NASA/LANGLEY LS(1)-0417 (GA(W)-1) AIRFOIL (ls417-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: NASA/LANGLEY LS(1)-0417 (GA(W)-1) AIRFOIL (ls417-il) Reynolds number: 1,000,000 Max Cl/Cd: 91.33 at α=1° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ls417-il-1000000-n5.txt Download as CSV file: xf-ls417-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: NASA/LANGLEY LS(1)-0417 (GA(W)-1) 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
------ -------- --------- --------- -------- -------- --------
-19.750 -0.9669 0.10974 0.10656 -0.0500 1.0000 0.0119
-19.500 -0.9897 0.10175 0.09844 -0.0544 1.0000 0.0120
-19.250 -1.0101 0.09436 0.09093 -0.0585 1.0000 0.0120
-19.000 -1.0292 0.08733 0.08377 -0.0623 1.0000 0.0120
-18.750 -1.0446 0.08100 0.07732 -0.0658 1.0000 0.0120
-18.500 -1.0580 0.07513 0.07133 -0.0689 1.0000 0.0120
-18.250 -1.0686 0.06976 0.06584 -0.0718 1.0000 0.0121
-18.000 -1.0763 0.06495 0.06093 -0.0744 1.0000 0.0121
-17.750 -1.0824 0.06053 0.05640 -0.0766 1.0000 0.0121
-17.500 -1.0858 0.05661 0.05238 -0.0785 1.0000 0.0122
-17.250 -1.0875 0.05305 0.04873 -0.0801 1.0000 0.0122
-17.000 -1.0879 0.04981 0.04540 -0.0814 1.0000 0.0123
-16.750 -1.0865 0.04689 0.04240 -0.0825 1.0000 0.0123
-16.500 -1.0837 0.04426 0.03969 -0.0834 1.0000 0.0124
-16.250 -1.0798 0.04188 0.03723 -0.0840 1.0000 0.0125
-16.000 -1.0750 0.03969 0.03497 -0.0844 0.9986 0.0125
-15.750 -1.0650 0.03760 0.03279 -0.0858 0.9724 0.0126
-15.500 -1.0577 0.03577 0.03085 -0.0859 0.9500 0.0126
-15.250 -1.0510 0.03418 0.02914 -0.0854 0.9315 0.0127
-15.000 -1.0435 0.03267 0.02751 -0.0850 0.9168 0.0128
-14.750 -1.0339 0.03124 0.02598 -0.0847 0.9057 0.0128
-14.500 -1.0230 0.02994 0.02457 -0.0844 0.8963 0.0129
-14.250 -1.0111 0.02868 0.02323 -0.0842 0.8882 0.0129
-14.000 -0.9981 0.02754 0.02200 -0.0839 0.8803 0.0130
-13.750 -0.9856 0.02634 0.02072 -0.0836 0.8737 0.0131
-13.500 -0.9743 0.02505 0.01936 -0.0832 0.8666 0.0132
-13.250 -0.9611 0.02394 0.01816 -0.0828 0.8596 0.0134
-13.000 -0.9462 0.02293 0.01710 -0.0825 0.8538 0.0135
-12.750 -0.9299 0.02202 0.01614 -0.0822 0.8478 0.0136
-12.500 -0.9130 0.02120 0.01526 -0.0819 0.8421 0.0138
-12.250 -0.8954 0.02044 0.01443 -0.0816 0.8370 0.0139
-12.000 -0.8780 0.01971 0.01367 -0.0812 0.8325 0.0141
-11.750 -0.8610 0.01906 0.01298 -0.0806 0.8272 0.0142
-11.500 -0.8396 0.01844 0.01230 -0.0807 0.8223 0.0144
-11.000 -0.7930 0.01728 0.01105 -0.0815 0.8143 0.0148
-10.750 -0.7680 0.01676 0.01049 -0.0820 0.8107 0.0151
-10.500 -0.7426 0.01629 0.00998 -0.0824 0.8070 0.0153
-10.250 -0.7169 0.01586 0.00950 -0.0828 0.8033 0.0155
-10.000 -0.6908 0.01546 0.00906 -0.0832 0.7998 0.0157
-9.750 -0.6645 0.01503 0.00859 -0.0836 0.7967 0.0159
-9.500 -0.6379 0.01456 0.00811 -0.0840 0.7941 0.0163
-9.250 -0.6106 0.01417 0.00770 -0.0845 0.7913 0.0166
-9.000 -0.5829 0.01382 0.00734 -0.0851 0.7884 0.0170
