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GOE 701 AIRFOIL (goe701-il)

GOE 701 AIRFOIL - Gottingen 701 airfoil


Airfoil goe701-il
Details Dat file Parser  
(goe701-il) GOE 701 AIRFOIL
Gottingen 701 airfoil
Max thickness 12.5% at 29.6% chord.
Max camber 4.9% at 39.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 701 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0116900 0.0239000
 0.0238200 0.0348100
 0.0481900 0.0531400
 0.0727600 0.0659700
 0.0974200 0.0758100
 0.1469200 0.0897100
 0.1966600 0.0981900
 0.2963400 0.1075800
 0.3963000 0.1089700
 0.4964900 0.1033800
 0.5968800 0.0917900
 0.6974600 0.0747100
 0.7981800 0.0536400
 0.8990100 0.0290700
 0.9495000 0.0147800
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0130600 -.0165600
 0.0257900 -.0231200
 0.0509800 -.0287700
 0.0760500 -.0309100
 0.1010400 -.0305600
 0.1509500 -.0278700
 0.2008100 -.0236700
 0.3005700 -.0167800
 0.4003900 -.0113900
 0.5002900 -.0084900
 0.6002200 -.0065900
 0.7002100 -.0061900
 0.8001800 -.0052900
 0.9001200 -.0034000
 0.9500600 -.0017000
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 701 AIRFOIL (goe701-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe701-il50,000919.5 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe701-il50,000531.6 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe701-il100,000954.7 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe701-il100,000553.7 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe701-il200,000978.9 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe701-il200,000573.7 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe701-il500,0009108.7 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe701-il500,000594.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe701-il1,000,0009127.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe701-il1,000,0005101.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
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