WORTMANN FX 05-191 AIRFOIL (fx05191-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: WORTMANN FX 05-191 AIRFOIL (fx05191-il) Reynolds number: 500,000 Max Cl/Cd: 89.92 at α=5.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx05191-il-500000-n5.txt Download as CSV file: xf-fx05191-il-500000-n5.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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.500 -0.5802 0.10965 0.10655 -0.0960 0.9342 0.0147
-18.000 -0.6688 0.08165 0.07789 -0.1150 0.9257 0.0146
-17.750 -0.6725 0.07530 0.07133 -0.1211 0.9187 0.0148
-17.500 -0.6815 0.06913 0.06493 -0.1261 0.9101 0.0148
-17.250 -0.6797 0.06475 0.06036 -0.1302 0.9015 0.0150
-17.000 -0.6781 0.06094 0.05638 -0.1333 0.8936 0.0153
-16.750 -0.6798 0.05705 0.05228 -0.1358 0.8873 0.0153
-16.500 -0.6784 0.05392 0.04898 -0.1377 0.8824 0.0155
-16.250 -0.6781 0.05083 0.04572 -0.1391 0.8779 0.0156
-16.000 -0.6727 0.04841 0.04313 -0.1405 0.8740 0.0159
-15.750 -0.6679 0.04607 0.04063 -0.1414 0.8708 0.0160
-15.500 -0.6624 0.04394 0.03837 -0.1420 0.8679 0.0162
-15.250 -0.6556 0.04199 0.03629 -0.1425 0.8651 0.0163
-15.000 -0.6471 0.04026 0.03442 -0.1429 0.8625 0.0165
-14.750 -0.6375 0.03868 0.03271 -0.1432 0.8601 0.0165
-14.500 -0.6280 0.03711 0.03104 -0.1433 0.8580 0.0167
-14.000 -0.6071 0.03430 0.02808 -0.1432 0.8542 0.0171
-13.750 -0.5960 0.03308 0.02683 -0.1430 0.8522 0.0175
-13.500 -0.5839 0.03196 0.02565 -0.1427 0.8501 0.0176
-13.250 -0.5710 0.03091 0.02453 -0.1425 0.8480 0.0178
-13.000 -0.5577 0.02992 0.02349 -0.1422 0.8463 0.0181
-12.750 -0.5429 0.02909 0.02260 -0.1420 0.8446 0.0186
-12.500 -0.5290 0.02815 0.02159 -0.1416 0.8430 0.0188
-12.250 -0.5147 0.02727 0.02065 -0.1411 0.8415 0.0191
-12.000 -0.4993 0.02649 0.01978 -0.1408 0.8400 0.0195
-11.750 -0.4847 0.02569 0.01893 -0.1402 0.8386 0.0197
-11.500 -0.4702 0.02493 0.01811 -0.1395 0.8373 0.0201
-11.250 -0.4552 0.02422 0.01736 -0.1388 0.8358 0.0203
-11.000 -0.4411 0.02349 0.01658 -0.1379 0.8341 0.0204
-10.750 -0.4297 0.02262 0.01569 -0.1368 0.8322 0.0208
-10.500 -0.4160 0.02191 0.01496 -0.1358 0.8303 0.0211
-10.250 -0.4022 0.02122 0.01425 -0.1348 0.8283 0.0216
-10.000 -0.3874 0.02061 0.01359 -0.1338 0.8260 0.0219
-9.750 -0.3719 0.02004 0.01297 -0.1329 0.8238 0.0225
-9.500 -0.3566 0.01950 0.01241 -0.1319 0.8218 0.0231
-9.250 -0.3420 0.01897 0.01185 -0.1306 0.8194 0.0236
-9.000 -0.3273 0.01844 0.01129 -0.1293 0.8169 0.0241
-8.750 -0.3114 0.01796 0.01078 -0.1282 0.8146 0.0247
-8.500 -0.2978 0.01739 0.01019 -0.1268 0.8125 0.0254
-8.250 -0.2825 0.01690 0.00968 -0.1255 0.8105 0.0262
-8.000 -0.2662 0.01646 0.00921 -0.1243 0.8086 0.0270
-7.750 -0.2494 0.01605 0.00876 -0.1232 0.8066 0.0280
-7.500 -0.2334 0.01566 0.00835 -0.1218 0.8046 0.0291
-7.250 -0.2181 0.01526 0.00796 -0.1203 0.8024 0.0303
