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GOE 571 AIRFOIL (goe571-il)

GOE 571 AIRFOIL - Gottingen 571 airfoil


Airfoil goe571-il
Details Dat file Parser  
(goe571-il) GOE 571 AIRFOIL
Gottingen 571 airfoil
Max thickness 24.9% at 29.4% chord.
Max camber 9.8% at 29.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 571 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0113900 0.0403100
 0.0232100 0.0651400
 0.0471900 0.1023000
 0.0714000 0.1309600
 0.0957600 0.1541300
 0.1448900 0.1859800
 0.1943400 0.2058400
 0.2938700 0.2230800
 0.3940400 0.2168400
 0.4945900 0.1966000
 0.5954400 0.1658700
 0.6964100 0.1306500
 0.7974401 0.0929300
 0.8985600 0.0522100
 0.9491900 0.0296000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0131200 -.0226400
 0.0257000 -.0252900
 0.0507700 -.0281000
 0.0758000 -.0289200
 0.1007900 -.0287300
 0.1507900 -.0288500
 0.2007800 -.0284800
 0.3007200 -.0262300
 0.4006600 -.0239800
 0.5005800 -.0212300
 0.6005100 -.0184900
 0.7004300 -.0157400
 0.8003399 -.0124900
 0.9002500 -.0092400
 0.9502000 -.0073700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 571 AIRFOIL (goe571-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe571-il50,00093.7 at α=-12°Mach=0 Ncrit=9Xfoil predictionDetails
   goe571-il50,00055.7 at α=-7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe571-il100,00098.1 at α=-8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe571-il100,00058.6 at α=0.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe571-il200,000933.1 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe571-il200,000534 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe571-il500,000956.1 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe571-il500,000542.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe571-il1,000,000962.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe571-il1,000,000552.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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