FX 60-157 AIRFOIL (fx60157-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: FX 60-157 AIRFOIL (fx60157-il) Reynolds number: 1,000,000 Max Cl/Cd: 95.78 at α=0.75° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-fx60157-il-1000000.txt Download as CSV file: xf-fx60157-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-17.000 -0.7637 0.09858 0.09629 -0.0635 1.0000 0.0062
-16.750 -0.7952 0.08911 0.08668 -0.0679 1.0000 0.0062
-16.500 -0.8305 0.07964 0.07705 -0.0723 1.0000 0.0062
-16.250 -0.8517 0.07125 0.06847 -0.0780 0.9996 0.0061
-16.000 -0.8711 0.06312 0.06011 -0.0839 0.9988 0.0061
-15.750 -0.8732 0.05811 0.05497 -0.0880 0.9978 0.0061
-15.500 -0.8743 0.05345 0.05018 -0.0919 0.9966 0.0062
-15.250 -0.8772 0.04872 0.04525 -0.0956 0.9954 0.0061
-15.000 -0.8749 0.04492 0.04132 -0.0987 0.9943 0.0062
-14.750 -0.8673 0.04202 0.03829 -0.1012 0.9934 0.0062
-14.500 -0.8638 0.03938 0.03555 -0.1022 0.9910 0.0063
-14.250 -0.8603 0.03651 0.03252 -0.1036 0.9888 0.0063
-14.000 -0.8469 0.03463 0.03055 -0.1051 0.9871 0.0065
-13.750 -0.8343 0.03255 0.02835 -0.1067 0.9856 0.0065
-13.500 -0.8191 0.03068 0.02636 -0.1083 0.9844 0.0066
-13.250 -0.8025 0.02891 0.02447 -0.1099 0.9834 0.0066
-13.000 -0.7820 0.02752 0.02300 -0.1116 0.9826 0.0068
-12.750 -0.7747 0.02612 0.02151 -0.1105 0.9781 0.0068
-12.500 -0.7582 0.02481 0.02010 -0.1111 0.9755 0.0068
-12.250 -0.7372 0.02365 0.01887 -0.1121 0.9738 0.0070
-12.000 -0.7150 0.02246 0.01758 -0.1134 0.9724 0.0071
-11.750 -0.6904 0.02143 0.01648 -0.1149 0.9714 0.0072
-11.500 -0.6652 0.02036 0.01533 -0.1164 0.9705 0.0072
-11.250 -0.6383 0.01942 0.01433 -0.1181 0.9696 0.0073
-11.000 -0.6285 0.01868 0.01353 -0.1161 0.9637 0.0074
-10.750 -0.6057 0.01774 0.01252 -0.1168 0.9613 0.0076
-10.500 -0.5798 0.01676 0.01148 -0.1182 0.9597 0.0081
-10.250 -0.5497 0.01603 0.01073 -0.1201 0.9585 0.0087
-10.000 -0.5189 0.01539 0.01006 -0.1220 0.9573 0.0091
-9.750 -0.4876 0.01479 0.00942 -0.1238 0.9560 0.0094
-9.500 -0.4746 0.01435 0.00897 -0.1219 0.9505 0.0103
-9.250 -0.4512 0.01391 0.00853 -0.1219 0.9470 0.0111
-9.000 -0.4244 0.01348 0.00807 -0.1226 0.9444 0.0124
-8.750 -0.3945 0.01316 0.00775 -0.1237 0.9422 0.0144
-8.500 -0.3713 0.01283 0.00739 -0.1236 0.9385 0.0160
-8.250 -0.3546 0.01249 0.00703 -0.1222 0.9334 0.0170
-8.000 -0.3280 0.01221 0.00672 -0.1225 0.9302 0.0185
-7.750 -0.3023 0.01177 0.00624 -0.1229 0.9273 0.0203
-7.500 -0.2742 0.01145 0.00589 -0.1236 0.9245 0.0214
-7.250 -0.2571 0.01123 0.00564 -0.1219 0.9201 0.0224
-7.000 -0.2335 0.01094 0.00533 -0.1216 0.9166 0.0239
-6.750 -0.2070 0.01066 0.00506 -0.1217 0.9137 0.0252
-6.500 -0.1784 0.01041 0.00479 -0.1224 0.9110 0.0264
