Bambino 6 (bambino6-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
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Airfoil: Bambino 6 (bambino6-il) Reynolds number: 1,000,000 Max Cl/Cd: 73.54 at α=6.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-bambino6-il-1000000.txt Download as CSV file: xf-bambino6-il-1000000.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 = 1.000 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.750 -0.7853 0.07291 0.07096 -0.0595 1.0000 0.0067
-13.500 -0.9684 0.04029 0.03790 -0.0790 1.0000 0.0058
-13.250 -0.9936 0.03688 0.03430 -0.0748 1.0000 0.0059
-13.000 -1.0079 0.03485 0.03213 -0.0701 1.0000 0.0060
-12.750 -1.0247 0.03331 0.03046 -0.0639 1.0000 0.0060
-12.500 -1.0480 0.03192 0.02894 -0.0561 1.0000 0.0059
-12.250 -1.0592 0.03043 0.02730 -0.0502 1.0000 0.0059
-12.000 -1.0408 0.02906 0.02580 -0.0496 0.9988 0.0062
-11.750 -1.0191 0.02729 0.02384 -0.0499 0.9966 0.0063
-11.500 -0.9908 0.02645 0.02290 -0.0507 0.9950 0.0064
-11.250 -0.9836 0.02318 0.01923 -0.0490 0.9913 0.0069
-11.000 -0.9631 0.02153 0.01739 -0.0485 0.9882 0.0073
-10.750 -0.9362 0.02050 0.01625 -0.0489 0.9861 0.0076
-10.500 -0.9072 0.01963 0.01528 -0.0495 0.9845 0.0082
-10.250 -0.8781 0.01872 0.01424 -0.0502 0.9833 0.0085
-10.000 -0.8552 0.01785 0.01325 -0.0493 0.9799 0.0089
-9.750 -0.8296 0.01718 0.01247 -0.0490 0.9763 0.0091
-9.500 -0.8020 0.01624 0.01139 -0.0491 0.9738 0.0099
-9.250 -0.7731 0.01529 0.01033 -0.0495 0.9719 0.0109
-9.000 -0.7413 0.01464 0.00964 -0.0504 0.9705 0.0119
-8.750 -0.7087 0.01405 0.00897 -0.0515 0.9693 0.0128
-8.500 -0.6889 0.01353 0.00838 -0.0496 0.9622 0.0141
-8.250 -0.6591 0.01294 0.00780 -0.0500 0.9593 0.0168
-8.000 -0.6264 0.01247 0.00730 -0.0510 0.9569 0.0196
-7.750 -0.5924 0.01216 0.00704 -0.0522 0.9538 0.0232
-7.500 -0.5632 0.01206 0.00691 -0.0524 0.9467 0.0250
-7.250 -0.5262 0.01158 0.00642 -0.0543 0.9434 0.0284
-7.000 -0.4853 0.01137 0.00621 -0.0571 0.9405 0.0307
-6.750 -0.4516 0.01124 0.00606 -0.0583 0.9330 0.0325
-6.500 -0.4107 0.01110 0.00587 -0.0610 0.9272 0.0335
-6.250 -0.3778 0.01053 0.00522 -0.0621 0.9177 0.0356
-6.000 -0.3429 0.01025 0.00491 -0.0636 0.9086 0.0382
-5.750 -0.3110 0.01009 0.00471 -0.0644 0.8978 0.0399
-5.500 -0.2830 0.00999 0.00456 -0.0643 0.8860 0.0416
-5.250 -0.2557 0.00997 0.00449 -0.0640 0.8741 0.0431
-5.000 -0.2297 0.00994 0.00439 -0.0634 0.8615 0.0439
-4.750 -0.2076 0.00944 0.00380 -0.0621 0.8481 0.0470
