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GOE 280 (DAIMLER XI) AIRFOIL (goe280-il)

GOE 280 (DAIMLER XI) AIRFOIL - Gottingen 280 (DAIMLER XI) airfoil


Airfoil goe280-il
Details Dat file Parser  
(goe280-il) GOE 280 (DAIMLER XI) AIRFOIL
Gottingen 280 (DAIMLER XI) airfoil
Max thickness 7.9% at 30% chord.
Max camber 4.5% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 280 (DAIMLER XI) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124500 0.0167300
 0.0249200 0.0306700
 0.0498800 0.0461300
 0.0748400 0.0575000
 0.0998300 0.0645700
 0.1498000 0.0741000
 0.1997800 0.0800400
 0.2997700 0.0851100
 0.3997700 0.0833800
 0.4997900 0.0771500
 0.5998200 0.0683200
 0.6998500 0.0558900
 0.7998900 0.0417600
 0.8999400 0.0234300
 0.9499600 0.0138600
 1.0000000 0.0040000

 0.0000000 0.0000000
 0.0125200 -.0066700
 0.0250200 -.0057300
 0.0500100 -.0025600
 0.0750000 -.0006000
 0.1000000 0.0010700
 0.1499900 0.0033000
 0.1999900 0.0048400
 0.2999800 0.0058100
 0.3999800 0.0055800
 0.4999900 0.0052500
 0.5999900 0.0045200
 0.6999900 0.0030400
 0.8000000 0.0013600
 0.9000000 -.0007700
 0.9500100 -.0023300
 1.0000000 -.0040000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 280 (DAIMLER XI) AIRFOIL (goe280-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe280-il50,000937.3 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe280-il50,000541.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe280-il100,000955.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe280-il100,000556.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe280-il200,000972.9 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe280-il200,000570.2 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe280-il500,000991.6 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe280-il500,000579.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe280-il1,000,000998.7 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe280-il1,000,000587.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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