WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 75-141 (fx75141-il) Reynolds number: 1,000,000 Max Cl/Cd: 134.87 at α=4.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx75141-il-1000000.txt Download as CSV file: xf-fx75141-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-15.750 -0.7627 0.07353 0.07064 -0.0818 0.8556 0.0117
-15.500 -0.7998 0.06213 0.05898 -0.0904 0.8499 0.0116
-15.250 -0.8099 0.05576 0.05244 -0.0959 0.8444 0.0116
-15.000 -0.8227 0.04947 0.04596 -0.1014 0.8403 0.0117
-14.750 -0.8259 0.04486 0.04121 -0.1057 0.8366 0.0118
-14.500 -0.8256 0.04070 0.03688 -0.1099 0.8330 0.0119
-14.250 -0.8176 0.03732 0.03334 -0.1141 0.8298 0.0120
-14.000 -0.8089 0.03415 0.02999 -0.1181 0.8266 0.0122
-13.750 -0.7946 0.03234 0.02808 -0.1202 0.8244 0.0125
-13.500 -0.7862 0.02982 0.02542 -0.1226 0.8221 0.0125
-13.250 -0.7667 0.02862 0.02412 -0.1243 0.8200 0.0129
-13.000 -0.7527 0.02678 0.02215 -0.1261 0.8178 0.0130
-12.750 -0.7339 0.02552 0.02078 -0.1276 0.8157 0.0132
-12.500 -0.7264 0.02303 0.01811 -0.1292 0.8133 0.0135
-12.250 -0.7111 0.02159 0.01657 -0.1303 0.8110 0.0138
-12.000 -0.6972 0.02061 0.01555 -0.1302 0.8096 0.0142
-11.750 -0.6812 0.02002 0.01493 -0.1297 0.8080 0.0146
-11.500 -0.6647 0.01917 0.01400 -0.1293 0.8062 0.0149
-11.250 -0.6451 0.01855 0.01332 -0.1289 0.8045 0.0153
-11.000 -0.6249 0.01794 0.01264 -0.1286 0.8030 0.0156
-10.750 -0.6037 0.01739 0.01200 -0.1283 0.8016 0.0160
-10.500 -0.5811 0.01694 0.01148 -0.1280 0.8003 0.0163
-10.250 -0.5637 0.01595 0.01040 -0.1274 0.7988 0.0170
-10.000 -0.5418 0.01536 0.00977 -0.1271 0.7973 0.0176
-9.750 -0.5174 0.01496 0.00933 -0.1271 0.7956 0.0182
-9.500 -0.4934 0.01459 0.00892 -0.1269 0.7944 0.0188
-9.250 -0.4695 0.01419 0.00848 -0.1266 0.7934 0.0194
-9.000 -0.4444 0.01390 0.00815 -0.1265 0.7923 0.0200
-8.750 -0.4220 0.01326 0.00748 -0.1261 0.7911 0.0211
-8.500 -0.3974 0.01288 0.00707 -0.1259 0.7898 0.0220
-8.250 -0.3718 0.01258 0.00675 -0.1258 0.7883 0.0230
-8.000 -0.3458 0.01230 0.00643 -0.1257 0.7868 0.0240
-7.750 -0.3202 0.01196 0.00604 -0.1256 0.7852 0.0251
-7.500 -0.2950 0.01155 0.00562 -0.1255 0.7835 0.0268
-7.250 -0.2681 0.01136 0.00541 -0.1255 0.7818 0.0285
-7.000 -0.2405 0.01123 0.00524 -0.1257 0.7797 0.0298
-6.750 -0.2152 0.01082 0.00483 -0.1255 0.7783 0.0325
-6.500 -0.1885 0.01060 0.00461 -0.1254 0.7769 0.0348
-6.250 -0.1618 0.01035 0.00435 -0.1254 0.7752 0.0372
-6.000 -0.1350 0.01010 0.00412 -0.1254 0.7735 0.0411
-5.750 -0.1076 0.00993 0.00393 -0.1254 0.7718 0.0440
-5.500 -0.0805 0.00967 0.00369 -0.1255 0.7702 0.0495
-5.250 -0.0528 0.00949 0.00349 -0.1255 0.7686 0.0546
