FX 60-157 AIRFOIL (fx60157-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: FX 60-157 AIRFOIL (fx60157-il) Reynolds number: 1,000,000 Max Cl/Cd: 72.77 at α=1.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-fx60157-il-1000000-n5.txt Download as CSV file: xf-fx60157-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: FX 60-157 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
------ -------- --------- --------- -------- -------- --------
-18.250 -0.6561 0.13539 0.13317 -0.0513 0.9994 0.0040
-18.000 -0.7024 0.12041 0.11804 -0.0589 0.9992 0.0039
-17.750 -0.7356 0.10863 0.10613 -0.0652 0.9989 0.0038
-17.500 -0.7718 0.09647 0.09380 -0.0719 0.9985 0.0038
-17.250 -0.8027 0.08560 0.08276 -0.0785 0.9981 0.0038
-17.000 -0.8376 0.07438 0.07132 -0.0859 0.9974 0.0038
-16.750 -0.8451 0.06835 0.06518 -0.0903 0.9966 0.0038
-16.500 -0.8569 0.06180 0.05846 -0.0951 0.9957 0.0038
-16.250 -0.8606 0.05685 0.05339 -0.0989 0.9947 0.0038
-15.750 -0.8697 0.04793 0.04420 -0.1046 0.9921 0.0038
-15.500 -0.8691 0.04458 0.04073 -0.1065 0.9904 0.0038
-15.250 -0.8646 0.04168 0.03772 -0.1083 0.9885 0.0038
-15.000 -0.8712 0.03762 0.03347 -0.1104 0.9864 0.0039
-14.750 -0.8569 0.03594 0.03172 -0.1117 0.9851 0.0039
-14.500 -0.8516 0.03322 0.02887 -0.1134 0.9836 0.0040
-14.250 -0.8399 0.03112 0.02666 -0.1150 0.9825 0.0040
-14.000 -0.8338 0.02959 0.02506 -0.1143 0.9782 0.0041
-13.750 -0.8211 0.02813 0.02352 -0.1146 0.9753 0.0041
-13.500 -0.8064 0.02666 0.02197 -0.1153 0.9732 0.0042
-13.250 -0.7889 0.02535 0.02057 -0.1162 0.9714 0.0042
-13.000 -0.7687 0.02417 0.01933 -0.1173 0.9700 0.0044
-12.750 -0.7542 0.02312 0.01821 -0.1171 0.9661 0.0044
-12.500 -0.7370 0.02215 0.01717 -0.1172 0.9625 0.0044
-12.250 -0.7150 0.02122 0.01618 -0.1181 0.9601 0.0046
-12.000 -0.6905 0.02031 0.01521 -0.1194 0.9583 0.0047
-11.750 -0.6632 0.01948 0.01433 -0.1211 0.9567 0.0048
-11.500 -0.6337 0.01866 0.01344 -0.1232 0.9555 0.0049
-11.250 -0.6133 0.01802 0.01276 -0.1232 0.9508 0.0051
-11.000 -0.5870 0.01729 0.01196 -0.1245 0.9475 0.0052
-10.750 -0.5585 0.01665 0.01127 -0.1260 0.9446 0.0053
-10.500 -0.5288 0.01603 0.01059 -0.1277 0.9421 0.0055
-10.250 -0.5045 0.01541 0.00992 -0.1283 0.9383 0.0057
-10.000 -0.4850 0.01491 0.00937 -0.1278 0.9331 0.0058
-9.750 -0.4613 0.01441 0.00882 -0.1281 0.9291 0.0060
-9.500 -0.4370 0.01385 0.00821 -0.1285 0.9256 0.0064
-9.250 -0.4215 0.01344 0.00778 -0.1270 0.9208 0.0066
-9.000 -0.4053 0.01303 0.00733 -0.1256 0.9157 0.0068
-8.750 -0.3864 0.01264 0.00690 -0.1247 0.9114 0.0073
-8.500 -0.3683 0.01228 0.00652 -0.1236 0.9070 0.0082
-8.250 -0.3504 0.01196 0.00621 -0.1224 0.9022 0.0091
-8.000 -0.3278 0.01167 0.00592 -0.1220 0.8982 0.0123
-7.750 -0.3022 0.01146 0.00568 -0.1221 0.8949 0.0145
