AG26 Bubble Dancer DLG by Mark Drela (ag26-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: AG26 Bubble Dancer DLG by Mark Drela (ag26-il) Reynolds number: 1,000,000 Max Cl/Cd: 95.97 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ag26-il-1000000-n5.txt Download as CSV file: xf-ag26-il-1000000-n5.csv |
XFOIL Version 6.96
Calculated polar for: AG26 Bubble Dancer DLG by Mark Drela
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
------ -------- --------- --------- -------- -------- --------
-10.750 -0.5479 0.13046 0.12880 0.0197 1.0000 0.0044
-10.500 -0.5439 0.12719 0.12554 0.0187 1.0000 0.0038
-10.250 -0.5397 0.12323 0.12159 0.0172 1.0000 0.0035
-10.000 -0.5363 0.11902 0.11739 0.0155 1.0000 0.0032
-9.750 -0.5340 0.11433 0.11271 0.0137 1.0000 0.0030
-9.500 -0.5357 0.10830 0.10669 0.0113 1.0000 0.0027
-9.250 -0.5336 0.10378 0.10219 0.0093 1.0000 0.0027
-9.000 -0.5307 0.09958 0.09800 0.0073 1.0000 0.0027
-8.750 -0.5275 0.09549 0.09392 0.0051 1.0000 0.0027
-8.500 -0.5244 0.09139 0.08984 0.0028 1.0000 0.0028
-8.250 -0.5207 0.08747 0.08594 0.0005 1.0000 0.0028
-8.000 -0.5175 0.08338 0.08186 -0.0023 1.0000 0.0029
-7.750 -0.5133 0.07896 0.07746 -0.0061 1.0000 0.0030
-7.500 -0.5034 0.07355 0.07206 -0.0125 1.0000 0.0031
-7.250 -0.4900 0.06701 0.06552 -0.0211 1.0000 0.0033
-7.000 -0.4720 0.05849 0.05696 -0.0325 1.0000 0.0035
-6.750 -0.4590 0.02107 0.01810 -0.0602 1.0000 0.0036
-6.500 -0.4325 0.01715 0.01362 -0.0616 0.9984 0.0037
-6.250 -0.4005 0.01523 0.01137 -0.0632 0.9951 0.0039
-6.000 -0.3692 0.01400 0.00992 -0.0643 0.9907 0.0041
-5.750 -0.3374 0.01285 0.00857 -0.0654 0.9854 0.0042
-5.500 -0.3057 0.01167 0.00716 -0.0665 0.9794 0.0043
-5.250 -0.2747 0.01070 0.00602 -0.0672 0.9712 0.0044
-5.000 -0.2449 0.00996 0.00512 -0.0676 0.9607 0.0045
-4.750 -0.2163 0.00940 0.00444 -0.0677 0.9473 0.0045
-4.500 -0.1890 0.00870 0.00357 -0.0674 0.9316 0.0049
-4.250 -0.1623 0.00827 0.00302 -0.0670 0.9147 0.0055
-4.000 -0.1356 0.00804 0.00271 -0.0666 0.8971 0.0062
-3.750 -0.1086 0.00784 0.00240 -0.0662 0.8787 0.0069
-3.500 -0.0814 0.00768 0.00213 -0.0659 0.8597 0.0075
-3.250 -0.0539 0.00748 0.00183 -0.0657 0.8404 0.0090
-3.000 -0.0265 0.00736 0.00163 -0.0654 0.8199 0.0116
-2.750 0.0012 0.00723 0.00144 -0.0653 0.7988 0.0168
-2.500 0.0289 0.00714 0.00127 -0.0651 0.7772 0.0242
-2.250 0.0567 0.00704 0.00114 -0.0650 0.7554 0.0363
-2.000 0.0845 0.00694 0.00102 -0.0649 0.7333 0.0580
-1.750 0.1124 0.00681 0.00092 -0.0649 0.7112 0.0891
-1.500 0.1403 0.00672 0.00083 -0.0649 0.6898 0.1228
-1.000 0.1963 0.00651 0.00071 -0.0650 0.6446 0.2122
-0.750 0.2242 0.00642 0.00068 -0.0650 0.6220 0.2646
-0.500 0.2522 0.00636 0.00066 -0.0651 0.5993 0.3138
-0.250 0.2801 0.00632 0.00066 -0.0651 0.5773 0.3596
0.000 0.3080 0.00630 0.00067 -0.0651 0.5539 0.4050
0.250 0.3360 0.00628 0.00069 -0.0651 0.5313 0.4501
0.500 0.3639 0.00628 0.00073 -0.0651 0.5081 0.4971
0.750 0.3917 0.00627 0.00077 -0.0651 0.4846 0.5531
1.000 0.4193 0.00620 0.00083 -0.0652 0.4597 0.6298
1.250 0.4462 0.00607 0.00091 -0.0650 0.4334 0.7390
