E. Bambino (ebambino7-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: E. Bambino (ebambino7-il) Reynolds number: 1,000,000 Max Cl/Cd: 58.41 at α=6° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ebambino7-il-1000000-n5.txt Download as CSV file: xf-ebambino7-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-6.500 -0.5808 0.09903 0.09559 0.0268 0.2841 0.0020
-6.250 -0.5782 0.09516 0.09170 0.0240 0.2692 0.0021
-6.000 -0.5756 0.09130 0.08766 0.0200 0.1775 0.0021
-5.750 -0.5673 0.08690 0.08321 0.0156 0.1605 0.0021
-5.500 -0.5569 0.08251 0.07878 0.0117 0.1541 0.0021
-5.250 -0.5444 0.07808 0.07431 0.0080 0.1485 0.0021
-5.000 -0.5298 0.07364 0.06980 0.0046 0.1439 0.0022
-4.750 -0.5131 0.06923 0.06532 0.0016 0.1404 0.0023
-4.500 -0.4944 0.06487 0.06086 -0.0010 0.1344 0.0023
-4.000 -0.4513 0.05646 0.05211 -0.0052 0.0797 0.0024
-1.500 -0.1841 0.00692 0.00089 -0.0065 0.0473 0.0025
-1.250 -0.1673 0.01966 0.01290 -0.0052 0.0455 0.0019
-1.000 -0.1378 0.01699 0.00990 -0.0043 0.0443 0.0017
-0.750 -0.1086 0.01495 0.00754 -0.0036 0.0433 0.0016
-0.500 -0.0798 0.01352 0.00587 -0.0030 0.0425 0.0019
-0.250 -0.0514 0.01257 0.00474 -0.0026 0.0420 0.0023
0.000 -0.0237 0.01217 0.00426 -0.0026 0.0414 0.0035
0.250 0.0042 0.01144 0.00342 -0.0023 0.0408 0.0033
0.500 0.0322 0.01094 0.00284 -0.0022 0.0402 0.0033
0.750 0.0604 0.01067 0.00249 -0.0022 0.0396 0.0034
1.000 0.0888 0.01055 0.00229 -0.0022 0.0393 0.0044
1.250 0.1170 0.01046 0.00214 -0.0023 0.0392 0.0078
1.500 0.1453 0.01037 0.00201 -0.0025 0.0391 0.0329
1.750 0.1735 0.01037 0.00202 -0.0026 0.0389 0.0511
2.000 0.2017 0.01040 0.00203 -0.0028 0.0387 0.0569
2.250 0.2299 0.01044 0.00204 -0.0030 0.0385 0.0629
2.500 0.2580 0.01036 0.00208 -0.0033 0.0382 0.1243
2.750 0.2819 0.00859 0.00214 -0.0036 0.0378 0.8030
3.500 0.3582 0.00841 0.00234 -0.0019 0.0361 0.9292
3.750 0.3838 0.00837 0.00230 -0.0014 0.0350 0.9651
4.000 0.4155 0.00841 0.00232 -0.0024 0.0339 0.9847
4.250 0.4493 0.00849 0.00232 -0.0040 0.0313 1.0000
4.500 0.4768 0.00870 0.00249 -0.0042 0.0128 1.0000
4.750 0.5044 0.00897 0.00283 -0.0043 0.0072 1.0000
5.000 0.5320 0.00930 0.00323 -0.0044 0.0046 1.0000
5.250 0.5592 0.00977 0.00381 -0.0045 0.0029 1.0000
5.500 0.5858 0.01045 0.00458 -0.0046 0.0025 1.0000
5.750 0.6136 0.01065 0.00487 -0.0047 0.0024 1.0000
6.000 0.6408 0.01097 0.00523 -0.0048 0.0017 1.0000
6.250 0.6679 0.01149 0.00580 -0.0048 0.0011 1.0000
6.500 0.6943 0.01230 0.00665 -0.0047 0.0009 1.0000
6.750 0.7200 0.01330 0.00766 -0.0046 0.0009 1.0000
7.000 0.7448 0.01447 0.00875 -0.0043 0.0010 1.0000
7.250 0.7696 0.01581 0.00996 -0.0039 0.0012 1.0000
7.500 0.7927 0.01900 0.01300 -0.0035 0.0015 1.0000
7.750 0.8195 0.02087 0.01479 -0.0034 0.0015 1.0000
8.000 0.8457 0.02269 0.01667 -0.0032 0.0015 1.0000
8.250 0.8709 0.02458 0.01871 -0.0029 0.0015 1.0000
8.500 0.8948 0.02656 0.02090 -0.0024 0.0015 1.0000
8.750 0.9170 0.02870 0.02331 -0.0019 0.0015 1.0000
9.000 0.9372 0.03095 0.02588 -0.0012 0.0015 1.0000
9.250 0.9551 0.03332 0.02859 -0.0004 0.0015 1.0000
9.500 0.9705 0.03580 0.03143 0.0006 0.0015 1.0000
9.750 0.9833 0.03832 0.03431 0.0016 0.0015 1.0000
10.000 0.9952 0.04046 0.03678 0.0028 0.0014 1.0000
10.250 1.0011 0.04262 0.03937 0.0041 0.0014 1.0000
10.500 0.9995 0.04580 0.04294 0.0053 0.0013 1.0000
10.750 0.9918 0.04946 0.04691 0.0062 0.0013 1.0000
11.000 0.9767 0.05295 0.05060 0.0074 0.0013 1.0000
11.250 0.9606 0.05729 0.05510 0.0059 0.0013 1.0000
11.500 0.9458 0.06317 0.06112 0.0011 0.0014 1.0000
11.750 0.9327 0.07005 0.06810 -0.0046 0.0014 1.0000
12.000 0.9206 0.07761 0.07574 -0.0104 0.0014 1.0000
12.250 0.9093 0.08620 0.08440 -0.0170 0.0015 1.0000
12.500 0.8972 0.09474 0.09299 -0.0227 0.0015 1.0000
12.750 0.8848 0.10353 0.10184 -0.0281 0.0015 1.0000
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Polar data table (+)
Polar graphs
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