FX 60-177 AIRFOIL (fx60177-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 60-177 AIRFOIL (fx60177-il) Reynolds number: 500,000 Max Cl/Cd: 74.64 at α=1.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx60177-il-500000-n5.txt Download as CSV file: xf-fx60177-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -0.6213 0.14955 0.14665 -0.0480 1.0001 0.0041
-18.500 -0.6540 0.13796 0.13490 -0.0527 1.0001 0.0040
-18.250 -0.6779 0.12901 0.12582 -0.0564 1.0001 0.0040
-18.000 -0.7039 0.11999 0.11668 -0.0601 1.0001 0.0040
-17.750 -0.7282 0.11167 0.10823 -0.0636 1.0001 0.0040
-17.500 -0.7492 0.10361 0.10004 -0.0675 1.0000 0.0039
-17.250 -0.7654 0.09572 0.09200 -0.0722 0.9995 0.0039
-17.000 -0.7790 0.08857 0.08470 -0.0765 0.9989 0.0039
-16.750 -0.7899 0.08205 0.07803 -0.0806 0.9982 0.0039
-16.500 -0.7983 0.07612 0.07195 -0.0844 0.9974 0.0039
-16.250 -0.8039 0.07079 0.06647 -0.0880 0.9965 0.0039
-16.000 -0.8071 0.06593 0.06146 -0.0912 0.9956 0.0039
-15.750 -0.8083 0.06154 0.05694 -0.0941 0.9947 0.0039
-15.500 -0.8072 0.05765 0.05291 -0.0967 0.9938 0.0039
-15.250 -0.8060 0.05411 0.04925 -0.0986 0.9920 0.0039
-15.000 -0.8024 0.05092 0.04594 -0.1003 0.9902 0.0039
-14.750 -0.7972 0.04800 0.04290 -0.1019 0.9886 0.0039
-14.500 -0.7898 0.04531 0.04009 -0.1036 0.9870 0.0039
-14.250 -0.7803 0.04283 0.03750 -0.1052 0.9857 0.0039
-14.000 -0.7691 0.04055 0.03511 -0.1069 0.9846 0.0039
-13.750 -0.7563 0.03847 0.03292 -0.1084 0.9837 0.0040
-13.500 -0.7496 0.03673 0.03110 -0.1080 0.9797 0.0040
-13.250 -0.7375 0.03501 0.02929 -0.1087 0.9772 0.0040
-13.000 -0.7230 0.03339 0.02758 -0.1096 0.9753 0.0040
-12.500 -0.6886 0.03033 0.02435 -0.1120 0.9725 0.0040
-12.250 -0.6689 0.02892 0.02286 -0.1134 0.9716 0.0041
-12.000 -0.6601 0.02785 0.02173 -0.1120 0.9662 0.0041
-11.750 -0.6416 0.02669 0.02050 -0.1126 0.9638 0.0041
-11.500 -0.6211 0.02559 0.01934 -0.1134 0.9620 0.0042
-11.250 -0.5993 0.02457 0.01826 -0.1144 0.9603 0.0043
-11.000 -0.5761 0.02360 0.01722 -0.1154 0.9589 0.0043
-10.750 -0.5616 0.02286 0.01643 -0.1145 0.9543 0.0044
-10.500 -0.5432 0.02208 0.01560 -0.1142 0.9507 0.0045
-10.250 -0.5213 0.02132 0.01479 -0.1146 0.9482 0.0046
-10.000 -0.4978 0.02056 0.01399 -0.1153 0.9460 0.0047
-9.750 -0.4726 0.01984 0.01321 -0.1162 0.9442 0.0048
-9.500 -0.4605 0.01935 0.01268 -0.1143 0.9383 0.0050
-9.250 -0.4402 0.01876 0.01206 -0.1140 0.9348 0.0051
-9.000 -0.4173 0.01816 0.01142 -0.1142 0.9320 0.0054
-8.750 -0.3921 0.01755 0.01078 -0.1149 0.9298 0.0059
-8.500 -0.3801 0.01714 0.01036 -0.1128 0.9238 0.0066
-8.250 -0.3608 0.01664 0.00984 -0.1121 0.9196 0.0082
-8.000 -0.3372 0.01613 0.00931 -0.1122 0.9165 0.0106
-7.750 -0.3181 0.01571 0.00887 -0.1113 0.9125 0.0128
-7.500 -0.3038 0.01535 0.00851 -0.1095 0.9075 0.0152