-5.000 -0.0253 0.00929 0.00331 -0.1257 0.7669 0.0618
-4.750 0.0024 0.00910 0.00316 -0.1258 0.7652 0.0723
-4.500 0.0303 0.00895 0.00305 -0.1260 0.7632 0.0873
-4.250 0.0572 0.00869 0.00289 -0.1260 0.7619 0.1090
-4.000 0.0843 0.00844 0.00274 -0.1260 0.7602 0.1356
-3.750 0.1113 0.00815 0.00260 -0.1261 0.7583 0.1751
-3.500 0.1383 0.00784 0.00245 -0.1261 0.7562 0.2237
-3.250 0.1652 0.00750 0.00231 -0.1262 0.7543 0.2828
-3.000 0.1917 0.00708 0.00217 -0.1263 0.7524 0.3683
-2.750 0.2188 0.00681 0.00208 -0.1264 0.7505 0.4393
-2.500 0.2469 0.00670 0.00205 -0.1265 0.7484 0.4776
-2.250 0.2748 0.00661 0.00204 -0.1266 0.7463 0.5072
-2.000 0.3024 0.00650 0.00199 -0.1265 0.7443 0.5313
-1.750 0.3302 0.00642 0.00196 -0.1265 0.7418 0.5511
-1.500 0.3581 0.00633 0.00193 -0.1265 0.7393 0.5749
-1.250 0.3862 0.00627 0.00191 -0.1265 0.7368 0.5957
-1.000 0.4144 0.00624 0.00190 -0.1265 0.7344 0.6129
-0.750 0.4432 0.00627 0.00192 -0.1266 0.7315 0.6259
-0.500 0.4708 0.00624 0.00194 -0.1265 0.7289 0.6403
-0.250 0.4988 0.00623 0.00195 -0.1265 0.7257 0.6523
0.000 0.5269 0.00622 0.00195 -0.1264 0.7223 0.6609
0.250 0.5551 0.00622 0.00194 -0.1264 0.7190 0.6694
0.500 0.5835 0.00628 0.00198 -0.1264 0.7155 0.6783
0.750 0.6109 0.00627 0.00201 -0.1263 0.7115 0.6857
1.000 0.6386 0.00627 0.00203 -0.1262 0.7070 0.6907
1.250 0.6665 0.00628 0.00203 -0.1261 0.7026 0.6955
1.500 0.6942 0.00630 0.00204 -0.1260 0.6972 0.6994
1.750 0.7211 0.00626 0.00202 -0.1257 0.6893 0.7032
2.000 0.7476 0.00626 0.00202 -0.1254 0.6783 0.7069
2.250 0.7735 0.00629 0.00201 -0.1249 0.6639 0.7106
2.500 0.7993 0.00637 0.00203 -0.1244 0.6490 0.7140
2.750 0.8249 0.00644 0.00207 -0.1239 0.6360 0.7173
3.000 0.8503 0.00654 0.00215 -0.1234 0.6238 0.7203
3.250 0.8754 0.00667 0.00224 -0.1228 0.6103 0.7232
3.500 0.9006 0.00680 0.00234 -0.1222 0.5969 0.7263
3.750 0.9258 0.00695 0.00245 -0.1217 0.5844 0.7292
4.000 0.9509 0.00709 0.00256 -0.1212 0.5726 0.7319
4.250 0.9751 0.00723 0.00268 -0.1205 0.5594 0.7347
4.500 0.9983 0.00742 0.00283 -0.1196 0.5410 0.7372
4.750 1.0202 0.00766 0.00300 -0.1184 0.5187 0.7398
5.000 1.0423 0.00791 0.00317 -0.1173 0.4995 0.7427
5.250 1.0648 0.00814 0.00334 -0.1163 0.4793 0.7453
5.500 1.0861 0.00841 0.00354 -0.1151 0.4566 0.7475
5.750 1.1054 0.00872 0.00376 -0.1135 0.4297 0.7501
6.000 1.1224 0.00913 0.00403 -0.1115 0.3955 0.7527
6.250 1.1364 0.00965 0.00437 -0.1090 0.3561 0.7553
6.500 1.1470 0.01029 0.00479 -0.1059 0.3105 0.7579
6.750 1.1572 0.01090 0.00521 -0.1027 0.2710 0.7605
7.000 1.1642 0.01147 0.00560 -0.0989 0.2377 0.7628
