Bambino 6 (bambino6-il) Xfoil prediction polar at RE=100,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: Bambino 6 (bambino6-il) Reynolds number: 100,000 Max Cl/Cd: 35.99 at α=1.75° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-bambino6-il-100000-n5.txt Download as CSV file: xf-bambino6-il-100000-n5.csv |
XFOIL Version 6.96
Calculated polar for: Bambino 6
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
------ -------- --------- --------- -------- -------- --------
-9.750 -0.4331 0.09110 0.08650 -0.0431 1.0000 0.0290
-9.500 -0.4495 0.08525 0.08075 -0.0455 1.0000 0.0296
-9.250 -0.4646 0.08024 0.07584 -0.0475 1.0000 0.0294
-9.000 -0.4893 0.07462 0.07031 -0.0497 1.0000 0.0294
-8.750 -0.5157 0.07045 0.06620 -0.0486 1.0000 0.0290
-8.500 -0.5439 0.06739 0.06318 -0.0448 1.0000 0.0286
-8.250 -0.5709 0.06390 0.05969 -0.0406 1.0000 0.0282
-8.000 -0.5999 0.05943 0.05515 -0.0361 1.0000 0.0283
-7.750 -0.6298 0.05428 0.04983 -0.0309 1.0000 0.0286
-7.500 -0.6497 0.04577 0.04069 -0.0286 0.9939 0.0296
-7.250 -0.6452 0.03996 0.03416 -0.0278 0.9859 0.0327
-7.000 -0.6171 0.03996 0.03412 -0.0285 0.9795 0.0366
-6.750 -0.6082 0.03506 0.02820 -0.0265 0.9714 0.0420
-6.500 -0.5768 0.03554 0.02885 -0.0278 0.9654 0.0468
-6.250 -0.5578 0.03343 0.02600 -0.0265 0.9572 0.0528
-6.000 -0.5291 0.03258 0.02515 -0.0275 0.9512 0.0581
-5.750 -0.5061 0.03127 0.02347 -0.0268 0.9432 0.0633
-5.500 -0.4778 0.02939 0.02096 -0.0267 0.9369 0.0659
-5.250 -0.4494 0.02771 0.01893 -0.0269 0.9302 0.0678
-5.000 -0.4181 0.02624 0.01733 -0.0277 0.9237 0.0701
-4.750 -0.3810 0.02508 0.01599 -0.0295 0.9195 0.0745
-4.500 -0.3535 0.02414 0.01481 -0.0293 0.9101 0.0778
-4.250 -0.3141 0.02298 0.01341 -0.0313 0.9056 0.0800
-4.000 -0.2829 0.02187 0.01231 -0.0320 0.8973 0.0824
-3.750 -0.2450 0.02092 0.01134 -0.0339 0.8913 0.0859
-3.500 -0.2133 0.02020 0.01055 -0.0345 0.8823 0.0895
-3.250 -0.1766 0.01944 0.00977 -0.0362 0.8754 0.0939
-3.000 -0.1470 0.01895 0.00933 -0.0364 0.8648 0.1002
-2.750 -0.1120 0.01852 0.00897 -0.0378 0.8561 0.1108
-2.500 -0.0777 0.01814 0.00861 -0.0389 0.8462 0.1250
-2.250 -0.0467 0.01783 0.00822 -0.0393 0.8345 0.1431
-2.000 -0.0131 0.01746 0.00786 -0.0403 0.8240 0.1668
-1.750 0.0248 0.01706 0.00747 -0.0423 0.8146 0.1908
-1.500 0.0562 0.01679 0.00725 -0.0429 0.8023 0.2093
-1.250 0.0879 0.01653 0.00705 -0.0437 0.7904 0.2347
-1.000 0.1185 0.01613 0.00678 -0.0441 0.7722 0.2800
-0.750 0.1917 0.01491 0.00732 -0.0513 0.7258 0.8373
-0.500 0.1864 0.01493 0.00716 -0.0440 0.7077 0.8637
-0.250 0.2208 0.01519 0.00722 -0.0446 0.6874 0.8890
0.000 0.2816 0.01564 0.00748 -0.0505 0.6692 0.9105
0.250 0.3525 0.01628 0.00792 -0.0584 0.6515 0.9360
0.500 0.4485 0.01673 0.00816 -0.0719 0.6288 0.9680
0.750 0.4936 0.01683 0.00805 -0.0755 0.6006 0.9789
1.000 0.5258 0.01692 0.00802 -0.0766 0.5740 0.9850
1.250 0.5567 0.01691 0.00793 -0.0774 0.5487 0.9885
1.500 0.5861 0.01694 0.00788 -0.0780 0.5236 0.9921
1.750 0.6126 0.01702 0.00787 -0.0780 0.4847 0.9949
