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GOE 284 AIRFOIL (goe284-il)

GOE 284 AIRFOIL - Gottingen 284 airfoil


Airfoil goe284-il
Details Dat file Parser  
(goe284-il) GOE 284 AIRFOIL
Gottingen 284 airfoil
Max thickness 17.7% at 29.3% chord.
Max camber 5.1% at 39.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 284 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0108800 0.0317600
 0.0227000 0.0450600
 0.0466400 0.0657900
 0.0708600 0.0810200
 0.0952400 0.0931700
 0.1441800 0.1138700
 0.1935400 0.1264000
 0.2929700 0.1373900
 0.3930100 0.1366000
 0.4937100 0.1229500
 0.5947200 0.1033200
 0.6958600 0.0808900
 0.7971300 0.0560700
 0.8985200 0.0288600
 0.9492300 0.0150500
 1.0000000 0.0029500

 0.0000000 0.0000000
 0.0137300 -.0240000
 0.0266100 -.0315400
 0.0520900 -.0408400
 0.0772900 -.0446500
 0.1023200 -.0453700
 0.1523100 -.0451100
 0.2022400 -.0437600
 0.3019800 -.0386500
 0.4017200 -.0335500
 0.5014600 -.0284500
 0.6012000 -.0233500
 0.7009300 -.0182500
 0.8006700 -.0131500
 0.9004100 -.0080400
 0.9502800 -.0054900
 1.0000000 -.0029500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 284 AIRFOIL (goe284-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe284-il50,00094.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe284-il50,000518 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe284-il100,000934.1 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe284-il100,000545.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe284-il200,000969 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe284-il200,000569.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe284-il500,0009103.5 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe284-il500,000595 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe284-il1,000,0009126.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe284-il1,000,0005107.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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