NASA/LANGLEY LS(1)-0417 (GA(W)-1) AIRFOIL (ls417-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| 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: 112.62 at α=2.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ls417-il-1000000.txt Download as CSV file: xf-ls417-il-1000000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-18.750 -0.8636 0.10904 0.10626 -0.0535 1.0000 0.0155
-18.500 -0.8958 0.09877 0.09580 -0.0596 1.0000 0.0154
-18.250 -0.9195 0.09040 0.08726 -0.0647 1.0000 0.0154
-18.000 -0.9380 0.08321 0.07992 -0.0690 1.0000 0.0155
-17.750 -0.9517 0.07700 0.07358 -0.0728 1.0000 0.0155
-17.500 -0.9625 0.07147 0.06791 -0.0760 1.0000 0.0155
-17.250 -0.9709 0.06650 0.06281 -0.0789 1.0000 0.0156
-17.000 -0.9767 0.06211 0.05830 -0.0814 1.0000 0.0156
-16.750 -0.9808 0.05816 0.05423 -0.0834 1.0000 0.0157
-16.500 -0.9832 0.05463 0.05059 -0.0851 1.0000 0.0157
-16.250 -0.9842 0.05145 0.04730 -0.0865 1.0000 0.0158
-16.000 -0.9842 0.04856 0.04432 -0.0875 1.0000 0.0158
-15.750 -0.9887 0.04535 0.04097 -0.0880 1.0000 0.0159
-15.500 -0.9910 0.04246 0.03796 -0.0880 1.0000 0.0160
-15.250 -0.9895 0.04005 0.03547 -0.0880 1.0000 0.0161
-15.000 -0.9850 0.03798 0.03333 -0.0880 1.0000 0.0162
-14.750 -0.9792 0.03611 0.03142 -0.0879 1.0000 0.0163
-14.500 -0.9690 0.03441 0.02966 -0.0883 0.9951 0.0164
-14.250 -0.9523 0.03270 0.02789 -0.0898 0.9818 0.0165
-14.000 -0.9383 0.03123 0.02635 -0.0903 0.9655 0.0167
-13.750 -0.9288 0.02994 0.02498 -0.0896 0.9480 0.0168
-13.500 -0.9189 0.02876 0.02370 -0.0887 0.9337 0.0169
-13.250 -0.9072 0.02762 0.02247 -0.0880 0.9219 0.0170
-13.000 -0.8944 0.02654 0.02130 -0.0874 0.9122 0.0172
-12.750 -0.8806 0.02552 0.02019 -0.0869 0.9031 0.0173
-12.500 -0.8660 0.02453 0.01912 -0.0864 0.8955 0.0175
-12.250 -0.8503 0.02358 0.01810 -0.0860 0.8885 0.0177
-12.000 -0.8346 0.02268 0.01711 -0.0855 0.8814 0.0178
-11.750 -0.8178 0.02183 0.01619 -0.0850 0.8752 0.0180
-11.500 -0.8005 0.02101 0.01532 -0.0846 0.8692 0.0182
-11.250 -0.7843 0.02028 0.01451 -0.0839 0.8632 0.0184
-11.000 -0.7665 0.01964 0.01379 -0.0834 0.8574 0.0186
-10.750 -0.7445 0.01900 0.01311 -0.0836 0.8535 0.0187
-10.500 -0.7247 0.01804 0.01210 -0.0838 0.8490 0.0190
-10.250 -0.7037 0.01711 0.01112 -0.0841 0.8444 0.0194
-10.000 -0.6798 0.01650 0.01046 -0.0845 0.8400 0.0197
-9.750 -0.6545 0.01602 0.00995 -0.0849 0.8362 0.0201
-9.500 -0.6284 0.01556 0.00947 -0.0853 0.8332 0.0206
-9.250 -0.6020 0.01511 0.00900 -0.0857 0.8298 0.0210
-9.000 -0.5752 0.01469 0.00854 -0.0861 0.8264 0.0214
-8.750 -0.5480 0.01431 0.00811 -0.0865 0.8230 0.0218
-8.500 -0.5207 0.01391 0.00766 -0.0870 0.8192 0.0222
-8.250 -0.4935 0.01334 0.00707 -0.0877 0.8160 0.0229
-8.000 -0.4651 0.01295 0.00668 -0.0883 0.8134 0.0236
-7.750 -0.4362 0.01261 0.00633 -0.0889 0.8106 0.0244
