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GOE 795 smoothed (goe795sm-il)

GOE 795 smoothed - Gottingen 795 airfoil (smoothed)


Airfoil goe795sm-il
Details Dat file Parser  
(goe795sm-il) GOE 795 smoothed
Gottingen 795 airfoil (smoothed)
Max thickness 8% at 30.9% chord.
Max camber 2.4% at 43.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
   GOE 795 smoothed
   1.00000  0.0
   0.99572  0.00101
   0.98296  0.00382
   0.96194  0.00793
   0.93301  0.01294
   0.89668  0.01862
   0.85355  0.02487
   0.80438  0.03156
   0.75000  0.03845
   0.69134  0.04524
   0.62941  0.05149
   0.56526  0.05680
   0.50000  0.06078
   0.43474  0.06319
   0.37059  0.06395
   0.33928  0.06373
   0.30866  0.06312
   0.27886  0.06210
   0.25000  0.06066
   0.22221  0.05877
   0.19562  0.05643
   0.17033  0.05367
   0.14645  0.05053
   0.12408  0.04706
   0.10332  0.04332
   0.08427  0.03934
   0.06699  0.03513
   0.05156  0.03071
   0.03806  0.02610
   0.02653  0.02135
   0.01704  0.01659
   0.00961  0.01195
   0.00428  0.00759
   0.00107  0.00357
   0.0     -0.00009
   0.00107 -0.00349
   0.00428 -0.00669
   0.00961 -0.00966
   0.01704 -0.01230
   0.02653 -0.01450
   0.03806 -0.01622
   0.05156 -0.01753
   0.06699 -0.01857
   0.08427 -0.01943
   0.10332 -0.02013
   0.12408 -0.02058
   0.14645 -0.02071
   0.17033 -0.02049
   0.19562 -0.01997
   0.22221 -0.01928
   0.25000 -0.01855
   0.27886 -0.01784
   0.30866 -0.01716
   0.33928 -0.01648
   0.37059 -0.01579
   0.43474 -0.01440
   0.50000 -0.01301
   0.56526 -0.01166
   0.62941 -0.01035
   0.69134 -0.00910
   0.75000 -0.00788
   0.80438 -0.00674
   0.85355 -0.00569
   0.89668 -0.00475
   0.93301 -0.00382
   0.96194 -0.00275
   0.98296 -0.00153
   0.99572 -0.00044
   1.00000  0.0
ZZ
Dat file parser warnings
  • Line 71 - Invalid characters : ZZ
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Selig format dat file

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Polars for GOE 795 smoothed (goe795sm-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe795sm-il50,000937.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe795sm-il50,000538 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe795sm-il100,000956.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe795sm-il100,000554.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe795sm-il200,000976.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe795sm-il200,000569.7 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe795sm-il500,0009101.5 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe795sm-il500,000586.2 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe795sm-il1,000,0009116.2 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe795sm-il1,000,000596.4 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
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