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Griffith 30% Suction Airfoil (griffith30symsuction-il)

Griffith 30% Suction Airfoil - Griffith 30% suction airfoil


Airfoil griffith30symsuction-il
Details Dat file Parser  
(griffith30symsuction-il) Griffith 30% Suction Airfoil
Griffith 30% suction airfoil
Max thickness 30.6% at 49.3% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
Griffith 30% Suction Airfoil
   1.000000       0.001000
   0.982693       0.001731
   0.952682       0.006072
   0.921669       0.011284
   0.888056       0.019998
   0.860746       0.029582
   0.835936       0.041796
   0.814728       0.057502
   0.790480       0.081301
   0.756160       0.104403
   0.720430       0.120788
   0.683590       0.131748
   0.645940       0.139612
   0.607780       0.145664
   0.569370       0.150001
   0.530990       0.152381
   0.492650       0.152852
   0.454350       0.151863
   0.416380       0.149988
   0.378870       0.147428
   0.342040       0.143962
   0.306090       0.139333
   0.271200       0.133699
   0.237600       0.127444
   0.205490       0.120757
   0.175040       0.113430
   0.146480       0.105132
   0.119990       0.095739
   0.095760       0.085388
   0.073950       0.074535
   0.054680       0.063419
   0.038110       0.051949
   0.024330       0.040344
   0.013380       0.029086
   0.005480       0.018515
   0.000980       0.008705
   0.000000       0.000000
   0.000980      -0.008705
   0.005480      -0.018515
   0.013380      -0.029086
   0.024330      -0.040344
   0.038110      -0.051949
   0.054680      -0.063419
   0.073950      -0.074535
   0.095760      -0.085388
   0.119990      -0.095739
   0.146480      -0.105132
   0.175040      -0.113430
   0.205490      -0.120757
   0.237600      -0.127444
   0.271200      -0.133699
   0.306090      -0.139333
   0.342040      -0.143962
   0.378870      -0.147428
   0.416380      -0.149988
   0.454350      -0.151863
   0.492650      -0.152852
   0.530990      -0.152381
   0.569370      -0.150001
   0.607780      -0.145664
   0.645940      -0.139612
   0.683590      -0.131748
   0.720430      -0.120788
   0.756160      -0.104403
   0.790480      -0.081301
   0.814728      -0.057502
   0.835936      -0.041796
   0.860746      -0.029582
   0.888056      -0.019998
   0.921669      -0.011284
   0.952682      -0.006072
   0.982693      -0.001731
   1.000000      -0.001000
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Selig format dat file

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Polars for Griffith 30% Suction Airfoil (griffith30symsuction-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   griffith30symsuction-il50,00094.7 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   griffith30symsuction-il50,000510.8 at α=14.5°Mach=0 Ncrit=5Xfoil predictionDetails
   griffith30symsuction-il100,000917.2 at α=14°Mach=0 Ncrit=9Xfoil predictionDetails
   griffith30symsuction-il100,000511 at α=15.5°Mach=0 Ncrit=5Xfoil predictionDetails
   griffith30symsuction-il200,000913.5 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   griffith30symsuction-il200,000510.7 at α=15.25°Mach=0 Ncrit=5Xfoil predictionDetails
   griffith30symsuction-il500,000915 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   griffith30symsuction-il500,000512.5 at α=14.75°Mach=0 Ncrit=5Xfoil predictionDetails
   griffith30symsuction-il1,000,000917.3 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   griffith30symsuction-il1,000,000515.3 at α=13.75°Mach=0 Ncrit=5Xfoil predictionDetails
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