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GOE 404 AIRFOIL (goe404-il)

GOE 404 AIRFOIL - Gottingen 404 airfoil


Airfoil goe404-il
Details Dat file Parser  
(goe404-il) GOE 404 AIRFOIL
Gottingen 404 airfoil
Max thickness 13.2% at 29.6% chord.
Max camber 5% at 29.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 404 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0115300 0.0312600
 0.0235700 0.0459300
 0.0480200 0.0636900
 0.0726000 0.0772600
 0.0972900 0.0871300
 0.1468800 0.1003700
 0.1965900 0.1098100
 0.2964000 0.1156200
 0.3965600 0.1107300
 0.4968700 0.1005500
 0.5973500 0.0850800
 0.6979200 0.0669100
 0.7985300 0.0472300
 0.8992500 0.0242700
 0.9496100 0.0125300
 1.0000000 0.0008000

 0.0000000 0.0000000
 0.0131500 -.0208900
 0.0258000 -.0258000
 0.0509300 -.0298200
 0.0759200 -.0295400
 0.1008600 -.0276600
 0.1507500 -.0240100
 0.2006300 -.0203600
 0.3005000 -.0161500
 0.4004100 -.0130500
 0.5003400 -.0110400
 0.6002800 -.0089300
 0.7001800 -.0058200
 0.8001300 -.0043200
 0.9001100 -.0034100
 0.9500700 -.0023500
 1.0000000 -.0008000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 404 AIRFOIL (goe404-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe404-il50,000915.2 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe404-il50,000531.6 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe404-il100,000945.2 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe404-il100,000550.8 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe404-il200,000968.8 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe404-il200,000569.7 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe404-il500,000998.8 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe404-il500,000594.2 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe404-il1,000,0009121.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe404-il1,000,0005110.7 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
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