-4.500 -0.1851 0.00934 0.00364 -0.0608 0.8287 0.0492
-4.250 -0.1656 0.00935 0.00352 -0.0587 0.7962 0.0514
-4.000 -0.1487 0.00940 0.00339 -0.0561 0.7508 0.0531
-3.750 -0.1321 0.00952 0.00331 -0.0535 0.7003 0.0547
-3.500 -0.1151 0.00974 0.00331 -0.0510 0.6541 0.0555
-3.250 -0.0955 0.00948 0.00294 -0.0492 0.6363 0.0597
-3.000 -0.0733 0.00943 0.00284 -0.0479 0.6224 0.0623
-2.750 -0.0507 0.00939 0.00273 -0.0467 0.6104 0.0647
-2.500 -0.0281 0.00937 0.00264 -0.0454 0.5962 0.0669
-2.250 -0.0049 0.00937 0.00258 -0.0444 0.5832 0.0682
-2.000 0.0180 0.00928 0.00243 -0.0432 0.5706 0.0701
-1.750 0.0390 0.00920 0.00225 -0.0417 0.5499 0.0732
-1.500 0.0593 0.00920 0.00213 -0.0400 0.5153 0.0755
-1.250 0.0627 0.01004 0.00222 -0.0351 0.3304 0.0773
-1.000 0.0654 0.01112 0.00250 -0.0301 0.0932 0.0789
-0.750 0.0862 0.01123 0.00248 -0.0286 0.0588 0.0806
-0.500 0.1091 0.01123 0.00246 -0.0275 0.0562 0.0828
-0.250 0.1315 0.01119 0.00246 -0.0262 0.0546 0.0908
0.000 0.1524 0.01110 0.00252 -0.0248 0.0537 0.1289
0.250 0.1754 0.01114 0.00259 -0.0238 0.0527 0.1397
0.500 0.1984 0.01119 0.00266 -0.0227 0.0520 0.1471
0.750 0.2212 0.01126 0.00275 -0.0216 0.0513 0.1525
1.000 0.2436 0.01130 0.00280 -0.0205 0.0511 0.1582
1.250 0.2660 0.01137 0.00288 -0.0194 0.0508 0.1618
1.500 0.2885 0.01145 0.00296 -0.0183 0.0503 0.1646
1.750 0.3100 0.01151 0.00304 -0.0170 0.0492 0.1694
2.000 0.3317 0.01157 0.00311 -0.0158 0.0475 0.1742
2.250 0.3534 0.01164 0.00317 -0.0147 0.0456 0.1786
2.500 0.3733 0.01175 0.00330 -0.0131 0.0432 0.1877
2.750 0.3949 0.01163 0.00323 -0.0120 0.0408 0.2185
3.000 0.3762 0.01034 0.00314 -0.0022 0.0405 0.6375
3.250 0.3646 0.00980 0.00318 0.0068 0.0394 0.8396
3.500 0.3820 0.00990 0.00320 0.0089 0.0339 0.8521
3.750 0.3949 0.01014 0.00335 0.0121 0.0170 0.8611
4.000 0.4110 0.01026 0.00348 0.0146 0.0161 0.8692
4.250 0.4282 0.01040 0.00362 0.0167 0.0157 0.8754
4.500 0.4464 0.01054 0.00379 0.0187 0.0148 0.8811
4.750 0.4626 0.01073 0.00399 0.0211 0.0142 0.8854
5.000 0.4809 0.01093 0.00424 0.0229 0.0135 0.8892
5.250 0.5014 0.01109 0.00443 0.0242 0.0137 0.8936
5.500 0.5216 0.01124 0.00459 0.0255 0.0141 0.8965
5.750 0.5404 0.01139 0.00473 0.0271 0.0146 0.8996
6.000 0.5608 0.01162 0.00503 0.0283 0.0142 0.9048
6.250 0.5850 0.01176 0.00517 0.0286 0.0152 0.9090
6.500 1.3892 0.01889 0.01606 -0.0620 0.0059 0.9548
6.750 0.6334 0.01212 0.00553 0.0291 0.0173 0.9190
7.000 0.6584 0.01243 0.00590 0.0291 0.0170 0.9213
