Bambino 6 (bambino6-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: Bambino 6 (bambino6-il) Reynolds number: 1,000,000 Max Cl/Cd: 53.05 at α=12° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-bambino6-il-1000000-n5.txt Download as CSV file: xf-bambino6-il-1000000-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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-13.500 -0.6583 0.09240 0.09044 -0.0458 1.0000 0.0028
-13.250 -0.9562 0.04569 0.04328 -0.0722 1.0000 0.0022
-13.000 -1.0051 0.03770 0.03497 -0.0674 1.0000 0.0021
-12.750 -1.0101 0.03464 0.03170 -0.0650 0.9988 0.0021
-12.500 -1.0089 0.03126 0.02805 -0.0637 0.9956 0.0021
-12.250 -1.0007 0.02865 0.02522 -0.0624 0.9925 0.0023
-12.000 -0.9877 0.02656 0.02292 -0.0613 0.9893 0.0023
-11.750 -0.9706 0.02480 0.02098 -0.0607 0.9870 0.0024
-11.500 -0.9508 0.02345 0.01950 -0.0601 0.9849 0.0026
-11.250 -0.9340 0.02245 0.01839 -0.0585 0.9806 0.0026
-11.000 -0.9132 0.02123 0.01701 -0.0578 0.9775 0.0027
-10.500 -0.8715 0.01941 0.01496 -0.0557 0.9683 0.0029
-10.250 -0.8481 0.01848 0.01389 -0.0552 0.9647 0.0030
-10.000 -0.8244 0.01778 0.01309 -0.0545 0.9605 0.0032
-9.750 -0.8005 0.01706 0.01227 -0.0539 0.9549 0.0032
-9.500 -0.7705 0.01632 0.01142 -0.0545 0.9509 0.0035
-9.250 -0.7393 0.01565 0.01066 -0.0554 0.9451 0.0038
-9.000 -0.7041 0.01477 0.00966 -0.0572 0.9391 0.0042
-8.750 -0.6632 0.01403 0.00883 -0.0602 0.9346 0.0046
-8.500 -0.6257 0.01345 0.00816 -0.0624 0.9267 0.0050
-8.250 -0.5859 0.01291 0.00751 -0.0651 0.9177 0.0054
-8.000 -0.5489 0.01240 0.00688 -0.0672 0.9036 0.0060
-7.750 -0.5194 0.01189 0.00626 -0.0675 0.8898 0.0073
-7.500 -0.4928 0.01157 0.00585 -0.0672 0.8756 0.0081
-7.250 -0.4686 0.01119 0.00539 -0.0664 0.8609 0.0111
-7.000 -0.4454 0.01085 0.00501 -0.0654 0.8481 0.0154
-6.750 -0.4225 0.01053 0.00473 -0.0643 0.8356 0.0253
-6.500 -0.3992 0.01038 0.00454 -0.0632 0.8230 0.0293
-6.250 -0.3761 0.01027 0.00435 -0.0621 0.8111 0.0306
-6.000 -0.3534 0.01017 0.00417 -0.0608 0.7967 0.0313
-5.750 -0.3308 0.01005 0.00397 -0.0596 0.7818 0.0325
-5.500 -0.3086 0.00991 0.00376 -0.0582 0.7634 0.0347
-5.250 -0.2878 0.00985 0.00362 -0.0566 0.7373 0.0368
-4.500 -0.2336 0.01007 0.00328 -0.0499 0.6087 0.0412
-4.250 -0.2104 0.00999 0.00313 -0.0488 0.5976 0.0419
-4.000 -0.1876 0.00989 0.00296 -0.0476 0.5846 0.0443
-3.750 -0.1630 0.00978 0.00286 -0.0468 0.5800 0.0475
-3.500 -0.1396 0.00973 0.00277 -0.0458 0.5677 0.0502
-3.250 -0.1163 0.00971 0.00269 -0.0447 0.5517 0.0524
-3.000 -0.0934 0.00971 0.00259 -0.0436 0.5308 0.0535
-2.750 -0.0712 0.00969 0.00247 -0.0423 0.5083 0.0555
-2.500 -0.0519 0.00980 0.00239 -0.0405 0.4568 0.0579
-2.250 -0.0569 0.01129 0.00274 -0.0340 0.1090 0.0590
-2.000 -0.0350 0.01137 0.00270 -0.0327 0.0665 0.0612
-1.500 0.0121 0.01136 0.00262 -0.0308 0.0542 0.0645
-1.250 0.0358 0.01136 0.00260 -0.0299 0.0532 0.0657
-1.000 0.0595 0.01137 0.00259 -0.0289 0.0519 0.0665
-0.750 0.0831 0.01138 0.00259 -0.0280 0.0510 0.0670
-0.500 0.1061 0.01136 0.00256 -0.0270 0.0504 0.0691
-0.250 0.1290 0.01137 0.00255 -0.0259 0.0490 0.0711
0.000 0.1517 0.01138 0.00256 -0.0248 0.0478 0.0736
0.250 0.1742 0.01141 0.00260 -0.0237 0.0462 0.0764
0.500 0.1965 0.01147 0.00267 -0.0225 0.0448 0.0782
0.750 0.2195 0.01151 0.00270 -0.0215 0.0446 0.0792
1.250 0.2647 0.01158 0.00278 -0.0194 0.0441 0.0875
1.500 0.2862 0.01150 0.00280 -0.0182 0.0428 0.1275
1.750 0.3091 0.01153 0.00284 -0.0172 0.0413 0.1349
