Bambino 6 (bambino6-il) Xfoil prediction polar at RE=500,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: Bambino 6 (bambino6-il) Reynolds number: 500,000 Max Cl/Cd: 39.38 at α=8.25° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-bambino6-il-500000-n5.txt Download as CSV file: xf-bambino6-il-500000-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 = 0.500 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-12.500 -0.6333 0.08350 0.08113 -0.0492 1.0000 0.0049
-12.250 -0.6937 0.07053 0.06817 -0.0570 1.0000 0.0046
-12.000 -0.8593 0.04682 0.04404 -0.0651 1.0000 0.0037
-11.750 -0.8960 0.04034 0.03728 -0.0606 1.0000 0.0036
-11.500 -0.9211 0.03681 0.03354 -0.0550 0.9991 0.0038
-11.250 -0.9105 0.03356 0.03004 -0.0551 0.9957 0.0040
-11.000 -0.9008 0.03067 0.02685 -0.0543 0.9914 0.0039
-10.750 -0.8839 0.02867 0.02464 -0.0539 0.9879 0.0041
-10.500 -0.8623 0.02704 0.02283 -0.0540 0.9852 0.0044
-10.250 -0.8466 0.02540 0.02098 -0.0526 0.9797 0.0046
-10.000 -0.8235 0.02406 0.01945 -0.0525 0.9764 0.0048
-9.750 -0.8045 0.02289 0.01811 -0.0513 0.9713 0.0049
-9.500 -0.7832 0.02169 0.01671 -0.0505 0.9667 0.0053
-9.000 -0.7381 0.01976 0.01445 -0.0489 0.9565 0.0057
-8.750 -0.7145 0.01854 0.01304 -0.0484 0.9518 0.0063
-8.500 -0.6877 0.01763 0.01200 -0.0484 0.9476 0.0068
-8.250 -0.6627 0.01690 0.01113 -0.0479 0.9412 0.0073
-8.000 -0.6315 0.01614 0.01024 -0.0487 0.9370 0.0082
-7.750 -0.5981 0.01539 0.00934 -0.0499 0.9326 0.0095
-7.500 -0.5658 0.01459 0.00848 -0.0510 0.9264 0.0122
-7.250 -0.5278 0.01386 0.00778 -0.0533 0.9214 0.0207
-7.000 -0.4910 0.01351 0.00744 -0.0552 0.9143 0.0279
-6.750 -0.4526 0.01323 0.00704 -0.0574 0.9066 0.0312
-6.500 -0.4176 0.01293 0.00671 -0.0590 0.8975 0.0346
-6.250 -0.3826 0.01274 0.00646 -0.0604 0.8882 0.0373
-6.000 -0.3523 0.01252 0.00616 -0.0609 0.8772 0.0390
-5.750 -0.3228 0.01246 0.00601 -0.0611 0.8659 0.0412
-5.500 -0.2954 0.01220 0.00568 -0.0610 0.8537 0.0438
-5.250 -0.2692 0.01196 0.00537 -0.0606 0.8411 0.0453
-5.000 -0.2441 0.01175 0.00508 -0.0599 0.8275 0.0466
-4.750 -0.2196 0.01158 0.00482 -0.0590 0.8137 0.0481
-4.500 -0.1961 0.01142 0.00458 -0.0579 0.7974 0.0499
-4.250 -0.1733 0.01132 0.00437 -0.0567 0.7765 0.0519
-4.000 -0.1570 0.01138 0.00415 -0.0539 0.7149 0.0531
-3.750 -0.1406 0.01141 0.00394 -0.0513 0.6690 0.0547
-3.500 -0.1236 0.01142 0.00375 -0.0489 0.6333 0.0569
-3.250 -0.1019 0.01137 0.00360 -0.0476 0.6178 0.0592
-3.000 -0.0807 0.01135 0.00347 -0.0461 0.5979 0.0615
-2.750 -0.0578 0.01129 0.00334 -0.0450 0.5870 0.0638
-2.500 -0.0347 0.01124 0.00322 -0.0439 0.5745 0.0655
-2.250 -0.0122 0.01123 0.00312 -0.0427 0.5582 0.0666
-2.000 0.0091 0.01115 0.00294 -0.0413 0.5396 0.0690
-1.750 0.0289 0.01113 0.00279 -0.0395 0.5050 0.0714
-1.500 0.0450 0.01134 0.00269 -0.0371 0.4341 0.0734
-1.250 0.0400 0.01291 0.00309 -0.0309 0.1083 0.0745
-1.000 0.0608 0.01301 0.00305 -0.0294 0.0658 0.0766
-0.750 0.0832 0.01303 0.00300 -0.0282 0.0604 0.0789
-0.500 0.1057 0.01301 0.00297 -0.0271 0.0579 0.0829
-0.250 0.1275 0.01295 0.00295 -0.0258 0.0554 0.0897
0.000 0.1485 0.01287 0.00302 -0.0245 0.0547 0.1280
0.250 0.1711 0.01291 0.00307 -0.0234 0.0540 0.1359
0.500 0.1938 0.01297 0.00313 -0.0223 0.0533 0.1431
0.750 0.2162 0.01304 0.00320 -0.0212 0.0522 0.1462
