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GOE 677 (= M 6) AIRFOIL (goe677-il)

GOE 677 (= M 6) AIRFOIL - Gottingen 677 (= M 6) airfoil


Airfoil goe677-il
Details Dat file Parser  
(goe677-il) GOE 677 (= M 6) AIRFOIL
Gottingen 677 (= M 6) airfoil
Max thickness 12% at 30% chord.
Max camber 2.2% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 677 (= M 6) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125000 0.0180300
 0.0250000 0.0275500
 0.0500000 0.0406000
 0.0750000 0.0491500
 0.1000000 0.0567000
 0.1500000 0.0678000
 0.2000000 0.0754000
 0.3000000 0.0826000
 0.4000000 0.0808000
 0.5000000 0.0745000
 0.6000000 0.0617000
 0.7000000 0.0474000
 0.8000000 0.0331000
 0.9000000 0.0183000
 0.9500000 0.0114000
 1.0000000 0.0040000

 0.0000000 0.0000000
 0.0125000 -.0169700
 0.0250000 -.0224500
 0.0500000 -.0274000
 0.0750000 -.0298500
 0.1000000 -.0318000
 0.1500000 -.0337000
 0.2000000 -.0356000
 0.3000000 -.0369000
 0.4000000 -.0377000
 0.5000000 -.0370000
 0.6000000 -.0358000
 0.7000000 -.0321000
 0.8000000 -.0259000
 0.9000000 -.0147000
 0.9500000 -.0076000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 677 (= M 6) AIRFOIL (goe677-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe677-il50,000929.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe677-il50,000533 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe677-il100,000949.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe677-il100,000548.9 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe677-il200,000966.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe677-il200,000563.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe677-il500,000987.2 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe677-il500,000573.3 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe677-il1,000,000994.1 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe677-il1,000,000581.1 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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