WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il) Reynolds number: 1,000,000 Max Cl/Cd: 118.89 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx05191-il-1000000.txt Download as CSV file: xf-fx05191-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: WORTMANN FX 05-191 AIRFOIL
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
------ -------- --------- --------- -------- -------- --------
-19.000 -0.7408 0.09771 0.09513 -0.0909 0.9513 0.0144
-18.750 -0.7592 0.08810 0.08529 -0.0990 0.9450 0.0144
-18.500 -0.7668 0.08080 0.07779 -0.1057 0.9378 0.0145
-18.250 -0.7713 0.07422 0.07102 -0.1120 0.9304 0.0145
-18.000 -0.7645 0.06970 0.06637 -0.1172 0.9221 0.0147
-17.750 -0.7556 0.06530 0.06184 -0.1227 0.9155 0.0149
-17.500 -0.7585 0.06023 0.05656 -0.1271 0.9080 0.0149
-17.250 -0.7512 0.05669 0.05289 -0.1309 0.9004 0.0151
-17.000 -0.7483 0.05310 0.04913 -0.1339 0.8943 0.0152
-16.750 -0.7427 0.05013 0.04602 -0.1363 0.8888 0.0153
-16.500 -0.7331 0.04771 0.04348 -0.1386 0.8839 0.0155
-16.250 -0.7279 0.04507 0.04069 -0.1402 0.8797 0.0157
-16.000 -0.7177 0.04320 0.03875 -0.1417 0.8763 0.0160
-15.750 -0.7111 0.04100 0.03641 -0.1427 0.8733 0.0162
-15.500 -0.7015 0.03917 0.03447 -0.1436 0.8705 0.0163
-15.250 -0.6924 0.03732 0.03248 -0.1443 0.8678 0.0165
-15.000 -0.6800 0.03578 0.03083 -0.1453 0.8650 0.0167
-14.750 -0.6692 0.03443 0.02940 -0.1455 0.8632 0.0169
-14.500 -0.6581 0.03308 0.02796 -0.1455 0.8614 0.0169
-14.250 -0.6494 0.03143 0.02619 -0.1451 0.8596 0.0173
-14.000 -0.6371 0.03018 0.02488 -0.1448 0.8578 0.0176
-13.750 -0.6238 0.02907 0.02373 -0.1446 0.8560 0.0178
-13.500 -0.6093 0.02808 0.02270 -0.1445 0.8542 0.0180
-13.250 -0.5945 0.02716 0.02173 -0.1444 0.8524 0.0184
-13.000 -0.5780 0.02636 0.02089 -0.1445 0.8503 0.0187
-12.750 -0.5610 0.02559 0.02006 -0.1446 0.8481 0.0190
-12.500 -0.5469 0.02474 0.01916 -0.1439 0.8471 0.0192
-12.250 -0.5312 0.02404 0.01843 -0.1434 0.8459 0.0196
-12.000 -0.5161 0.02328 0.01763 -0.1428 0.8445 0.0198
-11.750 -0.5006 0.02258 0.01689 -0.1421 0.8431 0.0201
-11.500 -0.4843 0.02194 0.01621 -0.1415 0.8416 0.0204
-11.250 -0.4677 0.02135 0.01557 -0.1409 0.8397 0.0206
-11.000 -0.4544 0.02057 0.01473 -0.1398 0.8375 0.0209
-10.750 -0.4454 0.01960 0.01372 -0.1382 0.8351 0.0215
-10.500 -0.4302 0.01898 0.01307 -0.1374 0.8326 0.0218
-10.250 -0.4152 0.01841 0.01249 -0.1364 0.8308 0.0223
-10.000 -0.4010 0.01782 0.01189 -0.1352 0.8292 0.0227
-9.750 -0.3852 0.01733 0.01138 -0.1341 0.8274 0.0231
-9.500 -0.3692 0.01684 0.01087 -0.1330 0.8253 0.0238
-9.250 -0.3534 0.01635 0.01035 -0.1318 0.8235 0.0242
-9.000 -0.3357 0.01595 0.00992 -0.1309 0.8217 0.0247
-8.750 -0.3194 0.01550 0.00943 -0.1298 0.8199 0.0249
-8.500 -0.3099 0.01479 0.00868 -0.1277 0.8178 0.0258
-8.250 -0.2942 0.01436 0.00824 -0.1264 0.8155 0.0269