-7.500 -0.2780 0.01126 0.00545 -0.1218 0.8918 0.0152
-7.250 -0.2573 0.01100 0.00519 -0.1209 0.8879 0.0162
-7.000 -0.2338 0.01078 0.00495 -0.1204 0.8841 0.0172
-6.750 -0.2086 0.01057 0.00472 -0.1203 0.8809 0.0180
-6.500 -0.1820 0.01037 0.00448 -0.1205 0.8779 0.0185
-6.250 -0.1580 0.01018 0.00427 -0.1201 0.8744 0.0191
-6.000 -0.1340 0.00996 0.00405 -0.1196 0.8701 0.0199
-5.750 -0.1082 0.00976 0.00383 -0.1195 0.8657 0.0205
-5.250 -0.0564 0.00940 0.00344 -0.1193 0.8562 0.0223
-5.000 -0.0302 0.00924 0.00327 -0.1193 0.8513 0.0235
-4.750 -0.0030 0.00907 0.00310 -0.1194 0.8467 0.0259
-4.500 0.0232 0.00888 0.00295 -0.1194 0.8421 0.0365
-4.250 0.0497 0.00876 0.00282 -0.1193 0.8364 0.0396
-4.000 0.0770 0.00863 0.00267 -0.1194 0.8304 0.0435
-3.750 0.1037 0.00845 0.00254 -0.1195 0.8250 0.0527
-3.500 0.1306 0.00831 0.00242 -0.1195 0.8180 0.0666
-3.250 0.1576 0.00819 0.00230 -0.1196 0.8103 0.0760
-3.000 0.1846 0.00802 0.00218 -0.1197 0.8025 0.0992
-2.750 0.2120 0.00779 0.00204 -0.1200 0.7949 0.1374
-2.500 0.2397 0.00749 0.00189 -0.1204 0.7859 0.1929
-2.250 0.2678 0.00718 0.00175 -0.1210 0.7758 0.2544
-2.000 0.2968 0.00675 0.00159 -0.1219 0.7623 0.3518
-1.750 0.3235 0.00666 0.00151 -0.1219 0.7434 0.3825
-1.500 0.3492 0.00648 0.00141 -0.1220 0.7140 0.4490
-1.250 0.3753 0.00630 0.00136 -0.1222 0.6754 0.5351
-1.000 0.3999 0.00635 0.00142 -0.1218 0.6393 0.5887
-0.750 0.4223 0.00657 0.00152 -0.1208 0.6031 0.6117
-0.500 0.4469 0.00675 0.00161 -0.1202 0.5759 0.6230
-0.250 0.4700 0.00699 0.00171 -0.1194 0.5441 0.6309
0.000 0.4939 0.00722 0.00182 -0.1187 0.5151 0.6398
0.250 0.5175 0.00746 0.00194 -0.1180 0.4857 0.6465
0.500 0.5415 0.00769 0.00207 -0.1174 0.4585 0.6527
0.750 0.5642 0.00800 0.00221 -0.1165 0.4232 0.6599
1.000 0.5871 0.00830 0.00238 -0.1157 0.3905 0.6665
1.250 0.6095 0.00863 0.00255 -0.1147 0.3556 0.6719
1.500 0.6340 0.00886 0.00267 -0.1142 0.3374 0.6766
1.750 0.6586 0.00905 0.00281 -0.1137 0.3198 0.6802
2.000 0.6798 0.00939 0.00300 -0.1126 0.2869 0.6830
2.250 0.7015 0.00969 0.00317 -0.1116 0.2581 0.6851
2.500 0.7217 0.01007 0.00338 -0.1103 0.2264 0.6873
2.750 0.7444 0.01032 0.00354 -0.1095 0.2073 0.6896
3.000 0.7651 0.01070 0.00377 -0.1083 0.1789 0.6917
3.250 0.7874 0.01100 0.00397 -0.1074 0.1609 0.6932
3.500 0.8083 0.01137 0.00421 -0.1063 0.1354 0.6949
3.750 0.8311 0.01164 0.00443 -0.1055 0.1226 0.6970
4.000 0.8544 0.01188 0.00465 -0.1048 0.1129 0.6991
4.250 0.8747 0.01230 0.00496 -0.1036 0.0907 0.7013
4.500 0.8969 0.01260 0.00522 -0.1028 0.0815 0.7032
5.000 0.9389 0.01335 0.00582 -0.1007 0.0533 0.7064
5.250 0.9616 0.01363 0.00607 -0.1000 0.0489 0.7078
5.500 0.9830 0.01398 0.00639 -0.0991 0.0361 0.7091
6.000 1.0255 0.01467 0.00703 -0.0972 0.0271 0.7118
