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Eiffel 10 (Wright) - 1903 Wright Flyer airfoil (eiffel10-il)

Eiffel 10 (Wright) - 1903 Wright Flyer airfoil - Eiffel 10 (Wright) - 1903 Wright Flyer airfoil


Airfoil eiffel10-il
Details Dat file Parser  
(eiffel10-il) Eiffel 10 (Wright) - 1903 Wright Flyer airfoil
Eiffel 10 (Wright) - 1903 Wright Flyer airfoil
Max thickness 2.7% at 0% chord.
Max camber 6.1% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
Eiffel 10 (Wright) - 1903 Wright Flyer airfoil
1.0000  0.0064  
 .9500  0.0143  
 .9000  0.0220  
 .8000  0.0370  
 .7000  0.0510  
 .6000  0.0623  
 .5000  0.0693  
 .4000  0.0718  
 .3000  0.0701  
 .2000  0.0614  
 .1500  0.0550  
 .1000  0.0468  
 .0750  0.0423  
 .0500  0.0375  
 .0250  0.0323  
 .0125  0.0296  
 .0000  0.0273    
 .0000  0.0000
 .0125  0.0032
 .0250  0.0060
 .0500  0.0117
 .0750  0.0170
 .1000  0.0223
 .1500  0.0315
 .2000  0.0390
 .3000  0.0486
 .4000  0.0527
 .5000  0.0518
 .6000  0.0456
 .7000  0.0370
 .8000  0.0255
 .9000  0.0127
 .9500  0.0065
1.0000  0.0000
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Selig format dat file

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Polars for Eiffel 10 (Wright) - 1903 Wright Flyer airfoil (eiffel10-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   eiffel10-il50,000925.5 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   eiffel10-il50,000527 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   eiffel10-il100,000927.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   eiffel10-il100,000529.9 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   eiffel10-il200,000928.7 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   eiffel10-il200,000534.3 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   eiffel10-il500,000932.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   eiffel10-il500,000538.4 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   eiffel10-il1,000,000936.7 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   eiffel10-il1,000,000545.2 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
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