FX 61-184 AIRFOIL (fx61184-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 61-184 AIRFOIL (fx61184-il) Reynolds number: 1,000,000 Max Cl/Cd: 131.08 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx61184-il-1000000.txt Download as CSV file: xf-fx61184-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.250 -0.6955 0.13836 0.13623 -0.0393 1.0000 0.0070
-19.000 -0.7620 0.11994 0.11754 -0.0487 1.0000 0.0068
-18.750 -0.7851 0.11104 0.10850 -0.0535 1.0000 0.0070
-18.500 -0.8193 0.10079 0.09809 -0.0589 1.0000 0.0067
-18.250 -0.8356 0.09391 0.09107 -0.0626 1.0000 0.0068
-18.000 -0.8557 0.08672 0.08374 -0.0664 1.0000 0.0068
-17.750 -0.8615 0.08193 0.07885 -0.0689 1.0000 0.0069
-17.500 -0.8741 0.07638 0.07317 -0.0717 1.0000 0.0070
-17.250 -0.8705 0.07321 0.06992 -0.0733 1.0000 0.0071
-17.000 -0.8804 0.06839 0.06498 -0.0755 1.0000 0.0071
-16.750 -0.8860 0.06434 0.06082 -0.0772 1.0000 0.0072
-16.500 -0.9045 0.05890 0.05524 -0.0791 1.0000 0.0074
-16.250 -0.9061 0.05572 0.05197 -0.0802 1.0000 0.0075
-16.000 -0.9090 0.05253 0.04870 -0.0810 1.0000 0.0075
-15.750 -0.9042 0.05024 0.04639 -0.0817 1.0000 0.0078
-15.500 -0.9000 0.04799 0.04410 -0.0821 1.0000 0.0079
-15.250 -0.8920 0.04621 0.04228 -0.0825 1.0000 0.0082
-15.000 -0.8746 0.04315 0.03914 -0.0859 0.9615 0.0083
-14.750 -0.8177 0.04063 0.03645 -0.0968 0.9280 0.0089
-14.500 -0.7634 0.03852 0.03401 -0.1066 0.8827 0.0093
-14.250 -0.7280 0.03661 0.03185 -0.1126 0.8527 0.0095
-14.000 -0.7179 0.03413 0.02916 -0.1149 0.8332 0.0100
-13.750 -0.6992 0.03286 0.02782 -0.1165 0.8209 0.0103
-13.500 -0.6821 0.03168 0.02655 -0.1175 0.8119 0.0106
-13.250 -0.6673 0.03041 0.02518 -0.1182 0.8042 0.0109
-13.000 -0.6520 0.02931 0.02400 -0.1187 0.7980 0.0111
-12.750 -0.6337 0.02848 0.02311 -0.1192 0.7921 0.0116
-12.500 -0.6175 0.02751 0.02204 -0.1194 0.7869 0.0119
-12.250 -0.5994 0.02675 0.02121 -0.1196 0.7826 0.0122
-12.000 -0.5906 0.02541 0.01981 -0.1191 0.7783 0.0126
-11.750 -0.5785 0.02432 0.01867 -0.1188 0.7742 0.0130
-11.500 -0.5634 0.02345 0.01774 -0.1187 0.7701 0.0134
-11.250 -0.5467 0.02273 0.01700 -0.1184 0.7669 0.0138
-11.000 -0.5323 0.02190 0.01613 -0.1179 0.7635 0.0140
-10.750 -0.5158 0.02121 0.01540 -0.1175 0.7602 0.0145
-10.500 -0.4995 0.02054 0.01468 -0.1170 0.7568 0.0149
-10.250 -0.4796 0.02007 0.01415 -0.1169 0.7530 0.0156
-10.000 -0.4716 0.01898 0.01302 -0.1155 0.7503 0.0160
-9.750 -0.4599 0.01812 0.01215 -0.1144 0.7474 0.0164
-9.500 -0.4461 0.01740 0.01141 -0.1134 0.7445 0.0170
-9.250 -0.4276 0.01697 0.01096 -0.1128 0.7416 0.0178
-9.000 -0.4139 0.01632 0.01026 -0.1117 0.7385 0.0183
-8.750 -0.3996 0.01579 0.00970 -0.1104 0.7357 0.0188
-8.500 -0.3875 0.01528 0.00916 -0.1089 0.7333 0.0191
-8.250 -0.3769 0.01425 0.00809 -0.1080 0.7305 0.0201
-8.000 -0.3572 0.01364 0.00745 -0.1080 0.7278 0.0210