2.000 0.6088 0.01937 0.00823 -0.0729 0.1477 0.9969
2.250 0.6244 0.02041 0.00869 -0.0713 0.0702 0.9986
2.500 0.6473 0.02074 0.00898 -0.0708 0.0645 1.0000
2.750 0.6642 0.02112 0.00937 -0.0690 0.0607 1.0000
3.000 0.6789 0.02167 0.00989 -0.0668 0.0548 1.0000
3.250 0.6971 0.02190 0.01018 -0.0653 0.0526 1.0000
3.500 0.7141 0.02221 0.01051 -0.0635 0.0494 1.0000
3.750 0.7301 0.02257 0.01089 -0.0617 0.0470 1.0000
4.000 0.7451 0.02298 0.01133 -0.0596 0.0452 1.0000
4.250 0.7623 0.02320 0.01158 -0.0579 0.0435 1.0000
4.500 0.7799 0.02337 0.01177 -0.0564 0.0405 1.0000
4.750 0.7956 0.02366 0.01209 -0.0544 0.0389 1.0000
5.000 0.8110 0.02394 0.01237 -0.0525 0.0375 1.0000
5.250 0.8286 0.02414 0.01305 -0.0501 0.0226 1.0000
5.500 0.8407 0.02448 0.01290 -0.0484 0.0205 1.0000
5.750 0.8518 0.02496 0.01347 -0.0456 0.0194 1.0000
6.000 0.8612 0.02549 0.01411 -0.0426 0.0189 1.0000
6.250 0.8706 0.02597 0.01468 -0.0395 0.0187 1.0000
6.500 0.8784 0.02647 0.01527 -0.0362 0.0186 1.0000
6.750 0.8842 0.02701 0.01590 -0.0325 0.0185 1.0000
7.000 0.8880 0.02754 0.01651 -0.0285 0.0184 1.0000
7.250 0.8891 0.02798 0.01707 -0.0241 0.0184 1.0000
7.500 0.8884 0.02843 0.01759 -0.0193 0.0184 1.0000
7.750 0.8876 0.02892 0.01816 -0.0146 0.0183 1.0000
8.000 0.8870 0.02952 0.01883 -0.0101 0.0181 1.0000
8.250 0.8880 0.03017 0.01956 -0.0061 0.0180 1.0000
8.500 0.8908 0.03088 0.02035 -0.0025 0.0178 1.0000
8.750 0.8932 0.03182 0.02140 0.0010 0.0174 1.0000
9.000 0.8981 0.03271 0.02236 0.0039 0.0171 1.0000
9.250 0.9045 0.03357 0.02330 0.0064 0.0172 1.0000
9.500 0.9113 0.03451 0.02435 0.0088 0.0173 1.0000
9.750 0.9186 0.03547 0.02540 0.0110 0.0173 1.0000
10.000 0.9262 0.03647 0.02655 0.0130 0.0174 1.0000
10.250 0.9339 0.03752 0.02769 0.0148 0.0175 1.0000
10.500 0.9419 0.03859 0.02886 0.0165 0.0177 1.0000
10.750 0.9497 0.03973 0.03009 0.0180 0.0178 1.0000
11.000 0.9574 0.04093 0.03137 0.0195 0.0179 1.0000
11.250 0.9648 0.04219 0.03271 0.0208 0.0181 1.0000
11.500 0.9721 0.04351 0.03411 0.0219 0.0183 1.0000
11.750 0.9787 0.04494 0.03563 0.0230 0.0184 1.0000
12.000 0.9845 0.04650 0.03728 0.0240 0.0187 1.0000
12.250 0.9913 0.04803 0.03890 0.0248 0.0189 1.0000
12.500 0.9963 0.04978 0.04076 0.0254 0.0191 1.0000
12.750 1.0007 0.05167 0.04276 0.0260 0.0193 1.0000
13.000 1.0039 0.05375 0.04495 0.0264 0.0195 1.0000
13.250 1.0057 0.05605 0.04737 0.0267 0.0196 1.0000
13.500 1.0060 0.05862 0.05006 0.0269 0.0198 1.0000
13.750 1.0003 0.06203 0.05363 0.0269 0.0197 1.0000
14.000 1.0023 0.06452 0.05630 0.0266 0.0200 1.0000
14.250 0.9952 0.06832 0.06026 0.0262 0.0199 1.0000
14.500 0.9880 0.07233 0.06441 0.0254 0.0199 1.0000
14.750 0.9830 0.07614 0.06836 0.0245 0.0200 1.0000
15.000 0.9743 0.08068 0.07304 0.0232 0.0200 1.0000
15.250 0.9665 0.08529 0.07779 0.0217 0.0201 1.0000
15.500 0.9596 0.08990 0.08249 0.0201 0.0203 1.0000
15.750 0.9471 0.09574 0.08850 0.0179 0.0202 1.0000
16.000 0.9377 0.10122 0.09409 0.0156 0.0203 1.0000
|
Polar data table (+)
Polar graphs
<< Back to Bambino 6 (bambino6-il)