FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 60-177 AIRFOIL (fx60177-il) Reynolds number: 1,000,000 Max Cl/Cd: 85.76 at α=3.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx60177-il-1000000-n5.txt Download as CSV file: xf-fx60177-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 60-177 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 = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-19.000 -0.7101 0.12767 0.12502 -0.0617 0.9990 0.0028
-18.750 -0.7271 0.11940 0.11665 -0.0662 0.9987 0.0027
-18.500 -0.7441 0.11142 0.10856 -0.0706 0.9983 0.0027
-18.250 -0.7605 0.10360 0.10063 -0.0750 0.9980 0.0027
-18.000 -0.7756 0.09618 0.09309 -0.0793 0.9976 0.0027
-17.750 -0.7884 0.08935 0.08614 -0.0834 0.9971 0.0027
-17.500 -0.7997 0.08285 0.07951 -0.0874 0.9966 0.0027
-17.250 -0.8094 0.07679 0.07333 -0.0913 0.9961 0.0027
-17.000 -0.8168 0.07128 0.06769 -0.0948 0.9955 0.0027
-16.750 -0.8225 0.06617 0.06245 -0.0980 0.9950 0.0027
-16.500 -0.8264 0.06148 0.05764 -0.1011 0.9944 0.0027
-16.250 -0.8276 0.05737 0.05342 -0.1036 0.9937 0.0027
-16.000 -0.8289 0.05363 0.04957 -0.1054 0.9922 0.0027
-15.750 -0.8276 0.05019 0.04603 -0.1073 0.9907 0.0027
-15.500 -0.8231 0.04716 0.04289 -0.1090 0.9893 0.0027
-15.250 -0.8175 0.04428 0.03991 -0.1107 0.9880 0.0027
-15.000 -0.8096 0.04169 0.03723 -0.1123 0.9868 0.0027
-14.750 -0.8003 0.03929 0.03473 -0.1138 0.9858 0.0027
-14.500 -0.7893 0.03705 0.03240 -0.1154 0.9849 0.0027
-14.250 -0.7765 0.03500 0.03026 -0.1169 0.9841 0.0027
-14.000 -0.7652 0.03320 0.02838 -0.1176 0.9823 0.0027
-13.750 -0.7555 0.03160 0.02671 -0.1175 0.9789 0.0027
-13.500 -0.7414 0.03002 0.02506 -0.1183 0.9767 0.0027
-13.250 -0.7257 0.02854 0.02351 -0.1192 0.9748 0.0027
-13.000 -0.7085 0.02718 0.02207 -0.1201 0.9731 0.0028
-12.750 -0.6897 0.02585 0.02068 -0.1212 0.9715 0.0028
-12.500 -0.6777 0.02481 0.01958 -0.1205 0.9664 0.0028
-12.250 -0.6605 0.02373 0.01844 -0.1207 0.9631 0.0028
-12.000 -0.6408 0.02271 0.01736 -0.1213 0.9605 0.0028
-11.750 -0.6206 0.02175 0.01635 -0.1219 0.9578 0.0028
-11.500 -0.6056 0.02094 0.01549 -0.1212 0.9527 0.0028
-11.250 -0.5866 0.02014 0.01464 -0.1212 0.9486 0.0028
-11.000 -0.5661 0.01936 0.01380 -0.1214 0.9453 0.0028
-10.750 -0.5477 0.01871 0.01310 -0.1210 0.9412 0.0029
-10.500 -0.5297 0.01806 0.01241 -0.1205 0.9364 0.0029
-10.250 -0.5093 0.01743 0.01174 -0.1204 0.9323 0.0029
-10.000 -0.4883 0.01685 0.01111 -0.1203 0.9288 0.0029
-9.750 -0.4698 0.01633 0.01055 -0.1196 0.9243 0.0029
-9.500 -0.4496 0.01581 0.01000 -0.1192 0.9199 0.0030
-9.250 -0.4276 0.01533 0.00947 -0.1191 0.9160 0.0030
-9.000 -0.4070 0.01486 0.00898 -0.1187 0.9119 0.0030
-8.750 -0.3862 0.01443 0.00851 -0.1183 0.9075 0.0031
-8.500 -0.3639 0.01401 0.00805 -0.1181 0.9035 0.0031
-8.000 -0.3206 0.01325 0.00724 -0.1173 0.8963 0.0032
