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GOE 210 (DAIMLER) AIRFOIL (goe210-il)

GOE 210 (DAIMLER) AIRFOIL - Gottingen 210 (DAIMLER) airfoil


Airfoil goe210-il
Details Dat file Parser  
(goe210-il) GOE 210 (DAIMLER) AIRFOIL
Gottingen 210 (DAIMLER) airfoil
Max thickness 6.6% at 30% chord.
Max camber 4.3% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 210 (DAIMLER) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0124100 0.0181600
 0.0248600 0.0281200
 0.0498000 0.0395500
 0.0747600 0.0486700
 0.0997200 0.0557000
 0.1496800 0.0639500
 0.1996500 0.0695000
 0.2996200 0.0753000
 0.3996200 0.0762000
 0.4996400 0.0726000
 0.5996800 0.0640000
 0.6997400 0.0512000
 0.7998200 0.0366000
 0.8999000 0.0207000
 0.9499500 0.0109500
 1.0000000 0.0008000

 0.0000000 0.0000000
 0.0125300 -.0057400
 0.0250300 -.0056000
 0.0500200 -.0044500
 0.0750100 -.0022700
 0.1000000 0.0000000
 0.1499800 0.0032500
 0.1999700 0.0058000
 0.2999600 0.0090000
 0.3999500 0.0106600
 0.4999400 0.0118000
 0.5999400 0.0112000
 0.6999600 0.0093900
 0.7999600 0.0072000
 0.8999800 0.0038000
 0.9499900 0.0014500
 1.0000000 -.0008000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 210 (DAIMLER) AIRFOIL (goe210-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe210-il50,000940.7 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe210-il50,000543.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe210-il100,000962 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe210-il100,000562 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe210-il200,000982.3 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe210-il200,000577.9 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe210-il500,0009105.1 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe210-il500,000586.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe210-il1,000,0009116.7 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe210-il1,000,000599.8 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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