FX 61-184 AIRFOIL (fx61184-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 61-184 AIRFOIL (fx61184-il) Reynolds number: 500,000 Max Cl/Cd: 100.71 at α=5.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx61184-il-500000-n5.txt Download as CSV file: xf-fx61184-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 61-184 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 -0.6957 0.12446 0.12149 -0.0476 1.0000 0.0073
-18.250 -0.7329 0.11243 0.10926 -0.0539 1.0000 0.0073
-18.000 -0.7594 0.10310 0.09976 -0.0588 1.0000 0.0073
-17.750 -0.7773 0.09573 0.09226 -0.0628 1.0000 0.0073
-17.500 -0.7936 0.08894 0.08534 -0.0665 1.0000 0.0074
-17.250 -0.8019 0.08367 0.07999 -0.0694 1.0000 0.0075
-17.000 -0.8143 0.07800 0.07418 -0.0722 1.0000 0.0075
-16.750 -0.8210 0.07339 0.06947 -0.0745 1.0000 0.0076
-16.500 -0.8257 0.06922 0.06520 -0.0765 1.0000 0.0077
-16.250 -0.8296 0.06535 0.06122 -0.0782 1.0000 0.0077
-16.000 -0.8326 0.06175 0.05753 -0.0796 1.0000 0.0078
-15.750 -0.8311 0.05882 0.05453 -0.0808 1.0000 0.0080
-15.500 -0.8279 0.05578 0.05140 -0.0824 0.9997 0.0081
-15.250 -0.8082 0.05225 0.04774 -0.0869 0.9417 0.0084
-15.000 -0.7693 0.04817 0.04340 -0.0971 0.9157 0.0087
-14.750 -0.7217 0.04484 0.03977 -0.1078 0.8917 0.0092
-14.500 -0.6896 0.04247 0.03709 -0.1139 0.8609 0.0096
-14.250 -0.6757 0.04033 0.03476 -0.1162 0.8403 0.0097
-14.000 -0.6639 0.03859 0.03288 -0.1174 0.8261 0.0099
-13.750 -0.6487 0.03730 0.03149 -0.1184 0.8155 0.0104
-13.500 -0.6355 0.03600 0.03008 -0.1189 0.8067 0.0107
-13.250 -0.6249 0.03454 0.02850 -0.1191 0.7994 0.0109
-13.000 -0.6128 0.03330 0.02717 -0.1192 0.7930 0.0111
-12.750 -0.5975 0.03235 0.02612 -0.1194 0.7876 0.0117
-12.500 -0.5849 0.03122 0.02488 -0.1192 0.7830 0.0120
-12.250 -0.5711 0.03020 0.02378 -0.1191 0.7784 0.0123
-12.000 -0.5598 0.02906 0.02260 -0.1188 0.7739 0.0128
-11.500 -0.5335 0.02711 0.02053 -0.1181 0.7661 0.0134
-11.250 -0.5175 0.02636 0.01974 -0.1179 0.7624 0.0140
-11.000 -0.5034 0.02550 0.01882 -0.1174 0.7589 0.0144
-10.750 -0.4881 0.02474 0.01799 -0.1169 0.7557 0.0149
-10.500 -0.4733 0.02398 0.01714 -0.1163 0.7527 0.0153
-10.250 -0.4620 0.02301 0.01615 -0.1155 0.7494 0.0158
-10.000 -0.4492 0.02216 0.01528 -0.1146 0.7461 0.0163
-9.750 -0.4355 0.02140 0.01448 -0.1138 0.7430 0.0167
-9.500 -0.4213 0.02068 0.01372 -0.1130 0.7400 0.0173
-9.000 -0.3937 0.01926 0.01220 -0.1110 0.7341 0.0183
-8.750 -0.3803 0.01856 0.01146 -0.1099 0.7311 0.0188
-8.500 -0.3684 0.01786 0.01073 -0.1085 0.7281 0.0195
-8.250 -0.3597 0.01720 0.01006 -0.1066 0.7252 0.0205
-8.000 -0.3455 0.01661 0.00943 -0.1056 0.7225 0.0214
-7.750 -0.3277 0.01603 0.00879 -0.1052 0.7199 0.0225
-7.500 -0.3076 0.01549 0.00821 -0.1051 0.7174 0.0236
