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GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL (goe304-il)

GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL - Gottingen 304 (Friedrichshafen G02) airfoil


Airfoil goe304-il
Details Dat file Parser  
(goe304-il) GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL
Gottingen 304 (Friedrichshafen G02) airfoil
Max thickness 9% at 29.8% chord.
Max camber 6.3% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121000 0.0269800
 0.0244400 0.0379600
 0.0491900 0.0542300
 0.0740300 0.0651000
 0.0989000 0.0742700
 0.1487000 0.0873100
 0.1985700 0.0960500
 0.2984300 0.1057300
 0.3984200 0.1065200
 0.4985100 0.1004000
 0.5986900 0.0880900
 0.6989400 0.0714800
 0.7992401 0.0513700
 0.8995800 0.0282600
 0.9497700 0.0153000
 1.0000000 0.0011500

 0.0000000 0.0000000
 0.0127100 -.0142100
 0.0252300 -.0156300
 0.0501700 -.0117500
 0.0751200 -.0078800
 0.1000600 -.0039100
 0.1499600 0.0027300
 0.1998800 0.0082700
 0.2997600 0.0159500
 0.3997000 0.0199400
 0.4996900 0.0207200
 0.5997100 0.0195100
 0.6997800 0.0148900
 0.7998500 0.0098800
 0.8999400 0.0040600
 0.9499800 0.0013100
 1.0000000 -.0011500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 304 (FRIEDRICHSHAFEN G02) AIRFOIL (goe304-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe304-il50,000933.1 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   goe304-il50,000538.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe304-il100,000962 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe304-il100,000564.1 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe304-il200,000988.8 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe304-il200,000586.1 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe304-il500,0009122.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe304-il500,0005109.7 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe304-il1,000,0009145.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe304-il1,000,0005117.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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