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SIKORSKY GS-1 AIRFOIL (gs1-il)

SIKORSKY GS-1 AIRFOIL - Gluharoff/Sikorsky GS-1 airfoil


Airfoil gs1-il
Details Dat file Parser  
(gs1-il) SIKORSKY GS-1 AIRFOIL
Gluharoff/Sikorsky GS-1 airfoil
Max thickness 13.9% at 30% chord.
Max camber 4.1% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
SIKORSKY GS-1 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0125000 0.0252300
 0.0250000 0.0357500
 0.0500000 0.0504000
 0.0750000 0.0618500
 0.1500000 0.0867000
 0.2000000 0.0968000
 0.3000000 0.1065000
 0.4000000 0.1059000
 0.5000000 0.0980000
 0.6000000 0.0847000
 0.7000000 0.0679000
 0.8000000 0.0476000
 0.9000000 0.0248000
 0.9500000 0.0124000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125000 -.0210800
 0.0250000 -.0281500
 0.0500000 -.0355000
 0.0750000 -.0393500
 0.1500000 -.0417000
 0.2000000 -.0400000
 0.3000000 -.0325000
 0.4000000 -.0234000
 0.5000000 -.0153000
 0.6000000 -.0089000
 0.7000000 -.0045000
 0.8000000 -.0017000
 0.9000000 0.0009000
 0.9500000 0.0011000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for SIKORSKY GS-1 AIRFOIL (gs1-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   gs1-il50,00099.2 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   gs1-il50,000529.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   gs1-il100,000951 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   gs1-il100,000554.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   gs1-il200,000974.6 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   gs1-il200,000574.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   gs1-il500,0009105.4 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   gs1-il500,0005100.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   gs1-il1,000,0009129.4 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   gs1-il1,000,0005119.8 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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