Bambino 6 (bambino6-il) Xfoil prediction polar at RE=200,000 Ncrit=9
| Details | Polar file |
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Airfoil: Bambino 6 (bambino6-il) Reynolds number: 200,000 Max Cl/Cd: 47.77 at α=1.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-bambino6-il-200000.txt Download as CSV file: xf-bambino6-il-200000.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 = 0.200 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.500 -0.3953 0.11275 0.10929 -0.0385 1.0000 0.0549
-10.250 -0.4021 0.10876 0.10536 -0.0409 1.0000 0.0552
-10.000 -0.4128 0.10457 0.10124 -0.0440 1.0000 0.0555
-9.750 -0.4175 0.10048 0.09720 -0.0454 1.0000 0.0555
-9.500 -0.4314 0.09565 0.09242 -0.0489 1.0000 0.0556
-9.250 -0.4202 0.09180 0.08858 -0.0425 1.0000 0.0573
-9.000 -0.4190 0.08923 0.08604 -0.0412 1.0000 0.0582
-8.750 -0.4256 0.08608 0.08294 -0.0410 1.0000 0.0589
-8.500 -0.4353 0.08310 0.08002 -0.0408 1.0000 0.0599
-8.250 -0.4574 0.07985 0.07683 -0.0403 1.0000 0.0599
-8.000 -0.4872 0.07753 0.07457 -0.0370 1.0000 0.0596
-7.750 -0.5184 0.07575 0.07283 -0.0320 1.0000 0.0594
-7.500 -0.6097 0.06215 0.05894 -0.0269 1.0000 0.0451
-7.250 -0.6026 0.05649 0.05308 -0.0274 0.9958 0.0423
-7.000 -0.6029 0.04826 0.04443 -0.0280 0.9885 0.0415
-6.750 -0.6052 0.03984 0.03510 -0.0263 0.9806 0.0429
-6.500 -0.5902 0.03639 0.03129 -0.0258 0.9732 0.0462
-6.250 -0.5533 0.03566 0.03057 -0.0282 0.9696 0.0502
-6.000 -0.5399 0.03237 0.02663 -0.0258 0.9607 0.0535
-5.750 -0.5115 0.02991 0.02382 -0.0267 0.9562 0.0588
-5.500 -0.4852 0.02874 0.02257 -0.0266 0.9485 0.0627
-5.250 -0.4520 0.02730 0.02065 -0.0274 0.9433 0.0672
-5.000 -0.4238 0.02507 0.01796 -0.0274 0.9370 0.0699
-4.750 -0.3901 0.02332 0.01619 -0.0288 0.9311 0.0742
-4.500 -0.3484 0.02186 0.01449 -0.0313 0.9280 0.0775
-4.250 -0.3136 0.02065 0.01305 -0.0323 0.9212 0.0799
-4.000 -0.2720 0.01921 0.01141 -0.0348 0.9166 0.0834
-3.750 -0.2243 0.01778 0.01002 -0.0387 0.9140 0.0885
-3.500 -0.1736 0.01668 0.00886 -0.0431 0.9117 0.0936
-3.250 -0.1406 0.01578 0.00800 -0.0439 0.9017 0.0985
-3.000 -0.0933 0.01501 0.00726 -0.0477 0.8972 0.1069
-2.750 -0.0595 0.01457 0.00689 -0.0487 0.8854 0.1169
-2.500 -0.0227 0.01416 0.00651 -0.0502 0.8737 0.1300
-2.250 0.0140 0.01376 0.00608 -0.0516 0.8602 0.1495
-2.000 0.0456 0.01323 0.00559 -0.0521 0.8421 0.1762
-1.750 0.0733 0.01274 0.00512 -0.0517 0.8188 0.2019
-1.500 0.0969 0.01247 0.00482 -0.0505 0.7957 0.2222
-1.250 0.1184 0.01222 0.00458 -0.0489 0.7730 0.2453
-1.000 0.1384 0.01198 0.00440 -0.0471 0.7540 0.2782
-0.750 0.1550 0.01159 0.00425 -0.0447 0.7376 0.3519
-0.500 0.1662 0.01062 0.00490 -0.0401 0.7230 0.8470
-0.250 0.1802 0.01085 0.00502 -0.0362 0.7074 0.8816
0.000 0.3255 0.01255 0.00638 -0.0586 0.6722 0.9271
0.250 0.4462 0.01361 0.00704 -0.0767 0.6292 0.9616
0.500 0.5258 0.01363 0.00681 -0.0874 0.5950 0.9847
0.750 0.5777 0.01333 0.00634 -0.0927 0.5637 0.9950
1.000 0.6160 0.01308 0.00598 -0.0951 0.5358 1.0000
1.250 0.6330 0.01325 0.00596 -0.0930 0.4853 1.0000
1.500 0.6236 0.01526 0.00638 -0.0863 0.1816 1.0000
1.750 0.6332 0.01628 0.00681 -0.0833 0.0766 1.0000
2.000 0.6509 0.01666 0.00706 -0.0815 0.0678 1.0000
2.250 0.6700 0.01691 0.00731 -0.0801 0.0646 1.0000
2.500 0.6879 0.01725 0.00765 -0.0784 0.0583 1.0000
2.750 0.7060 0.01756 0.00797 -0.0768 0.0555 1.0000
3.000 0.7217 0.01804 0.00850 -0.0747 0.0521 1.0000
3.250 0.7395 0.01835 0.00881 -0.0731 0.0510 1.0000