-7.250 -0.2872 0.01493 0.00765 -0.1050 0.7146 0.0256
-7.000 -0.2647 0.01452 0.00720 -0.1049 0.7118 0.0278
-6.750 -0.2415 0.01410 0.00677 -0.1048 0.7091 0.0313
-6.500 -0.2172 0.01375 0.00639 -0.1049 0.7065 0.0359
-6.250 -0.1923 0.01339 0.00602 -0.1051 0.7041 0.0431
-6.000 -0.1669 0.01301 0.00568 -0.1054 0.7014 0.0527
-5.750 -0.1411 0.01261 0.00534 -0.1057 0.6986 0.0667
-5.500 -0.1152 0.01213 0.00496 -0.1062 0.6957 0.0941
-5.250 -0.0892 0.01144 0.00450 -0.1070 0.6930 0.1522
-5.000 -0.0619 0.01045 0.00390 -0.1086 0.6905 0.2558
-4.750 -0.0317 0.00937 0.00328 -0.1108 0.6880 0.3838
-4.500 -0.0009 0.00886 0.00311 -0.1122 0.6852 0.4683
-4.250 0.0293 0.00879 0.00312 -0.1129 0.6825 0.5049
-4.000 0.0592 0.00883 0.00319 -0.1133 0.6795 0.5317
-3.750 0.0889 0.00894 0.00327 -0.1137 0.6766 0.5488
-3.500 0.1189 0.00899 0.00323 -0.1142 0.6739 0.5569
-3.250 0.1483 0.00903 0.00324 -0.1146 0.6712 0.5610
-3.000 0.1779 0.00905 0.00323 -0.1150 0.6680 0.5648
-2.750 0.2076 0.00905 0.00319 -0.1155 0.6645 0.5685
-2.500 0.2374 0.00906 0.00311 -0.1160 0.6611 0.5715
-2.250 0.2665 0.00907 0.00309 -0.1163 0.6580 0.5737
-2.000 0.2958 0.00908 0.00308 -0.1167 0.6549 0.5759
-1.750 0.3252 0.00910 0.00309 -0.1171 0.6512 0.5784
-1.500 0.3545 0.00911 0.00308 -0.1175 0.6474 0.5809
-1.250 0.3838 0.00913 0.00305 -0.1179 0.6439 0.5834
-1.000 0.4133 0.00916 0.00301 -0.1183 0.6406 0.5857
-0.750 0.4429 0.00916 0.00300 -0.1188 0.6366 0.5877
-0.500 0.4717 0.00916 0.00301 -0.1191 0.6322 0.5893
-0.250 0.5005 0.00918 0.00301 -0.1194 0.6281 0.5908
0.000 0.5294 0.00921 0.00303 -0.1197 0.6239 0.5925
0.250 0.5583 0.00923 0.00306 -0.1201 0.6188 0.5942
0.500 0.5870 0.00927 0.00307 -0.1204 0.6141 0.5959
0.750 0.6157 0.00931 0.00309 -0.1206 0.6097 0.5978
1.000 0.6446 0.00934 0.00312 -0.1210 0.6046 0.5996
1.250 0.6733 0.00939 0.00315 -0.1213 0.5994 0.6013
1.750 0.7304 0.00948 0.00322 -0.1219 0.5892 0.6044
2.000 0.7584 0.00953 0.00329 -0.1221 0.5832 0.6058
2.250 0.7862 0.00960 0.00335 -0.1222 0.5773 0.6072
2.500 0.8141 0.00966 0.00344 -0.1224 0.5704 0.6086
3.000 0.8694 0.00983 0.00361 -0.1226 0.5575 0.6117
3.250 0.8964 0.00994 0.00370 -0.1226 0.5500 0.6134
3.500 0.9236 0.01004 0.00381 -0.1227 0.5417 0.6151
3.750 0.9496 0.01019 0.00391 -0.1225 0.5319 0.6167
4.000 0.9762 0.01031 0.00404 -0.1225 0.5219 0.6181
4.250 1.0026 0.01046 0.00416 -0.1224 0.5140 0.6195
4.500 1.0289 0.01058 0.00431 -0.1223 0.5057 0.6208
4.750 1.0547 0.01073 0.00448 -0.1221 0.4974 0.6222
5.000 1.0801 0.01089 0.00466 -0.1219 0.4887 0.6237
5.250 1.1056 0.01105 0.00484 -0.1217 0.4805 0.6253
5.500 1.1297 0.01127 0.00505 -0.1212 0.4705 0.6270
5.750 1.1541 0.01146 0.00526 -0.1208 0.4589 0.6286
6.000 1.1773 0.01170 0.00549 -0.1201 0.4463 0.6302
