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WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il)

WORTMANN FX 05-H-126 AIRFOIL - Wortmann FX 05-H-126 rotorcraft airfoil


Airfoil fx05h126-il
Details Dat file Parser  
(fx05h126-il) WORTMANN FX 05-H-126 AIRFOIL
Wortmann FX 05-H-126 rotorcraft airfoil
Max thickness 12.6% at 37.1% chord.
Max camber 4.4% at 37.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
WORTMANN FX 05-H-126 AIRFOIL
      25.0      25.0
 
 0.0000000 0.0000000
 0.0042800 0.0118500
 0.0170400 0.0256700
 0.0380600 0.0398200
 0.0669900 0.0536200
 0.1033300 0.0675700
 0.1464400 0.0801300
 0.1956200 0.0912900
 0.2500000 0.1000200
 0.3086600 0.1055300
 0.3705900 0.1070600
 0.4347400 0.1042600
 0.5000000 0.0946200
 0.5652600 0.0788900
 0.6294100 0.0617200
 0.6913400 0.0457000
 0.7500000 0.0316300
 0.8043800 0.0203800
 0.8535600 0.0120000
 0.8966700 0.0060900
 0.9330100 0.0023200
 0.9616400 0.0005500
 0.9829600 -.0001900
 0.9957200 -.0001300
 1.0000000 0.0000000
 
 0.0000000 0.0000000
 0.0042800 -.0068800
 0.0170400 -.0113700
 0.0380600 -.0143600
 0.0669900 -.0158800
 0.1033300 -.0171900
 0.1464400 -.0177900
 0.1956200 -.0181700
 0.2500000 -.0186100
 0.3086600 -.0193000
 0.3705900 -.0190300
 0.4347400 -.0188000
 0.5000000 -.0179800
 0.5652600 -.0166000
 0.6294100 -.0153000
 0.6913400 -.0139600
 0.7500000 -.0124900
 0.8043800 -.0110800
 0.8535600 -.0093300
 0.8966700 -.0075300
 0.9330100 -.0056800
 0.9616400 -.0040700
 0.9829600 -.0023800
 0.9957200 -.0009200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fx05h126-il50,000919.1 at α=13.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx05h126-il50,000514.5 at α=12.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx05h126-il100,000925.1 at α=11.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx05h126-il100,000524.3 at α=11°Mach=0 Ncrit=5Xfoil predictionDetails
   fx05h126-il200,000966.3 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fx05h126-il200,000570.8 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fx05h126-il500,0009121.3 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx05h126-il500,0005116.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   fx05h126-il1,000,0009158.3 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fx05h126-il1,000,0005145.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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