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GOE 503 AIRFOIL (goe503-il)

GOE 503 AIRFOIL - Gottingen 503 airfoil


Airfoil goe503-il
Details Dat file Parser  
(goe503-il) GOE 503 AIRFOIL
Gottingen 503 airfoil
Max thickness 15.6% at 29.7% chord.
Max camber 7% at 39.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 503 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0118500 0.0277800
 0.0240000 0.0425600
 0.0484800 0.0646400
 0.0730600 0.0827200
 0.0977100 0.0973000
 0.1472400 0.1174600
 0.1969200 0.1311300
 0.2965900 0.1449700
 0.3965900 0.1453200
 0.4968200 0.1351800
 0.5972300 0.1180300
 0.6977700 0.0949000
 0.7983800 0.0687600
 0.8991200 0.0376300
 0.9495300 0.0198100
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0127600 -.0112000
 0.0254000 -.0169000
 0.0505200 -.0223100
 0.0755800 -.0247200
 0.1005900 -.0251400
 0.1505500 -.0234600
 0.2004500 -.0192900
 0.3002600 -.0109400
 0.4001300 -.0056000
 0.5001400 -.0057500
 0.6002200 -.0093900
 0.7002600 -.0110400
 0.8002000 -.0087000
 0.9001300 -.0053500
 0.9500600 -.0026700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 503 AIRFOIL (goe503-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe503-il50,00094.2 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe503-il50,000515.7 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe503-il100,000932.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe503-il100,000546.4 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe503-il200,000968.5 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe503-il200,000567 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe503-il500,000996.4 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe503-il500,000591.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe503-il1,000,0009120.3 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe503-il1,000,0005109.8 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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