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GOE 282 (DAIMLER XIII) AIRFOIL (goe282-il)

GOE 282 (DAIMLER XIII) AIRFOIL - Gottingen 282 (DAIMLER XIII) airfoil


Airfoil goe282-il
Details Dat file Parser  
(goe282-il) GOE 282 (DAIMLER XIII) AIRFOIL
Gottingen 282 (DAIMLER XIII) airfoil
Max thickness 9.1% at 19.9% chord.
Max camber 5% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 282 (DAIMLER XIII) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122600 0.0189600
 0.0245800 0.0325200
 0.0493800 0.0483400
 0.0742400 0.0588600
 0.0991300 0.0677800
 0.1489600 0.0807200
 0.1988700 0.0877700
 0.2987800 0.0946500
 0.3987900 0.0941400
 0.4988700 0.0874400
 0.5989900 0.0779300
 0.6991700 0.0647200
 0.7993700 0.0489100
 0.8996400 0.0282100
 0.9497899 0.0165500
 1.0000000 0.0032000

 0.0000000 0.0000000
 0.0126300 -.0100400
 0.0251700 -.0128800
 0.0501900 -.0145500
 0.0752000 -.0151300
 0.1001800 -.0139100
 0.1501100 -.0087600
 0.2000400 -.0033200
 0.2999500 0.0039700
 0.3998900 0.0063200
 0.4999000 0.0075500
 0.5999000 0.0077400
 0.6999199 0.0063300
 0.7999500 0.0039200
 0.8999900 0.0005100
 0.9500200 -.0013400
 1.0000000 -.0032000
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Polars for GOE 282 (DAIMLER XIII) AIRFOIL (goe282-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe282-il50,000934.8 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe282-il50,000541 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe282-il100,000957 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe282-il100,000559 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe282-il200,000977.4 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe282-il200,000575.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe282-il500,0009102.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe282-il500,000594.8 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe282-il1,000,0009118.3 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe282-il1,000,0005105.1 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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