-7.250 -0.2816 0.01492 0.00806 -0.1093 0.9041 0.0185
-7.000 -0.2553 0.01443 0.00760 -0.1100 0.9016 0.0244
-6.750 -0.2345 0.01403 0.00723 -0.1095 0.8977 0.0327
-6.500 -0.2156 0.01371 0.00693 -0.1085 0.8930 0.0388
-6.250 -0.1910 0.01335 0.00657 -0.1087 0.8896 0.0464
-6.000 -0.1629 0.01292 0.00617 -0.1096 0.8868 0.0586
-5.750 -0.1398 0.01241 0.00579 -0.1097 0.8827 0.0849
-5.500 -0.1209 0.01182 0.00539 -0.1091 0.8771 0.1287
-5.250 -0.0956 0.01099 0.00488 -0.1101 0.8732 0.2025
-5.000 -0.0638 0.00977 0.00420 -0.1132 0.8704 0.3307
-4.750 -0.0344 0.00889 0.00377 -0.1152 0.8663 0.4366
-4.500 -0.0008 0.00839 0.00352 -0.1173 0.8622 0.5043
-4.250 0.0341 0.00813 0.00338 -0.1192 0.8584 0.5451
-4.000 0.0702 0.00798 0.00328 -0.1211 0.8552 0.5768
-3.750 0.0975 0.00795 0.00328 -0.1212 0.8497 0.5941
-3.500 0.1281 0.00791 0.00323 -0.1218 0.8443 0.6074
-3.250 0.1620 0.00788 0.00315 -0.1232 0.8399 0.6189
-3.000 0.1901 0.00789 0.00313 -0.1234 0.8336 0.6291
-2.750 0.2201 0.00788 0.00311 -0.1238 0.8278 0.6354
-2.500 0.2512 0.00788 0.00306 -0.1246 0.8225 0.6408
-2.250 0.2804 0.00788 0.00302 -0.1250 0.8161 0.6461
-2.000 0.3108 0.00789 0.00300 -0.1256 0.8097 0.6502
-1.750 0.3387 0.00792 0.00301 -0.1257 0.8014 0.6550
-1.250 0.3973 0.00796 0.00296 -0.1264 0.7843 0.6636
-1.000 0.4260 0.00800 0.00297 -0.1266 0.7753 0.6668
-0.750 0.4541 0.00805 0.00296 -0.1268 0.7633 0.6704
-0.500 0.4824 0.00811 0.00295 -0.1270 0.7508 0.6747
-0.250 0.5103 0.00817 0.00296 -0.1271 0.7391 0.6780
0.000 0.5371 0.00825 0.00302 -0.1269 0.7277 0.6806
0.250 0.5638 0.00834 0.00307 -0.1267 0.7150 0.6835
0.500 0.5902 0.00845 0.00312 -0.1265 0.7000 0.6867
0.750 0.6163 0.00857 0.00316 -0.1263 0.6829 0.6902
1.000 0.6410 0.00873 0.00321 -0.1258 0.6619 0.6932
1.250 0.6623 0.00893 0.00334 -0.1245 0.6369 0.6954
1.500 0.6837 0.00916 0.00347 -0.1232 0.6129 0.6977
1.750 0.7036 0.00943 0.00362 -0.1217 0.5876 0.7002
2.000 0.7213 0.00974 0.00378 -0.1198 0.5555 0.7028
2.250 0.7402 0.01006 0.00396 -0.1182 0.5275 0.7054
2.500 0.7612 0.01036 0.00414 -0.1171 0.5024 0.7079
2.750 0.7817 0.01067 0.00436 -0.1159 0.4798 0.7097
3.000 0.8032 0.01097 0.00460 -0.1148 0.4605 0.7117
3.250 0.8253 0.01128 0.00484 -0.1139 0.4401 0.7139
3.500 0.8470 0.01161 0.00510 -0.1130 0.4198 0.7162
3.750 0.8690 0.01195 0.00536 -0.1121 0.4010 0.7185
4.000 0.8910 0.01230 0.00563 -0.1113 0.3804 0.7207
4.250 0.9127 0.01269 0.00591 -0.1105 0.3593 0.7228
4.500 0.9347 0.01305 0.00620 -0.1098 0.3426 0.7246
4.750 0.9561 0.01339 0.00650 -0.1088 0.3286 0.7261
5.000 0.9777 0.01373 0.00682 -0.1080 0.3139 0.7276
5.250 0.9982 0.01413 0.00716 -0.1069 0.2957 0.7293
5.500 1.0183 0.01457 0.00752 -0.1059 0.2785 0.7311
5.750 1.0390 0.01498 0.00789 -0.1049 0.2633 0.7332
