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GOE 438 AIRFOIL (goe438-il)

GOE 438 AIRFOIL - Gottingen 438 airfoil


Airfoil goe438-il
Details Dat file Parser  
(goe438-il) GOE 438 AIRFOIL
Gottingen 438 airfoil
Max thickness 11% at 29.8% chord.
Max camber 3.8% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 438 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0119400 0.0223000
 0.0241800 0.0326000
 0.0488400 0.0462200
 0.0735500 0.0578400
 0.0983400 0.0664600
 0.1480200 0.0792000
 0.1978300 0.0869500
 0.2976900 0.0924400
 0.3977400 0.0904400
 0.4979100 0.0834500
 0.5982000 0.0719600
 0.6985400 0.0584600
 0.7989800 0.0409700
 0.8994500 0.0219900
 0.9497200 0.0112400
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0128700 -.0146800
 0.0255100 -.0203600
 0.0505700 -.0227400
 0.0755700 -.0226100
 0.1005600 -.0224900
 0.1505300 -.0212400
 0.2005000 -.0199900
 0.3004400 -.0174900
 0.4003700 -.0149900
 0.5003100 -.0124900
 0.6002500 -.0099900
 0.7001899 -.0075000
 0.8001300 -.0050000
 0.9000599 -.0025000
 0.9500300 -.0012500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 438 AIRFOIL (goe438-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe438-il50,000924.7 at α=11.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe438-il50,000535.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe438-il100,000949.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe438-il100,000552.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe438-il200,000968.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe438-il200,000568.4 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe438-il500,000995 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe438-il500,000590.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe438-il1,000,0009115.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe438-il1,000,0005106 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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