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GOE 492 AIRFOIL (goe492-il)

GOE 492 AIRFOIL - Gottingen 492 airfoil


Airfoil goe492-il
Details Dat file Parser  
(goe492-il) GOE 492 AIRFOIL
Gottingen 492 airfoil
Max thickness 6.2% at 29.9% chord.
Max camber 3.4% at 49.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 492 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0123800 0.0096500
 0.0248100 0.0148100
 0.0497200 0.0226200
 0.0746300 0.0294300
 0.0995400 0.0344000
 0.1494500 0.0438700
 0.1993600 0.0514900
 0.2992300 0.0612400
 0.3991900 0.0644900
 0.4992200 0.0627400
 0.5992900 0.0564900
 0.6994000 0.0477400
 0.7995600 0.0349900
 0.8997700 0.0187500
 0.9498800 0.0098700
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0125900 -.0073400
 0.0251200 -.0096900
 0.0501400 -.0108700
 0.0751400 -.0115600
 0.1001400 -.0115500
 0.1501300 -.0109000
 0.2001100 -.0085000
 0.3000100 -.0007500
 0.3999900 0.0025000
 0.4999400 0.0047500
 0.5999100 0.0070000
 0.6999000 0.0077500
 0.7999099 0.0075000
 0.8999500 0.0039500
 0.9499700 0.0021700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 492 AIRFOIL (goe492-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe492-il50,000931.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe492-il50,000539 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe492-il100,000957.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe492-il100,000557.4 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe492-il200,000981.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe492-il200,000578.6 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   goe492-il500,0009112 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe492-il500,000599.4 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe492-il1,000,0009128.6 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe492-il1,000,000595.5 at α=2°Mach=0 Ncrit=5Xfoil predictionDetails
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