-8.750 -0.5548 0.01349 0.00699 -0.0856 0.7855 0.0174
-8.500 -0.5265 0.01319 0.00666 -0.0861 0.7826 0.0178
-8.250 -0.4980 0.01291 0.00635 -0.0867 0.7796 0.0182
-8.000 -0.4691 0.01265 0.00606 -0.0873 0.7769 0.0186
-7.750 -0.4399 0.01234 0.00576 -0.0879 0.7746 0.0192
-7.500 -0.4105 0.01206 0.00548 -0.0886 0.7723 0.0200
-7.250 -0.3809 0.01180 0.00523 -0.0893 0.7699 0.0208
-7.000 -0.3511 0.01158 0.00499 -0.0900 0.7675 0.0217
-6.750 -0.3212 0.01134 0.00475 -0.0907 0.7651 0.0228
-6.500 -0.2912 0.01111 0.00452 -0.0914 0.7627 0.0244
-6.250 -0.2611 0.01090 0.00431 -0.0922 0.7603 0.0264
-5.750 -0.2000 0.01043 0.00390 -0.0939 0.7563 0.0360
-5.500 -0.1691 0.01020 0.00373 -0.0948 0.7545 0.0470
-5.250 -0.1382 0.01001 0.00357 -0.0956 0.7525 0.0531
-5.000 -0.1072 0.00983 0.00342 -0.0965 0.7502 0.0590
-4.750 -0.0761 0.00963 0.00326 -0.0974 0.7478 0.0674
-4.500 -0.0444 0.00933 0.00309 -0.0986 0.7455 0.0936
-4.250 -0.0127 0.00909 0.00294 -0.0997 0.7434 0.1172
-4.000 0.0189 0.00889 0.00281 -0.1008 0.7414 0.1370
-3.750 0.0514 0.00858 0.00266 -0.1022 0.7391 0.1781
-3.500 0.0848 0.00822 0.00250 -0.1038 0.7373 0.2323
-3.250 0.1194 0.00774 0.00234 -0.1059 0.7353 0.3137
-3.000 0.1537 0.00736 0.00221 -0.1077 0.7332 0.3782
-2.750 0.1879 0.00704 0.00209 -0.1095 0.7308 0.4378
-2.500 0.2218 0.00678 0.00200 -0.1111 0.7284 0.4926
-2.250 0.2551 0.00660 0.00196 -0.1124 0.7260 0.5372
-2.000 0.2874 0.00652 0.00198 -0.1134 0.7237 0.5758
-1.750 0.3187 0.00652 0.00200 -0.1142 0.7205 0.5962
-1.500 0.3498 0.00652 0.00201 -0.1148 0.7167 0.6074
-1.250 0.3809 0.00652 0.00203 -0.1155 0.7109 0.6193
-1.000 0.4113 0.00656 0.00204 -0.1160 0.7026 0.6296
-0.750 0.4419 0.00658 0.00206 -0.1165 0.6926 0.6370
-0.500 0.4719 0.00665 0.00205 -0.1169 0.6818 0.6405
-0.250 0.5026 0.00668 0.00206 -0.1175 0.6746 0.6428
0.000 0.5329 0.00671 0.00208 -0.1180 0.6662 0.6455
0.250 0.5632 0.00676 0.00211 -0.1185 0.6570 0.6480
0.500 0.5932 0.00683 0.00215 -0.1189 0.6468 0.6524
0.750 0.6229 0.00693 0.00221 -0.1193 0.6316 0.6575
1.000 0.6512 0.00713 0.00227 -0.1194 0.5995 0.6611
1.250 0.6759 0.00764 0.00246 -0.1189 0.5337 0.6637
1.500 0.7000 0.00819 0.00273 -0.1184 0.4697 0.6666
1.750 0.7249 0.00868 0.00299 -0.1181 0.4205 0.6686
2.000 0.7501 0.00911 0.00322 -0.1178 0.3763 0.6704
2.250 0.7749 0.00956 0.00347 -0.1174 0.3334 0.6721
2.500 0.8001 0.00996 0.00370 -0.1171 0.2994 0.6739
2.750 0.8253 0.01033 0.00393 -0.1168 0.2703 0.6754
3.000 0.8505 0.01069 0.00415 -0.1164 0.2426 0.6769
3.250 0.8757 0.01104 0.00438 -0.1161 0.2204 0.6783
3.500 0.9011 0.01135 0.00459 -0.1158 0.2028 0.6796
3.750 0.9263 0.01166 0.00482 -0.1154 0.1856 0.6808
4.000 0.9510 0.01199 0.00505 -0.1150 0.1695 0.6820
4.250 0.9759 0.01228 0.00529 -0.1146 0.1571 0.6840
4.500 1.0007 0.01256 0.00553 -0.1142 0.1470 0.6859
4.750 1.0250 0.01286 0.00579 -0.1136 0.1380 0.6876
5.000 1.0495 0.01313 0.00604 -0.1132 0.1308 0.6892
