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GOE 298 AIRFOIL (goe298-il)

GOE 298 AIRFOIL - Gottingen 298 airfoil


Airfoil goe298-il
Details Dat file Parser  
(goe298-il) GOE 298 AIRFOIL
Gottingen 298 airfoil
Max thickness 12.8% at 19.6% chord.
Max camber 4.5% at 39.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 298 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0113300 0.0282700
 0.0233400 0.0399700
 0.0475900 0.0581700
 0.0720800 0.0703900
 0.0967700 0.0789100
 0.1462200 0.0912600
 0.1959500 0.0988200
 0.2956900 0.1039600
 0.3956900 0.1040000
 0.4960800 0.0944600
 0.5966500 0.0809300
 0.6973300 0.0626500
 0.7982100 0.0430900
 0.8990900 0.0218700
 0.9494700 0.0127600
 1.0000000 0.0029500

 0.0000000 0.0000000
 0.0135800 -.0260400
 0.0264000 -.0338100
 0.0516700 -.0402600
 0.0767100 -.0412200
 0.1016200 -.0389900
 0.1514100 -.0340200
 0.2012000 -.0289600
 0.3008300 -.0201300
 0.4005400 -.0130000
 0.5004100 -.0094700
 0.6002900 -.0070200
 0.7002400 -.0055300
 0.8001700 -.0041300
 0.9001000 -.0023900
 0.9500800 -.0020200
 1.0000000 -.0029500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 298 AIRFOIL (goe298-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe298-il50,000927.6 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe298-il50,000535.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe298-il100,000952.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe298-il100,000552.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe298-il200,000971.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe298-il200,000565.5 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe298-il500,000991.7 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe298-il500,000588.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe298-il1,000,0009112.4 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe298-il1,000,0005103.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
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