AG24 Bubble Dancer DLG by Mark Drela (ag24-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5
| Details | Polar file |
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Airfoil: AG24 Bubble Dancer DLG by Mark Drela (ag24-il) Reynolds number: 1,000,000 Max Cl/Cd: 96.82 at α=4.5° Description: Mach=0 Ncrit=5 Source: Xfoil prediction Download polar: xf-ag24-il-1000000-n5.txt Download as CSV file: xf-ag24-il-1000000-n5.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 = 1.000 e 6 Ncrit = 5.000
alpha CL CD CDp CM Top_Xtr Bot_Xtr
------ -------- --------- --------- -------- -------- --------
-10.500 -0.5584 0.11302 0.11142 0.0077 1.0000 0.0028
-10.250 -0.5578 0.10819 0.10660 0.0055 1.0000 0.0029
-9.250 -0.7208 0.02777 0.02520 -0.0569 1.0000 0.0031
-9.000 -0.7041 0.02415 0.02118 -0.0580 1.0000 0.0032
-8.750 -0.6841 0.02163 0.01834 -0.0584 1.0000 0.0033
-8.500 -0.6627 0.01965 0.01608 -0.0585 1.0000 0.0034
-8.250 -0.6407 0.01804 0.01424 -0.0583 1.0000 0.0035
-8.000 -0.6167 0.01666 0.01263 -0.0583 0.9994 0.0036
-7.750 -0.5857 0.01539 0.01114 -0.0597 0.9965 0.0037
-7.500 -0.5541 0.01431 0.00989 -0.0610 0.9938 0.0038
-7.250 -0.5239 0.01349 0.00893 -0.0619 0.9893 0.0039
-7.000 -0.4924 0.01288 0.00823 -0.0629 0.9849 0.0041
-6.750 -0.4613 0.01233 0.00759 -0.0638 0.9800 0.0042
-6.500 -0.4318 0.01131 0.00640 -0.0645 0.9732 0.0044
-6.250 -0.4025 0.01053 0.00547 -0.0650 0.9661 0.0048
-6.000 -0.3744 0.01007 0.00495 -0.0651 0.9569 0.0051
-5.750 -0.3470 0.00970 0.00452 -0.0650 0.9466 0.0055
-5.500 -0.3201 0.00937 0.00412 -0.0647 0.9355 0.0060
-5.250 -0.2932 0.00908 0.00375 -0.0644 0.9235 0.0065
-5.000 -0.2663 0.00883 0.00342 -0.0641 0.9106 0.0068
-4.750 -0.2392 0.00851 0.00299 -0.0639 0.8969 0.0076
-4.500 -0.2120 0.00827 0.00269 -0.0636 0.8827 0.0089
-4.250 -0.1845 0.00810 0.00245 -0.0635 0.8680 0.0102
-4.000 -0.1569 0.00792 0.00220 -0.0633 0.8530 0.0125
-3.750 -0.1291 0.00775 0.00199 -0.0632 0.8377 0.0159
-3.500 -0.1012 0.00761 0.00178 -0.0632 0.8221 0.0208
-3.250 -0.0733 0.00746 0.00161 -0.0631 0.8061 0.0297
-3.000 -0.0453 0.00730 0.00144 -0.0631 0.7897 0.0462
-2.750 -0.0173 0.00714 0.00130 -0.0631 0.7730 0.0680
-2.500 0.0109 0.00697 0.00116 -0.0632 0.7555 0.1001
-2.250 0.0390 0.00679 0.00104 -0.0633 0.7373 0.1379
-2.000 0.0671 0.00664 0.00095 -0.0634 0.7187 0.1804
-1.750 0.0952 0.00649 0.00087 -0.0635 0.6996 0.2265
-1.500 0.1234 0.00640 0.00081 -0.0636 0.6795 0.2658
-1.250 0.1516 0.00633 0.00077 -0.0637 0.6593 0.3014
-1.000 0.1798 0.00626 0.00074 -0.0638 0.6380 0.3427
-0.750 0.2080 0.00623 0.00072 -0.0639 0.6165 0.3789
-0.500 0.2361 0.00621 0.00071 -0.0640 0.5947 0.4142
-0.250 0.2643 0.00621 0.00072 -0.0641 0.5729 0.4496
0.000 0.2924 0.00621 0.00074 -0.0641 0.5507 0.4857
0.250 0.3206 0.00621 0.00076 -0.0642 0.5289 0.5221
0.500 0.3487 0.00623 0.00080 -0.0643 0.5071 0.5585
0.750 0.3767 0.00625 0.00084 -0.0644 0.4850 0.5965
1.000 0.4047 0.00628 0.00090 -0.0644 0.4646 0.6354
1.250 0.4326 0.00631 0.00096 -0.0644 0.4431 0.6760
1.500 0.4603 0.00634 0.00104 -0.0644 0.4224 0.7192
1.750 0.4878 0.00637 0.00113 -0.0643 0.4019 0.7638
2.000 0.5148 0.00642 0.00122 -0.0641 0.3823 0.8072
2.250 0.5413 0.00645 0.00132 -0.0637 0.3628 0.8495
