WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 75-141 (fx75141-il) Reynolds number: 500,000 Max Cl/Cd: 111.92 at α=5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx75141-il-500000.txt Download as CSV file: xf-fx75141-il-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.250 -0.4940 0.07288 0.06995 -0.0946 0.8932 0.0200
-13.000 -0.5382 0.05749 0.05427 -0.1096 0.8855 0.0194
-12.750 -0.5634 0.04781 0.04421 -0.1206 0.8781 0.0193
-12.500 -0.5781 0.04146 0.03753 -0.1273 0.8723 0.0191
-12.250 -0.5824 0.03739 0.03317 -0.1313 0.8672 0.0194
-12.000 -0.5842 0.03388 0.02933 -0.1343 0.8627 0.0198
-11.750 -0.5796 0.03127 0.02644 -0.1362 0.8588 0.0199
-11.500 -0.5770 0.02934 0.02429 -0.1362 0.8552 0.0201
-11.250 -0.5767 0.02722 0.02192 -0.1350 0.8514 0.0203
-11.000 -0.5674 0.02518 0.01973 -0.1344 0.8486 0.0208
-10.750 -0.5512 0.02414 0.01861 -0.1340 0.8462 0.0213
-10.500 -0.5329 0.02331 0.01770 -0.1337 0.8441 0.0218
-10.250 -0.5147 0.02254 0.01683 -0.1332 0.8421 0.0225
-10.000 -0.4966 0.02168 0.01587 -0.1325 0.8403 0.0232
-9.750 -0.4770 0.02101 0.01507 -0.1319 0.8382 0.0241
-9.500 -0.4564 0.02044 0.01435 -0.1314 0.8360 0.0247
-9.250 -0.4383 0.01901 0.01287 -0.1306 0.8341 0.0257
-9.000 -0.4163 0.01840 0.01223 -0.1303 0.8323 0.0265
-8.750 -0.3936 0.01787 0.01164 -0.1299 0.8307 0.0276
-8.500 -0.3702 0.01737 0.01105 -0.1296 0.8289 0.0287
-8.250 -0.3459 0.01699 0.01056 -0.1294 0.8270 0.0297
-8.000 -0.3261 0.01608 0.00966 -0.1286 0.8254 0.0314
-7.750 -0.3028 0.01568 0.00926 -0.1282 0.8235 0.0330
-7.500 -0.2789 0.01529 0.00883 -0.1278 0.8214 0.0347
-7.250 -0.2539 0.01501 0.00847 -0.1276 0.8193 0.0361
-7.000 -0.2322 0.01424 0.00772 -0.1270 0.8171 0.0387
-6.750 -0.2067 0.01394 0.00738 -0.1269 0.8151 0.0413
-6.500 -0.1804 0.01370 0.00707 -0.1268 0.8132 0.0438
-6.250 -0.1560 0.01324 0.00661 -0.1267 0.8110 0.0478
-6.000 -0.1308 0.01297 0.00633 -0.1264 0.8091 0.0514
-5.750 -0.1063 0.01255 0.00592 -0.1261 0.8068 0.0567
-5.500 -0.0802 0.01233 0.00569 -0.1259 0.8044 0.0620
-5.250 -0.0545 0.01197 0.00536 -0.1258 0.8021 0.0701
-5.000 -0.0279 0.01168 0.00509 -0.1258 0.8000 0.0808
-4.750 -0.0009 0.01141 0.00485 -0.1259 0.7979 0.0966
-4.500 0.0261 0.01114 0.00467 -0.1260 0.7959 0.1225
-4.250 0.0519 0.01082 0.00450 -0.1260 0.7938 0.1633
-4.000 0.0771 0.01040 0.00433 -0.1259 0.7914 0.2205
