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GOE 371 AIRFOIL (goe371-il)

GOE 371 AIRFOIL - Gottingen 371 airfoil


Airfoil goe371-il
Details Dat file Parser  
(goe371-il) GOE 371 AIRFOIL
Gottingen 371 airfoil
Max thickness 7% at 29.9% chord.
Max camber 4.6% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 371 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123900 0.0175800
 0.0248300 0.0266600
 0.0497500 0.0388200
 0.0746900 0.0479900
 0.0996400 0.0551500
 0.1495800 0.0649700
 0.1995300 0.0718000
 0.2994800 0.0794500
 0.3994900 0.0786000
 0.4995200 0.0737500
 0.5995700 0.0659000
 0.6996601 0.0525500
 0.7997600 0.0372000
 0.8998700 0.0198500
 0.9499300 0.0101700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125500 -.0074200
 0.0250500 -.0073400
 0.0500400 -.0061700
 0.0750300 -.0045100
 0.1000200 -.0023500
 0.1499900 0.0014700
 0.1999700 0.0048000
 0.2999400 0.0099500
 0.3999100 0.0136000
 0.4999000 0.0152500
 0.5999000 0.0149000
 0.6999199 0.0125500
 0.7999400 0.0092000
 0.8999700 0.0043500
 0.9499900 0.0016700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 371 AIRFOIL (goe371-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe371-il50,000937.6 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe371-il50,000543.3 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe371-il100,000961.1 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe371-il100,000562.1 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe371-il200,000982 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe371-il200,000580 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe371-il500,0009108.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe371-il500,0005103.9 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe371-il1,000,0009129.8 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe371-il1,000,0005120.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
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