AG25 Bubble Dancer DLG by Mark Drela (ag25-il) Xfoil prediction polar at RE=50,000 Ncrit=9
| Details | Polar file |
|---|---|
|
Airfoil: AG25 Bubble Dancer DLG by Mark Drela (ag25-il) Reynolds number: 50,000 Max Cl/Cd: 35.92 at α=5.5° Description: Mach=0 Ncrit=9 Source: Xfoil prediction Download polar: xf-ag25-il-50000.txt Download as CSV file: xf-ag25-il-50000.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 = 0.050 e 6 Ncrit = 9.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-7.500 -0.4633 0.09775 0.09129 0.0012 1.0000 0.2359
-7.250 -0.4729 0.09608 0.08977 -0.0014 1.0000 0.2456
-7.000 -0.4686 0.09313 0.08687 -0.0026 1.0000 0.2585
-6.750 -0.4580 0.08924 0.08303 -0.0020 1.0000 0.2718
-6.500 -0.4524 0.08599 0.07985 -0.0030 1.0000 0.2860
-6.250 -0.4467 0.08267 0.07661 -0.0042 1.0000 0.3010
-6.000 -0.4311 0.07851 0.07247 -0.0010 1.0000 0.3185
-5.750 -0.4287 0.07599 0.07005 -0.0024 1.0000 0.3431
-5.500 -0.4218 0.07321 0.06734 -0.0015 1.0000 0.3704
-5.250 -0.4055 0.06912 0.06328 0.0024 1.0000 0.3899
-5.000 -0.3436 0.04692 0.03970 -0.0506 1.0000 0.1323
-4.750 -0.3142 0.04090 0.03285 -0.0548 1.0000 0.1201
-4.500 -0.2894 0.03686 0.02850 -0.0556 1.0000 0.1180
-4.250 -0.2617 0.03296 0.02406 -0.0565 1.0000 0.1152
-4.000 -0.2330 0.02968 0.02018 -0.0569 1.0000 0.1160
-3.750 -0.2062 0.02728 0.01739 -0.0568 1.0000 0.1266
-3.500 -0.1784 0.02501 0.01477 -0.0564 1.0000 0.1385
-3.250 -0.1512 0.02313 0.01268 -0.0557 1.0000 0.1611
-3.000 -0.1251 0.02127 0.01094 -0.0549 1.0000 0.2034
-2.750 -0.0984 0.01925 0.00965 -0.0543 1.0000 0.3291
-2.500 -0.0790 0.01746 0.00913 -0.0514 1.0000 0.5574
-2.250 -0.0706 0.01641 0.00882 -0.0453 1.0000 0.7240
-2.000 -0.0559 0.01516 0.00790 -0.0404 1.0000 1.0000
-1.750 -0.0211 0.01515 0.00715 -0.0436 1.0000 1.0000
-1.500 0.0070 0.01525 0.00676 -0.0445 1.0000 1.0000
-1.250 0.0336 0.01540 0.00653 -0.0451 1.0000 1.0000
-1.000 0.0593 0.01558 0.00641 -0.0454 1.0000 1.0000
-0.750 0.0845 0.01581 0.00634 -0.0457 1.0000 1.0000
-0.500 0.1092 0.01607 0.00639 -0.0459 1.0000 1.0000
-0.250 0.1334 0.01639 0.00653 -0.0462 1.0000 1.0000
0.000 0.1571 0.01676 0.00674 -0.0465 1.0000 1.0000
0.250 0.1804 0.01719 0.00702 -0.0468 1.0000 1.0000
0.500 0.2032 0.01768 0.00741 -0.0471 1.0000 1.0000
0.750 0.2254 0.01825 0.00791 -0.0476 1.0000 1.0000
1.000 0.2470 0.01890 0.00851 -0.0481 1.0000 1.0000
1.250 0.2678 0.01965 0.00922 -0.0487 1.0000 1.0000
1.500 0.2879 0.02051 0.01007 -0.0495 1.0000 1.0000
1.750 0.3357 0.02155 0.01113 -0.0554 0.9860 1.0000
2.000 0.4028 0.02248 0.01213 -0.0640 0.9596 1.0000
2.250 0.4648 0.02312 0.01292 -0.0710 0.9317 1.0000
2.500 0.5238 0.02348 0.01343 -0.0767 0.9032 1.0000
2.750 0.5780 0.02355 0.01374 -0.0806 0.8748 1.0000
3.000 0.6234 0.02346 0.01382 -0.0821 0.8461 1.0000
3.250 0.6621 0.02326 0.01377 -0.0820 0.8172 1.0000
3.500 0.6925 0.02319 0.01382 -0.0804 0.7859 1.0000
3.750 0.7204 0.02311 0.01391 -0.0782 0.7539 1.0000
4.000 0.7474 0.02298 0.01385 -0.0756 0.7221 1.0000
4.250 0.7719 0.02303 0.01396 -0.0729 0.6880 1.0000
4.500 0.7961 0.02312 0.01406 -0.0702 0.6531 1.0000
4.750 0.8193 0.02339 0.01440 -0.0676 0.6159 1.0000
5.000 0.8428 0.02370 0.01467 -0.0651 0.5785 1.0000
5.250 0.8661 0.02412 0.01502 -0.0627 0.5402 1.0000
5.500 0.8887 0.02474 0.01560 -0.0606 0.4997 1.0000
5.750 0.9110 0.02548 0.01628 -0.0585 0.4589 1.0000
6.000 0.9331 0.02635 0.01708 -0.0566 0.4178 1.0000
6.250 0.9548 0.02736 0.01808 -0.0548 0.3767 1.0000
6.500 0.9759 0.02851 0.01915 -0.0530 0.3355 1.0000
6.750 0.9964 0.02984 0.02039 -0.0513 0.2949 1.0000
7.000 1.0162 0.03136 0.02185 -0.0496 0.2556 1.0000
7.250 1.0363 0.03323 0.02360 -0.0480 0.2199 1.0000
7.500 1.0549 0.03533 0.02575 -0.0463 0.1869 1.0000
7.750 1.0733 0.03765 0.02809 -0.0448 0.1588 1.0000
8.000 1.0921 0.04082 0.03148 -0.0433 0.1388 1.0000
8.250 1.1071 0.04381 0.03479 -0.0418 0.1212 1.0000
8.500 1.1218 0.04790 0.03924 -0.0403 0.1116 1.0000
8.750 1.1386 0.05169 0.04302 -0.0392 0.1019 1.0000
9.000 1.1373 0.05645 0.04871 -0.0373 0.0980 1.0000
9.250 1.1363 0.06130 0.05408 -0.0359 0.0947 1.0000
9.500 1.1291 0.06682 0.06006 -0.0349 0.0943 1.0000
9.750 1.1136 0.07271 0.06634 -0.0344 0.0952 1.0000
10.000 1.0915 0.07862 0.07252 -0.0347 0.0969 1.0000
10.250 1.0677 0.08432 0.07835 -0.0356 0.0985 1.0000
10.500 1.0470 0.09067 0.08478 -0.0381 0.1000 1.0000
10.750 1.0318 0.09748 0.09161 -0.0411 0.1012 1.0000
|
Polar data table (+)
Polar graphs
<< Back to AG25 Bubble Dancer DLG by Mark Drela (ag25-il)