6.250 1.0471 0.01498 0.00736 -0.0963 0.0249 0.7132
6.500 1.0691 0.01528 0.00767 -0.0955 0.0232 0.7146
6.750 1.0892 0.01569 0.00806 -0.0944 0.0156 0.7161
7.000 1.1094 0.01608 0.00845 -0.0933 0.0138 0.7177
7.250 1.1302 0.01644 0.00882 -0.0924 0.0132 0.7194
7.500 1.1510 0.01680 0.00921 -0.0915 0.0130 0.7213
7.750 1.1711 0.01720 0.00962 -0.0904 0.0127 0.7231
8.000 1.1909 0.01761 0.01006 -0.0894 0.0125 0.7247
8.250 1.2105 0.01804 0.01051 -0.0883 0.0123 0.7262
8.500 1.2297 0.01850 0.01100 -0.0873 0.0121 0.7277
8.750 1.2481 0.01900 0.01154 -0.0861 0.0118 0.7292
9.000 1.2662 0.01953 0.01210 -0.0849 0.0115 0.7306
9.250 1.2839 0.02009 0.01270 -0.0836 0.0112 0.7321
9.500 1.3010 0.02067 0.01333 -0.0823 0.0110 0.7339
9.750 1.3178 0.02130 0.01400 -0.0810 0.0108 0.7358
10.000 1.3351 0.02188 0.01462 -0.0799 0.0107 0.7375
10.250 1.3518 0.02250 0.01528 -0.0786 0.0106 0.7392
10.500 1.3683 0.02316 0.01598 -0.0774 0.0104 0.7408
10.750 1.3841 0.02386 0.01672 -0.0761 0.0102 0.7422
11.000 1.3994 0.02460 0.01750 -0.0749 0.0100 0.7434
11.250 1.4144 0.02537 0.01833 -0.0736 0.0098 0.7450
11.500 1.4286 0.02621 0.01923 -0.0723 0.0096 0.7467
11.750 1.4427 0.02707 0.02015 -0.0710 0.0094 0.7484
12.000 1.4556 0.02802 0.02115 -0.0696 0.0093 0.7501
12.250 1.4683 0.02901 0.02219 -0.0683 0.0091 0.7518
12.500 1.4796 0.03012 0.02336 -0.0669 0.0089 0.7534
12.750 1.4902 0.03131 0.02461 -0.0655 0.0087 0.7549
13.000 1.4989 0.03267 0.02604 -0.0640 0.0085 0.7564
13.250 1.5098 0.03388 0.02731 -0.0629 0.0083 0.7578
13.500 1.5226 0.03497 0.02844 -0.0619 0.0082 0.7591
13.750 1.5347 0.03613 0.02966 -0.0610 0.0080 0.7608
14.000 1.5468 0.03732 0.03092 -0.0601 0.0077 0.7625
14.250 1.5572 0.03869 0.03236 -0.0592 0.0074 0.7642
14.500 1.5674 0.04010 0.03383 -0.0584 0.0070 0.7659
14.750 1.5771 0.04160 0.03539 -0.0576 0.0066 0.7677
15.000 1.5855 0.04327 0.03712 -0.0568 0.0062 0.7695
15.250 1.5930 0.04508 0.03900 -0.0561 0.0058 0.7713
15.500 1.6011 0.04687 0.04084 -0.0555 0.0034 0.7731
15.750 1.6014 0.04953 0.04349 -0.0548 0.0023 0.7748
16.000 1.6017 0.05233 0.04638 -0.0543 0.0021 0.7765
16.250 1.6014 0.05532 0.04947 -0.0540 0.0020 0.7785
16.500 1.6006 0.05847 0.05274 -0.0539 0.0019 0.7804
16.750 1.5991 0.06185 0.05623 -0.0540 0.0018 0.7822
17.000 1.5969 0.06541 0.05990 -0.0544 0.0017 0.7840
17.500 1.5903 0.07329 0.06800 -0.0559 0.0016 0.7875
17.750 1.5856 0.07762 0.07245 -0.0570 0.0016 0.7891
18.000 1.5799 0.08224 0.07719 -0.0584 0.0015 0.7906
18.500 1.5641 0.09259 0.08779 -0.0622 0.0015 0.7938
18.750 1.5541 0.09831 0.09365 -0.0645 0.0015 0.7954
19.000 1.5433 0.10427 0.09975 -0.0672 0.0015 0.7970
19.250 1.5316 0.11051 0.10613 -0.0702 0.0015 0.7985
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