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GOE 187 (SCHTTE-LANZ 2U10) AIRFOIL (goe187-il)

GOE 187 (SCHTTE-LANZ 2U10) AIRFOIL - Gottingen 187 (Schatte-Lanz 2U10) airfoil


Airfoil goe187-il
Details Dat file Parser  
(goe187-il) GOE 187 (SCHTTE-LANZ 2U10) AIRFOIL
Gottingen 187 (Schatte-Lanz 2U10) airfoil
Max thickness 8.3% at 30% chord.
Max camber 4.8% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 187 (SCHTTE-LANZ 2U10) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0125200 0.0204900
 0.0250300 0.0315800
 0.0500400 0.0465600
 0.0750400 0.0560400
 0.1000500 0.0643200
 0.1500600 0.0759800
 0.2000700 0.0842400
 0.3000700 0.0897600
 0.4000700 0.0873800
 0.5000600 0.0807000
 0.6000600 0.0689200
 0.7000400 0.0544400
 0.8000300 0.0387600
 0.9000200 0.0214800
 0.9500100 0.0125400
 1.0000000 0.0025000

 0.0000000 0.0000000
 0.0125000 -.0017100
 0.0250000 -.0006200
 0.0500000 0.0011100
 0.0750000 0.0021800
 0.1000000 0.0029900
 0.1500000 0.0042800
 0.2000000 0.0053400
 0.3000100 0.0069600
 0.4000100 0.0079800
 0.5000100 0.0079000
 0.6000100 0.0067200
 0.7000000 0.0055400
 0.8000000 0.0032600
 0.9000000 -.0007200
 0.9500000 -.0024600
 1.0000000 -.0025000
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Lednicer format dat file
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Polars for GOE 187 (SCHTTE-LANZ 2U10) AIRFOIL (goe187-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe187-il50,000931.8 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe187-il50,000540.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe187-il100,000953.7 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe187-il100,000558.2 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe187-il200,000974.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe187-il200,000576.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe187-il500,0009100.9 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe187-il500,000598.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe187-il1,000,0009118.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe187-il1,000,0005112.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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