Bambino 6 (bambino6-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
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Airfoil: Bambino 6 (bambino6-il) Reynolds number: 500,000 Max Cl/Cd: 54.59 at α=8.25° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-bambino6-il-500000.txt Download as CSV file: xf-bambino6-il-500000.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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-11.750 -0.6082 0.07798 0.07589 -0.0516 1.0000 0.0139
-11.500 -0.8119 0.04284 0.04032 -0.0684 1.0000 0.0115
-11.250 -0.8682 0.03859 0.03576 -0.0590 1.0000 0.0111
-11.000 -0.8885 0.03712 0.03417 -0.0521 1.0000 0.0113
-10.750 -0.9086 0.03503 0.03188 -0.0454 1.0000 0.0112
-10.500 -0.9119 0.03406 0.03081 -0.0407 0.9999 0.0118
-10.250 -0.8971 0.03078 0.02715 -0.0409 0.9963 0.0121
-10.000 -0.8799 0.02807 0.02406 -0.0407 0.9928 0.0125
-9.750 -0.8581 0.02636 0.02207 -0.0406 0.9890 0.0129
-9.500 -0.8368 0.02398 0.01932 -0.0404 0.9854 0.0137
-9.250 -0.8099 0.02230 0.01745 -0.0411 0.9831 0.0148
-9.000 -0.7829 0.02190 0.01701 -0.0411 0.9790 0.0159
-8.750 -0.7547 0.02121 0.01622 -0.0414 0.9753 0.0171
-8.500 -0.7233 0.02045 0.01527 -0.0422 0.9727 0.0183
-8.250 -0.6947 0.01888 0.01354 -0.0428 0.9705 0.0204
-8.000 -0.6634 0.01858 0.01322 -0.0434 0.9671 0.0224
-7.750 -0.6351 0.01825 0.01279 -0.0433 0.9620 0.0246
-7.500 -0.6047 0.01743 0.01191 -0.0440 0.9592 0.0279
-7.250 -0.5690 0.01756 0.01204 -0.0455 0.9572 0.0311
-7.000 -0.5328 0.01741 0.01179 -0.0470 0.9556 0.0334
-6.750 -0.5104 0.01640 0.01067 -0.0460 0.9493 0.0363
-6.500 -0.4781 0.01643 0.01070 -0.0468 0.9457 0.0387
-6.250 -0.4426 0.01620 0.01040 -0.0482 0.9431 0.0413
-6.000 -0.4046 0.01602 0.01013 -0.0502 0.9411 0.0434
-5.750 -0.3781 0.01508 0.00909 -0.0500 0.9341 0.0460
-5.500 -0.3423 0.01482 0.00883 -0.0516 0.9296 0.0486
-5.250 -0.3017 0.01437 0.00832 -0.0543 0.9262 0.0510
-5.000 -0.2727 0.01401 0.00788 -0.0544 0.9171 0.0531
-4.750 -0.2322 0.01355 0.00733 -0.0569 0.9117 0.0548
-4.500 -0.2012 0.01286 0.00656 -0.0575 0.9018 0.0566
-4.250 -0.1672 0.01205 0.00575 -0.0589 0.8927 0.0600
-4.000 -0.1340 0.01171 0.00535 -0.0600 0.8818 0.0632
-3.750 -0.1061 0.01143 0.00500 -0.0598 0.8679 0.0662
-3.500 -0.0802 0.01129 0.00470 -0.0591 0.8391 0.0683
-3.250 -0.0590 0.01077 0.00405 -0.0575 0.8089 0.0720
-3.000 -0.0397 0.01052 0.00367 -0.0555 0.7766 0.0754
-2.750 -0.0211 0.01038 0.00339 -0.0533 0.7405 0.0785
-2.500 -0.0030 0.01033 0.00315 -0.0511 0.7049 0.0812
-2.250 0.0141 0.01030 0.00293 -0.0486 0.6731 0.0846
-2.000 0.0334 0.01022 0.00276 -0.0467 0.6525 0.0900
-1.750 0.0528 0.01018 0.00263 -0.0448 0.6326 0.0953
-1.500 0.0733 0.01012 0.00262 -0.0432 0.6176 0.1136
-1.250 0.0949 0.01013 0.00263 -0.0418 0.6028 0.1404
-1.000 0.1168 0.01017 0.00260 -0.0404 0.5872 0.1528
-0.750 0.1387 0.01018 0.00257 -0.0391 0.5726 0.1617
-0.500 0.1600 0.01018 0.00252 -0.0377 0.5557 0.1683
-0.250 0.1784 0.01025 0.00247 -0.0356 0.5218 0.1747
0.000 0.1958 0.01039 0.00242 -0.0334 0.4733 0.1809
0.250 0.1849 0.01206 0.00288 -0.0259 0.1744 0.1844
0.500 0.1995 0.01249 0.00303 -0.0233 0.0966 0.1902
0.750 0.2190 0.01263 0.00308 -0.0217 0.0685 0.1969
1.000 0.2400 0.01264 0.00312 -0.0202 0.0642 0.2089
1.250 0.2594 0.01257 0.00316 -0.0185 0.0622 0.2416
1.500 0.2693 0.01215 0.00322 -0.0149 0.0614 0.3886
1.750 0.2375 0.01074 0.00307 -0.0019 0.0612 0.7435
2.000 0.2443 0.01085 0.00339 0.0032 0.0605 0.8528