-3.500 0.1276 0.00942 0.00398 -0.1259 0.7863 0.3967
-3.250 0.1545 0.00918 0.00392 -0.1259 0.7839 0.4675
-3.000 0.1824 0.00906 0.00388 -0.1259 0.7817 0.5083
-2.750 0.2106 0.00906 0.00391 -0.1260 0.7794 0.5398
-2.500 0.2368 0.00897 0.00391 -0.1257 0.7767 0.5657
-2.250 0.2637 0.00894 0.00392 -0.1254 0.7737 0.5876
-2.000 0.2911 0.00894 0.00397 -0.1252 0.7709 0.6084
-1.750 0.3192 0.00896 0.00400 -0.1251 0.7683 0.6264
-1.500 0.3480 0.00901 0.00403 -0.1252 0.7658 0.6408
-1.250 0.3774 0.00912 0.00408 -0.1254 0.7634 0.6524
-1.000 0.4035 0.00916 0.00416 -0.1250 0.7600 0.6644
-0.750 0.4305 0.00921 0.00423 -0.1246 0.7564 0.6740
-0.500 0.4587 0.00924 0.00423 -0.1246 0.7531 0.6833
-0.250 0.4873 0.00928 0.00427 -0.1246 0.7503 0.6907
0.000 0.5167 0.00938 0.00432 -0.1247 0.7476 0.7003
0.250 0.5421 0.00940 0.00441 -0.1241 0.7435 0.7067
0.500 0.5694 0.00940 0.00441 -0.1239 0.7393 0.7131
0.750 0.5977 0.00935 0.00436 -0.1239 0.7357 0.7180
1.000 0.6267 0.00933 0.00432 -0.1240 0.7325 0.7224
1.250 0.6531 0.00933 0.00435 -0.1236 0.7279 0.7277
1.500 0.6802 0.00928 0.00431 -0.1234 0.7230 0.7325
1.750 0.7082 0.00921 0.00426 -0.1233 0.7188 0.7362
2.000 0.7361 0.00918 0.00423 -0.1232 0.7146 0.7405
2.250 0.7619 0.00914 0.00423 -0.1228 0.7080 0.7454
2.500 0.7895 0.00902 0.00409 -0.1226 0.7019 0.7491
2.750 0.8143 0.00890 0.00402 -0.1218 0.6918 0.7525
3.000 0.8399 0.00880 0.00392 -0.1211 0.6809 0.7566
3.250 0.8660 0.00876 0.00385 -0.1207 0.6706 0.7609
3.500 0.8915 0.00876 0.00387 -0.1202 0.6600 0.7644
3.750 0.9168 0.00877 0.00389 -0.1196 0.6498 0.7675
4.000 0.9419 0.00882 0.00393 -0.1190 0.6387 0.7711
4.250 0.9665 0.00890 0.00399 -0.1183 0.6261 0.7750
4.500 0.9911 0.00902 0.00408 -0.1176 0.6132 0.7786
4.750 1.0149 0.00912 0.00419 -0.1168 0.6007 0.7815
5.000 1.0375 0.00927 0.00432 -0.1157 0.5853 0.7848
5.250 1.0582 0.00950 0.00447 -0.1143 0.5645 0.7885
5.500 1.0789 0.00973 0.00464 -0.1129 0.5447 0.7920
5.750 1.1000 0.00994 0.00482 -0.1117 0.5265 0.7951
6.000 1.1196 0.01017 0.00502 -0.1101 0.5068 0.7983
6.250 1.1374 0.01046 0.00526 -0.1082 0.4846 0.8019
6.500 1.1549 0.01077 0.00552 -0.1063 0.4605 0.8057
6.750 1.1694 0.01117 0.00582 -0.1038 0.4320 0.8094
7.000 1.1795 0.01164 0.00617 -0.1006 0.3966 0.8132
7.250 1.1819 0.01223 0.00659 -0.0959 0.3575 0.8179
7.500 1.1838 0.01296 0.00712 -0.0913 0.3166 0.8233
