WORTMANN FX 75-141 (fx75141-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 75-141 (fx75141-il) Reynolds number: 200,000 Max Cl/Cd: 77.32 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx75141-il-200000-n5.txt Download as CSV file: xf-fx75141-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.500 -0.5485 0.05648 0.05195 -0.1049 0.9104 0.0204
-12.250 -0.5473 0.05053 0.04575 -0.1133 0.8994 0.0206
-12.000 -0.5411 0.04629 0.04127 -0.1195 0.8904 0.0210
-11.750 -0.5409 0.04215 0.03685 -0.1243 0.8820 0.0212
-11.500 -0.5357 0.03889 0.03333 -0.1279 0.8758 0.0215
-11.250 -0.5321 0.03623 0.03045 -0.1297 0.8702 0.0219
-11.000 -0.5288 0.03387 0.02783 -0.1305 0.8651 0.0222
-10.750 -0.5250 0.03199 0.02570 -0.1302 0.8609 0.0226
-10.500 -0.5169 0.03025 0.02369 -0.1297 0.8574 0.0233
-10.250 -0.5064 0.02864 0.02180 -0.1289 0.8537 0.0240
-10.000 -0.4926 0.02722 0.02012 -0.1282 0.8503 0.0248
-9.750 -0.4751 0.02630 0.01916 -0.1279 0.8474 0.0256
-9.500 -0.4559 0.02557 0.01835 -0.1276 0.8451 0.0265
-9.000 -0.4172 0.02371 0.01618 -0.1266 0.8408 0.0286
-8.750 -0.3975 0.02279 0.01508 -0.1259 0.8382 0.0297
-8.500 -0.3777 0.02194 0.01419 -0.1253 0.8356 0.0307
-8.250 -0.3562 0.02135 0.01357 -0.1249 0.8333 0.0322
-8.000 -0.3338 0.02076 0.01290 -0.1246 0.8313 0.0340
-7.750 -0.3106 0.02017 0.01216 -0.1242 0.8294 0.0359
-7.500 -0.2883 0.01947 0.01142 -0.1239 0.8274 0.0376
-7.250 -0.2661 0.01897 0.01090 -0.1234 0.8252 0.0396
-7.000 -0.2434 0.01852 0.01039 -0.1229 0.8229 0.0423
-6.750 -0.2210 0.01798 0.00982 -0.1225 0.8203 0.0451
-6.500 -0.1974 0.01754 0.00936 -0.1222 0.8178 0.0482
-6.250 -0.1726 0.01718 0.00891 -0.1219 0.8155 0.0520
-6.000 -0.1480 0.01670 0.00844 -0.1218 0.8132 0.0566
-5.750 -0.1219 0.01638 0.00803 -0.1218 0.8113 0.0619
-5.500 -0.0987 0.01599 0.00768 -0.1214 0.8086 0.0683
-5.250 -0.0743 0.01569 0.00737 -0.1211 0.8057 0.0760
-5.000 -0.0493 0.01537 0.00706 -0.1209 0.8029 0.0870
-4.750 -0.0235 0.01505 0.00677 -0.1208 0.8002 0.1017
-4.500 0.0028 0.01469 0.00648 -0.1209 0.7978 0.1230
-4.250 0.0297 0.01435 0.00622 -0.1212 0.7957 0.1535
-4.000 0.0541 0.01401 0.00604 -0.1210 0.7927 0.1947
-3.750 0.0784 0.01360 0.00586 -0.1208 0.7894 0.2507
-3.500 0.1032 0.01313 0.00568 -0.1208 0.7865 0.3283
-3.250 0.1287 0.01273 0.00562 -0.1207 0.7837 0.4212
-3.000 0.1556 0.01257 0.00560 -0.1206 0.7814 0.4821
