7807 0.0251
-7.500 -0.3003 0.01381 0.00685 -0.1228 0.7793 0.0266
-7.250 -0.2749 0.01350 0.00652 -0.1227 0.7779 0.0282
-7.000 -0.2490 0.01323 0.00621 -0.1226 0.7763 0.0299
-6.750 -0.2236 0.01288 0.00586 -0.1225 0.7743 0.0321
-6.500 -0.1974 0.01261 0.00558 -0.1224 0.7723 0.0345
-6.250 -0.1710 0.01235 0.00529 -0.1224 0.7704 0.0367
-6.000 -0.1446 0.01208 0.00501 -0.1223 0.7685 0.0400
-5.750 -0.1175 0.01187 0.00476 -0.1224 0.7666 0.0433
-5.500 -0.0906 0.01162 0.00451 -0.1224 0.7648 0.0479
-5.250 -0.0631 0.01145 0.00431 -0.1225 0.7631 0.0523
-5.000 -0.0366 0.01119 0.00410 -0.1225 0.7612 0.0593
-4.750 -0.0097 0.01098 0.00391 -0.1225 0.7591 0.0667
-4.500 0.0174 0.01077 0.00373 -0.1225 0.7570 0.0769
-4.250 0.0446 0.01054 0.00356 -0.1226 0.7550 0.0916
-4.000 0.0718 0.01031 0.00339 -0.1227 0.7530 0.1107
-3.750 0.0992 0.01007 0.00322 -0.1228 0.7510 0.1346
-3.500 0.1266 0.00981 0.00306 -0.1229 0.7492 0.1681
-3.250 0.1543 0.00957 0.00292 -0.1232 0.7473 0.2076
-3.000 0.1808 0.00926 0.00280 -0.1232 0.7451 0.2557
-2.750 0.2073 0.00890 0.00266 -0.1233 0.7425 0.3199
-2.500 0.2336 0.00852 0.00256 -0.1233 0.7399 0.4012
-2.250 0.2609 0.00832 0.00250 -0.1233 0.7373 0.4544
-2.000 0.2884 0.00818 0.00245 -0.1233 0.7350 0.4930
-1.750 0.3163 0.00808 0.00241 -0.1234 0.7329 0.5233
-1.500 0.3441 0.00801 0.00240 -0.1233 0.7305 0.5478
-1.250 0.3714 0.00795 0.00241 -0.1232 0.7273 0.5664
-1.000 0.3987 0.00790 0.00243 -0.1231 0.7240 0.5893
-0.750 0.4263 0.00788 0.00246 -0.1229 0.7207 0.6101
-0.500 0.4543 0.00788 0.00247 -0.1229 0.7178 0.6245
-0.250 0.4822 0.00789 0.00250 -0.1228 0.7146 0.6392
0.000 0.5096 0.00792 0.00256 -0.1227 0.7104 0.6530
0.250 0.5372 0.00794 0.00260 -0.1226 0.7061 0.6628
0.500 0.5651 0.00795 0.00259 -0.1225 0.7021 0.6689
0.750 0.5927 0.00796 0.00262 -0.1224 0.6975 0.6739
1.000 0.6202 0.00798 0.00264 -0.1223 0.6918 0.6795
1.250 0.6477 0.00799 0.00263 -0.1222 0.6865 0.6843
1.500 0.6749 0.00801 0.00268 -0.1220 0.6802 0.6881
1.750 0.7019 0.00803 0.00270 -0.1218 0.6733 0.6925
2.000 0.7291 0.00806 0.00273 -0.1216 0.6660 0.6971
2.250 0.7556 0.00810 0.00275 -0.1213 0.6571 0.7006
2.500 0.7814 0.00814 0.00278 -0.1208 0.6448 0.7037
2.750 0.8055 0.00824 0.00280 -0.1199 0.6262 0.7073
3.000 0.8284 0.00841 0.00286 -0.1189 0.6028 0.7111
3.250 0.8518 0.00860 0.00296 -0.1180 0.5838 0.7148
3.500 0.8762 0.00875 0.00308 -0.1173 0.5710 0.7174
3.750 0.9004 0.00891 0.00322 -0.1166 0.5597 0.7203
4.000 0.9245 0.00908 0.00338 -0.1158 0.5476 0.7234
4.250 0.9484 0.00925 0.00353 -0.1151 0.5344 0.7267
4.500 0.9720 0.00944 0.00369 -0.1143 0.5210 0.7297
4.750 0.9951 0.00964 0.00387 -0.1134 0.5077 0.7324
5.000 1.0169 0.00986 0.00407 -0.1123 0.4912 0.7350
5.250 1.0348 0.01021 0.00432 -0.1104 0.4626 0.7378
5.500 1.0496 0.01067 0.00462 -0.1080 0.4251 0.7407
