AG26 Bubble Dancer DLG by Mark Drela (ag26-il)
AG26 Bubble Dancer DLG by Mark Drela - Drela AG26 airfoil used on the Bubble Dancer R/C DLG
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(ag26-il) AG26 Bubble Dancer DLG by Mark Drela Drela AG26 airfoil used on the Bubble Dancer R/C DLG Max thickness 6.8% at 23.3% chord. Max camber 2.5% at 45.5% chord Source UIUC Airfoil Coordinates Database Source dat file The dat file is in Selig format |
AG26 Bubble Dancer DLG by Mark Drela
1.000000 0.000283
0.994061 0.000999
0.982066 0.002505
0.968526 0.004228
0.954693 0.006008
0.940816 0.007759
0.926936 0.009469
0.913054 0.011174
0.899169 0.012856
0.885285 0.014530
0.871402 0.016190
0.857523 0.017832
0.843640 0.019461
0.829761 0.021064
0.815882 0.022652
0.801998 0.024219
0.788119 0.025763
0.774238 0.027291
0.760352 0.028789
0.746468 0.030268
0.732578 0.031719
0.718685 0.033151
0.704794 0.034552
0.690902 0.035926
0.677007 0.037275
0.663114 0.038591
0.649222 0.039874
0.635327 0.041126
0.621434 0.042343
0.607542 0.043523
0.593649 0.044668
0.579754 0.045771
0.565865 0.046837
0.551976 0.047861
0.538085 0.048847
0.524196 0.049789
0.510314 0.050690
0.496430 0.051538
0.482545 0.052336
0.468664 0.053082
0.454789 0.053772
0.440913 0.054407
0.427041 0.054983
0.413176 0.055498
0.399313 0.055953
0.385454 0.056345
0.371607 0.056669
0.357762 0.056927
0.343921 0.057113
0.330095 0.057226
0.316280 0.057262
0.302471 0.057219
0.288679 0.057095
0.274904 0.056884
0.261136 0.056581
0.247392 0.056182
0.233671 0.055680
0.219967 0.055067
0.206299 0.054334
0.192663 0.053472
0.179063 0.052469
0.165520 0.051314
0.152029 0.049989
0.138611 0.048479
0.125281 0.046761
0.112050 0.044812
0.098958 0.042616
0.086022 0.040147
0.073305 0.037380
0.060851 0.034267
0.048780 0.030758
0.037275 0.026799
0.026717 0.022411
0.017800 0.017854
0.011195 0.013657
0.006815 0.010190
0.003988 0.007407
0.002136 0.005117
0.000931 0.003155
0.000227 0.001419
0.000002 -0.000157
0.000342 -0.001683
0.001369 -0.003136
0.003059 -0.004457
0.005487 -0.005761
0.008992 -0.007149
0.014252 -0.008701
0.022090 -0.010375
0.032419 -0.011934
0.044295 -0.013185
0.056934 -0.014106
0.069936 -0.014742
0.083154 -0.015148
0.096518 -0.015373
0.109982 -0.015460
0.123522 -0.015438
0.137115 -0.015327
0.150759 -0.015139
0.164436 -0.014883
0.178145 -0.014564
0.191880 -0.014188
0.205634 -0.013764
0.219407 -0.013295
0.233197 -0.012787
0.247000 -0.012246
0.260819 -0.011674
0.274650 -0.011077
0.288493 -0.010462
0.302352 -0.009830
0.316224 -0.009187
0.330108 -0.008536
0.344007 -0.007882
0.357919 -0.007225
0.371844 -0.006569
0.385781 -0.005919
0.399730 -0.005270
0.413682 -0.004629
0.427624 -0.004000
0.441553 -0.003380
0.455472 -0.002772
0.469385 -0.002184
0.483287 -0.001615
0.497181 -0.001064
0.511069 -0.000532
0.524956 -0.000023
0.538837 0.000463
0.552713 0.000926
0.566586 0.001366
0.580457 0.001780
0.594321 0.002166
0.608182 0.002528
0.622038 0.002860
0.635889 0.003166
0.649734 0.003442
0.663579 0.003691
0.677422 0.003909
0.691263 0.004098
0.705104 0.004259
0.718947 0.004390
0.732793 0.004493
0.746637 0.004565
0.760486 0.004608
0.774336 0.004619
0.788187 0.004597
0.802043 0.004544
0.815905 0.004455
0.829767 0.004330
0.843631 0.004169
0.857499 0.003966
0.871368 0.003725
0.885239 0.003440
0.899112 0.003111
0.912984 0.002735
0.926859 0.002311
0.940732 0.001837
0.954608 0.001313
0.968456 0.000739
0.982055 0.000127
0.994062 -0.000442
1.000000 -0.000716
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 AG26 Bubble Dancer DLG by Mark Drela (ag26-il)
| Plot | Airfoil | Reynolds # | Ncrit | Max Cl/Cd | Description | Source | |
|---|---|---|---|---|---|---|---|
| ag26-il | 50,000 | 9 | 36.8 at α=5.25° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag26-il | 50,000 | 5 | 39.4 at α=5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag26-il | 100,000 | 9 | 54.5 at α=4.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag26-il | 100,000 | 5 | 53.2 at α=4.25° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag26-il | 200,000 | 9 | 71.6 at α=4° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag26-il | 200,000 | 5 | 65.9 at α=4° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag26-il | 500,000 | 9 | 91.8 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag26-il | 500,000 | 5 | 83 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
| ag26-il | 1,000,000 | 9 | 104.7 at α=3.5° | Mach=0 Ncrit=9 | Xfoil prediction | Details | |
| ag26-il | 1,000,000 | 5 | 96 at α=4.5° | Mach=0 Ncrit=5 | Xfoil prediction | Details | |
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