E. Bambino (ebambino7-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
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Airfoil: E. Bambino (ebambino7-il) Reynolds number: 500,000 Max Cl/Cd: 48.39 at α=6.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ebambino7-il-500000-n5.txt Download as CSV file: xf-ebambino7-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-6.750 -0.5750 0.10069 0.09877 0.0263 1.0000 0.0033
-6.500 -0.5716 0.09686 0.09496 0.0239 1.0000 0.0033
-6.250 -0.5689 0.09298 0.09110 0.0211 1.0000 0.0034
-6.000 -0.5649 0.08891 0.08699 0.0172 0.9259 0.0034
-5.750 -0.5605 0.08507 0.08302 0.0146 0.8747 0.0034
-5.500 -0.5554 0.08169 0.07906 0.0127 0.7179 0.0035
-5.250 -0.5431 0.07746 0.07461 0.0090 0.6699 0.0035
-5.000 -0.5287 0.07313 0.07012 0.0056 0.6413 0.0036
-4.750 -0.5124 0.06882 0.06564 0.0025 0.6169 0.0037
-4.500 -0.4943 0.06453 0.06119 -0.0002 0.5940 0.0038
-4.250 -0.4744 0.06033 0.05679 -0.0025 0.5661 0.0040
-4.000 -0.4527 0.05647 0.05246 -0.0046 0.4535 0.0041
-3.750 -0.4282 0.05287 0.04828 -0.0064 0.3021 0.0043
-3.500 -0.4018 0.04913 0.04426 -0.0074 0.2699 0.0045
-3.250 -0.3755 0.04578 0.04045 -0.0081 0.1577 0.0046
-3.000 -0.3501 0.04236 0.03679 -0.0083 0.1448 0.0047
-2.750 -0.3244 0.03899 0.03319 -0.0082 0.1365 0.0047
-2.500 -0.2985 0.03577 0.02970 -0.0079 0.1249 0.0047
-2.000 -0.2452 0.02982 0.02307 -0.0070 0.0608 0.0047
-1.750 -0.2201 0.02582 0.01871 -0.0067 0.0586 0.0050
-1.500 -0.1918 0.02328 0.01585 -0.0060 0.0562 0.0050
-0.500 -0.0780 0.01584 0.00727 -0.0040 0.0490 0.0054
-0.250 -0.0498 0.01472 0.00595 -0.0036 0.0485 0.0055
0.000 -0.0216 0.01386 0.00489 -0.0031 0.0475 0.0050
0.250 0.0060 0.01318 0.00411 -0.0029 0.0464 0.0049
0.500 0.0335 0.01257 0.00343 -0.0027 0.0454 0.0051
0.750 0.0614 0.01218 0.00296 -0.0026 0.0447 0.0057
1.000 0.0895 0.01202 0.00273 -0.0026 0.0442 0.0087
1.250 0.1178 0.01185 0.00240 -0.0026 0.0436 0.0145
1.500 0.1458 0.01181 0.00241 -0.0027 0.0430 0.0567
1.750 0.1736 0.01168 0.00244 -0.0029 0.0424 0.1243
2.000 0.1926 0.00962 0.00248 -0.0020 0.0419 0.8297
2.250 0.2147 0.00953 0.00257 -0.0004 0.0413 0.8961
2.500 0.2400 0.00963 0.00271 0.0003 0.0407 0.9460
2.750 0.2718 0.01014 0.00319 -0.0007 0.0393 0.9725
3.000 0.3062 0.01027 0.00326 -0.0024 0.0390 0.9886
3.250 0.3411 0.01044 0.00339 -0.0042 0.0387 1.0000
3.500 0.3676 0.01062 0.00354 -0.0041 0.0383 1.0000
3.750 0.3943 0.01083 0.00372 -0.0040 0.0378 1.0000
4.000 0.4216 0.01073 0.00360 -0.0041 0.0366 1.0000
4.250 0.4488 0.01077 0.00361 -0.0041 0.0355 1.0000
4.500 0.4765 0.01044 0.00312 -0.0043 0.0318 1.0000
4.750 0.5035 0.01070 0.00338 -0.0044 0.0126 1.0000
5.000 0.5297 0.01151 0.00441 -0.0043 0.0078 1.0000
5.250 0.5560 0.01224 0.00521 -0.0043 0.0056 1.0000
5.500 0.5828 0.01270 0.00572 -0.0042 0.0044 1.0000
5.750 0.6099 0.01298 0.00611 -0.0042 0.0040 1.0000
6.000 0.6370 0.01332 0.00657 -0.0042 0.0039 1.0000
6.250 0.6639 0.01379 0.00714 -0.0042 0.0033 1.0000
6.500 0.6905 0.01427 0.00767 -0.0042 0.0022 1.0000
6.750 0.7163 0.01511 0.00848 -0.0040 0.0020 1.0000
7.000 0.7407 0.01625 0.00956 -0.0038 0.0021 1.0000
7.250 0.7647 0.01761 0.01079 -0.0033 0.0023 1.0000
7.500 0.7901 0.01909 0.01199 -0.0028 0.0038 1.0000
7.750 0.8164 0.02052 0.01330 -0.0025 0.0038 1.0000
8.000 0.8424 0.02200 0.01482 -0.0022 0.0036 1.0000
8.250 0.8673 0.02388 0.01687 -0.0019 0.0033 1.0000
8.500 0.8909 0.02649 0.01965 -0.0016 0.0031 1.0000
8.750 0.9127 0.03161 0.02494 -0.0014 0.0029 1.0000
9.000 0.9325 0.03467 0.02834 -0.0008 0.0029 1.0000
9.250 0.9501 0.03710 0.03118 0.0001 0.0029 1.0000
9.500 0.9647 0.03963 0.03414 0.0010 0.0029 1.0000
9.750 0.9762 0.04217 0.03713 0.0021 0.0029 1.0000
10.000 0.9835 0.04458 0.04001 0.0034 0.0028 1.0000
10.250 0.9873 0.04657 0.04248 0.0047 0.0028 1.0000
10.500 0.9867 0.04875 0.04511 0.0060 0.0027 1.0000
10.750 0.9793 0.05204 0.04875 0.0069 0.0026 1.0000
11.000 0.9647 0.05547 0.05240 0.0078 0.0026 1.0000
11.250 0.9495 0.05984 0.05693 0.0063 0.0026 1.0000
11.500 0.9355 0.06547 0.06271 0.0022 0.0027 1.0000
11.750 0.9229 0.07193 0.06927 -0.0025 0.0027 1.0000
12.000 0.9115 0.07886 0.07628 -0.0075 0.0028 1.0000
12.250 0.9002 0.08655 0.08404 -0.0130 0.0028 1.0000
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Polar data table (+)
Polar graphs
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