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GOE 770 AIRFOIL (goe770-il)

GOE 770 AIRFOIL - Gottingen 770 airfoil


Airfoil goe770-il
Details Dat file Parser  
(goe770-il) GOE 770 AIRFOIL
Gottingen 770 airfoil
Max thickness 21% at 30% chord.
Max camber 4% at 30% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 770 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0125000 0.0427200
 0.0250000 0.0562300
 0.0500000 0.0769600
 0.1000000 0.1056200
 0.1500000 0.1242800
 0.2000000 0.1369400
 0.3000000 0.1453600
 0.4000000 0.1394800
 0.5000000 0.1223000
 0.6000000 0.0991200
 0.7000000 0.0750400
 0.8000000 0.0505600
 0.9000000 0.0266800
 0.9500000 0.0146400
 1.0000000 0.0026000

 0.0000000 0.0000000
 0.0125000 -.0174800
 0.0250000 -.0255700
 0.0500000 -.0356400
 0.1000000 -.0473800
 0.1500000 -.0558200
 0.2000000 -.0613600
 0.3000000 -.0645400
 0.4000000 -.0640200
 0.5000000 -.0563000
 0.6000000 -.0454800
 0.7000000 -.0341600
 0.8000000 -.0227400
 0.9000000 -.0114200
 0.9500000 -.0059600
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 770 AIRFOIL (goe770-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe770-il50,00092.9 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe770-il50,000511.3 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe770-il100,000919.2 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe770-il100,000536.6 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe770-il200,000953.6 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe770-il200,000559.3 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe770-il500,000987.7 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe770-il500,000586.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe770-il1,000,0009112.7 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe770-il1,000,0005109 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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