AG26 Bubble Dancer DLG by Mark Drela (ag26-il) Xfoil prediction polar at RE=200,000 Ncrit=5
| Details | Polar file |
|---|---|
|
Airfoil: AG26 Bubble Dancer DLG by Mark Drela (ag26-il) Reynolds number: 200,000 Max Cl/Cd: 65.94 at α=4° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ag26-il-200000-n5.txt Download as CSV file: xf-ag26-il-200000-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 = 0.200 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-6.750 -0.4473 0.07006 0.06676 -0.0224 1.0000 0.0162
-6.500 -0.4318 0.06291 0.05960 -0.0309 1.0000 0.0147
-6.250 -0.4036 0.05059 0.04707 -0.0438 1.0000 0.0124
-6.000 -0.3860 0.04384 0.04011 -0.0490 1.0000 0.0120
-5.750 -0.3651 0.03713 0.03305 -0.0532 1.0000 0.0117
-5.500 -0.3425 0.03127 0.02666 -0.0559 1.0000 0.0115
-5.250 -0.3184 0.02657 0.02138 -0.0573 1.0000 0.0114
-5.000 -0.2933 0.02299 0.01721 -0.0578 1.0000 0.0115
-4.750 -0.2677 0.02036 0.01407 -0.0578 1.0000 0.0117
-4.500 -0.2421 0.01846 0.01176 -0.0575 1.0000 0.0121
-4.250 -0.2164 0.01656 0.00955 -0.0573 1.0000 0.0128
-4.000 -0.1917 0.01556 0.00847 -0.0570 1.0000 0.0146
-3.750 -0.1659 0.01493 0.00774 -0.0568 0.9996 0.0171
-3.500 -0.1290 0.01380 0.00641 -0.0586 0.9949 0.0188
-3.250 -0.0928 0.01267 0.00517 -0.0604 0.9896 0.0217
-3.000 -0.0555 0.01214 0.00456 -0.0624 0.9838 0.0289
-2.750 -0.0199 0.01148 0.00385 -0.0640 0.9761 0.0420
-2.500 0.0167 0.01089 0.00339 -0.0660 0.9688 0.0787
-2.250 0.0502 0.01037 0.00310 -0.0673 0.9580 0.1425
-2.000 0.0835 0.00988 0.00290 -0.0687 0.9467 0.2308
-1.750 0.1161 0.00945 0.00276 -0.0697 0.9342 0.3252
-1.500 0.1473 0.00911 0.00263 -0.0703 0.9200 0.4121
-1.250 0.1768 0.00879 0.00253 -0.0705 0.9041 0.4948
-1.000 0.2045 0.00847 0.00244 -0.0701 0.8867 0.5808
-0.750 0.2292 0.00812 0.00238 -0.0689 0.8673 0.6834
-0.500 0.2487 0.00765 0.00228 -0.0661 0.8475 0.8455
-0.250 0.2810 0.00750 0.00210 -0.0664 0.8264 1.0000
0.000 0.3079 0.00759 0.00202 -0.0658 0.8045 1.0000
0.250 0.3348 0.00768 0.00196 -0.0653 0.7819 1.0000
0.500 0.3616 0.00780 0.00192 -0.0648 0.7590 1.0000
0.750 0.3884 0.00792 0.00190 -0.0643 0.7354 1.0000
1.000 0.4152 0.00806 0.00190 -0.0639 0.7111 1.0000
1.250 0.4421 0.00822 0.00191 -0.0634 0.6863 1.0000
1.500 0.4689 0.00839 0.00196 -0.0630 0.6610 1.0000
1.750 0.4957 0.00857 0.00201 -0.0626 0.6351 1.0000
2.000 0.5225 0.00877 0.00208 -0.0622 0.6081 1.0000
2.250 0.5492 0.00898 0.00217 -0.0619 0.5804 1.0000
2.500 0.5759 0.00921 0.00228 -0.0615 0.5513 1.0000
