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GOE 288 AIRFOIL (goe288-il)

GOE 288 AIRFOIL - Gottingen 288 airfoil


Airfoil goe288-il
Details Dat file Parser  
(goe288-il) GOE 288 AIRFOIL
Gottingen 288 airfoil
Max thickness 17.4% at 29.3% chord.
Max camber 5.5% at 39.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 288 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0110700 0.0272800
 0.0228300 0.0414000
 0.0467300 0.0624500
 0.0709000 0.0784100
 0.0951800 0.0921800
 0.1440600 0.1134400
 0.1933700 0.1266200
 0.2928500 0.1365300
 0.3929200 0.1352700
 0.4935400 0.1234400
 0.5944900 0.1052200
 0.6956000 0.0840100
 0.7968600 0.0599200
 0.8982800 0.0329200
 0.9490300 0.0184800
 1.0000000 0.0029500

 0.0000000 0.0000000
 0.0137300 -.0233800
 0.0265600 -.0298100
 0.0519500 -.0372800
 0.0771900 -.0417600
 0.1023100 -.0440400
 0.1523800 -.0455200
 0.2023400 -.0447100
 0.3019200 -.0365900
 0.4012400 -.0237000
 0.5006600 -.0125900
 0.6002400 -.0044800
 0.6999900 0.0001400
 0.7999300 0.0012800
 0.8999700 0.0006100
 0.9500500 -.0009600
 1.0000000 -.0029500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 288 AIRFOIL (goe288-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe288-il50,00097.6 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe288-il50,000527.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe288-il100,000943.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe288-il100,000550.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe288-il200,000970.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe288-il200,000569.4 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe288-il500,000996.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe288-il500,000591.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe288-il1,000,0009117.1 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe288-il1,000,0005113.9 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
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