2.000 0.3317 0.01158 0.00287 -0.0163 0.0394 0.1406
2.250 0.3541 0.01166 0.00291 -0.0152 0.0373 0.1437
2.500 0.3743 0.01183 0.00299 -0.0138 0.0234 0.1460
2.750 0.3956 0.01192 0.00310 -0.0126 0.0145 0.1497
3.000 0.4170 0.01200 0.00320 -0.0113 0.0133 0.1539
3.250 0.4383 0.01210 0.00332 -0.0101 0.0119 0.1572
3.500 0.4592 0.01222 0.00346 -0.0088 0.0105 0.1589
3.750 0.4795 0.01233 0.00361 -0.0074 0.0101 0.1639
4.000 0.4994 0.01244 0.00377 -0.0059 0.0093 0.1700
4.250 0.5191 0.01258 0.00393 -0.0044 0.0083 0.1738
4.500 0.5368 0.01272 0.00416 -0.0025 0.0076 0.1890
4.750 0.5349 0.01226 0.00437 0.0036 0.0073 0.4491
5.000 0.5109 0.01120 0.00436 0.0149 0.0072 0.8059
5.250 0.5232 0.01142 0.00468 0.0181 0.0069 0.8378
5.500 0.5390 0.01168 0.00498 0.0204 0.0064 0.8464
5.750 0.5560 0.01195 0.00528 0.0223 0.0057 0.8512
6.000 0.5711 0.01223 0.00562 0.0247 0.0050 0.8583
6.250 0.5891 0.01253 0.00595 0.0263 0.0046 0.8596
6.500 0.6037 0.01289 0.00635 0.0287 0.0045 0.8638
6.750 0.6200 0.01320 0.00672 0.0306 0.0039 0.8684
7.000 0.6369 0.01356 0.00712 0.0323 0.0037 0.8706
7.250 0.6512 0.01391 0.00749 0.0346 0.0039 0.8760
7.500 0.6662 0.01437 0.00796 0.0365 0.0040 0.8776
7.750 0.6808 0.01490 0.00854 0.0384 0.0038 0.8796
8.000 0.6955 0.01552 0.00921 0.0400 0.0034 0.8810
8.250 0.7136 0.01596 0.00967 0.0412 0.0032 0.8826
8.500 0.7251 0.01678 0.01056 0.0432 0.0036 0.8845
8.750 0.7426 0.01730 0.01109 0.0442 0.0030 0.8849
9.000 0.7564 0.01803 0.01186 0.0457 0.0027 0.8874
9.250 0.7679 0.01897 0.01283 0.0473 0.0032 0.8881
9.500 0.7830 0.01963 0.01353 0.0485 0.0025 0.8906
10.000 0.8095 0.02159 0.01557 0.0504 0.0024 0.8947
10.250 0.8253 0.02266 0.01668 0.0506 0.0023 0.8973
10.500 0.8388 0.02386 0.01789 0.0511 0.0024 0.8987
10.750 0.8539 0.02502 0.01906 0.0516 0.0026 0.8999
11.000 0.8682 0.02620 0.02027 0.0519 0.0023 0.9005
11.250 0.8883 0.02722 0.02121 0.0522 0.0026 0.9013
11.500 0.9076 0.02822 0.02220 0.0523 0.0025 0.9018
11.750 0.9374 0.02911 0.02302 0.0515 0.0027 0.9053
12.000 0.8652 0.01631 0.01061 0.0584 0.0029 0.9080
12.500 1.1547 0.03674 0.02998 0.0298 0.0034 0.9040
13.000 1.1977 0.03991 0.03328 0.0296 0.0034 0.9058
13.500 1.2044 0.04133 0.03503 0.0351 0.0033 0.9117
13.750 1.1821 0.03993 0.03393 0.0402 0.0026 0.9192
14.000 1.2044 0.04193 0.03605 0.0391 0.0029 0.9213
14.250 1.2223 0.04376 0.03803 0.0376 0.0026 0.9284
14.500 1.2406 0.04616 0.04058 0.0358 0.0024 0.9335
14.750 1.2548 0.04849 0.04307 0.0343 0.0025 0.9382
15.000 1.2656 0.05120 0.04597 0.0329 0.0024 0.9435
15.250 1.2761 0.05416 0.04905 0.0313 0.0023 0.9480
15.500 1.2842 0.05716 0.05218 0.0298 0.0023 0.9543
15.750 1.2900 0.06060 0.05576 0.0287 0.0022 0.9724
16.000 1.2663 0.06205 0.05733 0.0332 0.0023 0.9920
16.250 1.2603 0.06536 0.06076 0.0340 0.0022 0.9937
16.500 1.2494 0.06793 0.06343 0.0359 0.0022 0.9967
16.750 1.2348 0.07122 0.06686 0.0360 0.0022 0.9978
17.000 1.2565 0.07555 0.07121 0.0349 0.0022 0.9982
17.250 1.2358 0.07898 0.07480 0.0344 0.0022 0.9989
17.500 1.2146 0.08621 0.08223 0.0334 0.0021 0.9993
17.750 1.1807 0.08787 0.08408 0.0308 0.0022 0.9998
18.000 1.1843 0.09219 0.08846 0.0296 0.0022 1.0000
18.250 1.1574 0.09699 0.09341 0.0275 0.0022 1.0000
18.500 1.1300 0.10260 0.09919 0.0248 0.0022 1.0000
18.750 1.1384 0.10646 0.10306 0.0248 0.0022 1.0000
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Polar data table (+)
Polar graphs
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