AG25 Bubble Dancer DLG by Mark Drela (ag25-il) Xfoil prediction polar at RE=500,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: AG25 Bubble Dancer DLG by Mark Drela (ag25-il) Reynolds number: 500,000 Max Cl/Cd: 92.08 at α=4° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ag25-il-500000.txt Download as CSV file: xf-ag25-il-500000.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 = 0.500 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.500 -0.3916 0.08240 0.08036 -0.0122 1.0000 0.0156
-8.250 -0.3914 0.07812 0.07609 -0.0137 1.0000 0.0161
-8.000 -0.3919 0.07371 0.07171 -0.0154 1.0000 0.0166
-4.750 -0.2872 0.01650 0.01151 -0.0559 0.9990 0.0143
-4.500 -0.2496 0.01408 0.00866 -0.0575 0.9970 0.0132
-4.250 -0.2125 0.01235 0.00673 -0.0595 0.9950 0.0136
-4.000 -0.1756 0.01129 0.00558 -0.0614 0.9922 0.0152
-3.750 -0.1385 0.01053 0.00474 -0.0633 0.9884 0.0174
-3.500 -0.1002 0.00983 0.00393 -0.0654 0.9852 0.0207
-3.250 -0.0606 0.00912 0.00317 -0.0679 0.9825 0.0282
-3.000 -0.0255 0.00844 0.00255 -0.0693 0.9763 0.0553
-2.750 0.0101 0.00781 0.00223 -0.0712 0.9705 0.1361
-2.500 0.0418 0.00732 0.00204 -0.0721 0.9614 0.2237
-2.250 0.0725 0.00694 0.00190 -0.0727 0.9514 0.3063
-2.000 0.1007 0.00663 0.00179 -0.0727 0.9394 0.3807
-1.750 0.1274 0.00637 0.00171 -0.0722 0.9258 0.4502
-1.500 0.1535 0.00615 0.00162 -0.0716 0.9107 0.5137
-1.250 0.1793 0.00594 0.00157 -0.0710 0.8948 0.5823
-1.000 0.2049 0.00572 0.00153 -0.0702 0.8781 0.6580
-0.750 0.2297 0.00549 0.00150 -0.0692 0.8609 0.7412
-0.500 0.2521 0.00525 0.00148 -0.0675 0.8432 0.8364
-0.250 0.2779 0.00498 0.00136 -0.0662 0.8241 1.0000
0.000 0.3053 0.00506 0.00131 -0.0659 0.8045 1.0000
0.250 0.3329 0.00515 0.00128 -0.0657 0.7838 1.0000
0.500 0.3603 0.00526 0.00126 -0.0654 0.7625 1.0000
0.750 0.3879 0.00537 0.00125 -0.0652 0.7401 1.0000
1.000 0.4154 0.00550 0.00126 -0.0650 0.7167 1.0000
1.500 0.4704 0.00579 0.00131 -0.0646 0.6665 1.0000
1.750 0.4978 0.00595 0.00136 -0.0644 0.6399 1.0000
2.000 0.5252 0.00613 0.00141 -0.0642 0.6122 1.0000
2.250 0.5525 0.00633 0.00149 -0.0641 0.5839 1.0000
2.500 0.5798 0.00653 0.00159 -0.0639 0.5551 1.0000
2.750 0.6070 0.00676 0.00169 -0.0638 0.5258 1.0000
3.000 0.6341 0.00699 0.00181 -0.0636 0.4959 1.0000
3.250 0.6613 0.00723 0.00195 -0.0635 0.4661 1.0000
3.500 0.6883 0.00749 0.00212 -0.0634 0.4364 1.0000
3.750 0.7153 0.00777 0.00228 -0.0632 0.4066 1.0000
4.000 0.7422 0.00806 0.00247 -0.0631 0.3770 1.0000
4.250 0.7689 0.00836 0.00267 -0.0630 0.3479 1.0000
4.750 0.8222 0.00902 0.00315 -0.0627 0.2899 1.0000
5.000 0.8486 0.00938 0.00341 -0.0625 0.2615 1.0000
5.250 0.8749 0.00976 0.00370 -0.0623 0.2326 1.0000
5.500 0.9011 0.01016 0.00401 -0.0622 0.2058 1.0000
5.750 0.9270 0.01060 0.00437 -0.0620 0.1780 1.0000
6.000 0.9526 0.01107 0.00474 -0.0617 0.1503 1.0000
6.250 0.9780 0.01158 0.00515 -0.0615 0.1242 1.0000
6.500 1.0031 0.01213 0.00560 -0.0612 0.0989 1.0000
6.750 1.0278 0.01274 0.00610 -0.0609 0.0753 1.0000
7.000 1.0522 0.01339 0.00665 -0.0605 0.0546 1.0000
7.250 1.0763 0.01409 0.00731 -0.0601 0.0375 1.0000
7.500 1.0996 0.01494 0.00810 -0.0595 0.0238 1.0000
7.750 1.1226 0.01588 0.00909 -0.0588 0.0166 1.0000
8.000 1.1428 0.01730 0.01064 -0.0576 0.0126 1.0000
8.250 1.1655 0.01816 0.01161 -0.0569 0.0109 1.0000
8.500 1.1875 0.01903 0.01254 -0.0562 0.0093 1.0000
8.750 1.2000 0.02153 0.01526 -0.0542 0.0080 1.0000
9.000 1.2208 0.02253 0.01640 -0.0533 0.0077 1.0000
9.250 1.2396 0.02382 0.01787 -0.0521 0.0073 1.0000
9.500 1.2569 0.02532 0.01955 -0.0508 0.0069 1.0000
9.750 1.2726 0.02699 0.02139 -0.0493 0.0065 1.0000
10.000 1.2870 0.02877 0.02336 -0.0478 0.0061 1.0000
10.250 1.2992 0.03073 0.02552 -0.0461 0.0059 1.0000
10.500 1.3088 0.03288 0.02787 -0.0443 0.0057 1.0000
10.750 1.3147 0.03531 0.03054 -0.0422 0.0056 1.0000
11.000 1.3152 0.03800 0.03349 -0.0397 0.0055 1.0000
11.250 1.3086 0.04089 0.03663 -0.0367 0.0055 1.0000
11.500 1.2976 0.04430 0.04031 -0.0343 0.0055 1.0000
11.750 1.2830 0.04847 0.04475 -0.0330 0.0056 1.0000
12.000 1.2658 0.05350 0.05005 -0.0332 0.0057 1.0000
12.250 1.2460 0.05955 0.05636 -0.0351 0.0058 1.0000
12.500 1.2242 0.06673 0.06380 -0.0387 0.0059 1.0000
12.750 1.2025 0.07476 0.07205 -0.0437 0.0060 1.0000
13.000 1.1807 0.08360 0.08108 -0.0495 0.0060 1.0000
13.250 1.1592 0.09295 0.09059 -0.0556 0.0061 1.0000
13.500 1.1361 0.10321 0.10100 -0.0621 0.0062 1.0000
13.750 1.1127 0.11393 0.11184 -0.0685 0.0063 1.0000
14.000 1.0873 0.12585 0.12387 -0.0753 0.0064 1.0000
14.250 1.0562 0.14026 0.13836 -0.0829 0.0067 1.0000
14.500 1.0125 0.16038 0.15846 -0.0923 0.0073 1.0000
|
Polar data table (+)
Polar graphs
<< Back to AG25 Bubble Dancer DLG by Mark Drela (ag25-il)