2.750 0.6024 0.00946 0.00244 -0.0612 0.5199 1.0000
3.000 0.6288 0.00975 0.00258 -0.0608 0.4865 1.0000
3.250 0.6550 0.01006 0.00275 -0.0605 0.4516 1.0000
3.500 0.6811 0.01040 0.00295 -0.0602 0.4165 1.0000
3.750 0.7073 0.01075 0.00321 -0.0599 0.3820 1.0000
4.000 0.7333 0.01112 0.00347 -0.0596 0.3493 1.0000
4.250 0.7593 0.01152 0.00376 -0.0594 0.3180 1.0000
4.500 0.7853 0.01192 0.00407 -0.0591 0.2883 1.0000
4.750 0.8112 0.01233 0.00444 -0.0589 0.2606 1.0000
5.000 0.8369 0.01278 0.00482 -0.0586 0.2331 1.0000
5.250 0.8625 0.01324 0.00522 -0.0583 0.2071 1.0000
5.500 0.8879 0.01373 0.00565 -0.0580 0.1817 1.0000
5.750 0.9131 0.01426 0.00612 -0.0577 0.1570 1.0000
6.000 0.9383 0.01479 0.00666 -0.0574 0.1348 1.0000
6.250 0.9629 0.01541 0.00722 -0.0571 0.1144 1.0000
6.500 0.9877 0.01600 0.00782 -0.0567 0.0976 1.0000
6.750 1.0120 0.01665 0.00846 -0.0563 0.0818 1.0000
7.000 1.0361 0.01732 0.00916 -0.0559 0.0684 1.0000
7.250 1.0599 0.01805 0.00990 -0.0554 0.0554 1.0000
7.500 1.0832 0.01882 0.01074 -0.0549 0.0440 1.0000
7.750 1.1061 0.01968 0.01165 -0.0543 0.0343 1.0000
8.000 1.1282 0.02066 0.01269 -0.0536 0.0266 1.0000
8.250 1.1486 0.02191 0.01398 -0.0528 0.0205 1.0000
8.500 1.1696 0.02301 0.01528 -0.0519 0.0172 1.0000
8.750 1.1888 0.02432 0.01669 -0.0510 0.0140 1.0000
9.000 1.2072 0.02574 0.01829 -0.0500 0.0121 1.0000
9.250 1.2246 0.02726 0.02002 -0.0488 0.0108 1.0000
9.500 1.2409 0.02885 0.02180 -0.0475 0.0099 1.0000
9.750 1.2553 0.03060 0.02379 -0.0462 0.0091 1.0000
10.000 1.2657 0.03283 0.02622 -0.0446 0.0086 1.0000
10.250 1.2706 0.03585 0.02949 -0.0425 0.0081 1.0000
10.500 1.2805 0.03785 0.03177 -0.0409 0.0077 1.0000
10.750 1.2875 0.03995 0.03415 -0.0393 0.0072 1.0000
11.000 1.2895 0.04212 0.03658 -0.0372 0.0067 1.0000
11.250 1.2872 0.04461 0.03930 -0.0353 0.0063 1.0000
11.500 1.2823 0.04749 0.04241 -0.0341 0.0061 1.0000
11.750 1.2741 0.05110 0.04627 -0.0337 0.0060 1.0000
12.000 1.2637 0.05543 0.05084 -0.0345 0.0059 1.0000
12.250 1.2515 0.06053 0.05618 -0.0365 0.0058 1.0000
12.500 1.2371 0.06662 0.06250 -0.0397 0.0058 1.0000
12.750 1.2206 0.07373 0.06983 -0.0440 0.0058 1.0000
13.000 1.2016 0.08191 0.07822 -0.0492 0.0059 1.0000
13.250 1.1802 0.09116 0.08766 -0.0551 0.0060 1.0000
13.500 1.1566 0.10134 0.09802 -0.0613 0.0061 1.0000
13.750 1.1291 0.11287 0.10969 -0.0680 0.0064 1.0000
14.000 1.0972 0.12596 0.12289 -0.0750 0.0070 1.0000
|
Polar data table (+)
Polar graphs
<< Back to AG26 Bubble Dancer DLG by Mark Drela (ag26-il)