-7.500 -0.4071 0.01231 0.00601 -0.0896 0.8078 0.0252
-7.250 -0.3779 0.01194 0.00562 -0.0903 0.8051 0.0263
-7.000 -0.3484 0.01162 0.00529 -0.0910 0.8023 0.0277
-6.750 -0.3185 0.01139 0.00502 -0.0917 0.7991 0.0293
-6.500 -0.2884 0.01107 0.00473 -0.0926 0.7966 0.0325
-6.250 -0.2580 0.01074 0.00447 -0.0935 0.7946 0.0401
-6.000 -0.2273 0.01044 0.00425 -0.0944 0.7924 0.0539
-5.750 -0.1964 0.01016 0.00402 -0.0954 0.7901 0.0650
-5.500 -0.1653 0.00985 0.00381 -0.0964 0.7877 0.0814
-5.250 -0.1339 0.00952 0.00360 -0.0976 0.7852 0.1097
-5.000 -0.1023 0.00924 0.00342 -0.0987 0.7827 0.1338
-4.750 -0.0700 0.00889 0.00323 -0.1002 0.7800 0.1749
-4.500 -0.0366 0.00845 0.00304 -0.1020 0.7774 0.2379
-4.250 -0.0025 0.00797 0.00285 -0.1040 0.7759 0.3092
-4.000 0.0316 0.00759 0.00269 -0.1058 0.7741 0.3698
-3.750 0.0665 0.00716 0.00252 -0.1078 0.7719 0.4425
-3.500 0.1025 0.00669 0.00240 -0.1101 0.7697 0.5372
-3.250 0.1353 0.00658 0.00243 -0.1112 0.7674 0.5900
-3.000 0.1668 0.00659 0.00246 -0.1120 0.7651 0.6097
-2.750 0.1980 0.00664 0.00248 -0.1126 0.7628 0.6218
-2.500 0.2291 0.00669 0.00251 -0.1133 0.7600 0.6294
-2.250 0.2601 0.00676 0.00257 -0.1139 0.7574 0.6356
-2.000 0.2914 0.00679 0.00258 -0.1146 0.7557 0.6420
-1.750 0.3222 0.00678 0.00260 -0.1152 0.7530 0.6485
-1.500 0.3529 0.00680 0.00262 -0.1157 0.7493 0.6537
-1.250 0.3836 0.00683 0.00262 -0.1162 0.7447 0.6597
-1.000 0.4139 0.00692 0.00265 -0.1166 0.7384 0.6661
-0.750 0.4441 0.00688 0.00266 -0.1169 0.7325 0.6711
-0.500 0.4745 0.00688 0.00264 -0.1174 0.7263 0.6740
-0.250 0.5049 0.00692 0.00264 -0.1179 0.7215 0.6766
0.000 0.5356 0.00695 0.00266 -0.1184 0.7171 0.6789
0.250 0.5664 0.00695 0.00267 -0.1190 0.7123 0.6808
0.500 0.5969 0.00696 0.00267 -0.1196 0.7076 0.6839
0.750 0.6267 0.00700 0.00269 -0.1199 0.7014 0.6881
1.000 0.6568 0.00702 0.00274 -0.1203 0.6941 0.6914
1.250 0.6866 0.00706 0.00276 -0.1206 0.6852 0.6940
1.500 0.7167 0.00710 0.00280 -0.1211 0.6771 0.6964
1.750 0.7467 0.00715 0.00283 -0.1215 0.6668 0.6985
2.000 0.7766 0.00722 0.00286 -0.1219 0.6553 0.7002
2.250 0.8058 0.00732 0.00290 -0.1222 0.6392 0.7014
2.500 0.8345 0.00741 0.00293 -0.1224 0.6166 0.7035
2.750 0.8603 0.00770 0.00304 -0.1221 0.5718 0.7055
3.000 0.8828 0.00829 0.00332 -0.1213 0.5057 0.7073
3.250 0.9047 0.00894 0.00367 -0.1204 0.4440 0.7090
3.500 0.9274 0.00950 0.00399 -0.1196 0.3932 0.7105
3.750 0.9496 0.01006 0.00431 -0.1188 0.3460 0.7122
4.000 0.9723 0.01057 0.00463 -0.1180 0.3062 0.7138
4.250 0.9949 0.01106 0.00494 -0.1173 0.2716 0.7155
4.500 1.0177 0.01151 0.00523 -0.1165 0.2417 0.7171
4.750 1.0402 0.01196 0.00555 -0.1157 0.2173 0.7188
5.000 1.0634 0.01235 0.00583 -0.1150 0.1976 0.7202
5.250 1.0859 0.01272 0.00612 -0.1143 0.1790 0.7223
5.500 1.1080 0.01310 0.00643 -0.1134 0.1638 0.7242
5.750 1.1298 0.01348 0.00675 -0.1124 0.1520 0.7260
