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GOE 176 (ALBATROS 7020) AIRFOIL (goe176-il)

GOE 176 (ALBATROS 7020) AIRFOIL - Gottingen 176 (Albatros 7020) airfoil


Airfoil goe176-il
Details Dat file Parser  
(goe176-il) GOE 176 (ALBATROS 7020) AIRFOIL
Gottingen 176 (Albatros 7020) airfoil
Max thickness 10.3% at 19.8% chord.
Max camber 5.6% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 176 (ALBATROS 7020) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0121400 0.0220000
 0.0244400 0.0343900
 0.0492100 0.0487900
 0.0739900 0.0625900
 0.0988400 0.0718000
 0.1486200 0.0854000
 0.1984700 0.0949100
 0.2983900 0.0994200
 0.3984100 0.0987300
 0.4985400 0.0904500
 0.5987300 0.0783700
 0.6989800 0.0630900
 0.7992700 0.0452100
 0.8995700 0.0264300
 0.9497400 0.0161400
 1.0000000 0.0011500

 0.0000000 0.0000000
 0.0126200 -.0072000
 0.0251600 -.0098900
 0.0501900 -.0132900
 0.0752300 -.0153900
 0.1002500 -.0156800
 0.1502200 -.0136700
 0.2001300 -.0082700
 0.2999400 0.0038400
 0.3998000 0.0124600
 0.4997100 0.0178700
 0.5997100 0.0180900
 0.6924500 0.0158200
 0.7998000 0.0125200
 0.8998900 0.0065300
 0.9499500 0.0032400
 1.0000000 -.0011500
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Lednicer format dat file
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Polars for GOE 176 (ALBATROS 7020) AIRFOIL (goe176-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe176-il50,000930.3 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe176-il50,000540.2 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe176-il100,000956 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe176-il100,000557.5 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe176-il200,000973.7 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe176-il200,000573.6 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe176-il500,000999.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe176-il500,000587 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe176-il1,000,0009113.1 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe176-il1,000,000593.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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