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GOE 626 AIRFOIL (goe626-il)

GOE 626 AIRFOIL - Gottingen 626 airfoil


Airfoil goe626-il
Details Dat file Parser  
(goe626-il) GOE 626 AIRFOIL
Gottingen 626 airfoil
Max thickness 16.5% at 19.3% chord.
Max camber 5.1% at 49.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 626 AIRFOIL
       17.       17.

 0.0000100 0.0000000
 0.0106300 0.0277200
 0.0221000 0.0429900
 0.0459100 0.0606000
 0.0699900 0.0742200
 0.0942400 0.0853600
 0.1432400 0.1001700
 0.1925100 0.1109900
 0.2918600 0.1207000
 0.3919700 0.1189600
 0.4925600 0.1102500
 0.5935200 0.0960600
 0.6946400 0.0793900
 0.7961400 0.0572400
 0.8979000 0.0311100
 0.9488800 0.0165500
 1.0000000 0.0000000

 0.0000100 0.0000000
 0.0140300 -.0225500
 0.0270100 -.0296800
 0.0527300 -.0404400
 0.0781600 -.0467200
 0.1034500 -.0510200
 0.1537300 -.0551200
 0.2036300 -.0537500
 0.3025700 -.0380800
 0.4014500 -.0214000
 0.5005200 -.0077100
 0.5998700 0.0019900
 0.6994800 0.0077100
 0.7993600 0.0094600
 0.8995500 0.0067200
 0.9497200 0.0041100
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 626 AIRFOIL (goe626-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe626-il50,00097.4 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe626-il50,000530.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe626-il100,000948.9 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe626-il100,000551.6 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe626-il200,000971.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe626-il200,000564.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe626-il500,000990.4 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe626-il500,000582.9 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe626-il1,000,0009107.3 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe626-il1,000,000594.9 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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