E. Bambino (ebambino7-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: E. Bambino (ebambino7-il) Reynolds number: 500,000 Max Cl/Cd: 53.63 at α=7.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ebambino7-il-500000.txt Download as CSV file: xf-ebambino7-il-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-7.000 -0.5952 0.10481 0.10287 0.0289 1.0000 0.0058
-6.750 -0.5920 0.10070 0.09878 0.0261 1.0000 0.0058
-6.500 -0.5897 0.09648 0.09458 0.0225 1.0000 0.0058
-6.250 -0.5848 0.09209 0.09019 0.0186 1.0000 0.0058
-6.000 -0.5765 0.08758 0.08566 0.0151 1.0000 0.0058
-5.750 -0.5665 0.08303 0.08105 0.0119 1.0000 0.0058
-5.500 -0.5548 0.07848 0.07645 0.0090 1.0000 0.0058
-5.250 -0.5416 0.07393 0.07185 0.0065 1.0000 0.0058
-5.000 -0.5363 0.06631 0.06416 0.0036 1.0000 0.0061
-4.750 -0.5242 0.06094 0.05869 0.0017 1.0000 0.0063
-4.500 -0.5092 0.05665 0.05431 0.0005 1.0000 0.0066
-4.250 -0.4919 0.05285 0.05042 -0.0005 1.0000 0.0069
-4.000 -0.4728 0.04925 0.04672 -0.0013 1.0000 0.0073
-3.750 -0.4483 0.04550 0.04281 -0.0027 0.9588 0.0079
-3.500 -0.4335 0.04267 0.03969 -0.0008 0.8809 0.0086
-3.250 -0.4180 0.04027 0.03655 0.0015 0.7211 0.0096
-3.000 -0.3900 0.03813 0.03389 0.0021 0.6422 0.0121
-2.750 -0.3604 0.03693 0.03227 0.0029 0.5811 0.0130
-2.500 -0.3343 0.03513 0.02941 0.0028 0.3157 0.0131
-2.250 -0.3141 0.02867 0.02238 0.0031 0.2807 0.0146
-2.000 -0.2888 0.02673 0.01987 0.0030 0.1512 0.0156
-1.750 -0.2622 0.02481 0.01764 0.0032 0.1345 0.0168
-1.500 -0.2347 0.02301 0.01555 0.0037 0.1225 0.0185
-1.250 -0.2062 0.02146 0.01359 0.0041 0.0709 0.0209
0.000 -0.0630 0.01388 0.00501 0.0072 0.0560 0.0154
0.500 -0.0074 0.01277 0.00375 0.0079 0.0545 0.0129
0.750 0.0205 0.01217 0.00301 0.0082 0.0542 0.0147
1.000 0.0489 0.01199 0.00274 0.0083 0.0541 0.0224
1.250 0.0772 0.01197 0.00272 0.0083 0.0542 0.0450
1.500 0.1054 0.01200 0.00279 0.0083 0.0545 0.0729
1.750 0.1163 0.00943 0.00290 0.0114 0.0548 0.8942
2.000 0.1557 0.00963 0.00317 0.0097 0.0554 0.9874
2.250 0.1960 0.00997 0.00343 0.0070 0.0563 0.9947
2.500 0.2388 0.01037 0.00376 0.0036 0.0574 0.9993
2.750 0.2653 0.01072 0.00406 0.0037 0.0584 1.0000
3.000 0.2889 0.01115 0.00444 0.0044 0.0606 1.0000
3.250 0.3131 0.01121 0.00445 0.0051 0.0616 1.0000
3.500 0.3372 0.01184 0.00504 0.0056 0.0608 1.0000
4.000 0.3854 0.01289 0.00595 0.0061 0.0471 1.0000
4.250 0.4118 0.01257 0.00563 0.0063 0.0447 1.0000
4.500 0.4382 0.01246 0.00554 0.0063 0.0421 1.0000
4.750 0.4644 0.01250 0.00549 0.0061 0.0375 1.0000
5.000 0.4939 0.01068 0.00343 0.0060 0.0340 1.0000
5.250 0.5208 0.01078 0.00329 0.0060 0.0181 1.0000
5.500 0.5478 0.01093 0.00347 0.0059 0.0170 1.0000
5.750 0.5750 0.01112 0.00366 0.0059 0.0167 1.0000
6.000 0.6013 0.01192 0.00473 0.0059 0.0145 1.0000
6.250 0.6274 0.01275 0.00569 0.0060 0.0130 1.0000
6.500 0.6545 0.01308 0.00606 0.0060 0.0131 1.0000
6.750 0.6819 0.01326 0.00630 0.0061 0.0143 1.0000
7.000 0.7095 0.01341 0.00646 0.0061 0.0158 1.0000
7.500 0.7637 0.01424 0.00763 0.0062 0.0152 1.0000
7.750 0.7884 0.01554 0.00905 0.0064 0.0126 1.0000
8.000 0.8082 0.01806 0.01140 0.0068 0.0110 1.0000
8.250 0.8286 0.02234 0.01539 0.0074 0.0098 1.0000
8.500 0.8535 0.02417 0.01736 0.0078 0.0098 1.0000
8.750 0.8773 0.02601 0.01943 0.0082 0.0098 1.0000
9.000 0.8996 0.02778 0.02151 0.0087 0.0097 1.0000
9.250 0.9207 0.02847 0.02263 0.0093 0.0094 1.0000
9.500 0.9439 0.02822 0.02276 0.0098 0.0081 1.0000
9.750 0.9630 0.03000 0.02487 0.0104 0.0074 1.0000
10.000 0.9790 0.03234 0.02759 0.0111 0.0068 1.0000
10.250 0.9917 0.03507 0.03065 0.0119 0.0065 1.0000
10.500 1.0006 0.03812 0.03402 0.0126 0.0062 1.0000
10.750 1.0054 0.04141 0.03761 0.0134 0.0059 1.0000
11.000 1.0054 0.04489 0.04136 0.0140 0.0058 1.0000
11.250 0.9997 0.04846 0.04518 0.0146 0.0057 1.0000
11.500 0.9859 0.05204 0.04896 0.0147 0.0057 1.0000
11.750 0.9715 0.05709 0.05421 0.0112 0.0057 1.0000
12.000 0.9570 0.06404 0.06136 0.0046 0.0058 1.0000
12.250 0.9418 0.07359 0.07111 -0.0047 0.0059 1.0000
12.500 0.9245 0.08503 0.08272 -0.0139 0.0062 1.0000
12.750 0.9041 0.09620 0.09398 -0.0208 0.0066 1.0000
13.000 0.8839 0.10624 0.10401 -0.0261 0.0070 1.0000
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Polar data table (+)
Polar graphs
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