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GOE 630 AIRFOIL (goe630-il)

GOE 630 AIRFOIL - Gottingen 630 airfoil


Airfoil goe630-il
Details Dat file Parser  
(goe630-il) GOE 630 AIRFOIL
Gottingen 630 airfoil
Max thickness 12.6% at 29.8% chord.
Max camber 7.7% at 39.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 630 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120600 0.0281900
 0.0243600 0.0413800
 0.0490300 0.0622600
 0.0737900 0.0781400
 0.0985800 0.0915300
 0.1482700 0.1118000
 0.1980500 0.1255700
 0.2978700 0.1371200
 0.3979000 0.1356700
 0.4980400 0.1262200
 0.5983000 0.1097700
 0.6986500 0.0868300
 0.7990600 0.0603900
 0.8995100 0.0314400
 0.9497500 0.0162200
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0127000 -.0128000
 0.0252300 -.0151100
 0.0502100 -.0137200
 0.0751800 -.0113300
 0.1001300 -.0084500
 0.1500400 -.0026700
 0.1999500 0.0031000
 0.2998200 0.0116500
 0.3997300 0.0177000
 0.4996900 0.0197500
 0.5997100 0.0188000
 0.6996800 0.0161100
 0.7998101 0.0124000
 0.8999100 0.0059500
 0.9499700 0.0022200
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 630 AIRFOIL (goe630-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe630-il50,00097.1 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe630-il50,000528.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe630-il100,000948.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe630-il100,000554.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe630-il200,000974.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe630-il200,000573.5 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe630-il500,0009103.7 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe630-il500,000599.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe630-il1,000,0009129 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe630-il1,000,0005123.1 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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