3.500 0.7591 0.01849 0.00897 -0.0718 0.0502 1.0000
3.750 0.7780 0.01868 0.00916 -0.0704 0.0487 1.0000
4.000 0.7973 0.01881 0.00922 -0.0692 0.0444 1.0000
4.250 0.8142 0.01911 0.00949 -0.0674 0.0426 1.0000
4.500 0.8299 0.01948 0.00986 -0.0655 0.0414 1.0000
4.750 0.8487 0.01960 0.00998 -0.0641 0.0407 1.0000
5.000 0.8660 0.01982 0.01021 -0.0624 0.0398 1.0000
5.250 0.8821 0.02009 0.01051 -0.0604 0.0391 1.0000
5.500 0.8973 0.02040 0.01085 -0.0584 0.0385 1.0000
5.750 0.9121 0.02070 0.01120 -0.0562 0.0377 1.0000
6.000 0.9274 0.02094 0.01147 -0.0542 0.0361 1.0000
6.250 0.9433 0.02110 0.01163 -0.0523 0.0343 1.0000
6.500 0.9573 0.02135 0.01192 -0.0500 0.0340 1.0000
6.750 0.9704 0.02160 0.01221 -0.0476 0.0339 1.0000
7.000 0.9814 0.02191 0.01258 -0.0448 0.0341 1.0000
7.250 0.9921 0.02217 0.01291 -0.0420 0.0337 1.0000
7.500 1.0003 0.02245 0.01325 -0.0386 0.0329 1.0000
7.750 1.0039 0.02272 0.01357 -0.0344 0.0326 1.0000
8.000 1.0054 0.02300 0.01391 -0.0298 0.0325 1.0000
8.250 1.0061 0.02329 0.01425 -0.0252 0.0324 1.0000
8.500 1.0046 0.02362 0.01464 -0.0202 0.0324 1.0000
8.750 1.0015 0.02396 0.01505 -0.0151 0.0326 1.0000
9.000 1.0000 0.02432 0.01545 -0.0103 0.0328 1.0000
9.250 1.0013 0.02481 0.01599 -0.0062 0.0331 1.0000
9.500 1.0059 0.02538 0.01664 -0.0028 0.0334 1.0000
9.750 1.0126 0.02599 0.01730 0.0000 0.0338 1.0000
10.000 1.0201 0.02669 0.01805 0.0026 0.0347 1.0000
10.250 1.0279 0.02745 0.01887 0.0050 0.0358 1.0000
10.500 1.0354 0.02831 0.01980 0.0072 0.0370 1.0000
10.750 1.0446 0.02915 0.02071 0.0092 0.0373 1.0000
11.000 1.0542 0.03001 0.02166 0.0109 0.0375 1.0000
11.250 1.0635 0.03096 0.02269 0.0126 0.0380 1.0000
11.500 1.0716 0.03203 0.02387 0.0143 0.0390 1.0000
11.750 1.0785 0.03327 0.02520 0.0159 0.0401 1.0000
12.000 1.0852 0.03456 0.02658 0.0174 0.0408 1.0000
12.250 1.0896 0.03612 0.02822 0.0190 0.0415 1.0000
12.500 1.1034 0.03698 0.02927 0.0200 0.0427 1.0000
12.750 1.1138 0.03813 0.03054 0.0209 0.0430 1.0000
13.000 1.1231 0.03938 0.03190 0.0218 0.0426 1.0000
13.250 1.1327 0.04067 0.03330 0.0226 0.0426 1.0000
13.500 1.1408 0.04211 0.03484 0.0233 0.0421 1.0000
13.750 1.1481 0.04368 0.03652 0.0240 0.0416 1.0000
14.000 1.1607 0.04481 0.03781 0.0243 0.0408 1.0000
14.250 1.1711 0.04616 0.03931 0.0248 0.0401 1.0000
14.500 1.1809 0.04763 0.04097 0.0253 0.0386 1.0000
14.750 1.1886 0.04934 0.04287 0.0258 0.0369 1.0000
15.000 1.1949 0.05130 0.04513 0.0268 0.0327 1.0000
15.250 1.1996 0.05335 0.04732 0.0271 0.0308 1.0000
15.500 1.2056 0.05528 0.04930 0.0268 0.0280 1.0000
15.750 1.2150 0.05695 0.05085 0.0258 0.0271 1.0000
16.000 1.2169 0.05955 0.05341 0.0254 0.0263 1.0000
16.250 1.2139 0.06278 0.05665 0.0249 0.0256 1.0000
16.500 1.2102 0.06614 0.06014 0.0245 0.0252 1.0000
16.750 1.2051 0.06979 0.06388 0.0238 0.0248 1.0000
17.000 1.1980 0.07382 0.06802 0.0229 0.0245 1.0000
17.250 1.1924 0.07775 0.07208 0.0220 0.0244 1.0000
17.500 1.1839 0.08221 0.07667 0.0207 0.0242 1.0000
17.750 1.1737 0.08708 0.08165 0.0193 0.0240 1.0000
18.000 1.1627 0.09221 0.08692 0.0176 0.0239 1.0000
18.250 1.1499 0.09778 0.09263 0.0156 0.0238 1.0000
18.500 1.1418 0.10273 0.09772 0.0137 0.0238 1.0000
18.750 1.1312 0.10821 0.10334 0.0115 0.0239 1.0000
19.000 1.1163 0.11456 0.10984 0.0089 0.0237 1.0000
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Polar data table (+)
Polar graphs
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