2.500 0.5663 0.00649 0.00141 -0.0630 0.3431 0.8955
2.750 0.5923 0.00648 0.00146 -0.0624 0.3238 1.0000
3.000 0.6202 0.00668 0.00157 -0.0625 0.3034 1.0000
3.250 0.6480 0.00688 0.00170 -0.0625 0.2835 1.0000
3.500 0.6757 0.00710 0.00184 -0.0625 0.2626 1.0000
3.750 0.7032 0.00733 0.00198 -0.0625 0.2421 1.0000
4.000 0.7307 0.00758 0.00214 -0.0625 0.2206 1.0000
4.250 0.7580 0.00784 0.00233 -0.0625 0.1994 1.0000
4.500 0.7852 0.00811 0.00252 -0.0625 0.1795 1.0000
4.750 0.8123 0.00841 0.00273 -0.0624 0.1587 1.0000
5.000 0.8391 0.00874 0.00296 -0.0624 0.1370 1.0000
5.250 0.8660 0.00904 0.00320 -0.0623 0.1205 1.0000
5.500 0.8923 0.00946 0.00351 -0.0622 0.0959 1.0000
5.750 0.9187 0.00981 0.00379 -0.0620 0.0785 1.0000
6.000 0.9447 0.01027 0.00414 -0.0619 0.0588 1.0000
6.250 0.9707 0.01068 0.00448 -0.0617 0.0436 1.0000
6.500 0.9965 0.01112 0.00486 -0.0615 0.0312 1.0000
6.750 1.0222 0.01157 0.00526 -0.0613 0.0215 1.0000
7.000 1.0480 0.01198 0.00565 -0.0610 0.0157 1.0000
7.250 1.0735 0.01242 0.00608 -0.0608 0.0112 1.0000
7.500 1.0991 0.01284 0.00651 -0.0605 0.0088 1.0000
7.750 1.1244 0.01328 0.00697 -0.0602 0.0068 1.0000
8.000 1.1496 0.01372 0.00745 -0.0599 0.0057 1.0000
8.250 1.1741 0.01427 0.00804 -0.0595 0.0045 1.0000
8.500 1.1990 0.01473 0.00855 -0.0591 0.0040 1.0000
8.750 1.2235 0.01522 0.00908 -0.0588 0.0035 1.0000
9.000 1.2475 0.01576 0.00967 -0.0583 0.0032 1.0000
9.250 1.2710 0.01636 0.01033 -0.0578 0.0028 1.0000
9.500 1.2933 0.01712 0.01117 -0.0572 0.0026 1.0000
9.750 1.3153 0.01790 0.01204 -0.0565 0.0024 1.0000
10.000 1.3376 0.01855 0.01277 -0.0558 0.0023 1.0000
10.250 1.3592 0.01927 0.01359 -0.0551 0.0023 1.0000
10.500 1.3802 0.02002 0.01444 -0.0543 0.0022 1.0000
10.750 1.4005 0.02083 0.01534 -0.0535 0.0021 1.0000
11.000 1.4199 0.02169 0.01630 -0.0526 0.0020 1.0000
11.250 1.4383 0.02261 0.01731 -0.0515 0.0019 1.0000
11.500 1.4558 0.02356 0.01837 -0.0504 0.0018 1.0000
11.750 1.4722 0.02457 0.01948 -0.0492 0.0017 1.0000
12.000 1.4873 0.02562 0.02064 -0.0478 0.0017 1.0000
12.250 1.5008 0.02673 0.02185 -0.0463 0.0016 1.0000
12.500 1.5121 0.02792 0.02317 -0.0446 0.0015 1.0000
12.750 1.5184 0.02918 0.02454 -0.0422 0.0015 1.0000
13.000 1.5217 0.03068 0.02615 -0.0398 0.0015 1.0000
13.250 1.5228 0.03245 0.02806 -0.0377 0.0014 1.0000
13.500 1.5215 0.03463 0.03037 -0.0360 0.0014 1.0000
13.750 1.5179 0.03729 0.03318 -0.0348 0.0013 1.0000
14.000 1.5112 0.04060 0.03666 -0.0343 0.0013 1.0000
14.250 1.5010 0.04475 0.04097 -0.0347 0.0013 1.0000
14.500 1.4907 0.04934 0.04574 -0.0360 0.0013 1.0000
14.750 1.4747 0.05527 0.05185 -0.0384 0.0012 1.0000
15.000 1.4589 0.06157 0.05832 -0.0414 0.0012 1.0000
15.250 1.4401 0.06878 0.06570 -0.0450 0.0012 1.0000
15.500 1.4212 0.07620 0.07326 -0.0487 0.0012 1.0000
15.750 1.3981 0.08461 0.08182 -0.0530 0.0012 1.0000
16.000 1.3742 0.09328 0.09063 -0.0572 0.0012 1.0000
16.250 1.3508 0.10206 0.09954 -0.0614 0.0013 1.0000
16.500 1.3275 0.11097 0.10857 -0.0657 0.0013 1.0000
16.750 1.3018 0.12061 0.11832 -0.0704 0.0013 1.0000
17.000 1.2776 0.13019 0.12801 -0.0752 0.0013 1.0000
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Polar data table (+)
Polar graphs
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