AG24 Bubble Dancer DLG by Mark Drela (ag24-il) Xfoil prediction polar at RE=50,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: AG24 Bubble Dancer DLG by Mark Drela (ag24-il) Reynolds number: 50,000 Max Cl/Cd: 34.73 at α=6° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ag24-il-50000.txt Download as CSV file: xf-ag24-il-50000.csv |
XFOIL Version 6.96
Calculated polar for: AG24 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 = 0.050 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-8.000 -0.4682 0.10178 0.09524 0.0012 1.0000 0.2447
-7.750 -0.4687 0.09888 0.09243 0.0003 1.0000 0.2558
-7.500 -0.4812 0.09760 0.09129 -0.0019 1.0000 0.2670
-7.250 -0.4593 0.09246 0.08609 0.0004 1.0000 0.2839
-6.750 -0.4485 0.08598 0.07973 0.0011 1.0000 0.3130
-6.500 -0.4441 0.08278 0.07661 0.0011 1.0000 0.3269
-6.250 -0.4380 0.07946 0.07336 0.0010 1.0000 0.3413
-6.000 -0.4317 0.07614 0.07010 0.0009 1.0000 0.3558
-5.750 -0.4257 0.07281 0.06684 0.0006 1.0000 0.3699
-5.500 -0.4000 0.04763 0.04034 -0.0501 1.0000 0.1263
-5.250 -0.3767 0.04139 0.03327 -0.0533 1.0000 0.1152
-5.000 -0.3533 0.03733 0.02871 -0.0538 1.0000 0.1126
-4.750 -0.3280 0.03363 0.02443 -0.0542 1.0000 0.1125
-4.500 -0.3041 0.03092 0.02152 -0.0540 1.0000 0.1202
-4.250 -0.2764 0.02832 0.01822 -0.0538 1.0000 0.1278
-4.000 -0.2508 0.02597 0.01577 -0.0532 1.0000 0.1388
-3.750 -0.2257 0.02413 0.01392 -0.0525 1.0000 0.1634
-3.500 -0.2002 0.02225 0.01214 -0.0516 1.0000 0.2026
-3.250 -0.1753 0.02033 0.01073 -0.0507 1.0000 0.3021
-3.000 -0.1542 0.01878 0.01015 -0.0486 1.0000 0.4806
-2.750 -0.1393 0.01805 0.00998 -0.0445 1.0000 0.6111
-2.500 -0.1289 0.01750 0.00978 -0.0391 1.0000 0.7169
-2.250 -0.1248 0.01690 0.00946 -0.0322 1.0000 0.8165
-2.000 -0.0894 0.01589 0.00838 -0.0326 1.0000 1.0000
-1.750 -0.0566 0.01578 0.00765 -0.0364 1.0000 1.0000
-1.500 -0.0281 0.01587 0.00730 -0.0380 1.0000 1.0000
-1.250 -0.0015 0.01603 0.00712 -0.0389 1.0000 1.0000
-1.000 0.0241 0.01624 0.00704 -0.0395 1.0000 1.0000
-0.750 0.0491 0.01650 0.00703 -0.0400 1.0000 1.0000
-0.500 0.0734 0.01681 0.00713 -0.0405 1.0000 1.0000
-0.250 0.0973 0.01717 0.00732 -0.0409 1.0000 1.0000
0.000 0.1207 0.01759 0.00760 -0.0414 1.0000 1.0000
0.250 0.1436 0.01808 0.00795 -0.0418 1.0000 1.0000
0.500 0.1658 0.01864 0.00841 -0.0424 1.0000 1.0000
0.750 0.1875 0.01928 0.00897 -0.0430 1.0000 1.0000
1.000 0.2085 0.02000 0.00965 -0.0436 1.0000 1.0000
1.250 0.2288 0.02083 0.01044 -0.0444 1.0000 1.0000
1.500 0.2740 0.02186 0.01145 -0.0497 0.9876 1.0000
1.750 0.3383 0.02287 0.01249 -0.0580 0.9644 1.0000
2.000 0.4017 0.02365 0.01337 -0.0655 0.9407 1.0000
2.250 0.4558 0.02420 0.01402 -0.0708 0.9148 1.0000
2.500 0.5071 0.02456 0.01452 -0.0750 0.8887 1.0000
2.750 0.5544 0.02474 0.01489 -0.0778 0.8628 1.0000
3.000 0.5968 0.02477 0.01507 -0.0791 0.8369 1.0000
3.250 0.6350 0.02468 0.01512 -0.0793 0.8110 1.0000
3.500 0.6694 0.02453 0.01515 -0.0784 0.7849 1.0000
3.750 0.7003 0.02437 0.01511 -0.0768 0.7581 1.0000
4.000 0.7279 0.02430 0.01513 -0.0747 0.7299 1.0000
4.250 0.7536 0.02431 0.01524 -0.0724 0.7003 1.0000
4.500 0.7787 0.02437 0.01542 -0.0700 0.6697 1.0000
4.750 0.8037 0.02444 0.01554 -0.0675 0.6384 1.0000
5.000 0.8289 0.02454 0.01563 -0.0651 0.6069 1.0000
5.250 0.8517 0.02497 0.01612 -0.0629 0.5715 1.0000
5.500 0.8761 0.02527 0.01636 -0.0606 0.5372 1.0000
5.750 0.8985 0.02588 0.01706 -0.0586 0.4995 1.0000
6.000 0.9211 0.02652 0.01766 -0.0565 0.4616 1.0000
6.250 0.9436 0.02721 0.01826 -0.0545 0.4229 1.0000
6.500 0.9654 0.02802 0.01895 -0.0525 0.3827 1.0000
6.750 0.9859 0.02900 0.01982 -0.0505 0.3410 1.0000
7.000 1.0052 0.03018 0.02092 -0.0486 0.2983 1.0000
7.250 1.0234 0.03161 0.02232 -0.0467 0.2554 1.0000
7.500 1.0415 0.03339 0.02393 -0.0448 0.2150 1.0000
7.750 1.0585 0.03546 0.02592 -0.0430 0.1790 1.0000
8.000 1.0764 0.03785 0.02818 -0.0415 0.1502 1.0000
8.250 1.0933 0.04117 0.03184 -0.0398 0.1311 1.0000
8.500 1.1087 0.04410 0.03499 -0.0383 0.1149 1.0000
8.750 1.1237 0.04821 0.03941 -0.0368 0.1066 1.0000
9.000 1.1348 0.05207 0.04370 -0.0352 0.0996 1.0000
9.250 1.1407 0.05637 0.04836 -0.0338 0.0942 1.0000
9.500 1.1369 0.06125 0.05385 -0.0321 0.0920 1.0000
9.750 1.1288 0.06649 0.05955 -0.0308 0.0915 1.0000
10.000 1.1151 0.07187 0.06530 -0.0300 0.0920 1.0000
10.250 1.0960 0.07722 0.07092 -0.0295 0.0929 1.0000
10.500 1.0742 0.08248 0.07633 -0.0297 0.0939 1.0000
10.750 1.0537 0.08835 0.08230 -0.0314 0.0950 1.0000
11.000 1.0374 0.09477 0.08877 -0.0338 0.0959 1.0000
11.250 0.9560 0.11816 0.11214 -0.0550 0.1211 1.0000
|
Polar data table (+)
Polar graphs
<< Back to AG24 Bubble Dancer DLG by Mark Drela (ag24-il)