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USA 34 AIRFOIL (usa34-il)

USA 34 AIRFOIL - USA-34 airfoil


Airfoil usa34-il
Details Dat file Parser  
(usa34-il) USA 34 AIRFOIL
USA-34 airfoil
Max thickness 18% at 29.5% chord.
Max camber 7.7% at 39.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
USA 34 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0110100 0.0433500
 0.0229800 0.0597400
 0.0472500 0.0825200
 0.0717500 0.0983100
 0.0963100 0.1121000
 0.1456900 0.1316700
 0.1952200 0.1462600
 0.2947200 0.1624500
 0.3947000 0.1636500
 0.4950200 0.1538600
 0.5955700 0.1370700
 0.6964400 0.1103000
 0.7974700 0.0785300
 0.8985900 0.0437600
 0.9492100 0.0243800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0128600 -.0145900
 0.0255600 -.0211900
 0.0508600 -.0303800
 0.0759500 -.0330800
 0.1009900 -.0337800
 0.1509000 -.0311800
 0.2007900 -.0275800
 0.3004800 -.0173900
 0.4002300 -.0091900
 0.5001000 -.0050000
 0.6000400 -.0028000
 0.7000500 -.0026000
 0.8000801 -.0034000
 0.9001300 -.0042000
 0.9501400 -.0046000
 1.0000000 0.0000000
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Lednicer format dat file
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Polars for USA 34 AIRFOIL (usa34-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   usa34-il50,00094 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   usa34-il50,00059.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   usa34-il100,00099 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   usa34-il100,000540.9 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   usa34-il200,000966.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   usa34-il200,000560.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   usa34-il500,000986.6 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   usa34-il500,000575 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   usa34-il1,000,0009104.8 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   usa34-il1,000,000587.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
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