-7.000 -0.2034 0.01484 0.00756 -0.1187 0.7999 0.0322
-6.750 -0.1875 0.01448 0.00719 -0.1172 0.7975 0.0345
-6.500 -0.1723 0.01411 0.00681 -0.1156 0.7951 0.0374
-6.250 -0.1580 0.01379 0.00649 -0.1137 0.7927 0.0419
-6.000 -0.1448 0.01350 0.00620 -0.1117 0.7905 0.0478
-5.750 -0.1311 0.01320 0.00594 -0.1097 0.7880 0.0556
-5.500 -0.1152 0.01288 0.00567 -0.1082 0.7852 0.0671
-5.250 -0.0976 0.01254 0.00539 -0.1070 0.7823 0.0834
-5.000 -0.0810 0.01208 0.00508 -0.1057 0.7794 0.1169
-4.750 -0.0646 0.01149 0.00471 -0.1045 0.7767 0.1738
-4.500 -0.0491 0.01065 0.00423 -0.1034 0.7743 0.2675
-4.250 -0.0320 0.00981 0.00382 -0.1027 0.7712 0.3739
-4.000 -0.0087 0.00927 0.00358 -0.1027 0.7677 0.4508
-3.750 0.0182 0.00895 0.00343 -0.1031 0.7644 0.5009
-3.500 0.0464 0.00869 0.00331 -0.1037 0.7615 0.5450
-3.250 0.0757 0.00852 0.00322 -0.1044 0.7587 0.5772
-3.000 0.1040 0.00844 0.00318 -0.1048 0.7551 0.5949
-2.750 0.1323 0.00839 0.00313 -0.1051 0.7507 0.6065
-2.500 0.1609 0.00832 0.00307 -0.1055 0.7467 0.6134
-2.250 0.1904 0.00827 0.00297 -0.1061 0.7432 0.6202
-2.000 0.2185 0.00824 0.00294 -0.1064 0.7384 0.6265
-1.750 0.2468 0.00820 0.00291 -0.1067 0.7329 0.6333
-1.500 0.2758 0.00816 0.00282 -0.1071 0.7279 0.6397
-1.250 0.3037 0.00815 0.00283 -0.1074 0.7222 0.6460
-1.000 0.3321 0.00813 0.00279 -0.1077 0.7157 0.6529
-0.750 0.3601 0.00812 0.00277 -0.1079 0.7091 0.6588
-0.500 0.3879 0.00813 0.00277 -0.1081 0.7010 0.6650
-0.250 0.4159 0.00815 0.00275 -0.1084 0.6935 0.6716
0.000 0.4430 0.00819 0.00278 -0.1084 0.6854 0.6771
0.250 0.4704 0.00824 0.00280 -0.1086 0.6778 0.6832
0.500 0.4977 0.00831 0.00282 -0.1087 0.6696 0.6885
0.750 0.5242 0.00840 0.00289 -0.1086 0.6621 0.6935
1.000 0.5511 0.00849 0.00296 -0.1086 0.6547 0.6991
1.250 0.5783 0.00858 0.00301 -0.1088 0.6485 0.7041
1.500 0.6047 0.00868 0.00312 -0.1087 0.6421 0.7079
1.750 0.6310 0.00881 0.00322 -0.1086 0.6357 0.7123
2.000 0.6583 0.00891 0.00330 -0.1088 0.6299 0.7174
2.250 0.6848 0.00902 0.00341 -0.1088 0.6241 0.7211
2.500 0.7104 0.00916 0.00355 -0.1086 0.6188 0.7244
2.750 0.7368 0.00927 0.00367 -0.1085 0.6136 0.7280
3.000 0.7633 0.00938 0.00379 -0.1086 0.6079 0.7319
3.250 0.7897 0.00952 0.00389 -0.1086 0.6024 0.7357
3.500 0.8138 0.00965 0.00406 -0.1081 0.5960 0.7383
3.750 0.8373 0.00980 0.00422 -0.1075 0.5884 0.7412
4.000 0.8610 0.00996 0.00437 -0.1069 0.5815 0.7442
4.250 0.8847 0.01009 0.00452 -0.1064 0.5738 0.7474
4.500 0.9073 0.01026 0.00465 -0.1057 0.5662 0.7509
4.750 0.9279 0.01039 0.00483 -0.1045 0.5582 0.7533
5.000 0.9465 0.01059 0.00502 -0.1029 0.5507 0.7555
5.250 0.9666 0.01075 0.00522 -0.1017 0.5422 0.7580
5.500 0.9841 0.01101 0.00546 -0.1000 0.5318 0.7608
5.750 0.9989 0.01133 0.00574 -0.0978 0.5171 0.7638
6.000 1.0136 0.01170 0.00606 -0.0958 0.5011 0.7669