7.750 1.1845 0.01377 0.00776 -0.0867 0.2797 0.8284
8.000 1.1874 0.01457 0.00843 -0.0827 0.2473 0.8337
8.250 1.1918 0.01540 0.00913 -0.0791 0.2196 0.8389
8.500 1.1980 0.01620 0.00985 -0.0760 0.1962 0.8443
8.750 1.2044 0.01704 0.01063 -0.0731 0.1756 0.8508
9.000 1.2118 0.01793 0.01146 -0.0705 0.1566 0.8578
9.250 1.2212 0.01884 0.01233 -0.0684 0.1364 0.8668
9.500 1.2302 0.01991 0.01333 -0.0666 0.1147 0.8802
9.750 1.2445 0.02113 0.01450 -0.0661 0.0909 0.9074
10.000 1.2635 0.02244 0.01577 -0.0668 0.0733 1.0000
10.250 1.2731 0.02370 0.01698 -0.0653 0.0637 1.0000
10.500 1.2829 0.02495 0.01820 -0.0638 0.0569 1.0000
10.750 1.2940 0.02613 0.01940 -0.0625 0.0523 1.0000
11.000 1.3042 0.02736 0.02063 -0.0612 0.0485 1.0000
11.250 1.3116 0.02883 0.02210 -0.0596 0.0449 1.0000
11.500 1.3237 0.02996 0.02329 -0.0586 0.0423 1.0000
11.750 1.3325 0.03134 0.02469 -0.0573 0.0400 1.0000
12.000 1.3354 0.03321 0.02658 -0.0556 0.0374 1.0000
12.250 1.3473 0.03440 0.02784 -0.0546 0.0361 1.0000
12.500 1.3564 0.03583 0.02933 -0.0535 0.0344 1.0000
12.750 1.3639 0.03740 0.03093 -0.0523 0.0327 1.0000
13.000 1.3662 0.03948 0.03304 -0.0509 0.0314 1.0000
13.250 1.3707 0.04143 0.03508 -0.0498 0.0302 1.0000
13.500 1.3791 0.04307 0.03680 -0.0489 0.0292 1.0000
13.750 1.3870 0.04479 0.03858 -0.0482 0.0280 1.0000
14.000 1.3934 0.04671 0.04055 -0.0474 0.0269 1.0000
14.250 1.3953 0.04911 0.04298 -0.0466 0.0258 1.0000
14.500 1.3925 0.05202 0.04596 -0.0456 0.0250 1.0000
14.750 1.4002 0.05397 0.04802 -0.0452 0.0244 1.0000
15.000 1.4057 0.05618 0.05033 -0.0447 0.0236 1.0000
15.250 1.4103 0.05854 0.05276 -0.0444 0.0229 1.0000
15.500 1.4141 0.06104 0.05533 -0.0442 0.0222 1.0000
15.750 1.4166 0.06371 0.05806 -0.0440 0.0216 1.0000
16.000 1.4161 0.06675 0.06115 -0.0439 0.0210 1.0000
16.250 1.4115 0.07027 0.06475 -0.0436 0.0203 1.0000
16.500 1.4161 0.07295 0.06755 -0.0439 0.0198 1.0000
16.750 1.4178 0.07595 0.07066 -0.0442 0.0193 1.0000
17.000 1.4190 0.07906 0.07388 -0.0446 0.0189 1.0000
17.250 1.4194 0.08236 0.07727 -0.0451 0.0184 1.0000
17.500 1.4190 0.08579 0.08079 -0.0457 0.0180 1.0000
17.750 1.4183 0.08933 0.08441 -0.0465 0.0176 1.0000
18.000 1.4171 0.09297 0.08812 -0.0474 0.0173 1.0000
18.250 1.4141 0.09684 0.09206 -0.0484 0.0169 1.0000
18.500 1.4084 0.10092 0.09621 -0.0491 0.0165 1.0000
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