6.000 1.1514 0.01384 0.00707 -0.1114 0.1426 0.7279
6.250 1.1728 0.01418 0.00739 -0.1104 0.1343 0.7298
6.500 1.1923 0.01460 0.00776 -0.1090 0.1256 0.7318
6.750 1.2103 0.01494 0.00808 -0.1073 0.1193 0.7339
7.000 1.2259 0.01536 0.00848 -0.1052 0.1129 0.7359
7.250 1.2446 0.01581 0.00890 -0.1038 0.1069 0.7377
7.500 1.2635 0.01628 0.00935 -0.1025 0.1013 0.7397
7.750 1.2825 0.01674 0.00981 -0.1012 0.0969 0.7422
8.000 1.3004 0.01728 0.01035 -0.0999 0.0927 0.7445
8.250 1.3203 0.01773 0.01082 -0.0988 0.0901 0.7469
8.500 1.3386 0.01828 0.01137 -0.0976 0.0873 0.7495
8.750 1.3553 0.01893 0.01202 -0.0961 0.0842 0.7521
9.000 1.3746 0.01944 0.01256 -0.0951 0.0825 0.7546
9.250 1.3935 0.01999 0.01313 -0.0941 0.0805 0.7569
9.500 1.4111 0.02062 0.01378 -0.0929 0.0785 0.7600
9.750 1.4270 0.02136 0.01454 -0.0915 0.0763 0.7628
10.000 1.4444 0.02202 0.01524 -0.0904 0.0747 0.7656
10.250 1.4628 0.02262 0.01589 -0.0894 0.0733 0.7685
10.500 1.4801 0.02331 0.01660 -0.0883 0.0718 0.7713
10.750 1.4961 0.02410 0.01740 -0.0872 0.0701 0.7741
11.000 1.5100 0.02502 0.01834 -0.0857 0.0682 0.7774
11.250 1.5270 0.02574 0.01912 -0.0847 0.0670 0.7806
11.500 1.5439 0.02647 0.01991 -0.0837 0.0658 0.7840
11.750 1.5599 0.02728 0.02075 -0.0827 0.0643 0.7875
12.000 1.5742 0.02823 0.02170 -0.0815 0.0629 0.7907
12.250 1.5863 0.02932 0.02282 -0.0801 0.0612 0.7944
12.500 1.6016 0.03018 0.02375 -0.0790 0.0601 0.7980
12.750 1.6169 0.03106 0.02469 -0.0780 0.0589 0.8017
13.000 1.6312 0.03203 0.02569 -0.0770 0.0573 0.8053
13.250 1.6431 0.03319 0.02686 -0.0758 0.0558 0.8087
13.500 1.6544 0.03439 0.02811 -0.0745 0.0543 0.8125
13.750 1.6689 0.03535 0.02914 -0.0736 0.0530 0.8163
14.000 1.6811 0.03653 0.03037 -0.0725 0.0514 0.8202
14.250 1.6919 0.03784 0.03169 -0.0714 0.0499 0.8238
14.500 1.7018 0.03926 0.03316 -0.0702 0.0484 0.8278
14.750 1.7140 0.04049 0.03446 -0.0693 0.0470 0.8321
15.000 1.7244 0.04187 0.03589 -0.0683 0.0455 0.8366
15.250 1.7316 0.04359 0.03764 -0.0671 0.0440 0.8409
15.500 1.7414 0.04509 0.03921 -0.0662 0.0428 0.8455
15.750 1.7500 0.04672 0.04091 -0.0653 0.0415 0.8504
16.000 1.7574 0.04851 0.04274 -0.0644 0.0402 0.8554
16.250 1.7614 0.05066 0.04493 -0.0634 0.0390 0.8601
16.500 1.7685 0.05249 0.04686 -0.0625 0.0381 0.8655
16.750 1.7744 0.05452 0.04896 -0.0618 0.0372 0.8713
17.000 1.7791 0.05669 0.05120 -0.0610 0.0362 0.8770
17.250 1.7810 0.05919 0.05377 -0.0603 0.0354 0.8836
17.750 1.7833 0.06450 0.05925 -0.0591 0.0339 0.8989
18.000 1.7852 0.06707 0.06194 -0.0587 0.0334 0.9091
18.250 1.7855 0.06974 0.06473 -0.0581 0.0327 0.9270
18.500 1.7807 0.07266 0.06777 -0.0572 0.0322 1.0000
18.750 1.7779 0.07614 0.07132 -0.0573 0.0317 1.0000
19.000 1.7724 0.08001 0.07526 -0.0576 0.0312 1.0000
19.250 1.7632 0.08443 0.07977 -0.0581 0.0307 1.0000
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