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GOE 174 (ALBATROS 5020) AIRFOIL (goe174-il)

GOE 174 (ALBATROS 5020) AIRFOIL - Gottingen 174 (Albatros 5020) airfoil


Airfoil goe174-il
Details Dat file Parser  
(goe174-il) GOE 174 (ALBATROS 5020) AIRFOIL
Gottingen 174 (Albatros 5020) airfoil
Max thickness 8.6% at 19.9% chord.
Max camber 5.6% at 39.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 174 (ALBATROS 5020) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123600 0.0212800
 0.0247900 0.0317700
 0.0496900 0.0465400
 0.0746000 0.0599000
 0.0995300 0.0689700
 0.1494400 0.0828100
 0.1993800 0.0913500
 0.2993500 0.0967200
 0.3993600 0.0945000
 0.4994200 0.0863700
 0.5995000 0.0737500
 0.6995900 0.0600200
 0.7997100 0.0425000
 0.8998400 0.0243700
 0.9499000 0.0147100
 1.0000000 0.0014500

 0.0000000 0.0000000
 0.0125500 -.0081200
 0.0250500 -.0080300
 0.0500500 -.0072600
 0.0750400 -.0058900
 0.1000200 -.0041200
 0.1500000 -.0000900
 0.1999600 0.0055500
 0.2999100 0.0126200
 0.3998900 0.0169000
 0.4998800 0.0175700
 0.5999000 0.0152500
 0.6999199 0.0124200
 0.7999400 0.0090000
 0.8999700 0.0037700
 0.9499900 0.0008100
 1.0000000 -.0014500
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Lednicer format dat file
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Polars for GOE 174 (ALBATROS 5020) AIRFOIL (goe174-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe174-il50,000929.1 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe174-il50,000540 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe174-il100,000953.2 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe174-il100,000559 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe174-il200,000975.3 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe174-il200,000576.6 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe174-il500,0009104.4 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe174-il500,0005101.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe174-il1,000,0009125.8 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe174-il1,000,0005117.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
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