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GOE 390 AIRFOIL (goe390-il)

GOE 390 AIRFOIL - Gottingen 390 airfoil


Airfoil goe390-il
Details Dat file Parser  
(goe390-il) GOE 390 AIRFOIL
Gottingen 390 airfoil
Max thickness 20.3% at 29.2% chord.
Max camber 6.9% at 39.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 390 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0106900 0.0363300
 0.0222600 0.0551100
 0.0459200 0.0819800
 0.0699600 0.1013800
 0.0941800 0.1169900
 0.1430700 0.1394200
 0.1923400 0.1539700
 0.2916400 0.1680100
 0.3917100 0.1665900
 0.4922700 0.1554900
 0.5932900 0.1348200
 0.6946300 0.1078600
 0.7962400 0.0755100
 0.8979900 0.0403800
 0.9489800 0.0205100
 1.0000000 0.0010500

 0.0000000 0.0000000
 0.0138000 -.0260100
 0.0266400 -.0329700
 0.0519800 -.0397100
 0.0771000 -.0421600
 0.1021900 -.0440200
 0.1521400 -.0429300
 0.2020300 -.0407500
 0.3017200 -.0344900
 0.4013900 -.0279300
 0.5010500 -.0210700
 0.6007200 -.0145100
 0.7005000 -.0100500
 0.8002900 -.0058900
 0.9001700 -.0033200
 0.9501200 -.0023300
 1.0000000 -.0010500
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Lednicer format dat file
Selig format dat file

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Polars for GOE 390 AIRFOIL (goe390-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe390-il50,00093.8 at α=12°Mach=0 Ncrit=9Xfoil predictionDetails
   goe390-il50,000511.3 at α=1.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe390-il100,000926.1 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe390-il100,000540.4 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe390-il200,000962.9 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe390-il200,000558.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe390-il500,000985.2 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe390-il500,000578.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe390-il1,000,0009105.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe390-il1,000,000598.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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