1.500 0.4671 0.00572 0.00099 -0.0632 0.4078 0.9186
1.750 0.4967 0.00584 0.00103 -0.0636 0.3776 1.0000
2.000 0.5243 0.00606 0.00111 -0.0635 0.3484 1.0000
2.250 0.5520 0.00626 0.00120 -0.0635 0.3218 1.0000
2.500 0.5796 0.00648 0.00130 -0.0634 0.2967 1.0000
2.750 0.6072 0.00668 0.00142 -0.0634 0.2753 1.0000
3.000 0.6347 0.00691 0.00154 -0.0633 0.2517 1.0000
3.250 0.6622 0.00710 0.00166 -0.0633 0.2334 1.0000
3.500 0.6896 0.00733 0.00180 -0.0632 0.2133 1.0000
3.750 0.7170 0.00757 0.00197 -0.0632 0.1933 1.0000
4.000 0.7443 0.00779 0.00213 -0.0631 0.1770 1.0000
4.500 0.7985 0.00832 0.00250 -0.0629 0.1396 1.0000
4.750 0.8254 0.00862 0.00274 -0.0628 0.1201 1.0000
5.000 0.8522 0.00892 0.00297 -0.0626 0.1043 1.0000
5.250 0.8789 0.00923 0.00321 -0.0625 0.0895 1.0000
5.500 0.9057 0.00953 0.00347 -0.0624 0.0775 1.0000
5.750 0.9323 0.00984 0.00374 -0.0622 0.0661 1.0000
6.000 0.9587 0.01017 0.00405 -0.0620 0.0552 1.0000
6.250 0.9850 0.01052 0.00436 -0.0618 0.0450 1.0000
6.500 1.0111 0.01089 0.00470 -0.0616 0.0358 1.0000
6.750 1.0370 0.01129 0.00506 -0.0614 0.0276 1.0000
7.000 1.0627 0.01173 0.00546 -0.0611 0.0201 1.0000
7.250 1.0883 0.01216 0.00588 -0.0609 0.0153 1.0000
7.500 1.1139 0.01258 0.00633 -0.0606 0.0116 1.0000
7.750 1.1389 0.01309 0.00684 -0.0602 0.0080 1.0000
8.000 1.1640 0.01355 0.00732 -0.0599 0.0063 1.0000
8.250 1.1887 0.01409 0.00788 -0.0595 0.0047 1.0000
8.500 1.2136 0.01455 0.00841 -0.0592 0.0042 1.0000
8.750 1.2380 0.01508 0.00898 -0.0587 0.0036 1.0000
9.000 1.2619 0.01569 0.00964 -0.0583 0.0030 1.0000
9.250 1.2850 0.01642 0.01049 -0.0577 0.0026 1.0000
9.500 1.3086 0.01700 0.01115 -0.0572 0.0025 1.0000
9.750 1.3317 0.01764 0.01188 -0.0566 0.0023 1.0000
10.000 1.3544 0.01834 0.01266 -0.0560 0.0021 1.0000
10.250 1.3765 0.01907 0.01348 -0.0554 0.0019 1.0000
10.500 1.3980 0.01985 0.01436 -0.0547 0.0018 1.0000
10.750 1.4187 0.02071 0.01530 -0.0539 0.0017 1.0000
11.000 1.4383 0.02168 0.01638 -0.0530 0.0015 1.0000
11.250 1.4559 0.02288 0.01774 -0.0519 0.0014 1.0000
11.500 1.4695 0.02454 0.01960 -0.0504 0.0013 1.0000
11.750 1.4807 0.02635 0.02161 -0.0487 0.0012 1.0000
12.000 1.4941 0.02771 0.02311 -0.0473 0.0012 1.0000
12.250 1.5053 0.02919 0.02474 -0.0457 0.0012 1.0000
12.500 1.5134 0.03082 0.02654 -0.0438 0.0012 1.0000
12.750 1.5158 0.03254 0.02842 -0.0413 0.0012 1.0000
13.000 1.5132 0.03453 0.03057 -0.0386 0.0012 1.0000
13.250 1.5086 0.03696 0.03316 -0.0367 0.0012 1.0000
13.500 1.5020 0.03997 0.03634 -0.0358 0.0011 1.0000
13.750 1.4931 0.04376 0.04031 -0.0360 0.0011 1.0000
14.000 1.4827 0.04836 0.04508 -0.0374 0.0011 1.0000
14.250 1.4697 0.05394 0.05084 -0.0400 0.0011 1.0000
14.500 1.4537 0.06067 0.05775 -0.0438 0.0011 1.0000
14.750 1.4320 0.06897 0.06623 -0.0486 0.0011 1.0000
15.000 1.4057 0.07856 0.07599 -0.0542 0.0011 1.0000
15.250 1.3764 0.08890 0.08648 -0.0597 0.0012 1.0000
15.500 1.3429 0.10012 0.09784 -0.0654 0.0012 1.0000
15.750 1.3097 0.11134 0.10918 -0.0708 0.0012 1.0000
|
Polar data table (+)
Polar graphs
<< Back to AG26 Bubble Dancer DLG by Mark Drela (ag26-il)