1.000 0.2380 0.01309 0.00328 -0.0200 0.0513 0.1507
1.250 0.2598 0.01316 0.00337 -0.0187 0.0500 0.1546
1.500 0.2813 0.01326 0.00349 -0.0175 0.0490 0.1582
1.750 0.3027 0.01337 0.00360 -0.0162 0.0483 0.1609
2.000 0.3218 0.01352 0.00381 -0.0145 0.0454 0.1662
2.250 0.3437 0.01355 0.00382 -0.0134 0.0440 0.1717
2.750 0.3870 0.01359 0.00385 -0.0112 0.0393 0.1852
3.000 0.4068 0.01365 0.00392 -0.0097 0.0376 0.1993
3.250 0.4026 0.01272 0.00390 -0.0033 0.0346 0.5190
3.500 0.3789 0.01182 0.00397 0.0083 0.0339 0.8295
3.750 0.3918 0.01205 0.00410 0.0113 0.0171 0.8474
4.000 0.4081 0.01219 0.00426 0.0137 0.0157 0.8572
4.250 0.4251 0.01236 0.00444 0.0158 0.0146 0.8624
4.500 0.4425 0.01255 0.00466 0.0178 0.0131 0.8686
4.750 0.4601 0.01276 0.00490 0.0198 0.0126 0.8729
5.000 0.4765 0.01301 0.00518 0.0219 0.0120 0.8766
5.250 0.4919 0.01335 0.00558 0.0242 0.0107 0.8797
5.500 0.5080 0.01372 0.00604 0.0263 0.0099 0.8835
5.750 0.5240 0.01400 0.00636 0.0284 0.0094 0.8890
6.000 0.5417 0.01429 0.00675 0.0301 0.0092 0.8987
6.250 0.5590 0.01467 0.00718 0.0317 0.0080 0.9002
6.500 0.5740 0.01510 0.00768 0.0338 0.0078 0.9058
6.750 0.5918 0.01552 0.00816 0.0351 0.0068 0.9078
7.000 0.6130 0.01596 0.00866 0.0357 0.0064 0.9101
7.250 0.6359 0.01643 0.00919 0.0357 0.0066 0.9132
7.500 0.6585 0.01694 0.00975 0.0358 0.0067 0.9160
7.750 0.6855 0.01749 0.01037 0.0348 0.0066 0.9199
8.000 0.7131 0.01816 0.01112 0.0335 0.0067 0.9232
8.250 0.7530 0.01912 0.01218 0.0292 0.0069 0.9293
8.500 0.7648 0.02194 0.01482 0.0283 0.0102 0.9329
9.000 0.8456 0.02294 0.01612 0.0204 0.0050 0.9405
9.250 0.8742 0.02351 0.01672 0.0189 0.0062 0.9430
9.500 0.8916 0.02536 0.01860 0.0181 0.0049 0.9468
9.750 0.9084 0.02694 0.02012 0.0180 0.0050 0.9490
10.250 0.9551 0.02886 0.02206 0.0167 0.0063 0.9853
10.500 0.9708 0.02996 0.02313 0.0176 0.0062 0.9916
10.750 0.9901 0.03105 0.02418 0.0178 0.0062 0.9939
11.000 1.0126 0.03223 0.02529 0.0181 0.0058 0.9959
11.250 1.0382 0.03331 0.02633 0.0177 0.0058 0.9971
11.500 1.2305 0.04030 0.03212 -0.0082 0.0052 0.9459
11.750 1.2616 0.04224 0.03407 -0.0100 0.0052 0.9470
12.000 1.2910 0.04426 0.03614 -0.0114 0.0052 0.9485
12.250 1.3167 0.04620 0.03819 -0.0124 0.0052 0.9506
12.500 1.3394 0.04811 0.04023 -0.0130 0.0052 0.9566
13.000 1.3591 0.05133 0.04377 -0.0092 0.0051 0.9837
13.250 1.3729 0.05330 0.04584 -0.0081 0.0051 0.9890
13.500 1.3721 0.05460 0.04739 -0.0049 0.0051 0.9941
13.750 1.3620 0.05538 0.04847 -0.0008 0.0051 0.9988
14.000 1.3694 0.05741 0.05069 0.0003 0.0051 1.0000
14.250 1.3408 0.05748 0.05095 0.0083 0.0050 1.0000
14.500 1.3098 0.05772 0.05135 0.0159 0.0050 1.0000
14.750 1.3108 0.05990 0.05367 0.0180 0.0050 1.0000
15.000 1.2859 0.06103 0.05499 0.0229 0.0050 1.0000
15.250 1.2565 0.06185 0.05599 0.0271 0.0049 1.0000
15.500 1.2349 0.06333 0.05764 0.0297 0.0047 1.0000
15.750 1.2176 0.06581 0.06029 0.0313 0.0046 1.0000
16.000 1.2075 0.06858 0.06319 0.0321 0.0046 1.0000
16.250 1.1924 0.07190 0.06668 0.0327 0.0045 1.0000
16.500 1.1794 0.07516 0.07009 0.0327 0.0045 1.0000
16.750 1.1645 0.07884 0.07392 0.0325 0.0044 1.0000
17.000 1.1502 0.08275 0.07797 0.0318 0.0044 1.0000
17.250 1.1337 0.08706 0.08243 0.0308 0.0044 1.0000
17.500 1.1176 0.09163 0.08715 0.0293 0.0041 1.0000
|
Polar data table (+)
Polar graphs
<< Back to Bambino 6 (bambino6-il)