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GOE 277 (DAIMLER VIII) AIRFOIL (goe277-il)

GOE 277 (DAIMLER VIII) AIRFOIL - Gottingen 277 (DAIMLER VIII) airfoil


Airfoil goe277-il
Details Dat file Parser  
(goe277-il) GOE 277 (DAIMLER VIII) AIRFOIL
Gottingen 277 (DAIMLER VIII) airfoil
Max thickness 8.3% at 29.9% chord.
Max camber 4.4% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 277 (DAIMLER VIII) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123300 0.0185100
 0.0247500 0.0283200
 0.0496200 0.0427500
 0.0745300 0.0526700
 0.0994500 0.0609000
 0.1493400 0.0735400
 0.1992700 0.0813900
 0.2992300 0.0855900
 0.3992500 0.0831900
 0.4993100 0.0761900
 0.5994000 0.0662900
 0.6995201 0.0533000
 0.7996500 0.0391000
 0.8998100 0.0214000
 0.9498900 0.0117500
 1.0000000 0.0016000

 0.0000000 0.0000000
 0.0125900 -.0094900
 0.0250900 -.0103700
 0.0500800 -.0090500
 0.0750600 -.0077500
 0.1000500 -.0063900
 0.1500300 -.0037500
 0.2000100 -.0015000
 0.2999800 0.0022000
 0.3999700 0.0038000
 0.4999600 0.0047000
 0.5999600 0.0044000
 0.6999700 0.0033600
 0.7999800 0.0022000
 0.8999900 0.0007000
 0.9500100 -.0005500
 1.0000000 -.0016000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 277 (DAIMLER VIII) AIRFOIL (goe277-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe277-il50,000934 at α=10°Mach=0 Ncrit=9Xfoil predictionDetails
   goe277-il50,000538.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe277-il100,000954.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe277-il100,000555.7 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe277-il200,000973.5 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe277-il200,000573.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe277-il500,0009100.9 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe277-il500,000598.7 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe277-il1,000,0009122.6 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe277-il1,000,0005118.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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