2.250 0.2581 0.01099 0.00355 0.0064 0.0599 0.8707
2.500 0.2743 0.01112 0.00372 0.0091 0.0588 0.8848
2.750 0.2955 0.01125 0.00389 0.0105 0.0573 0.8939
3.000 0.3109 0.01149 0.00417 0.0131 0.0534 0.9029
3.250 0.3359 0.01163 0.00434 0.0136 0.0501 0.9136
3.500 0.3761 0.01178 0.00449 0.0105 0.0471 0.9227
3.750 0.4090 0.01210 0.00478 0.0089 0.0418 0.9313
4.000 0.4703 0.01228 0.00486 0.0011 0.0391 0.9382
4.250 0.5053 0.01249 0.00503 -0.0009 0.0370 0.9428
4.500 0.5452 0.01277 0.00521 -0.0040 0.0329 0.9458
4.750 0.5929 0.01335 0.00568 -0.0089 0.0180 0.9498
5.000 0.6278 0.01376 0.00609 -0.0107 0.0175 0.9552
5.250 0.6531 0.01403 0.00635 -0.0105 0.0176 0.9584
5.500 0.6829 0.01434 0.00665 -0.0114 0.0177 0.9595
5.750 0.7098 0.01478 0.00717 -0.0118 0.0168 0.9610
6.000 0.7339 0.01508 0.00748 -0.0115 0.0169 0.9624
6.250 0.7591 0.01534 0.00774 -0.0114 0.0173 0.9643
6.500 0.7822 0.01552 0.00791 -0.0110 0.0179 0.9664
6.750 0.7989 0.01579 0.00820 -0.0092 0.0183 0.9697
7.000 0.8209 0.01620 0.00864 -0.0086 0.0189 0.9719
7.250 0.8496 0.01650 0.00897 -0.0095 0.0196 0.9737
7.500 0.8746 0.01681 0.00922 -0.0096 0.0226 0.9757
7.750 0.8841 0.01785 0.01024 -0.0070 0.0229 0.9801
8.000 0.9204 0.01733 0.00972 -0.0090 0.0219 0.9820
8.250 0.9493 0.01739 0.00983 -0.0098 0.0211 0.9841
8.500 0.9731 0.01823 0.01086 -0.0102 0.0200 0.9868
8.750 0.9913 0.01915 0.01194 -0.0095 0.0191 0.9902
9.000 1.0071 0.01998 0.01287 -0.0084 0.0183 0.9931
9.250 1.0215 0.02118 0.01424 -0.0074 0.0172 0.9958
9.500 1.0313 0.02294 0.01604 -0.0063 0.0165 0.9987
9.750 1.0250 0.02447 0.01759 -0.0023 0.0154 1.0000
10.000 1.0221 0.02534 0.01850 0.0021 0.0146 1.0000
10.250 1.0243 0.02632 0.01950 0.0051 0.0146 1.0000
10.500 1.0192 0.02812 0.02127 0.0089 0.0140 1.0000
10.750 1.0314 0.03035 0.02318 0.0105 0.0129 1.0000
11.000 1.0301 0.03110 0.02417 0.0134 0.0124 1.0000
11.250 1.0390 0.03219 0.02532 0.0151 0.0117 1.0000
11.500 1.0528 0.03335 0.02643 0.0162 0.0114 1.0000
11.750 1.2179 0.03653 0.02882 -0.0037 0.0100 1.0000
12.000 1.2040 0.03683 0.02925 0.0027 0.0100 1.0000
12.250 1.1828 0.03718 0.02979 0.0096 0.0098 1.0000
12.500 1.1727 0.03796 0.03073 0.0140 0.0096 1.0000
12.750 1.1715 0.03900 0.03190 0.0168 0.0094 1.0000
13.000 1.1810 0.04021 0.03319 0.0182 0.0092 1.0000
13.250 1.5147 0.05753 0.04916 -0.0339 0.0075 0.9994
13.500 1.5233 0.05920 0.05097 -0.0316 0.0075 1.0000
13.750 1.5266 0.06070 0.05264 -0.0283 0.0075 1.0000
14.000 1.5279 0.06219 0.05431 -0.0248 0.0075 1.0000
14.250 1.5295 0.06374 0.05603 -0.0216 0.0075 1.0000
14.500 1.5279 0.06521 0.05771 -0.0179 0.0075 1.0000
14.750 1.5150 0.06602 0.05878 -0.0127 0.0075 1.0000
15.000 1.5068 0.06758 0.06055 -0.0084 0.0074 1.0000
15.250 1.4930 0.06865 0.06184 -0.0035 0.0074 1.0000
15.500 1.4712 0.06939 0.06281 0.0024 0.0074 1.0000
15.750 1.4600 0.07101 0.06458 0.0065 0.0074 1.0000
16.000 1.4352 0.07187 0.06561 0.0128 0.0074 1.0000
16.250 1.4110 0.07300 0.06690 0.0181 0.0074 1.0000
16.500 1.3876 0.07444 0.06850 0.0223 0.0073 1.0000
16.750 1.3709 0.07656 0.07077 0.0251 0.0073 1.0000
17.000 1.3518 0.07897 0.07333 0.0275 0.0073 1.0000
17.250 1.3275 0.08119 0.07571 0.0296 0.0073 1.0000
17.500 1.3107 0.08418 0.07885 0.0306 0.0073 1.0000
17.750 1.2818 0.08717 0.08202 0.0315 0.0073 1.0000
18.000 1.2672 0.09085 0.08583 0.0316 0.0073 1.0000
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Polar data table (+)
Polar graphs
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