AG25 Bubble Dancer DLG by Mark Drela (ag25-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: AG25 Bubble Dancer DLG by Mark Drela (ag25-il) Reynolds number: 1,000,000 Max Cl/Cd: 106.51 at α=4° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ag25-il-1000000.txt Download as CSV file: xf-ag25-il-1000000.csv |
XFOIL Version 6.96
Calculated polar for: AG25 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 = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.750 -0.3969 0.08303 0.08155 -0.0112 1.0000 0.0077
-8.500 -0.3977 0.07825 0.07679 -0.0127 1.0000 0.0077
-8.250 -0.4150 0.07019 0.06876 -0.0154 1.0000 0.0080
-8.000 -0.4195 0.06511 0.06370 -0.0174 1.0000 0.0081
-7.750 -0.4245 0.06006 0.05868 -0.0198 1.0000 0.0082
-7.500 -0.4304 0.05475 0.05340 -0.0231 1.0000 0.0082
-7.250 -0.4306 0.04755 0.04620 -0.0311 1.0000 0.0083
-7.000 -0.4294 0.03646 0.03503 -0.0435 1.0000 0.0082
-6.750 -0.4314 0.02573 0.02405 -0.0497 1.0000 0.0082
-6.500 -0.4262 0.02054 0.01861 -0.0514 0.9997 0.0085
-5.500 -0.3312 0.01725 0.01345 -0.0617 0.9954 0.0076
-5.250 -0.2965 0.01435 0.01012 -0.0638 0.9937 0.0079
-5.000 -0.2634 0.01211 0.00757 -0.0653 0.9908 0.0080
-4.750 -0.2289 0.01083 0.00614 -0.0667 0.9879 0.0080
-4.500 -0.1946 0.00947 0.00460 -0.0682 0.9844 0.0082
-4.250 -0.1614 0.00859 0.00361 -0.0693 0.9795 0.0092
-4.000 -0.1304 0.00821 0.00320 -0.0699 0.9719 0.0108
-3.750 -0.1008 0.00790 0.00283 -0.0701 0.9629 0.0120
-3.500 -0.0725 0.00740 0.00221 -0.0699 0.9525 0.0151
-3.250 -0.0458 0.00720 0.00199 -0.0694 0.9403 0.0192
-3.000 -0.0191 0.00684 0.00164 -0.0689 0.9266 0.0369
-2.750 0.0075 0.00657 0.00144 -0.0686 0.9122 0.0693
-2.500 0.0344 0.00628 0.00127 -0.0683 0.8970 0.1183
-2.250 0.0615 0.00602 0.00114 -0.0681 0.8808 0.1734
-2.000 0.0888 0.00578 0.00104 -0.0680 0.8640 0.2365
-1.750 0.1161 0.00559 0.00096 -0.0678 0.8469 0.2989
-1.500 0.1436 0.00543 0.00090 -0.0677 0.8292 0.3586
-1.250 0.1713 0.00529 0.00085 -0.0677 0.8105 0.4156
-1.000 0.1990 0.00520 0.00082 -0.0675 0.7913 0.4664
-0.750 0.2267 0.00511 0.00080 -0.0675 0.7717 0.5238
-0.500 0.2544 0.00501 0.00079 -0.0674 0.7508 0.5845
-0.250 0.2820 0.00492 0.00079 -0.0672 0.7298 0.6477
0.000 0.3092 0.00481 0.00082 -0.0670 0.7080 0.7208
0.250 0.3354 0.00467 0.00085 -0.0665 0.6852 0.8061
0.500 0.3575 0.00448 0.00087 -0.0649 0.6623 0.9091
0.750 0.3864 0.00447 0.00084 -0.0649 0.6374 1.0000
1.000 0.4144 0.00461 0.00086 -0.0649 0.6118 1.0000
1.250 0.4424 0.00476 0.00089 -0.0649 0.5852 1.0000
1.500 0.4704 0.00492 0.00094 -0.0648 0.5589 1.0000
1.750 0.4983 0.00509 0.00099 -0.0648 0.5321 1.0000
2.000 0.5261 0.00526 0.00105 -0.0648 0.5050 1.0000
2.250 0.5539 0.00545 0.00113 -0.0648 0.4781 1.0000
2.500 0.5816 0.00564 0.00122 -0.0648 0.4510 1.0000
2.750 0.6093 0.00585 0.00132 -0.0647 0.4241 1.0000
3.000 0.6369 0.00606 0.00143 -0.0647 0.3975 1.0000