-8.000 -0.2779 0.01397 0.00784 -0.1251 0.8139 0.0275
-7.750 -0.2619 0.01358 0.00744 -0.1237 0.8122 0.0285
-7.500 -0.2450 0.01323 0.00708 -0.1224 0.8104 0.0292
-7.250 -0.2292 0.01284 0.00667 -0.1208 0.8083 0.0303
-7.000 -0.2153 0.01240 0.00623 -0.1190 0.8061 0.0321
-6.750 -0.1989 0.01209 0.00591 -0.1175 0.8040 0.0340
-6.500 -0.1845 0.01182 0.00561 -0.1155 0.8019 0.0361
-6.250 -0.1722 0.01154 0.00535 -0.1133 0.7994 0.0405
-6.000 -0.1554 0.01124 0.00508 -0.1119 0.7973 0.0478
-5.750 -0.1375 0.01090 0.00480 -0.1107 0.7953 0.0606
-5.500 -0.1189 0.01052 0.00452 -0.1096 0.7931 0.0814
-5.250 -0.1015 0.01000 0.00420 -0.1085 0.7906 0.1260
-5.000 -0.0851 0.00926 0.00379 -0.1074 0.7881 0.2070
-4.750 -0.0689 0.00819 0.00326 -0.1066 0.7857 0.3419
-4.500 -0.0443 0.00752 0.00294 -0.1071 0.7832 0.4420
-4.250 -0.0160 0.00728 0.00282 -0.1077 0.7809 0.4830
-4.000 0.0125 0.00710 0.00271 -0.1083 0.7786 0.5069
-3.750 0.0416 0.00695 0.00261 -0.1089 0.7760 0.5277
-3.500 0.0712 0.00681 0.00250 -0.1095 0.7732 0.5467
-3.250 0.1012 0.00668 0.00240 -0.1103 0.7704 0.5687
-3.000 0.1316 0.00655 0.00232 -0.1111 0.7677 0.5928
-2.750 0.1617 0.00649 0.00229 -0.1119 0.7647 0.6112
-2.500 0.1909 0.00642 0.00225 -0.1124 0.7614 0.6234
-2.250 0.2204 0.00635 0.00219 -0.1129 0.7577 0.6318
-2.000 0.2502 0.00629 0.00211 -0.1136 0.7539 0.6388
-1.750 0.2801 0.00626 0.00206 -0.1142 0.7501 0.6458
-1.500 0.3093 0.00622 0.00203 -0.1147 0.7459 0.6529
-1.250 0.3384 0.00617 0.00201 -0.1152 0.7408 0.6596
-1.000 0.3677 0.00616 0.00196 -0.1157 0.7357 0.6666
-0.750 0.3968 0.00614 0.00196 -0.1162 0.7299 0.6730
-0.500 0.4256 0.00613 0.00195 -0.1166 0.7230 0.6794
-0.250 0.4545 0.00615 0.00193 -0.1170 0.7164 0.6859
0.000 0.4827 0.00617 0.00196 -0.1173 0.7080 0.6913
0.250 0.5107 0.00621 0.00198 -0.1175 0.6996 0.6971
0.500 0.5388 0.00628 0.00199 -0.1178 0.6901 0.7026
0.750 0.5660 0.00634 0.00205 -0.1179 0.6812 0.7074
1.250 0.6208 0.00653 0.00218 -0.1181 0.6644 0.7168
1.750 0.6745 0.00675 0.00236 -0.1182 0.6494 0.7248
2.000 0.7010 0.00688 0.00247 -0.1181 0.6424 0.7286
2.250 0.7286 0.00699 0.00256 -0.1183 0.6364 0.7325
2.500 0.7560 0.00710 0.00265 -0.1185 0.6297 0.7358
2.750 0.7812 0.00724 0.00278 -0.1182 0.6225 0.7389
3.000 0.8078 0.00734 0.00290 -0.1181 0.6156 0.7419
3.250 0.8326 0.00751 0.00304 -0.1178 0.6082 0.7450
3.500 0.8595 0.00760 0.00315 -0.1178 0.6018 0.7481
3.750 0.8854 0.00773 0.00326 -0.1177 0.5948 0.7509
4.000 0.9105 0.00785 0.00338 -0.1174 0.5879 0.7536
4.250 0.9349 0.00797 0.00352 -0.1169 0.5800 0.7560
4.500 0.9575 0.00813 0.00367 -0.1161 0.5708 0.7584
4.750 0.9801 0.00829 0.00383 -0.1153 0.5613 0.7609
5.000 1.0028 0.00844 0.00397 -0.1145 0.5524 0.7635
5.250 1.0220 0.00862 0.00412 -0.1131 0.5427 0.7661
5.500 1.0427 0.00877 0.00427 -0.1119 0.5324 0.7682
5.750 1.0610 0.00895 0.00444 -0.1103 0.5237 0.7707
