lrn1007 (lrn1007-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: lrn1007 (lrn1007-il) Reynolds number: 500,000 Max Cl/Cd: 150.75 at α=4° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-lrn1007-il-500000-n5.txt Download as CSV file: xf-lrn1007-il-500000-n5.csv |
XFOIL Version 6.96
Calculated polar for: lrn1007
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
------ -------- --------- --------- -------- -------- --------
-7.500 -0.0997 0.08477 0.08149 -0.0713 0.7874 0.0015
-7.250 -0.0913 0.08235 0.07909 -0.0726 0.7868 0.0015
-7.000 -0.0838 0.08009 0.07685 -0.0738 0.7862 0.0015
-6.750 -0.0730 0.07756 0.07433 -0.0759 0.7856 0.0015
-6.500 -0.0601 0.07492 0.07169 -0.0785 0.7850 0.0015
-6.250 -0.0454 0.07219 0.06896 -0.0814 0.7842 0.0015
-5.750 -0.0113 0.06661 0.06332 -0.0880 0.7822 0.0015
-1.250 0.4910 0.02127 0.01636 -0.1330 0.7659 0.0023
-1.000 0.5200 0.01983 0.01478 -0.1334 0.7641 0.0031
-0.750 0.5501 0.01889 0.01369 -0.1332 0.7623 0.0045
-0.500 0.5812 0.01896 0.01360 -0.1325 0.7606 0.0052
-0.250 0.6097 0.01637 0.01080 -0.1331 0.7589 0.0060
0.250 0.6678 0.01421 0.00835 -0.1327 0.7543 0.0045
0.500 0.6960 0.01321 0.00724 -0.1326 0.7514 0.0084
1.500 0.8086 0.01025 0.00401 -0.1317 0.7405 0.0162
1.750 0.8362 0.00971 0.00343 -0.1314 0.7369 0.0067
2.250 0.8923 0.00899 0.00247 -0.1313 0.7298 0.0048
2.500 0.9199 0.00729 0.00261 -0.1320 0.7245 1.0000
2.750 0.9472 0.00727 0.00257 -0.1321 0.7194 1.0000
3.000 0.9744 0.00726 0.00256 -0.1322 0.7138 1.0000
3.250 1.0014 0.00725 0.00256 -0.1323 0.7051 1.0000
3.500 1.0282 0.00723 0.00257 -0.1324 0.6925 1.0000
3.750 1.0548 0.00714 0.00242 -0.1323 0.6715 1.0000
4.000 1.0794 0.00716 0.00225 -0.1318 0.6431 1.0000
4.250 1.1029 0.00741 0.00234 -0.1313 0.6128 1.0000
4.500 1.1241 0.00786 0.00257 -0.1304 0.5683 1.0000
4.750 1.1347 0.00912 0.00323 -0.1278 0.4649 1.0000
5.000 1.1156 0.01263 0.00499 -0.1210 0.1863 1.0000
5.250 1.1084 0.01524 0.00656 -0.1160 0.0019 1.0000
5.500 1.1300 0.01562 0.00703 -0.1151 0.0013 1.0000
5.750 1.1500 0.01613 0.00767 -0.1139 0.0013 1.0000
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Polar data table (+)
Polar graphs
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