-2.750 0.1832 0.01250 0.00561 -0.1205 0.7791 0.5246
-2.500 0.2071 0.01251 0.00573 -0.1197 0.7754 0.5567
-2.250 0.2326 0.01256 0.00584 -0.1191 0.7719 0.5833
-2.000 0.2594 0.01262 0.00591 -0.1187 0.7688 0.6041
-1.750 0.2870 0.01270 0.00598 -0.1184 0.7661 0.6226
-1.500 0.3156 0.01279 0.00604 -0.1184 0.7637 0.6399
-1.250 0.3401 0.01291 0.00617 -0.1177 0.7595 0.6533
-1.000 0.3662 0.01301 0.00625 -0.1172 0.7555 0.6663
-0.750 0.3928 0.01312 0.00636 -0.1167 0.7521 0.6775
-0.500 0.4209 0.01318 0.00639 -0.1166 0.7493 0.6874
-0.250 0.4486 0.01323 0.00640 -0.1165 0.7462 0.6947
0.000 0.4730 0.01329 0.00648 -0.1159 0.7411 0.7012
0.250 0.4994 0.01331 0.00651 -0.1155 0.7369 0.7063
0.500 0.5279 0.01330 0.00646 -0.1156 0.7336 0.7126
0.750 0.5556 0.01329 0.00644 -0.1155 0.7301 0.7177
1.000 0.5791 0.01335 0.00656 -0.1146 0.7242 0.7225
1.250 0.6063 0.01334 0.00654 -0.1145 0.7198 0.7282
1.500 0.6353 0.01328 0.00646 -0.1146 0.7164 0.7329
1.750 0.6585 0.01334 0.00660 -0.1137 0.7100 0.7371
2.000 0.6848 0.01333 0.00660 -0.1133 0.7048 0.7422
2.250 0.7139 0.01326 0.00651 -0.1135 0.7007 0.7474
2.500 0.7365 0.01332 0.00667 -0.1125 0.6933 0.7510
2.750 0.7632 0.01327 0.00665 -0.1122 0.6877 0.7553
3.000 0.7889 0.01328 0.00669 -0.1118 0.6812 0.7602
3.250 0.8146 0.01326 0.00672 -0.1113 0.6739 0.7643
3.500 0.8401 0.01322 0.00673 -0.1108 0.6661 0.7680
3.750 0.8666 0.01310 0.00660 -0.1103 0.6557 0.7723
4.000 0.8917 0.01300 0.00647 -0.1095 0.6405 0.7768
4.250 0.9162 0.01296 0.00641 -0.1087 0.6247 0.7805
4.500 0.9403 0.01300 0.00646 -0.1079 0.6117 0.7843
4.750 0.9646 0.01308 0.00655 -0.1072 0.5996 0.7885
5.000 0.9891 0.01320 0.00668 -0.1065 0.5874 0.7930
5.250 1.0125 0.01333 0.00681 -0.1056 0.5747 0.7967
5.500 1.0347 0.01349 0.00697 -0.1045 0.5604 0.8008
5.750 1.0566 0.01369 0.00718 -0.1034 0.5460 0.8055
6.000 1.0770 0.01393 0.00741 -0.1020 0.5285 0.8103
6.250 1.0937 0.01421 0.00765 -0.0999 0.5040 0.8149
6.500 1.1081 0.01457 0.00793 -0.0974 0.4751 0.8202
6.750 1.1204 0.01501 0.00827 -0.0946 0.4436 0.8257
7.000 1.1289 0.01549 0.00865 -0.0912 0.4111 0.8308
7.250 1.1332 0.01608 0.00911 -0.0872 0.3761 0.8367
7.500 1.1348 0.01689 0.00974 -0.0829 0.3375 0.8430
7.750 1.1356 0.01782 0.01050 -0.0788 0.3007 0.8504
8.000 1.1379 0.01883 0.01138 -0.0752 0.2682 0.8585
8.250 1.1419 0.01990 0.01234 -0.0723 0.2384 0.8686
