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GOE 275 (DAIMLER VI) AIRFOIL (goe275-il)

GOE 275 (DAIMLER VI) AIRFOIL - Gottingen 275 (DAIMLER VI) airfoil


Airfoil goe275-il
Details Dat file Parser  
(goe275-il) GOE 275 (DAIMLER VI) AIRFOIL
Gottingen 275 (DAIMLER VI) airfoil
Max thickness 7.7% at 19.9% chord.
Max camber 4.7% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 275 (DAIMLER VI) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123100 0.0240000
 0.0247200 0.0347000
 0.0496100 0.0483000
 0.0745300 0.0575000
 0.0994700 0.0657100
 0.1493900 0.0757100
 0.1993300 0.0825100
 0.2993100 0.0855200
 0.3993300 0.0831300
 0.4993800 0.0769400
 0.5994500 0.0676600
 0.6995500 0.0561700
 0.7996700 0.0409800
 0.8998200 0.0226900
 0.9499000 0.0128900
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125600 -.0080000
 0.0250500 -.0066000
 0.0500300 -.0033900
 0.0750100 -.0015900
 0.1000000 -.0003900
 0.1499800 0.0027100
 0.1999600 0.0052200
 0.2999300 0.0087300
 0.3999100 0.0106400
 0.4999100 0.0114500
 0.5999100 0.0111600
 0.6999199 0.0103700
 0.7999400 0.0079800
 0.8999700 0.0039900
 0.9499800 0.0022900
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 275 (DAIMLER VI) AIRFOIL (goe275-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe275-il50,000934.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe275-il50,000540.2 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe275-il100,000953.1 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe275-il100,000555.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe275-il200,000972 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe275-il200,000573.3 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe275-il500,000999.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe275-il500,000594.3 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe275-il1,000,0009118.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe275-il1,000,0005106.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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