5.750 1.0629 0.01120 0.00497 -0.1054 0.3866 0.7436
6.000 1.0746 0.01177 0.00536 -0.1025 0.3467 0.7466
6.250 1.0812 0.01243 0.00582 -0.0987 0.3042 0.7494
6.500 1.0870 0.01306 0.00629 -0.0948 0.2682 0.7523
6.750 1.0951 0.01370 0.00679 -0.0914 0.2378 0.7556
7.000 1.1047 0.01431 0.00730 -0.0884 0.2139 0.7596
7.250 1.1146 0.01493 0.00782 -0.0855 0.1917 0.7636
7.500 1.1243 0.01555 0.00839 -0.0826 0.1732 0.7673
8.000 1.1465 0.01681 0.00956 -0.0777 0.1428 0.7738
8.250 1.1574 0.01750 0.01021 -0.0755 0.1281 0.7770
8.500 1.1675 0.01828 0.01092 -0.0732 0.1116 0.7799
8.750 1.1778 0.01908 0.01169 -0.0711 0.0973 0.7828
9.000 1.1877 0.01995 0.01252 -0.0690 0.0834 0.7864
9.250 1.1979 0.02085 0.01339 -0.0670 0.0721 0.7903
9.500 1.2088 0.02175 0.01427 -0.0652 0.0636 0.7939
9.750 1.2197 0.02267 0.01519 -0.0635 0.0561 0.7977
10.000 1.2321 0.02352 0.01607 -0.0619 0.0510 0.8019
10.250 1.2434 0.02449 0.01705 -0.0604 0.0461 0.8067
10.500 1.2567 0.02539 0.01801 -0.0592 0.0426 0.8122
10.750 1.2695 0.02635 0.01902 -0.0580 0.0396 0.8194
11.000 1.2818 0.02739 0.02011 -0.0568 0.0371 0.8276
11.250 1.2951 0.02835 0.02115 -0.0558 0.0344 0.8390
11.500 1.3079 0.02944 0.02233 -0.0549 0.0322 0.8573
11.750 1.3327 0.03072 0.02377 -0.0566 0.0300 0.9025
12.250 1.3616 0.03318 0.02634 -0.0560 0.0267 1.0000
12.500 1.3703 0.03461 0.02780 -0.0549 0.0253 1.0000
12.750 1.3805 0.03594 0.02919 -0.0539 0.0243 1.0000
13.000 1.3904 0.03732 0.03064 -0.0529 0.0234 1.0000
13.250 1.3993 0.03881 0.03218 -0.0519 0.0224 1.0000
13.500 1.4073 0.04042 0.03384 -0.0510 0.0215 1.0000
13.750 1.4133 0.04225 0.03571 -0.0500 0.0206 1.0000
14.000 1.4210 0.04395 0.03749 -0.0492 0.0198 1.0000
14.250 1.4291 0.04567 0.03929 -0.0485 0.0190 1.0000
14.500 1.4357 0.04758 0.04127 -0.0478 0.0184 1.0000
14.750 1.4419 0.04958 0.04333 -0.0472 0.0177 1.0000
15.000 1.4465 0.05177 0.04558 -0.0466 0.0171 1.0000
15.250 1.4494 0.05419 0.04807 -0.0461 0.0166 1.0000
15.500 1.4532 0.05660 0.05056 -0.0458 0.0161 1.0000
15.750 1.4576 0.05898 0.05304 -0.0455 0.0157 1.0000
16.000 1.4610 0.06154 0.05569 -0.0453 0.0152 1.0000
16.250 1.4636 0.06421 0.05845 -0.0452 0.0147 1.0000
16.500 1.4666 0.06689 0.06121 -0.0453 0.0142 1.0000
16.750 1.4671 0.06995 0.06436 -0.0454 0.0139 1.0000
17.000 1.4665 0.07321 0.06769 -0.0457 0.0135 1.0000
17.250 1.4632 0.07690 0.07146 -0.0461 0.0131 1.0000
17.500 1.4622 0.08032 0.07499 -0.0467 0.0129 1.0000
17.750 1.4607 0.08390 0.07869 -0.0473 0.0126 1.0000
18.000 1.4584 0.08765 0.08255 -0.0481 0.0124 1.0000
18.250 1.4556 0.09155 0.08656 -0.0491 0.0121 1.0000
18.500 1.4512 0.09577 0.09089 -0.0503 0.0119 1.0000
18.750 1.4470 0.10001 0.09524 -0.0516 0.0116 1.0000
19.000 1.4418 0.10448 0.09982 -0.0532 0.0114 1.0000
19.250 1.4361 0.10913 0.10458 -0.0549 0.0112 1.0000
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