AG27 Bubble Dancer DLG by Mark Drela (ag27-il)
AG27 Bubble Dancer DLG by Mark Drela - Drela AG27 airfoil used on the Bubble Dancer R/C DLG
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(ag27-il) AG27 Bubble Dancer DLG by Mark Drela Drela AG27 airfoil used on the Bubble Dancer R/C DLG Max thickness 6.1% at 21.7% chord. Max camber 2.6% at 44% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
AG27 Bubble Dancer DLG by Mark Drela
1.000000 0.000283
0.994180 0.000967
0.982337 0.002388
0.968812 0.004026
0.955011 0.005695
0.941189 0.007338
0.927350 0.008957
0.913497 0.010556
0.899632 0.012140
0.885755 0.013711
0.871872 0.015274
0.857989 0.016826
0.844111 0.018368
0.830237 0.019895
0.816368 0.021406
0.802503 0.022898
0.788640 0.024370
0.774777 0.025821
0.760916 0.027248
0.747055 0.028652
0.733192 0.030032
0.719329 0.031386
0.705466 0.032715
0.691601 0.034018
0.677736 0.035294
0.663871 0.036542
0.650005 0.037761
0.636140 0.038952
0.622275 0.040111
0.608411 0.041238
0.594548 0.042333
0.580687 0.043392
0.566827 0.044415
0.552967 0.045401
0.539110 0.046347
0.525254 0.047252
0.511400 0.048115
0.497547 0.048934
0.483698 0.049707
0.469849 0.050432
0.456003 0.051109
0.442161 0.051733
0.428321 0.052305
0.414484 0.052821
0.400651 0.053281
0.386823 0.053681
0.372998 0.054019
0.359180 0.054294
0.345368 0.054502
0.331562 0.054641
0.317764 0.054708
0.303978 0.054698
0.290201 0.054610
0.276438 0.054438
0.262694 0.054177
0.248963 0.053822
0.235251 0.053368
0.221565 0.052809
0.207903 0.052138
0.194272 0.051347
0.180677 0.050427
0.167119 0.049369
0.153615 0.048164
0.140172 0.046796
0.126808 0.045252
0.113548 0.043510
0.100419 0.041546
0.087469 0.039332
0.074753 0.036830
0.062354 0.033994
0.050378 0.030783
0.039021 0.027161
0.028597 0.023137
0.019601 0.018856
0.012624 0.014716
0.007802 0.011144
0.004640 0.008212
0.002567 0.005804
0.001215 0.003765
0.000386 0.001982
0.000020 0.000381
0.000157 -0.001116
0.000954 -0.002587
0.002432 -0.003886
0.004578 -0.005075
0.007597 -0.006275
0.012003 -0.007561
0.018644 -0.008938
0.028138 -0.010257
0.039834 -0.011302
0.052555 -0.011999
0.065723 -0.012396
0.079132 -0.012562
0.092688 -0.012550
0.106349 -0.012399
0.120081 -0.012141
0.133859 -0.011795
0.147675 -0.011377
0.161512 -0.010899
0.175373 -0.010368
0.189252 -0.009794
0.203145 -0.009183
0.217055 -0.008541
0.230978 -0.007875
0.244912 -0.007189
0.258861 -0.006488
0.272820 -0.005778
0.286786 -0.005062
0.300754 -0.004344
0.314716 -0.003631
0.328675 -0.002926
0.342626 -0.002229
0.356566 -0.001545
0.370505 -0.000878
0.384445 -0.000225
0.398379 0.000411
0.412307 0.001027
0.426235 0.001622
0.440162 0.002196
0.454076 0.002747
0.467978 0.003267
0.481879 0.003754
0.495783 0.004209
0.509687 0.004633
0.523590 0.005023
0.537494 0.005381
0.551400 0.005706
0.565305 0.005999
0.579210 0.006258
0.593117 0.006484
0.607024 0.006678
0.620930 0.006839
0.634836 0.006965
0.648742 0.007058
0.662647 0.007118
0.676552 0.007143
0.690457 0.007134
0.704362 0.007090
0.718266 0.007013
0.732172 0.006901
0.746080 0.006756
0.759988 0.006578
0.773899 0.006368
0.787814 0.006127
0.801731 0.005858
0.815650 0.005559
0.829572 0.005234
0.843496 0.004883
0.857422 0.004507
0.871349 0.004106
0.885276 0.003682
0.899202 0.003235
0.913125 0.002764
0.927043 0.002268
0.940954 0.001745
0.954854 0.001194
0.968713 0.000612
0.982285 0.000012
0.994170 -0.000515
1.000000 -0.000752
The AG2x airfoils are intended to be used on composite versions of the
Bubble Dancer and the Allegro-Lite.
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Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file |
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Polars for AG27 Bubble Dancer DLG by Mark Drela (ag27-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ag27-il | 50,000 | 9 | 37.8 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag27-il | 50,000 | 5 | 39.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag27-il | 100,000 | 9 | 55.1 at α=4.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag27-il | 100,000 | 5 | 53 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag27-il | 200,000 | 9 | 71.7 at α=3.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag27-il | 200,000 | 5 | 65.3 at α=3.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag27-il | 500,000 | 9 | 91.3 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag27-il | 500,000 | 5 | 81.1 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag27-il | 1,000,000 | 9 | 103.4 at α=3.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag27-il | 1,000,000 | 5 | 95.4 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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