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GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL (goe318-il)

GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL - Gottingen 318 (Hansa-Brandenburg VI.5) airfoil


Airfoil goe318-il
Details Dat file Parser  
(goe318-il) GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL
Gottingen 318 (Hansa-Brandenburg VI.5) airfoil
Max thickness 9.1% at 29.9% chord.
Max camber 4.3% at 29.9% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0122900 0.0195300
 0.0246900 0.0290600
 0.0495400 0.0431300
 0.0744200 0.0544900
 0.0993300 0.0634500
 0.1491800 0.0773800
 0.1991100 0.0840100
 0.2990600 0.0888700
 0.3990900 0.0855300
 0.4992000 0.0755900
 0.5993600 0.0600500
 0.6995500 0.0429200
 0.7997200 0.0262800
 0.8998700 0.0125400
 0.9499300 0.0068700
 1.0000000 0.0020000

 0.0000000 0.0000000
 0.0126300 -.0108700
 0.0251300 -.0123300
 0.0501200 -.0117700
 0.0751200 -.0112000
 0.1001100 -.0098900
 0.1500800 -.0071100
 0.2000500 -.0049800
 0.3000300 -.0024200
 0.4000200 -.0017600
 0.5000200 -.0018000
 0.6000200 -.0018400
 0.7000300 -.0023800
 0.8000300 -.0030200
 0.9000300 -.0024600
 0.9500300 -.0025300
 1.0000000 -.0020000
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Lednicer format dat file
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Polars for GOE 318 (HANSA-BRANDENBURG VI.5) AIRFOIL (goe318-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe318-il50,000920.7 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe318-il50,000535.5 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe318-il100,000950.4 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe318-il100,000553.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe318-il200,000969 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe318-il200,000570 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   goe318-il500,000993.3 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe318-il500,000592.1 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe318-il1,000,0009113.9 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe318-il1,000,0005111 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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