7.250 1.1736 0.01198 0.00601 -0.0955 0.2112 0.7658
7.500 1.1831 0.01252 0.00645 -0.0923 0.1885 0.7688
7.750 1.1945 0.01302 0.00688 -0.0895 0.1707 0.7721
8.000 1.2052 0.01355 0.00734 -0.0866 0.1526 0.7758
8.250 1.2156 0.01410 0.00782 -0.0838 0.1362 0.7796
8.500 1.2238 0.01475 0.00840 -0.0808 0.1178 0.7833
8.750 1.2318 0.01546 0.00903 -0.0779 0.1008 0.7864
9.000 1.2402 0.01622 0.00973 -0.0752 0.0851 0.7897
9.250 1.2488 0.01703 0.01048 -0.0727 0.0722 0.7929
9.500 1.2583 0.01784 0.01126 -0.0704 0.0620 0.7962
9.750 1.2681 0.01867 0.01207 -0.0682 0.0543 0.8001
10.000 1.2797 0.01945 0.01286 -0.0664 0.0489 0.8044
10.250 1.2914 0.02027 0.01368 -0.0646 0.0441 0.8087
10.500 1.3030 0.02109 0.01453 -0.0629 0.0405 0.8135
10.750 1.3141 0.02199 0.01546 -0.0612 0.0372 0.8194
11.000 1.3280 0.02273 0.01626 -0.0598 0.0355 0.8262
11.250 1.3396 0.02362 0.01720 -0.0583 0.0333 0.8366
11.500 1.3490 0.02468 0.01834 -0.0566 0.0307 0.8547
11.750 1.3796 0.02550 0.01939 -0.0589 0.0291 0.9148
12.000 1.4272 0.02706 0.02099 -0.0655 0.0264 1.0000
12.250 1.4381 0.02831 0.02228 -0.0644 0.0249 1.0000
12.500 1.4522 0.02934 0.02336 -0.0636 0.0238 1.0000
12.750 1.4643 0.03050 0.02454 -0.0626 0.0227 1.0000
13.000 1.4746 0.03180 0.02587 -0.0615 0.0218 1.0000
13.250 1.4797 0.03353 0.02763 -0.0601 0.0205 1.0000
13.500 1.4908 0.03479 0.02896 -0.0591 0.0200 1.0000
13.750 1.5016 0.03609 0.03030 -0.0582 0.0193 1.0000
14.000 1.5116 0.03747 0.03173 -0.0573 0.0184 1.0000
14.250 1.5195 0.03907 0.03337 -0.0563 0.0178 1.0000
14.500 1.5244 0.04097 0.03530 -0.0552 0.0171 1.0000
14.750 1.5252 0.04327 0.03768 -0.0539 0.0164 1.0000
15.000 1.5346 0.04484 0.03931 -0.0533 0.0160 1.0000
15.250 1.5423 0.04661 0.04114 -0.0526 0.0155 1.0000
15.500 1.5491 0.04849 0.04308 -0.0519 0.0150 1.0000
15.750 1.5539 0.05061 0.04527 -0.0512 0.0146 1.0000
16.000 1.5576 0.05285 0.04757 -0.0506 0.0142 1.0000
16.250 1.5582 0.05546 0.05023 -0.0500 0.0136 1.0000
16.500 1.5542 0.05866 0.05351 -0.0494 0.0133 1.0000
16.750 1.5546 0.06143 0.05637 -0.0490 0.0129 1.0000
17.000 1.5575 0.06395 0.05897 -0.0487 0.0127 1.0000
17.250 1.5591 0.06663 0.06173 -0.0485 0.0124 1.0000
17.500 1.5577 0.06971 0.06490 -0.0484 0.0122 1.0000
17.750 1.5578 0.07267 0.06794 -0.0484 0.0119 1.0000
18.000 1.5566 0.07583 0.07118 -0.0485 0.0117 1.0000
18.250 1.5543 0.07919 0.07462 -0.0487 0.0114 1.0000
18.500 1.5494 0.08289 0.07840 -0.0490 0.0112 1.0000
18.750 1.5438 0.08678 0.08237 -0.0495 0.0110 1.0000
19.000 1.5354 0.09114 0.08682 -0.0503 0.0108 1.0000
19.250 1.5246 0.09596 0.09174 -0.0514 0.0107 1.0000
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