6.000 1.0602 0.01539 0.00825 -0.1041 0.2505 0.7354
6.250 1.0820 0.01577 0.00861 -0.1034 0.2401 0.7375
6.500 1.1033 0.01619 0.00899 -0.1026 0.2299 0.7394
6.750 1.1228 0.01665 0.00943 -0.1016 0.2192 0.7409
7.000 1.1431 0.01707 0.00984 -0.1006 0.2071 0.7423
7.250 1.1626 0.01754 0.01030 -0.0996 0.1954 0.7439
7.500 1.1812 0.01805 0.01079 -0.0984 0.1849 0.7457
7.750 1.1990 0.01863 0.01132 -0.0972 0.1747 0.7477
8.000 1.2184 0.01914 0.01183 -0.0962 0.1642 0.7498
8.250 1.2368 0.01971 0.01237 -0.0951 0.1538 0.7520
8.500 1.2541 0.02035 0.01297 -0.0939 0.1418 0.7540
8.750 1.2712 0.02104 0.01360 -0.0927 0.1318 0.7558
9.000 1.2887 0.02162 0.01421 -0.0916 0.1242 0.7572
9.250 1.3044 0.02233 0.01491 -0.0902 0.1163 0.7588
9.500 1.3214 0.02296 0.01557 -0.0890 0.1080 0.7605
9.750 1.3356 0.02379 0.01637 -0.0874 0.0979 0.7622
10.000 1.3496 0.02466 0.01720 -0.0860 0.0892 0.7639
10.250 1.3631 0.02556 0.01809 -0.0845 0.0792 0.7656
10.500 1.3753 0.02657 0.01906 -0.0829 0.0680 0.7674
10.750 1.3860 0.02770 0.02014 -0.0812 0.0590 0.7691
11.000 1.3977 0.02880 0.02122 -0.0797 0.0514 0.7708
11.250 1.4080 0.02999 0.02240 -0.0781 0.0442 0.7723
11.500 1.4166 0.03128 0.02368 -0.0764 0.0361 0.7737
11.750 1.4253 0.03259 0.02501 -0.0747 0.0317 0.7751
12.000 1.4347 0.03389 0.02634 -0.0732 0.0275 0.7766
12.250 1.4427 0.03534 0.02781 -0.0716 0.0231 0.7784
12.500 1.4452 0.03727 0.02972 -0.0697 0.0140 0.7801
12.750 1.4480 0.03924 0.03172 -0.0679 0.0094 0.7820
13.000 1.4469 0.04164 0.03416 -0.0660 0.0037 0.7837
13.250 1.4520 0.04357 0.03617 -0.0648 0.0032 0.7853
13.500 1.4579 0.04549 0.03818 -0.0637 0.0029 0.7869
13.750 1.4632 0.04750 0.04029 -0.0627 0.0028 0.7883
14.000 1.4674 0.04964 0.04254 -0.0618 0.0027 0.7896
14.250 1.4698 0.05204 0.04505 -0.0609 0.0025 0.7910
14.500 1.4716 0.05458 0.04772 -0.0601 0.0024 0.7924
14.750 1.4718 0.05736 0.05062 -0.0595 0.0023 0.7938
15.000 1.4718 0.06025 0.05363 -0.0590 0.0022 0.7953
15.250 1.4722 0.06319 0.05669 -0.0587 0.0022 0.7968
15.500 1.4717 0.06632 0.05994 -0.0586 0.0021 0.7984
15.750 1.4699 0.06970 0.06345 -0.0587 0.0021 0.8000
16.000 1.4669 0.07335 0.06721 -0.0590 0.0020 0.8016
16.250 1.4626 0.07723 0.07121 -0.0595 0.0020 0.8031
16.500 1.4573 0.08131 0.07543 -0.0601 0.0019 0.8044
16.750 1.4499 0.08577 0.08004 -0.0610 0.0019 0.8055
17.000 1.4417 0.09045 0.08486 -0.0620 0.0018 0.8067
17.250 1.4322 0.09543 0.08998 -0.0634 0.0018 0.8079
17.500 1.4223 0.10052 0.09521 -0.0649 0.0018 0.8092
17.750 1.4119 0.10579 0.10062 -0.0667 0.0018 0.8104
18.000 1.3999 0.11142 0.10640 -0.0688 0.0018 0.8118
18.250 1.3876 0.11723 0.11234 -0.0711 0.0018 0.8130
18.500 1.3745 0.12325 0.11850 -0.0738 0.0017 0.8143
18.750 1.3626 0.12912 0.12450 -0.0765 0.0017 0.8155
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