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GOE 384 AIRFOIL (goe384-il)

GOE 384 AIRFOIL - Gottingen 384 airfoil


Airfoil goe384-il
Details Dat file Parser  
(goe384-il) GOE 384 AIRFOIL
Gottingen 384 airfoil
Max thickness 19.6% at 29.3% chord.
Max camber 6.9% at 39.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 384 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0111900 0.0323500
 0.0230300 0.0487300
 0.0470400 0.0731000
 0.0711900 0.0942800
 0.0955400 0.1101600
 0.1446000 0.1334500
 0.1939400 0.1498400
 0.2933300 0.1649700
 0.3933800 0.1637100
 0.4938200 0.1528700
 0.5947300 0.1303600
 0.6957700 0.1046400
 0.7970600 0.0726400
 0.8985299 0.0363500
 0.9492700 0.0181000
 1.0000000 0.0021500

 0.0000000 0.0000000
 0.0133400 -.0207600
 0.0261000 -.0271400
 0.0512800 -.0315300
 0.0763400 -.0331100
 0.1013400 -.0332000
 0.1513700 -.0337800
 0.2013500 -.0333600
 0.3012300 -.0304200
 0.4010700 -.0263800
 0.5009000 -.0223400
 0.6007400 -.0183000
 0.7005800 -.0142600
 0.8004100 -.0102200
 0.9002500 -.0061800
 0.9501700 -.0041700
 1.0000000 -.0021500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 384 AIRFOIL (goe384-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe384-il50,00093.9 at α=12.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe384-il50,000511.7 at α=1.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe384-il100,000927.3 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe384-il100,000539.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe384-il200,000963.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe384-il200,000559.1 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe384-il500,000987.1 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   goe384-il500,000578.4 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe384-il1,000,0009105.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe384-il1,000,0005100.5 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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