E. Bambino (ebambino7-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: E. Bambino (ebambino7-il) Reynolds number: 200,000 Max Cl/Cd: 46.32 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ebambino7-il-200000.txt Download as CSV file: xf-ebambino7-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-6.750 -0.5945 0.10015 0.09714 0.0272 1.0000 0.0176
-6.500 -0.5921 0.09617 0.09315 0.0245 1.0000 0.0180
-6.250 -0.5906 0.09209 0.08910 0.0211 1.0000 0.0183
-6.000 -0.5856 0.08777 0.08478 0.0172 1.0000 0.0187
-5.750 -0.5778 0.08336 0.08037 0.0136 1.0000 0.0192
-5.500 -0.5677 0.07893 0.07590 0.0101 1.0000 0.0198
-5.250 -0.5554 0.07447 0.07139 0.0069 1.0000 0.0206
-5.000 -0.5400 0.07005 0.06688 0.0038 1.0000 0.0216
-4.750 -0.5173 0.06599 0.06266 0.0003 1.0000 0.0230
-4.500 -0.4891 0.06335 0.05971 -0.0020 1.0000 0.0239
-4.250 -0.4803 0.05648 0.05277 -0.0032 1.0000 0.0249
-4.000 -0.4698 0.05282 0.04920 -0.0031 1.0000 0.0273
-3.750 -0.4334 0.05293 0.04878 -0.0037 1.0000 0.0351
-3.500 -0.4213 0.04591 0.04174 -0.0046 1.0000 0.0368
-3.250 -0.4037 0.04244 0.03830 -0.0047 1.0000 0.0394
-3.000 -0.3800 0.03960 0.03528 -0.0048 1.0000 0.0436
-2.500 -0.3288 0.03357 0.02870 -0.0046 1.0000 0.0512
-2.250 -0.3040 0.03119 0.02619 -0.0044 1.0000 0.0566
-2.000 -0.2774 0.02861 0.02323 -0.0041 1.0000 0.0643
-1.750 -0.2471 0.02741 0.02159 -0.0040 0.9850 0.0755
-1.500 -0.2143 0.02403 0.01819 -0.0055 0.9291 0.0803
-1.250 -0.1910 0.02245 0.01624 -0.0037 0.8651 0.0918
-1.000 -0.1725 0.02158 0.01481 -0.0002 0.7549 0.0986
-0.750 -0.1375 0.01841 0.01066 0.0037 0.7011 0.0328
-0.500 -0.1111 0.01661 0.00824 0.0052 0.6304 0.0280
-0.250 -0.0838 0.01538 0.00656 0.0063 0.5626 0.0251
0.000 -0.0584 0.01511 0.00537 0.0069 0.3311 0.0246
0.250 -0.0324 0.01457 0.00419 0.0071 0.1781 0.0265
0.500 -0.0048 0.01437 0.00386 0.0072 0.1522 0.0373
0.750 0.0229 0.01390 0.00324 0.0076 0.1343 0.0552
1.000 0.0308 0.01088 0.00299 0.0121 0.1172 0.8767
1.250 0.1174 0.01151 0.00319 0.0009 0.0739 1.0000
1.500 0.1421 0.01160 0.00312 0.0015 0.0724 1.0000
1.750 0.1668 0.01170 0.00312 0.0021 0.0717 1.0000
2.000 0.1914 0.01183 0.00317 0.0026 0.0714 1.0000
2.250 0.2161 0.01199 0.00327 0.0032 0.0712 1.0000
2.500 0.2409 0.01218 0.00340 0.0037 0.0711 1.0000
2.750 0.2658 0.01240 0.00358 0.0041 0.0711 1.0000
3.000 0.2908 0.01265 0.00382 0.0046 0.0711 1.0000
3.250 0.3158 0.01295 0.00408 0.0050 0.0713 1.0000
3.500 0.3410 0.01330 0.00439 0.0054 0.0714 1.0000
3.750 0.3663 0.01370 0.00476 0.0058 0.0716 1.0000
4.000 0.3916 0.01416 0.00520 0.0061 0.0718 1.0000
4.250 0.4171 0.01450 0.00553 0.0063 0.0683 1.0000
4.500 0.4409 0.01554 0.00650 0.0064 0.0616 1.0000
4.750 0.4651 0.01677 0.00772 0.0067 0.0599 1.0000
5.000 0.4917 0.01667 0.00770 0.0067 0.0581 1.0000
5.250 0.5172 0.01687 0.00787 0.0066 0.0521 1.0000
5.500 0.5428 0.01688 0.00785 0.0063 0.0442 1.0000
5.750 0.5703 0.01640 0.00734 0.0061 0.0399 1.0000
6.000 0.5969 0.01645 0.00739 0.0060 0.0374 1.0000
6.250 0.6242 0.01637 0.00728 0.0060 0.0367 1.0000
6.500 0.6518 0.01617 0.00714 0.0061 0.0340 1.0000
6.750 0.6745 0.01877 0.01000 0.0071 0.0227 1.0000
7.000 0.7039 0.01730 0.00844 0.0065 0.0200 1.0000
7.250 0.7303 0.01768 0.00889 0.0066 0.0202 1.0000
7.500 0.7572 0.01793 0.00944 0.0067 0.0207 1.0000
8.000 0.8129 0.01793 0.00967 0.0070 0.0225 1.0000
8.250 0.8403 0.01814 0.00991 0.0072 0.0229 1.0000
8.500 0.8639 0.01959 0.01163 0.0077 0.0208 1.0000
8.750 0.8920 0.01972 0.01179 0.0081 0.0219 1.0000
9.000 0.9198 0.01996 0.01212 0.0084 0.0230 1.0000
9.250 0.9454 0.02079 0.01316 0.0090 0.0238 1.0000
9.500 0.9689 0.02207 0.01473 0.0097 0.0245 1.0000
9.750 0.9906 0.02378 0.01684 0.0105 0.0247 1.0000
10.000 1.0104 0.02600 0.01937 0.0115 0.0245 1.0000
10.250 1.0276 0.02887 0.02261 0.0126 0.0240 1.0000
10.500 1.0400 0.03278 0.02702 0.0137 0.0234 1.0000
10.750 1.0453 0.03759 0.03244 0.0148 0.0231 1.0000
11.000 1.0454 0.04239 0.03781 0.0158 0.0228 1.0000
11.250 1.0386 0.04737 0.04327 0.0165 0.0227 1.0000
11.500 1.0256 0.05229 0.04854 0.0167 0.0227 1.0000
11.750 1.0068 0.05685 0.05333 0.0162 0.0228 1.0000
12.000 0.9881 0.06283 0.05951 0.0119 0.0230 1.0000
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Polar data table (+)
Polar graphs
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