-7.750 -0.3009 0.01293 0.00690 -0.1165 0.8919 0.0033
-7.500 -0.2785 0.01261 0.00655 -0.1162 0.8880 0.0034
-7.250 -0.2538 0.01230 0.00620 -0.1163 0.8848 0.0035
-7.000 -0.2316 0.01200 0.00591 -0.1159 0.8807 0.0036
-6.750 -0.2078 0.01171 0.00560 -0.1158 0.8764 0.0038
-6.500 -0.1822 0.01143 0.00530 -0.1160 0.8725 0.0043
-6.250 -0.1569 0.01109 0.00498 -0.1163 0.8688 0.0093
-6.000 -0.1322 0.01080 0.00471 -0.1164 0.8642 0.0133
-5.750 -0.1059 0.01052 0.00444 -0.1167 0.8596 0.0181
-5.500 -0.0789 0.01015 0.00412 -0.1173 0.8553 0.0342
-5.250 -0.0535 0.00987 0.00389 -0.1174 0.8500 0.0466
-5.000 -0.0279 0.00947 0.00361 -0.1178 0.8444 0.0756
-4.500 0.0258 0.00838 0.00297 -0.1194 0.8342 0.1939
-4.250 0.0556 0.00762 0.00258 -0.1211 0.8273 0.2931
-4.000 0.0871 0.00713 0.00232 -0.1228 0.8204 0.3615
-3.750 0.1224 0.00653 0.00203 -0.1255 0.8137 0.4511
-3.500 0.1605 0.00603 0.00183 -0.1286 0.8076 0.5403
-3.250 0.1920 0.00594 0.00177 -0.1296 0.8007 0.5661
-3.000 0.2225 0.00591 0.00173 -0.1303 0.7929 0.5813
-2.750 0.2528 0.00589 0.00172 -0.1310 0.7847 0.5946
-2.500 0.2826 0.00590 0.00171 -0.1316 0.7771 0.6070
-2.250 0.3124 0.00591 0.00170 -0.1321 0.7693 0.6160
-2.000 0.3407 0.00596 0.00170 -0.1323 0.7579 0.6218
-1.750 0.3680 0.00603 0.00170 -0.1323 0.7429 0.6268
-1.500 0.3950 0.00612 0.00170 -0.1322 0.7270 0.6307
-1.250 0.4225 0.00619 0.00174 -0.1322 0.7135 0.6356
-1.000 0.4502 0.00627 0.00177 -0.1323 0.7006 0.6409
-0.750 0.4775 0.00636 0.00179 -0.1323 0.6866 0.6450
-0.500 0.5039 0.00648 0.00185 -0.1321 0.6706 0.6483
-0.250 0.5290 0.00663 0.00193 -0.1317 0.6499 0.6522
0.000 0.5529 0.00683 0.00202 -0.1310 0.6231 0.6563
0.250 0.5769 0.00705 0.00211 -0.1303 0.5994 0.6599
0.500 0.6008 0.00727 0.00222 -0.1297 0.5730 0.6627
0.750 0.6232 0.00755 0.00237 -0.1287 0.5424 0.6655
1.000 0.6457 0.00783 0.00252 -0.1278 0.5127 0.6688
1.250 0.6678 0.00811 0.00267 -0.1268 0.4849 0.6723
1.500 0.6910 0.00835 0.00281 -0.1261 0.4622 0.6754
1.750 0.7148 0.00857 0.00294 -0.1255 0.4411 0.6778
2.000 0.7386 0.00880 0.00310 -0.1249 0.4212 0.6801
2.250 0.7629 0.00902 0.00325 -0.1243 0.4053 0.6826
2.500 0.7875 0.00924 0.00342 -0.1239 0.3895 0.6852
2.750 0.8118 0.00949 0.00359 -0.1234 0.3709 0.6879
3.000 0.8352 0.00979 0.00379 -0.1228 0.3505 0.6901
3.250 0.8588 0.01009 0.00399 -0.1222 0.3319 0.6921
3.500 0.8832 0.01033 0.00419 -0.1218 0.3167 0.6941
3.750 0.9073 0.01058 0.00440 -0.1213 0.3026 0.6964
4.000 0.9302 0.01089 0.00464 -0.1206 0.2864 0.6988
4.250 0.9526 0.01122 0.00489 -0.1198 0.2690 0.7011
4.500 0.9748 0.01157 0.00516 -0.1190 0.2505 0.7031
4.750 0.9981 0.01185 0.00540 -0.1184 0.2390 0.7049
5.000 1.0216 0.01212 0.00563 -0.1179 0.2302 0.7067
5.250 1.0439 0.01245 0.00591 -0.1171 0.2195 0.7082
5.500 1.0665 0.01275 0.00618 -0.1165 0.2071 0.7099
5.750 1.0871 0.01316 0.00652 -0.1154 0.1907 0.7116