6.000 1.0815 0.00912 0.00464 -0.1091 0.5146 0.7728
6.250 1.0978 0.00939 0.00490 -0.1071 0.5012 0.7748
6.500 1.1111 0.00976 0.00522 -0.1047 0.4828 0.7772
6.750 1.1250 0.01015 0.00556 -0.1024 0.4653 0.7797
7.000 1.1378 0.01060 0.00595 -0.1001 0.4466 0.7821
7.250 1.1480 0.01119 0.00643 -0.0974 0.4229 0.7843
7.500 1.1538 0.01194 0.00705 -0.0941 0.3911 0.7866
7.750 1.1529 0.01299 0.00791 -0.0898 0.3487 0.7890
8.000 1.1496 0.01427 0.00897 -0.0854 0.3021 0.7913
8.250 1.1462 0.01568 0.01013 -0.0812 0.2543 0.7937
8.500 1.1438 0.01715 0.01136 -0.0774 0.2087 0.7961
8.750 1.1443 0.01855 0.01255 -0.0741 0.1716 0.7984
9.000 1.1473 0.01989 0.01373 -0.0714 0.1390 0.8002
9.250 1.1499 0.02130 0.01496 -0.0687 0.1074 0.8016
9.500 1.1574 0.02243 0.01601 -0.0667 0.0910 0.8037
9.750 1.1696 0.02333 0.01690 -0.0653 0.0830 0.8053
10.000 1.1807 0.02432 0.01788 -0.0638 0.0764 0.8068
10.250 1.1957 0.02510 0.01870 -0.0628 0.0730 0.8084
10.500 1.2075 0.02610 0.01970 -0.0615 0.0684 0.8100
10.750 1.2208 0.02705 0.02067 -0.0604 0.0645 0.8115
11.000 1.2358 0.02791 0.02155 -0.0595 0.0611 0.8131
11.250 1.2468 0.02907 0.02270 -0.0583 0.0565 0.8146
11.500 1.2610 0.03003 0.02369 -0.0575 0.0532 0.8159
11.750 1.2728 0.03120 0.02483 -0.0565 0.0486 0.8170
12.000 1.2849 0.03236 0.02601 -0.0556 0.0448 0.8182
12.250 1.2959 0.03362 0.02726 -0.0547 0.0407 0.8198
12.500 1.3068 0.03492 0.02859 -0.0538 0.0375 0.8210
12.750 1.3169 0.03630 0.02997 -0.0528 0.0347 0.8223
13.000 1.3264 0.03777 0.03148 -0.0519 0.0325 0.8236
13.250 1.3375 0.03916 0.03290 -0.0512 0.0307 0.8249
13.500 1.3460 0.04081 0.03458 -0.0504 0.0290 0.8261
13.750 1.3544 0.04251 0.03632 -0.0496 0.0275 0.8272
14.000 1.3653 0.04403 0.03790 -0.0491 0.0265 0.8284
14.250 1.3753 0.04566 0.03956 -0.0486 0.0254 0.8295
14.500 1.3826 0.04759 0.04152 -0.0480 0.0242 0.8307
14.750 1.3879 0.04978 0.04374 -0.0475 0.0231 0.8318
15.000 1.3986 0.05146 0.04548 -0.0472 0.0224 0.8327
15.250 1.4079 0.05329 0.04737 -0.0470 0.0217 0.8334
15.500 1.4163 0.05525 0.04939 -0.0468 0.0210 0.8347
15.750 1.4225 0.05747 0.05166 -0.0466 0.0202 0.8358
16.000 1.4248 0.06017 0.05441 -0.0463 0.0193 0.8368
16.250 1.4320 0.06237 0.05669 -0.0462 0.0188 0.8378
16.500 1.4406 0.06442 0.05881 -0.0463 0.0183 0.8388
16.750 1.4475 0.06670 0.06116 -0.0463 0.0177 0.8399
17.000 1.4539 0.06905 0.06357 -0.0465 0.0171 0.8410
17.250 1.4580 0.07175 0.06631 -0.0467 0.0165 0.8422
17.500 1.4574 0.07509 0.06971 -0.0469 0.0159 0.8432
17.750 1.4628 0.07771 0.07241 -0.0473 0.0155 0.8442
18.000 1.4690 0.08028 0.07506 -0.0477 0.0151 0.8452
18.250 1.4745 0.08293 0.07777 -0.0483 0.0146 0.8461
18.500 1.4787 0.08581 0.08073 -0.0489 0.0142 0.8470
18.750 1.4823 0.08878 0.08375 -0.0495 0.0138 0.8477
19.000 1.4831 0.09222 0.08726 -0.0504 0.0134 0.8484
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