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GOE 702 AIRFOIL (goe702-il)

GOE 702 AIRFOIL - Gottingen 702 airfoil


Airfoil goe702-il
Details Dat file Parser  
(goe702-il) GOE 702 AIRFOIL
Gottingen 702 airfoil
Max thickness 16.6% at 19.4% chord.
Max camber 5.1% at 39.4% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 702 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0109000 0.0310600
 0.0226500 0.0456700
 0.0466100 0.0659000
 0.0708200 0.0811500
 0.0951700 0.0939000
 0.1441900 0.1129300
 0.1935700 0.1249700
 0.2931700 0.1326000
 0.3935000 0.1262600
 0.4941800 0.1129500
 0.5952800 0.0916600
 0.6965800 0.0663700
 0.7979100 0.0405900
 0.8991300 0.0168100
 0.9495700 0.0084000
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0136800 -.0228000
 0.0265800 -.0306300
 0.0519800 -.0383200
 0.0771700 -.0420300
 0.1022300 -.0432400
 0.1522200 -.0431600
 0.2021200 -.0410900
 0.3016700 -.0324600
 0.4012000 -.0233400
 0.5008600 -.0167100
 0.6006700 -.0130700
 0.7005400 -.0104200
 0.8004500 -.0087800
 0.9002600 -.0051400
 0.9501300 -.0025700
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 702 AIRFOIL (goe702-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe702-il50,00094.1 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe702-il50,000520.6 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   goe702-il100,000932 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   goe702-il100,000543.1 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe702-il200,000957.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe702-il200,000561.6 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe702-il500,000988.2 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe702-il500,000589.7 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe702-il1,000,0009117.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe702-il1,000,0005116.2 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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