8.500 1.1484 0.02097 0.01334 -0.0699 0.2128 0.8831
8.750 1.1593 0.02204 0.01439 -0.0685 0.1897 0.9104
9.000 1.1666 0.02306 0.01537 -0.0665 0.1710 1.0000
9.250 1.1767 0.02422 0.01646 -0.0650 0.1526 1.0000
9.500 1.1862 0.02544 0.01762 -0.0635 0.1345 1.0000
9.750 1.1949 0.02674 0.01883 -0.0619 0.1168 1.0000
10.000 1.2035 0.02808 0.02009 -0.0604 0.1015 1.0000
10.250 1.2120 0.02944 0.02140 -0.0590 0.0877 1.0000
10.500 1.2199 0.03089 0.02279 -0.0576 0.0769 1.0000
10.750 1.2292 0.03225 0.02417 -0.0563 0.0689 1.0000
11.000 1.2373 0.03372 0.02564 -0.0550 0.0628 1.0000
11.250 1.2456 0.03521 0.02715 -0.0537 0.0576 1.0000
11.500 1.2527 0.03682 0.02878 -0.0525 0.0535 1.0000
11.750 1.2612 0.03833 0.03037 -0.0513 0.0500 1.0000
12.000 1.2678 0.04004 0.03211 -0.0502 0.0470 1.0000
12.250 1.2733 0.04189 0.03402 -0.0491 0.0447 1.0000
12.500 1.2811 0.04357 0.03580 -0.0482 0.0422 1.0000
12.750 1.2872 0.04545 0.03774 -0.0473 0.0400 1.0000
13.000 1.2914 0.04757 0.03991 -0.0464 0.0384 1.0000
13.250 1.2957 0.04974 0.04214 -0.0456 0.0368 1.0000
13.500 1.3020 0.05176 0.04428 -0.0450 0.0353 1.0000
13.750 1.3076 0.05392 0.04654 -0.0444 0.0338 1.0000
14.000 1.3121 0.05623 0.04892 -0.0440 0.0323 1.0000
14.250 1.3142 0.05888 0.05162 -0.0437 0.0312 1.0000
14.500 1.3174 0.06145 0.05428 -0.0433 0.0302 1.0000
14.750 1.3220 0.06393 0.05689 -0.0431 0.0291 1.0000
15.000 1.3261 0.06651 0.05958 -0.0431 0.0279 1.0000
15.250 1.3293 0.06925 0.06242 -0.0431 0.0270 1.0000
15.500 1.3312 0.07223 0.06548 -0.0434 0.0261 1.0000
15.750 1.3315 0.07543 0.06875 -0.0436 0.0255 1.0000
16.000 1.3324 0.07860 0.07202 -0.0439 0.0248 1.0000
16.250 1.3344 0.08172 0.07530 -0.0443 0.0241 1.0000
16.500 1.3357 0.08499 0.07871 -0.0448 0.0235 1.0000
16.750 1.3363 0.08841 0.08226 -0.0455 0.0228 1.0000
17.000 1.3361 0.09197 0.08594 -0.0464 0.0222 1.0000
17.250 1.3353 0.09570 0.08978 -0.0475 0.0216 1.0000
17.500 1.3338 0.09958 0.09375 -0.0487 0.0212 1.0000
17.750 1.3315 0.10362 0.09786 -0.0502 0.0207 1.0000
18.000 1.3293 0.10767 0.10202 -0.0516 0.0202 1.0000
18.250 1.3260 0.11208 0.10664 -0.0533 0.0198 1.0000
18.500 1.3220 0.11667 0.11141 -0.0553 0.0193 1.0000
18.750 1.3175 0.12139 0.11630 -0.0574 0.0189 1.0000
19.000 1.3126 0.12627 0.12134 -0.0598 0.0186 1.0000
19.250 1.3068 0.13138 0.12660 -0.0625 0.0183 1.0000
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