3.250 0.6644 0.00628 0.00154 -0.0647 0.3714 1.0000
3.500 0.6919 0.00652 0.00169 -0.0646 0.3446 1.0000
3.750 0.7193 0.00676 0.00183 -0.0646 0.3189 1.0000
4.000 0.7466 0.00701 0.00198 -0.0645 0.2931 1.0000
4.250 0.7738 0.00727 0.00215 -0.0645 0.2676 1.0000
4.500 0.8009 0.00755 0.00235 -0.0644 0.2430 1.0000
4.750 0.8278 0.00785 0.00256 -0.0643 0.2171 1.0000
5.000 0.8546 0.00816 0.00278 -0.0642 0.1944 1.0000
5.250 0.8812 0.00850 0.00301 -0.0641 0.1698 1.0000
5.500 0.9077 0.00887 0.00328 -0.0639 0.1446 1.0000
5.750 0.9340 0.00924 0.00358 -0.0638 0.1227 1.0000
6.000 0.9600 0.00967 0.00390 -0.0636 0.0995 1.0000
6.250 0.9857 0.01015 0.00425 -0.0634 0.0769 1.0000
6.500 1.0115 0.01059 0.00462 -0.0632 0.0588 1.0000
6.750 1.0369 0.01109 0.00503 -0.0629 0.0433 1.0000
7.000 1.0623 0.01158 0.00547 -0.0626 0.0307 1.0000
7.250 1.0875 0.01212 0.00598 -0.0623 0.0203 1.0000
7.500 1.1121 0.01274 0.00657 -0.0619 0.0128 1.0000
7.750 1.1359 0.01354 0.00740 -0.0613 0.0080 1.0000
8.000 1.1611 0.01398 0.00789 -0.0609 0.0069 1.0000
8.250 1.1853 0.01460 0.00856 -0.0604 0.0058 1.0000
8.500 1.2060 0.01590 0.01003 -0.0594 0.0048 1.0000
8.750 1.2295 0.01657 0.01078 -0.0588 0.0046 1.0000
9.000 1.2526 0.01726 0.01159 -0.0582 0.0043 1.0000
9.250 1.2750 0.01805 0.01247 -0.0575 0.0040 1.0000
9.500 1.2967 0.01889 0.01340 -0.0568 0.0036 1.0000
9.750 1.3177 0.01978 0.01438 -0.0560 0.0034 1.0000
10.000 1.3372 0.02085 0.01555 -0.0550 0.0031 1.0000
10.250 1.3524 0.02247 0.01734 -0.0535 0.0029 1.0000
10.500 1.3619 0.02479 0.01990 -0.0514 0.0028 1.0000
10.750 1.3678 0.02744 0.02280 -0.0489 0.0027 1.0000
11.000 1.3712 0.03018 0.02580 -0.0464 0.0027 1.0000
11.250 1.3729 0.03280 0.02865 -0.0438 0.0027 1.0000
11.500 1.3693 0.03524 0.03129 -0.0407 0.0027 1.0000
11.750 1.3627 0.03779 0.03403 -0.0378 0.0027 1.0000
12.000 1.3550 0.04069 0.03711 -0.0359 0.0027 1.0000
12.250 1.3460 0.04414 0.04075 -0.0351 0.0027 1.0000
12.500 1.3364 0.04811 0.04491 -0.0354 0.0027 1.0000
12.750 1.3255 0.05279 0.04978 -0.0368 0.0027 1.0000
13.000 1.3146 0.05802 0.05517 -0.0391 0.0027 1.0000
13.250 1.3009 0.06420 0.06152 -0.0425 0.0027 1.0000
13.500 1.2892 0.07053 0.06799 -0.0463 0.0027 1.0000
13.750 1.2748 0.07765 0.07525 -0.0506 0.0027 1.0000
14.000 1.2588 0.08537 0.08311 -0.0551 0.0027 1.0000
14.250 1.2432 0.09312 0.09097 -0.0595 0.0028 1.0000
14.500 1.2265 0.10127 0.09923 -0.0640 0.0028 1.0000
14.750 1.2090 0.10980 0.10786 -0.0686 0.0028 1.0000
15.000 1.1923 0.11835 0.11649 -0.0731 0.0028 1.0000
15.250 1.1762 0.12707 0.12530 -0.0776 0.0028 1.0000
15.500 1.1599 0.13605 0.13436 -0.0823 0.0029 1.0000
15.750 1.1417 0.14591 0.14431 -0.0873 0.0029 1.0000
16.000 1.1173 0.15827 0.15678 -0.0937 0.0030 1.0000
|
Polar data table (+)
Polar graphs
<< Back to AG25 Bubble Dancer DLG by Mark Drela (ag25-il)