-7.750 -0.3351 0.01321 0.00699 -0.1078 0.7251 0.0219
-7.500 -0.3114 0.01287 0.00660 -0.1078 0.7224 0.0229
-7.250 -0.2875 0.01248 0.00616 -0.1079 0.7197 0.0244
-7.000 -0.2634 0.01205 0.00574 -0.1079 0.7174 0.0268
-6.750 -0.2378 0.01172 0.00539 -0.1081 0.7150 0.0299
-6.500 -0.2119 0.01135 0.00503 -0.1083 0.7124 0.0354
-6.250 -0.1857 0.01095 0.00469 -0.1086 0.7100 0.0461
-6.000 -0.1589 0.01058 0.00437 -0.1091 0.7074 0.0621
-5.750 -0.1317 0.01012 0.00403 -0.1098 0.7045 0.0963
-5.500 -0.1047 0.00926 0.00352 -0.1110 0.7025 0.1803
-5.250 -0.0755 0.00818 0.00294 -0.1129 0.7002 0.3047
-5.000 -0.0443 0.00735 0.00250 -0.1147 0.6977 0.4126
-4.750 -0.0132 0.00698 0.00233 -0.1159 0.6950 0.4762
-4.500 0.0172 0.00690 0.00228 -0.1166 0.6925 0.5045
-4.250 0.0475 0.00691 0.00227 -0.1172 0.6897 0.5244
-4.000 0.0776 0.00694 0.00229 -0.1177 0.6871 0.5381
-3.750 0.1076 0.00696 0.00231 -0.1182 0.6844 0.5482
-3.500 0.1376 0.00704 0.00238 -0.1186 0.6815 0.5601
-3.250 0.1674 0.00712 0.00244 -0.1190 0.6787 0.5669
-3.000 0.1975 0.00721 0.00246 -0.1195 0.6758 0.5715
-2.750 0.2271 0.00723 0.00244 -0.1199 0.6725 0.5747
-2.500 0.2566 0.00723 0.00245 -0.1203 0.6699 0.5775
-2.250 0.2863 0.00724 0.00246 -0.1208 0.6669 0.5802
-2.000 0.3160 0.00726 0.00245 -0.1212 0.6638 0.5827
-1.750 0.3457 0.00728 0.00243 -0.1217 0.6605 0.5849
-1.500 0.3754 0.00735 0.00242 -0.1221 0.6568 0.5868
-1.250 0.4050 0.00731 0.00239 -0.1226 0.6537 0.5889
-1.000 0.4344 0.00728 0.00237 -0.1230 0.6499 0.5911
-0.750 0.4637 0.00729 0.00238 -0.1234 0.6459 0.5930
-0.500 0.4928 0.00734 0.00239 -0.1237 0.6419 0.5949
-0.250 0.5223 0.00735 0.00241 -0.1241 0.6382 0.5968
0.000 0.5517 0.00736 0.00242 -0.1245 0.6340 0.5987
0.250 0.5810 0.00739 0.00242 -0.1249 0.6297 0.6004
0.500 0.6100 0.00745 0.00244 -0.1253 0.6254 0.6018
0.750 0.6396 0.00747 0.00246 -0.1258 0.6212 0.6031
1.000 0.6687 0.00745 0.00245 -0.1262 0.6162 0.6049
1.250 0.6971 0.00748 0.00245 -0.1264 0.6109 0.6066
1.500 0.7262 0.00749 0.00249 -0.1268 0.6056 0.6081
1.750 0.7549 0.00753 0.00254 -0.1271 0.5998 0.6097
2.000 0.7830 0.00761 0.00258 -0.1273 0.5942 0.6112
2.250 0.8120 0.00764 0.00263 -0.1276 0.5881 0.6127
2.500 0.8400 0.00771 0.00269 -0.1278 0.5812 0.6143
2.750 0.8684 0.00777 0.00275 -0.1280 0.5738 0.6159
3.000 0.8960 0.00787 0.00281 -0.1281 0.5653 0.6174
3.250 0.9243 0.00794 0.00288 -0.1284 0.5583 0.6186
3.500 0.9521 0.00804 0.00296 -0.1285 0.5514 0.6196
3.750 0.9799 0.00809 0.00303 -0.1287 0.5444 0.6214
4.000 1.0073 0.00818 0.00312 -0.1288 0.5366 0.6231
4.250 1.0347 0.00828 0.00323 -0.1289 0.5299 0.6247
4.500 1.0621 0.00838 0.00335 -0.1290 0.5223 0.6262
4.750 1.0888 0.00851 0.00347 -0.1290 0.5142 0.6276
5.000 1.1154 0.00865 0.00360 -0.1289 0.5046 0.6291
5.250 1.1419 0.00878 0.00374 -0.1289 0.4949 0.6306
5.500 1.1673 0.00897 0.00390 -0.1286 0.4849 0.6321
5.750 1.1936 0.00912 0.00405 -0.1285 0.4747 0.6335
