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GOE 527 AIRFOIL (goe527-il)

GOE 527 AIRFOIL - Gottingen 527 airfoil


Airfoil goe527-il
Details Dat file Parser  
(goe527-il) GOE 527 AIRFOIL
Gottingen 527 airfoil
Max thickness 16.5% at 29.5% chord.
Max camber 5.8% at 39.5% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 527 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0112500 0.0339200
 0.0231900 0.0488600
 0.0474000 0.0702500
 0.0717900 0.0866600
 0.0963500 0.0985700
 0.1456800 0.1168900
 0.1952600 0.1282200
 0.2948400 0.1394100
 0.3948900 0.1381100
 0.4953300 0.1263300
 0.5960000 0.1080500
 0.6968600 0.0847800
 0.7978300 0.0585200
 0.8988800 0.0302600
 0.9494200 0.0156300
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0130900 -.0160200
 0.0258000 -.0215500
 0.0510000 -.0271100
 0.0760800 -.0291900
 0.1011000 -.0297600
 0.1511300 -.0304100
 0.2010900 -.0295600
 0.3009600 -.0258600
 0.4007800 -.0211700
 0.5005900 -.0159800
 0.6004200 -.0112800
 0.7002800 -.0075900
 0.8001600 -.0043900
 0.9000800 -.0022000
 0.9500100 -.0003500
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for GOE 527 AIRFOIL (goe527-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe527-il50,00094.3 at α=10.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe527-il50,000515.9 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe527-il100,000936.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe527-il100,000547 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   goe527-il200,000969.5 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   goe527-il200,000569.4 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe527-il500,0009102.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   goe527-il500,000596.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe527-il1,000,0009128.8 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe527-il1,000,0005116.9 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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