-6.250 -0.1524 0.01021 0.00458 -0.1224 0.9077 0.0281
-6.000 -0.1299 0.01001 0.00440 -0.1216 0.9035 0.0301
-5.750 -0.1031 0.00981 0.00419 -0.1216 0.8998 0.0323
-5.500 -0.0748 0.00957 0.00394 -0.1221 0.8962 0.0364
-5.250 -0.0455 0.00939 0.00374 -0.1227 0.8925 0.0411
-5.000 -0.0225 0.00919 0.00355 -0.1220 0.8882 0.0462
-4.750 0.0037 0.00893 0.00336 -0.1220 0.8842 0.0610
-4.500 0.0318 0.00866 0.00315 -0.1224 0.8805 0.0793
-4.250 0.0608 0.00832 0.00293 -0.1231 0.8765 0.1177
-4.000 0.0848 0.00786 0.00270 -0.1230 0.8716 0.1797
-3.750 0.1124 0.00734 0.00244 -0.1237 0.8673 0.2591
-3.500 0.1437 0.00675 0.00218 -0.1252 0.8630 0.3598
-3.250 0.1726 0.00648 0.00202 -0.1258 0.8579 0.3964
-3.000 0.2027 0.00607 0.00184 -0.1268 0.8528 0.4688
-2.750 0.2354 0.00570 0.00170 -0.1284 0.8481 0.5455
-2.500 0.2658 0.00557 0.00166 -0.1291 0.8428 0.5835
-2.250 0.2944 0.00551 0.00165 -0.1293 0.8362 0.6113
-2.000 0.3245 0.00551 0.00162 -0.1298 0.8292 0.6293
-1.750 0.3516 0.00550 0.00163 -0.1296 0.8198 0.6402
-1.500 0.3795 0.00552 0.00162 -0.1296 0.8091 0.6496
-1.250 0.4074 0.00559 0.00162 -0.1296 0.7980 0.6600
-1.000 0.4347 0.00564 0.00168 -0.1295 0.7881 0.6675
-0.750 0.4627 0.00572 0.00170 -0.1295 0.7794 0.6728
-0.500 0.4905 0.00578 0.00171 -0.1295 0.7689 0.6766
-0.250 0.5172 0.00583 0.00175 -0.1293 0.7565 0.6806
0.000 0.5434 0.00593 0.00181 -0.1289 0.7422 0.6846
0.250 0.5688 0.00606 0.00186 -0.1284 0.7251 0.6888
0.500 0.5928 0.00624 0.00193 -0.1276 0.7018 0.6930
0.750 0.6149 0.00642 0.00202 -0.1264 0.6738 0.6974
1.000 0.6359 0.00667 0.00215 -0.1250 0.6425 0.7010
1.250 0.6570 0.00693 0.00228 -0.1236 0.6122 0.7040
1.500 0.6787 0.00719 0.00241 -0.1224 0.5846 0.7070
1.750 0.6995 0.00751 0.00256 -0.1211 0.5502 0.7096
2.000 0.7184 0.00785 0.00273 -0.1194 0.5083 0.7121
2.250 0.7376 0.00820 0.00291 -0.1178 0.4717 0.7141
2.500 0.7582 0.00851 0.00308 -0.1165 0.4380 0.7158
2.750 0.7779 0.00883 0.00326 -0.1150 0.4072 0.7179
3.000 0.7965 0.00920 0.00346 -0.1134 0.3692 0.7200
3.250 0.8162 0.00955 0.00366 -0.1119 0.3391 0.7221
3.500 0.8374 0.00986 0.00385 -0.1108 0.3118 0.7238
3.750 0.8580 0.01021 0.00406 -0.1096 0.2869 0.7254
4.000 0.8800 0.01051 0.00427 -0.1087 0.2658 0.7270
4.250 0.8998 0.01088 0.00451 -0.1074 0.2377 0.7292
4.500 0.9212 0.01119 0.00475 -0.1064 0.2198 0.7312
4.750 0.9406 0.01162 0.00505 -0.1050 0.1917 0.7329
5.000 0.9614 0.01197 0.00531 -0.1039 0.1759 0.7346
5.250 0.9824 0.01231 0.00559 -0.1029 0.1590 0.7362
5.500 1.0011 0.01280 0.00593 -0.1015 0.1339 0.7378
5.750 1.0229 0.01312 0.00621 -0.1006 0.1231 0.7394
6.000 1.0417 0.01361 0.00658 -0.0993 0.1012 0.7409
6.250 1.0619 0.01402 0.00692 -0.0982 0.0896 0.7422
6.750 1.1028 0.01477 0.00759 -0.0961 0.0673 0.7452