5.250 1.0734 0.01342 0.00629 -0.1126 0.1242 0.6909
5.500 1.0969 0.01371 0.00656 -0.1119 0.1177 0.6926
5.750 1.1197 0.01401 0.00684 -0.1111 0.1119 0.6944
6.000 1.1419 0.01432 0.00713 -0.1102 0.1061 0.6961
6.250 1.1633 0.01465 0.00744 -0.1092 0.1010 0.6978
6.500 1.1826 0.01499 0.00776 -0.1077 0.0962 0.6994
6.750 1.1991 0.01536 0.00811 -0.1058 0.0923 0.7009
7.000 1.2191 0.01571 0.00847 -0.1045 0.0893 0.7027
7.250 1.2384 0.01615 0.00891 -0.1032 0.0855 0.7048
7.500 1.2582 0.01658 0.00934 -0.1021 0.0822 0.7069
7.750 1.2778 0.01703 0.00979 -0.1009 0.0790 0.7091
8.000 1.2966 0.01753 0.01030 -0.0997 0.0763 0.7115
8.250 1.3163 0.01799 0.01078 -0.0986 0.0744 0.7140
8.500 1.3359 0.01847 0.01127 -0.0976 0.0726 0.7164
8.750 1.3548 0.01899 0.01181 -0.0965 0.0708 0.7186
9.250 1.3916 0.02014 0.01298 -0.0942 0.0672 0.7229
9.500 1.4104 0.02069 0.01358 -0.0932 0.0659 0.7255
9.750 1.4287 0.02129 0.01420 -0.0922 0.0643 0.7281
10.000 1.4460 0.02196 0.01488 -0.0910 0.0626 0.7308
10.250 1.4626 0.02268 0.01561 -0.0898 0.0609 0.7335
10.500 1.4807 0.02331 0.01628 -0.0888 0.0599 0.7361
10.750 1.4978 0.02402 0.01701 -0.0878 0.0586 0.7383
11.000 1.5145 0.02475 0.01778 -0.0867 0.0571 0.7409
11.250 1.5300 0.02557 0.01862 -0.0855 0.0555 0.7437
11.500 1.5457 0.02640 0.01948 -0.0844 0.0542 0.7468
11.750 1.5621 0.02717 0.02030 -0.0833 0.0531 0.7500
12.000 1.5774 0.02804 0.02120 -0.0822 0.0518 0.7531
12.250 1.5918 0.02896 0.02215 -0.0811 0.0504 0.7557
12.500 1.6055 0.02995 0.02316 -0.0798 0.0490 0.7586
12.750 1.6199 0.03090 0.02417 -0.0788 0.0479 0.7616
13.000 1.6340 0.03188 0.02520 -0.0777 0.0464 0.7648
13.250 1.6465 0.03298 0.02633 -0.0765 0.0447 0.7680
13.500 1.6583 0.03414 0.02752 -0.0753 0.0433 0.7711
14.000 1.6822 0.03651 0.02998 -0.0730 0.0402 0.7777
14.250 1.6927 0.03784 0.03134 -0.0718 0.0388 0.7815
14.500 1.7038 0.03915 0.03270 -0.0708 0.0376 0.7855
14.750 1.7137 0.04058 0.03417 -0.0697 0.0363 0.7894
15.000 1.7228 0.04207 0.03571 -0.0686 0.0350 0.7929
15.250 1.7312 0.04368 0.03738 -0.0675 0.0340 0.7968
15.500 1.7405 0.04524 0.03899 -0.0666 0.0330 0.8008
15.750 1.7479 0.04700 0.04080 -0.0656 0.0321 0.8044
16.000 1.7549 0.04882 0.04267 -0.0647 0.0312 0.8076
16.250 1.7603 0.05083 0.04474 -0.0637 0.0304 0.8108
16.500 1.7674 0.05269 0.04668 -0.0629 0.0299 0.8144
16.750 1.7731 0.05474 0.04880 -0.0622 0.0292 0.8181
17.000 1.7783 0.05688 0.05101 -0.0615 0.0286 0.8217
17.250 1.7818 0.05924 0.05343 -0.0608 0.0281 0.8249
17.500 1.7850 0.06167 0.05594 -0.0603 0.0275 0.8286
17.750 1.7857 0.06442 0.05876 -0.0598 0.0270 0.8325
18.000 1.7870 0.06713 0.06156 -0.0594 0.0266 0.8365
18.250 1.7891 0.06981 0.06433 -0.0591 0.0262 0.8405
18.500 1.7895 0.07277 0.06739 -0.0590 0.0258 0.8446
18.750 1.7890 0.07586 0.07057 -0.0589 0.0254 0.8493
19.000 1.7875 0.07914 0.07395 -0.0590 0.0251 0.8542
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