6.250 1.0285 0.01206 0.00640 -0.0938 0.4867 0.7692
6.500 1.0446 0.01241 0.00677 -0.0921 0.4741 0.7713
6.750 1.0585 0.01284 0.00720 -0.0900 0.4592 0.7737
7.000 1.0680 0.01345 0.00774 -0.0873 0.4386 0.7764
7.250 1.0755 0.01420 0.00839 -0.0845 0.4113 0.7793
7.500 1.0754 0.01534 0.00933 -0.0807 0.3713 0.7824
7.750 1.0717 0.01676 0.01050 -0.0766 0.3243 0.7849
8.000 1.0672 0.01830 0.01180 -0.0725 0.2760 0.7868
8.250 1.0634 0.01992 0.01318 -0.0688 0.2274 0.7888
8.500 1.0654 0.02132 0.01441 -0.0660 0.1914 0.7908
8.750 1.0702 0.02263 0.01558 -0.0636 0.1620 0.7929
9.000 1.0750 0.02399 0.01681 -0.0614 0.1338 0.7949
9.250 1.0802 0.02539 0.01807 -0.0594 0.1069 0.7969
9.500 1.0894 0.02660 0.01921 -0.0579 0.0925 0.7987
9.750 1.1011 0.02770 0.02028 -0.0567 0.0840 0.8003
10.000 1.1135 0.02871 0.02132 -0.0556 0.0787 0.8017
10.250 1.1247 0.02982 0.02244 -0.0543 0.0735 0.8031
10.500 1.1384 0.03079 0.02347 -0.0534 0.0701 0.8045
10.750 1.1504 0.03191 0.02462 -0.0524 0.0661 0.8059
11.000 1.1616 0.03314 0.02586 -0.0514 0.0623 0.8075
11.250 1.1750 0.03423 0.02701 -0.0506 0.0596 0.8090
11.500 1.1879 0.03540 0.02821 -0.0499 0.0563 0.8104
11.750 1.1986 0.03677 0.02960 -0.0491 0.0528 0.8118
12.000 1.2111 0.03804 0.03091 -0.0484 0.0496 0.8133
12.250 1.2225 0.03944 0.03233 -0.0478 0.0461 0.8147
12.500 1.2331 0.04094 0.03384 -0.0472 0.0429 0.8159
12.750 1.2441 0.04242 0.03536 -0.0466 0.0400 0.8169
13.000 1.2532 0.04406 0.03702 -0.0459 0.0369 0.8179
13.250 1.2632 0.04566 0.03868 -0.0454 0.0346 0.8190
13.500 1.2724 0.04736 0.04042 -0.0449 0.0323 0.8203
13.750 1.2804 0.04924 0.04233 -0.0444 0.0304 0.8215
14.000 1.2902 0.05098 0.04414 -0.0440 0.0290 0.8227
14.250 1.2991 0.05285 0.04606 -0.0437 0.0277 0.8237
14.500 1.3070 0.05485 0.04811 -0.0434 0.0264 0.8248
14.750 1.3140 0.05699 0.05030 -0.0432 0.0253 0.8259
15.000 1.3226 0.05899 0.05238 -0.0431 0.0244 0.8270
15.250 1.3307 0.06110 0.05455 -0.0431 0.0235 0.8280
15.500 1.3379 0.06333 0.05685 -0.0431 0.0227 0.8292
15.750 1.3442 0.06570 0.05926 -0.0431 0.0219 0.8303
16.000 1.3486 0.06833 0.06195 -0.0432 0.0211 0.8313
16.250 1.3561 0.07061 0.06432 -0.0434 0.0205 0.8323
16.500 1.3625 0.07304 0.06684 -0.0436 0.0198 0.8333
16.750 1.3686 0.07552 0.06941 -0.0439 0.0191 0.8342
17.000 1.3735 0.07821 0.07217 -0.0442 0.0185 0.8351
17.250 1.3776 0.08103 0.07506 -0.0447 0.0179 0.8360
17.500 1.3796 0.08416 0.07826 -0.0452 0.0173 0.8368
17.750 1.3843 0.08699 0.08118 -0.0458 0.0169 0.8378
18.000 1.3889 0.08986 0.08416 -0.0465 0.0164 0.8387
18.250 1.3926 0.09288 0.08728 -0.0472 0.0159 0.8397
18.500 1.3964 0.09591 0.09040 -0.0481 0.0154 0.8407
18.750 1.3988 0.09918 0.09376 -0.0491 0.0150 0.8416
19.000 1.4007 0.10254 0.09718 -0.0501 0.0145 0.8426
19.250 1.4006 0.10624 0.10096 -0.0514 0.0141 0.8435
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