7.250 0.6801 0.01302 0.00664 0.0294 0.0157 0.9241
7.500 0.7046 0.01362 0.00731 0.0292 0.0142 0.9268
7.750 0.7260 0.01451 0.00830 0.0291 0.0127 0.9291
8.000 0.7593 0.01500 0.00883 0.0269 0.0118 0.9324
8.250 0.7933 0.01596 0.00985 0.0239 0.0111 0.9363
8.500 0.8032 0.01885 0.01271 0.0236 0.0103 0.9415
8.750 0.8493 0.01842 0.01243 0.0197 0.0099 0.9439
9.000 0.8830 0.01869 0.01275 0.0176 0.0089 0.9463
9.250 0.9063 0.01997 0.01406 0.0164 0.0083 0.9501
9.500 0.9281 0.02146 0.01556 0.0153 0.0081 0.9538
9.750 0.9728 0.02461 0.01815 0.0115 0.0075 0.9545
10.000 1.0035 0.02543 0.01905 0.0093 0.0074 0.9622
10.250 1.0322 0.02632 0.01992 0.0081 0.0074 0.9736
10.500 1.0196 0.02655 0.02039 0.0138 0.0073 0.9906
10.750 1.0217 0.02685 0.02095 0.0160 0.0065 0.9955
11.000 1.0427 0.02790 0.02199 0.0158 0.0061 0.9969
11.250 1.0678 0.02903 0.02306 0.0153 0.0058 0.9976
11.500 1.0963 0.03015 0.02413 0.0143 0.0056 0.9980
11.750 1.2872 0.03766 0.03059 -0.0129 0.0051 0.9568
12.000 1.3168 0.03944 0.03239 -0.0144 0.0051 0.9590
12.250 1.3440 0.04126 0.03426 -0.0155 0.0051 0.9633
12.500 1.3680 0.04305 0.03611 -0.0160 0.0050 0.9690
12.750 1.3822 0.04452 0.03766 -0.0144 0.0050 0.9805
13.000 1.3968 0.04605 0.03928 -0.0131 0.0050 0.9861
13.250 1.4118 0.04757 0.04093 -0.0122 0.0050 0.9900
13.500 1.4250 0.04910 0.04258 -0.0111 0.0050 0.9930
13.750 1.4361 0.05070 0.04434 -0.0099 0.0050 0.9953
14.000 1.4418 0.05203 0.04587 -0.0082 0.0050 0.9978
14.250 1.4462 0.05332 0.04737 -0.0066 0.0049 0.9995
14.500 1.4379 0.05410 0.04832 -0.0024 0.0049 1.0000
14.750 1.4277 0.05513 0.04948 0.0025 0.0049 1.0000
15.000 1.3983 0.05505 0.04955 0.0106 0.0048 1.0000
15.250 1.3829 0.05600 0.05062 0.0153 0.0048 1.0000
15.500 1.3652 0.05722 0.05198 0.0195 0.0047 1.0000
15.750 1.3556 0.05909 0.05397 0.0221 0.0047 1.0000
16.000 1.3280 0.06043 0.05548 0.0258 0.0046 1.0000
16.250 1.3092 0.06267 0.05787 0.0280 0.0046 1.0000
16.500 1.2964 0.06531 0.06065 0.0293 0.0046 1.0000
16.750 1.2816 0.06817 0.06364 0.0302 0.0045 1.0000
17.000 1.2638 0.07144 0.06705 0.0307 0.0045 1.0000
17.250 1.2502 0.07483 0.07057 0.0308 0.0045 1.0000
17.500 1.2360 0.07859 0.07446 0.0304 0.0045 1.0000
17.750 1.2175 0.08279 0.07880 0.0297 0.0045 1.0000
18.000 1.1994 0.08719 0.08334 0.0285 0.0044 1.0000
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Polar data table (+)
Polar graphs
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