6.000 1.2190 0.00930 0.00422 -0.1283 0.4637 0.6348
6.250 1.2434 0.00953 0.00442 -0.1279 0.4517 0.6360
6.500 1.2673 0.00974 0.00461 -0.1274 0.4381 0.6382
6.750 1.2902 0.01000 0.00484 -0.1267 0.4213 0.6399
7.000 1.3119 0.01031 0.00511 -0.1259 0.4023 0.6414
7.250 1.3304 0.01076 0.00545 -0.1244 0.3777 0.6429
7.500 1.3468 0.01127 0.00584 -0.1227 0.3495 0.6445
7.750 1.3628 0.01177 0.00625 -0.1208 0.3267 0.6462
8.000 1.3763 0.01227 0.00666 -0.1185 0.3041 0.6478
8.250 1.3852 0.01284 0.00713 -0.1154 0.2827 0.6493
8.500 1.3936 0.01350 0.00768 -0.1123 0.2587 0.6508
8.750 1.3994 0.01428 0.00835 -0.1089 0.2364 0.6521
9.000 1.4062 0.01504 0.00903 -0.1059 0.2160 0.6544
9.250 1.4111 0.01592 0.00985 -0.1027 0.1966 0.6564
9.500 1.4156 0.01691 0.01077 -0.0997 0.1800 0.6581
9.750 1.4208 0.01796 0.01178 -0.0971 0.1650 0.6599
10.000 1.4269 0.01906 0.01284 -0.0948 0.1510 0.6617
10.250 1.4327 0.02028 0.01401 -0.0926 0.1373 0.6635
10.500 1.4373 0.02165 0.01533 -0.0905 0.1232 0.6653
10.750 1.4423 0.02307 0.01670 -0.0886 0.1104 0.6669
11.000 1.4461 0.02464 0.01821 -0.0867 0.0975 0.6683
11.250 1.4512 0.02617 0.01973 -0.0851 0.0862 0.6708
11.500 1.4543 0.02790 0.02142 -0.0834 0.0741 0.6730
11.750 1.4578 0.02965 0.02315 -0.0818 0.0639 0.6752
12.000 1.4619 0.03142 0.02490 -0.0804 0.0555 0.6773
12.250 1.4651 0.03329 0.02675 -0.0790 0.0479 0.6793
12.500 1.4689 0.03518 0.02863 -0.0778 0.0416 0.6813
12.750 1.4744 0.03700 0.03045 -0.0768 0.0365 0.6832
13.000 1.4790 0.03895 0.03242 -0.0758 0.0326 0.6852
13.250 1.4866 0.04069 0.03422 -0.0751 0.0303 0.6878
13.500 1.4920 0.04270 0.03626 -0.0744 0.0279 0.6903
13.750 1.4988 0.04463 0.03824 -0.0738 0.0261 0.6928
14.000 1.5069 0.04647 0.04014 -0.0734 0.0248 0.6955
14.250 1.5127 0.04860 0.04231 -0.0729 0.0233 0.6981
14.500 1.5175 0.05088 0.04463 -0.0725 0.0218 0.7006
14.750 1.5246 0.05300 0.04684 -0.0723 0.0210 0.7040
15.000 1.5322 0.05510 0.04901 -0.0721 0.0201 0.7072
15.250 1.5382 0.05740 0.05136 -0.0720 0.0191 0.7105
15.500 1.5423 0.05997 0.05399 -0.0720 0.0180 0.7138
15.750 1.5463 0.06262 0.05670 -0.0720 0.0170 0.7170
16.000 1.5530 0.06502 0.05919 -0.0722 0.0164 0.7211
16.250 1.5584 0.06760 0.06184 -0.0724 0.0155 0.7254
16.500 1.5619 0.07045 0.06474 -0.0727 0.0145 0.7298
16.750 1.5637 0.07361 0.06797 -0.0732 0.0134 0.7343
17.000 1.5688 0.07636 0.07082 -0.0736 0.0124 0.7400
17.250 1.5698 0.07973 0.07425 -0.0743 0.0111 0.7458
17.500 1.5711 0.08313 0.07773 -0.0750 0.0097 0.7524
17.750 1.5698 0.08693 0.08159 -0.0759 0.0081 0.7602
18.000 1.5683 0.09085 0.08560 -0.0769 0.0064 0.7690
18.250 1.5655 0.09507 0.08991 -0.0781 0.0053 0.7799
18.750 1.5597 0.10378 0.09887 -0.0811 0.0042 0.8136
19.000 1.5573 0.10815 0.10341 -0.0827 0.0039 0.8476
19.250 1.5471 0.11161 0.10715 -0.0823 0.0038 1.0000
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