7.000 1.1209 0.01528 0.00803 -0.0947 0.0560 0.7468
7.250 1.1407 0.01568 0.00843 -0.0936 0.0511 0.7483
7.500 1.1619 0.01600 0.00877 -0.0927 0.0485 0.7499
7.750 1.1794 0.01656 0.00928 -0.0913 0.0348 0.7516
8.000 1.1981 0.01704 0.00974 -0.0900 0.0317 0.7535
8.250 1.2174 0.01749 0.01020 -0.0889 0.0286 0.7553
8.500 1.2367 0.01794 0.01067 -0.0878 0.0263 0.7570
8.750 1.2551 0.01846 0.01121 -0.0866 0.0239 0.7584
9.000 1.2739 0.01893 0.01170 -0.0855 0.0201 0.7600
9.250 1.2909 0.01952 0.01229 -0.0842 0.0174 0.7621
9.500 1.3084 0.02007 0.01286 -0.0829 0.0163 0.7638
9.750 1.3254 0.02066 0.01349 -0.0816 0.0158 0.7656
10.000 1.3421 0.02129 0.01415 -0.0803 0.0153 0.7674
10.250 1.3579 0.02196 0.01486 -0.0789 0.0149 0.7692
10.500 1.3735 0.02268 0.01561 -0.0776 0.0145 0.7711
10.750 1.3886 0.02344 0.01642 -0.0762 0.0140 0.7727
11.000 1.4029 0.02426 0.01729 -0.0747 0.0137 0.7742
11.250 1.4169 0.02512 0.01820 -0.0733 0.0134 0.7754
11.500 1.4312 0.02594 0.01908 -0.0720 0.0133 0.7774
11.750 1.4451 0.02682 0.02002 -0.0707 0.0132 0.7793
12.000 1.4578 0.02777 0.02105 -0.0693 0.0130 0.7811
12.250 1.4701 0.02879 0.02214 -0.0679 0.0129 0.7830
12.500 1.4811 0.02991 0.02333 -0.0665 0.0127 0.7849
12.750 1.4920 0.03108 0.02457 -0.0651 0.0125 0.7868
13.000 1.5014 0.03239 0.02594 -0.0637 0.0122 0.7886
13.250 1.5098 0.03381 0.02744 -0.0623 0.0120 0.7903
13.500 1.5169 0.03539 0.02908 -0.0609 0.0117 0.7917
13.750 1.5221 0.03717 0.03095 -0.0595 0.0114 0.7939
14.000 1.5238 0.03933 0.03321 -0.0580 0.0111 0.7959
14.250 1.5233 0.04179 0.03579 -0.0565 0.0109 0.7978
14.500 1.5324 0.04340 0.03747 -0.0558 0.0107 0.7998
14.750 1.5428 0.04493 0.03907 -0.0552 0.0105 0.8019
15.000 1.5513 0.04670 0.04092 -0.0547 0.0103 0.8040
15.250 1.5578 0.04874 0.04304 -0.0542 0.0100 0.8060
15.500 1.5643 0.05082 0.04519 -0.0538 0.0097 0.8078
15.750 1.5701 0.05305 0.04750 -0.0535 0.0094 0.8103
16.000 1.5740 0.05557 0.05011 -0.0534 0.0091 0.8127
16.250 1.5747 0.05856 0.05319 -0.0533 0.0088 0.8151
16.500 1.5707 0.06228 0.05702 -0.0535 0.0086 0.8174
16.750 1.5658 0.06627 0.06112 -0.0540 0.0084 0.8197
17.000 1.5808 0.06762 0.06253 -0.0543 0.0081 0.8224
17.250 1.5931 0.06937 0.06434 -0.0547 0.0077 0.8252
17.500 1.5998 0.07192 0.06697 -0.0553 0.0072 0.8280
17.750 1.6046 0.07481 0.06994 -0.0561 0.0068 0.8309
18.000 1.6080 0.07795 0.07314 -0.0570 0.0063 0.8338
18.250 1.6062 0.08195 0.07726 -0.0582 0.0059 0.8366
18.500 1.6023 0.08638 0.08181 -0.0597 0.0050 0.8391
18.750 1.6030 0.09010 0.08549 -0.0611 0.0033 0.8423
19.000 1.5921 0.09586 0.09137 -0.0634 0.0031 0.8449
19.250 1.5817 0.10167 0.09731 -0.0660 0.0031 0.8475
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