6.000 1.1092 0.01348 0.00682 -0.1147 0.1819 0.7133
6.250 1.1307 0.01384 0.00715 -0.1138 0.1742 0.7151
6.500 1.1526 0.01417 0.00747 -0.1130 0.1655 0.7171
6.750 1.1729 0.01459 0.00785 -0.1120 0.1537 0.7191
7.000 1.1918 0.01509 0.00826 -0.1108 0.1391 0.7210
7.250 1.2113 0.01555 0.00868 -0.1097 0.1296 0.7226
7.500 1.2308 0.01602 0.00911 -0.1086 0.1201 0.7241
7.750 1.2510 0.01644 0.00952 -0.1076 0.1136 0.7257
8.000 1.2688 0.01699 0.01003 -0.1063 0.1016 0.7273
8.250 1.2854 0.01762 0.01060 -0.1048 0.0904 0.7290
8.500 1.3017 0.01827 0.01120 -0.1033 0.0789 0.7311
8.750 1.3154 0.01908 0.01192 -0.1014 0.0633 0.7332
9.000 1.3306 0.01980 0.01260 -0.0999 0.0548 0.7353
9.250 1.3466 0.02049 0.01326 -0.0984 0.0471 0.7371
9.500 1.3587 0.02142 0.01413 -0.0965 0.0358 0.7387
9.750 1.3726 0.02225 0.01492 -0.0948 0.0301 0.7403
10.000 1.3882 0.02297 0.01566 -0.0934 0.0262 0.7420
10.250 1.3980 0.02409 0.01674 -0.0913 0.0161 0.7435
10.500 1.4063 0.02531 0.01795 -0.0891 0.0089 0.7450
10.750 1.4146 0.02656 0.01922 -0.0869 0.0028 0.7466
11.000 1.4275 0.02751 0.02022 -0.0853 0.0024 0.7482
11.250 1.4411 0.02843 0.02119 -0.0840 0.0022 0.7498
11.500 1.4541 0.02939 0.02221 -0.0826 0.0021 0.7514
11.750 1.4663 0.03042 0.02329 -0.0812 0.0020 0.7529
12.000 1.4777 0.03153 0.02446 -0.0797 0.0018 0.7543
12.250 1.4881 0.03275 0.02574 -0.0782 0.0017 0.7556
12.500 1.4981 0.03403 0.02710 -0.0768 0.0016 0.7570
12.750 1.5069 0.03543 0.02857 -0.0753 0.0015 0.7586
13.000 1.5166 0.03676 0.02998 -0.0740 0.0014 0.7601
13.250 1.5257 0.03819 0.03148 -0.0728 0.0014 0.7618
13.500 1.5341 0.03972 0.03307 -0.0715 0.0014 0.7635
13.750 1.5414 0.04138 0.03481 -0.0703 0.0013 0.7652
14.000 1.5481 0.04314 0.03664 -0.0691 0.0013 0.7668
14.250 1.5537 0.04504 0.03862 -0.0680 0.0012 0.7682
14.500 1.5586 0.04704 0.04071 -0.0670 0.0012 0.7696
14.750 1.5626 0.04920 0.04294 -0.0660 0.0012 0.7709
15.250 1.5681 0.05398 0.04790 -0.0644 0.0011 0.7734
15.500 1.5695 0.05662 0.05063 -0.0638 0.0011 0.7748
15.750 1.5698 0.05943 0.05354 -0.0633 0.0011 0.7761
16.000 1.5691 0.06243 0.05663 -0.0629 0.0010 0.7775
16.250 1.5668 0.06571 0.06002 -0.0627 0.0010 0.7788
16.500 1.5640 0.06915 0.06356 -0.0627 0.0010 0.7802
16.750 1.5588 0.07299 0.06751 -0.0628 0.0010 0.7815
17.000 1.5527 0.07702 0.07164 -0.0632 0.0010 0.7828
17.250 1.5447 0.08140 0.07615 -0.0638 0.0009 0.7841
17.500 1.5363 0.08596 0.08082 -0.0646 0.0009 0.7854
17.750 1.5268 0.09077 0.08574 -0.0657 0.0009 0.7865
18.000 1.5146 0.09607 0.09116 -0.0671 0.0009 0.7875
18.250 1.5015 0.10156 0.09678 -0.0687 0.0009 0.7885
18.500 1.4870 0.10741 0.10277 -0.0706 0.0009 0.7897
18.750 1.4732 0.11323 0.10872 -0.0728 0.0009 0.7908
19.000 1.4565 0.11967 0.11530 -0.0754 0.0009 0.7918
19.250 1.4411 0.12597 0.12172 -0.0781 0.0009 0.7929
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