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AG17 (ag17-il)

AG17 - Drela AG17 airfoil


Airfoil ag17-il
Details Dat file Parser  
(ag17-il) AG17
Drela AG17 airfoil
Max thickness 6.5% at 22.1% chord.
Max camber 2% at 45.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
AG17
   0.999985  0.000254
   0.994060  0.000877
   0.982067  0.002158
   0.968523  0.003570
   0.954679  0.004997
   0.940794  0.006406
   0.926907  0.007801
   0.913017  0.009183
   0.899126  0.010558
   0.885237  0.011924
   0.871348  0.013280
   0.857464  0.014625
   0.843579  0.015960
   0.829697  0.017281
   0.815815  0.018589
   0.801930  0.019883
   0.788050  0.021162
   0.774167  0.022424
   0.760282  0.023672
   0.746399  0.024905
   0.732513  0.026123
   0.718624  0.027325
   0.704739  0.028513
   0.690854  0.029685
   0.676966  0.030839
   0.663082  0.031975
   0.649202  0.033090
   0.635318  0.034180
   0.621435  0.035246
   0.607557  0.036286
   0.593678  0.037300
   0.579799  0.038286
   0.565925  0.039244
   0.552052  0.040170
   0.538178  0.041065
   0.524307  0.041927
   0.510442  0.042754
   0.496577  0.043544
   0.482711  0.044298
   0.468851  0.045013
   0.454997  0.045687
   0.441142  0.046320
   0.427293  0.046910
   0.413451  0.047453
   0.399610  0.047949
   0.385774  0.048396
   0.371948  0.048790
   0.358127  0.049130
   0.344310  0.049414
   0.330505  0.049638
   0.316712  0.049797
   0.302923  0.049888
   0.289150  0.049911
   0.275394  0.049856
   0.261644  0.049721
   0.247916  0.049500
   0.234209  0.049186
   0.220519  0.048772
   0.206860  0.048250
   0.193233  0.047610
   0.179639  0.046842
   0.166099  0.045935
   0.152607  0.044871
   0.139184  0.043639
   0.125846  0.042218
   0.112599  0.040587
   0.099488  0.038723
   0.086527  0.036593
   0.073782  0.034165
   0.061297  0.031395
   0.049192  0.028241
   0.037643  0.024669
   0.027028  0.020699
   0.018045  0.016557
   0.011377  0.012720
   0.006944  0.009528
   0.004076  0.006955
   0.002198  0.004819
   0.000966  0.002984
   0.000232  0.001348
   0.000000 -0.000158
   0.000353 -0.001632
   0.001387 -0.003053
   0.003064 -0.004384
   0.005465 -0.005740
   0.008937 -0.007231
   0.014154 -0.008951
   0.021949 -0.010873
   0.032246 -0.012732
   0.044105 -0.014262
   0.056736 -0.015450
   0.069736 -0.016335
   0.082955 -0.016967
   0.096323 -0.017399
   0.109792 -0.017665
   0.123336 -0.017797
   0.136936 -0.017812
   0.150585 -0.017728
   0.164266 -0.017555
   0.177981 -0.017301
   0.191719 -0.016977
   0.205476 -0.016593
   0.219253 -0.016155
   0.233046 -0.015669
   0.246850 -0.015141
   0.260671 -0.014578
   0.274503 -0.013983
   0.288347 -0.013366
   0.302207 -0.012732
   0.316079 -0.012080
   0.329962 -0.011417
   0.343862 -0.010744
   0.357774 -0.010065
   0.371698 -0.009382
   0.385636 -0.008701
   0.399584 -0.008019
   0.413536 -0.007342
   0.427477 -0.006673
   0.441406 -0.006013
   0.455325 -0.005363
   0.469238 -0.004729
   0.483140 -0.004112
   0.497034 -0.003513
   0.510923 -0.002931
   0.524811 -0.002372
   0.538693 -0.001834
   0.552571 -0.001319
   0.566445 -0.000828
   0.580319 -0.000364
   0.594185  0.000075
   0.608049  0.000486
   0.621908  0.000870
   0.635763  0.001224
   0.649612  0.001549
   0.663460  0.001844
   0.677307  0.002109
   0.691153  0.002342
   0.704999  0.002543
   0.718847  0.002714
   0.732698  0.002851
   0.746549  0.002956
   0.760403  0.003032
   0.774259  0.003071
   0.788116  0.003080
   0.801978  0.003057
   0.815846  0.002999
   0.829713  0.002909
   0.843583  0.002787
   0.857456  0.002632
   0.871329  0.002447
   0.885203  0.002232
   0.899081  0.001983
   0.912957  0.001702
   0.926835  0.001395
   0.940713  0.001061
   0.954593  0.000693
   0.968446  0.000298
   0.982051 -0.000118
   0.994064 -0.000501
   1.000004 -0.000685
Dat file parser warnings
  • Line 161 - X value too large but included: 1.000004 -0.000685
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Polars for AG17 (ag17-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ag17-il50,000934.6 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ag17-il50,000536.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ag17-il100,000949.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   ag17-il100,000548.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ag17-il200,000964.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   ag17-il200,000560.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ag17-il500,000982.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   ag17-il500,000576.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   ag17-il1,000,000995.4 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ag17-il1,000,000589.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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