AG25 Bubble Dancer DLG by Mark Drela (ag25-il)
AG25 Bubble Dancer DLG by Mark Drela - Drela AG25 airfoil used on the Bubble Dancer R/C DLG
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(ag25-il) AG25 Bubble Dancer DLG by Mark Drela Drela AG25 airfoil used on the Bubble Dancer R/C DLG Max thickness 7.6% at 24.7% chord. Max camber 2.4% at 45.4% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
AG25 Bubble Dancer DLG by Mark Drela
1.000000 0.000283
0.994054 0.001020
0.982050 0.002599
0.968503 0.004411
0.954662 0.006281
0.940783 0.008151
0.926901 0.010007
0.913016 0.011840
0.899128 0.013652
0.885240 0.015440
0.871350 0.017206
0.857464 0.018949
0.843575 0.020673
0.829689 0.022375
0.815801 0.024054
0.801909 0.025710
0.788021 0.027341
0.774128 0.028945
0.760232 0.030524
0.746336 0.032074
0.732435 0.033595
0.718530 0.035088
0.704627 0.036550
0.690721 0.037981
0.676812 0.039379
0.662904 0.040743
0.648998 0.042070
0.635087 0.043359
0.621176 0.044609
0.607268 0.045818
0.593358 0.046987
0.579446 0.048114
0.565539 0.049198
0.551631 0.050238
0.537721 0.051233
0.523813 0.052182
0.509910 0.053082
0.496007 0.053933
0.482101 0.054735
0.468201 0.055484
0.454307 0.056180
0.440410 0.056821
0.426520 0.057405
0.412636 0.057929
0.398752 0.058392
0.384874 0.058791
0.371005 0.059123
0.357141 0.059386
0.343282 0.059577
0.329435 0.059690
0.315600 0.059723
0.301770 0.059669
0.287958 0.059528
0.274163 0.059290
0.260376 0.058951
0.246613 0.058504
0.232873 0.057942
0.219153 0.057257
0.205468 0.056441
0.191818 0.055484
0.178207 0.054374
0.164654 0.053101
0.151157 0.051646
0.137735 0.049999
0.124408 0.048138
0.111182 0.046040
0.098104 0.043683
0.085190 0.041032
0.072510 0.038059
0.060109 0.034720
0.048112 0.030979
0.036699 0.026809
0.026246 0.022257
0.017438 0.017599
0.010935 0.013364
0.006635 0.009902
0.003867 0.007154
0.002062 0.004904
0.000891 0.002993
0.000210 0.001313
0.000000 -0.000205
0.000317 -0.001680
0.001267 -0.003128
0.002864 -0.004509
0.005203 -0.005914
0.008626 -0.007447
0.013801 -0.009205
0.021556 -0.011179
0.031817 -0.013115
0.043646 -0.014757
0.056256 -0.016068
0.069243 -0.017079
0.082454 -0.017840
0.095819 -0.018399
0.109288 -0.018791
0.122835 -0.019045
0.136441 -0.019178
0.150097 -0.019207
0.163786 -0.019145
0.177511 -0.018999
0.191260 -0.018780
0.205028 -0.018498
0.218817 -0.018158
0.232623 -0.017766
0.246439 -0.017328
0.260273 -0.016850
0.274118 -0.016335
0.287975 -0.015791
0.301848 -0.015223
0.315733 -0.014632
0.329629 -0.014022
0.343541 -0.013395
0.357465 -0.012756
0.371401 -0.012106
0.385350 -0.011449
0.399308 -0.010787
0.413271 -0.010122
0.427222 -0.009457
0.441160 -0.008795
0.455088 -0.008136
0.469010 -0.007485
0.482920 -0.006843
0.496821 -0.006211
0.510717 -0.005588
0.524612 -0.004979
0.538500 -0.004384
0.552383 -0.003803
0.566262 -0.003237
0.580141 -0.002690
0.594011 -0.002160
0.607879 -0.001650
0.621742 -0.001160
0.635601 -0.000692
0.649453 -0.000246
0.663305 0.000177
0.677155 0.000576
0.691004 0.000952
0.704853 0.001303
0.718703 0.001631
0.732557 0.001934
0.746411 0.002212
0.760268 0.002464
0.774128 0.002684
0.787988 0.002875
0.801855 0.003031
0.815728 0.003149
0.829601 0.003225
0.843477 0.003258
0.857358 0.003240
0.871239 0.003171
0.885123 0.003045
0.899010 0.002855
0.912897 0.002596
0.926785 0.002269
0.940673 0.001866
0.954562 0.001387
0.968423 0.000836
0.982034 0.000226
0.994050 -0.000374
1.000000 -0.000680
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 AG25 Bubble Dancer DLG by Mark Drela (ag25-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ag25-il | 50,000 | 9 | 35.9 at α=5.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag25-il | 50,000 | 5 | 38.9 at α=5.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag25-il | 100,000 | 9 | 53.6 at α=4.75° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag25-il | 100,000 | 5 | 53.1 at α=4.75° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag25-il | 200,000 | 9 | 70.9 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag25-il | 200,000 | 5 | 66.6 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag25-il | 500,000 | 9 | 92.1 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag25-il | 500,000 | 5 | 84 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag25-il | 1,000,000 | 9 | 106.5 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag25-il | 1,000,000 | 5 | 97 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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