6.250 1.1996 0.01197 0.00575 -0.1194 0.4331 0.6318
6.500 1.2211 0.01226 0.00602 -0.1185 0.4197 0.6333
6.750 1.2415 0.01259 0.00631 -0.1174 0.4058 0.6349
7.000 1.2605 0.01295 0.00664 -0.1161 0.3900 0.6363
7.250 1.2769 0.01336 0.00702 -0.1143 0.3712 0.6378
7.500 1.2874 0.01385 0.00746 -0.1115 0.3499 0.6395
7.750 1.2960 0.01447 0.00800 -0.1084 0.3277 0.6412
8.000 1.3038 0.01517 0.00862 -0.1054 0.3041 0.6430
8.250 1.3081 0.01606 0.00939 -0.1020 0.2793 0.6447
8.500 1.3101 0.01710 0.01032 -0.0985 0.2535 0.6464
8.750 1.3132 0.01820 0.01133 -0.0954 0.2312 0.6481
9.000 1.3169 0.01938 0.01244 -0.0927 0.2116 0.6498
9.250 1.3223 0.02059 0.01359 -0.0905 0.1951 0.6514
9.500 1.3288 0.02181 0.01477 -0.0885 0.1811 0.6530
9.750 1.3364 0.02304 0.01600 -0.0868 0.1687 0.6547
10.000 1.3442 0.02430 0.01727 -0.0852 0.1571 0.6565
10.250 1.3511 0.02569 0.01864 -0.0836 0.1448 0.6585
10.500 1.3569 0.02719 0.02012 -0.0821 0.1318 0.6606
10.750 1.3623 0.02878 0.02167 -0.0806 0.1193 0.6626
11.000 1.3666 0.03048 0.02334 -0.0791 0.1065 0.6645
11.250 1.3708 0.03226 0.02508 -0.0778 0.0946 0.6663
11.500 1.3736 0.03418 0.02696 -0.0764 0.0820 0.6680
11.750 1.3775 0.03608 0.02884 -0.0752 0.0711 0.6697
12.000 1.3810 0.03806 0.03082 -0.0741 0.0614 0.6715
12.250 1.3852 0.04005 0.03282 -0.0731 0.0535 0.6733
12.500 1.3898 0.04208 0.03487 -0.0723 0.0475 0.6754
12.750 1.3949 0.04413 0.03693 -0.0716 0.0418 0.6776
13.000 1.4009 0.04616 0.03901 -0.0710 0.0381 0.6800
13.250 1.4067 0.04826 0.04114 -0.0705 0.0348 0.6824
13.500 1.4124 0.05043 0.04336 -0.0701 0.0322 0.6846
13.750 1.4188 0.05259 0.04560 -0.0698 0.0301 0.6869
14.000 1.4239 0.05495 0.04801 -0.0696 0.0279 0.6892
14.250 1.4290 0.05736 0.05048 -0.0694 0.0260 0.6916
14.500 1.4348 0.05973 0.05293 -0.0694 0.0244 0.6942
14.750 1.4397 0.06226 0.05553 -0.0694 0.0229 0.6968
15.000 1.4433 0.06502 0.05835 -0.0695 0.0216 0.6994
15.250 1.4487 0.06760 0.06102 -0.0696 0.0207 0.7020
15.500 1.4534 0.07031 0.06383 -0.0699 0.0196 0.7048
15.750 1.4570 0.07322 0.06683 -0.0703 0.0186 0.7079
16.000 1.4597 0.07628 0.06997 -0.0707 0.0176 0.7112
16.250 1.4626 0.07940 0.07317 -0.0713 0.0167 0.7146
16.500 1.4660 0.08249 0.07636 -0.0719 0.0159 0.7182
16.750 1.4687 0.08570 0.07968 -0.0726 0.0151 0.7223
17.000 1.4700 0.08918 0.08325 -0.0735 0.0144 0.7266
17.250 1.4702 0.09286 0.08702 -0.0745 0.0136 0.7309
17.500 1.4723 0.09632 0.09059 -0.0755 0.0130 0.7355
17.750 1.4735 0.09996 0.09435 -0.0767 0.0123 0.7406
18.000 1.4736 0.10379 0.09828 -0.0779 0.0115 0.7459
18.250 1.4729 0.10779 0.10238 -0.0794 0.0108 0.7514
18.500 1.4729 0.11172 0.10644 -0.0809 0.0101 0.7581
18.750 1.4723 0.11580 0.11063 -0.0825 0.0093 0.7653
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