E. Bambino (ebambino7-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
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Airfoil: E. Bambino (ebambino7-il) Reynolds number: 100,000 Max Cl/Cd: 33.02 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ebambino7-il-100000-n5.txt Download as CSV file: xf-ebambino7-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: E. Bambino
1 1 Reynolds number fixed Mach number fixed
xtrf = 1.000 (top) 1.000 (bottom)
Mach = 0.000 Re = 0.100 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-7.250 -0.5692 0.11202 0.10770 0.0181 1.0000 0.0258
-7.000 -0.5665 0.10851 0.10423 0.0143 1.0000 0.0259
-6.750 -0.5639 0.10485 0.10062 0.0099 1.0000 0.0260
-6.500 -0.5553 0.09920 0.09500 0.0165 1.0000 0.0286
-6.250 -0.5519 0.09552 0.09136 0.0141 1.0000 0.0301
-6.000 -0.5467 0.09164 0.08750 0.0104 1.0000 0.0315
-5.750 -0.5374 0.08772 0.08357 0.0053 1.0000 0.0334
-5.500 -0.5228 0.08409 0.07985 -0.0016 1.0000 0.0344
-5.250 -0.5062 0.08065 0.07624 -0.0065 1.0000 0.0347
-5.000 -0.5033 0.07482 0.07060 -0.0041 1.0000 0.0363
-4.750 -0.4909 0.07099 0.06674 -0.0050 1.0000 0.0390
-4.500 -0.4678 0.06776 0.06331 -0.0090 1.0000 0.0431
-4.000 -0.4342 0.05896 0.05429 -0.0121 1.0000 0.0464
-3.750 -0.4177 0.05514 0.05043 -0.0125 1.0000 0.0493
-3.500 -0.3952 0.05177 0.04686 -0.0136 1.0000 0.0538
-3.250 -0.3671 0.04885 0.04346 -0.0150 1.0000 0.0583
-3.000 -0.3497 0.04454 0.03922 -0.0150 1.0000 0.0612
-2.750 -0.3254 0.04126 0.03574 -0.0153 1.0000 0.0629
-2.250 -0.2661 0.03401 0.02771 -0.0142 1.0000 0.0323
-2.000 -0.2376 0.03065 0.02393 -0.0134 1.0000 0.0241
-1.750 -0.2109 0.02785 0.02083 -0.0127 1.0000 0.0213
-1.500 -0.1770 0.02499 0.01747 -0.0127 0.9812 0.0185
-1.250 -0.1378 0.02290 0.01490 -0.0135 0.9482 0.0168
-1.000 -0.1045 0.02082 0.01243 -0.0137 0.9142 0.0169
-0.750 -0.0756 0.01887 0.01019 -0.0130 0.8732 0.0183
-0.500 -0.0527 0.01767 0.00856 -0.0105 0.7802 0.0192
-0.250 -0.0340 0.01693 0.00716 -0.0072 0.6762 0.0195
0.000 -0.0112 0.01632 0.00596 -0.0055 0.5859 0.0204
0.250 0.0115 0.01665 0.00498 -0.0044 0.3177 0.0228
0.500 0.0379 0.01668 0.00444 -0.0041 0.1845 0.0325
1.000 0.1209 0.01385 0.00388 -0.0084 0.1478 1.0000
1.250 0.1460 0.01394 0.00367 -0.0079 0.1413 1.0000
1.500 0.1711 0.01402 0.00353 -0.0074 0.1226 1.0000
1.750 0.1960 0.01433 0.00344 -0.0070 0.0780 1.0000
2.000 0.2212 0.01452 0.00343 -0.0066 0.0742 1.0000
2.250 0.2466 0.01472 0.00347 -0.0062 0.0726 1.0000
2.500 0.2721 0.01494 0.00359 -0.0058 0.0713 1.0000
2.750 0.2976 0.01520 0.00377 -0.0055 0.0699 1.0000
3.000 0.3231 0.01555 0.00408 -0.0052 0.0673 1.0000
3.250 0.3484 0.01600 0.00449 -0.0049 0.0640 1.0000
3.500 0.3738 0.01642 0.00490 -0.0047 0.0615 1.0000
3.750 0.3994 0.01679 0.00528 -0.0045 0.0601 1.0000
4.000 0.4250 0.01718 0.00575 -0.0042 0.0595 1.0000
4.250 0.4506 0.01761 0.00623 -0.0040 0.0590 1.0000
4.500 0.4761 0.01807 0.00676 -0.0038 0.0585 1.0000
4.750 0.5015 0.01855 0.00731 -0.0036 0.0582 1.0000
5.000 0.5251 0.01946 0.00827 -0.0036 0.0510 1.0000
5.250 0.5516 0.01943 0.00830 -0.0037 0.0434 1.0000
5.500 0.5778 0.01950 0.00834 -0.0038 0.0393 1.0000
5.750 0.6055 0.01913 0.00809 -0.0038 0.0356 1.0000
6.000 0.6313 0.01961 0.00875 -0.0035 0.0166 1.0000
6.250 0.6571 0.02013 0.00940 -0.0033 0.0154 1.0000
6.500 0.6829 0.02068 0.01009 -0.0030 0.0148 1.0000
6.750 0.7080 0.02148 0.01107 -0.0027 0.0137 1.0000
7.000 0.7328 0.02239 0.01220 -0.0023 0.0125 1.0000
7.250 0.7576 0.02329 0.01331 -0.0019 0.0123 1.0000
7.500 0.7819 0.02438 0.01457 -0.0015 0.0123 1.0000
7.750 0.8051 0.02569 0.01607 -0.0011 0.0125 1.0000
8.000 0.8254 0.02753 0.01811 -0.0005 0.0130 1.0000
8.250 0.8493 0.02845 0.01917 0.0000 0.0137 1.0000
8.500 0.8746 0.02906 0.02004 0.0006 0.0146 1.0000
8.750 0.9003 0.02969 0.02099 0.0013 0.0160 1.0000
9.000 0.9230 0.03113 0.02288 0.0022 0.0171 1.0000
9.250 0.9428 0.03326 0.02542 0.0032 0.0177 1.0000
9.500 0.9601 0.03599 0.02860 0.0043 0.0183 1.0000
9.750 0.9742 0.03931 0.03239 0.0054 0.0188 1.0000
10.000 0.9838 0.04324 0.03679 0.0065 0.0194 1.0000
11.500 0.9399 0.07118 0.06668 0.0026 0.0210 1.0000
11.750 0.9208 0.07955 0.07517 -0.0049 0.0207 1.0000
12.000 0.8999 0.09089 0.08655 -0.0141 0.0204 1.0000
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Polar data table (+)
Polar graphs
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