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GOE 229 (MVA H.39) AIRFOIL (goe229-il)

GOE 229 (MVA H.39) AIRFOIL - Gottingen 229 (MVA H.39) airfoil


Airfoil goe229-il
Details Dat file Parser  
(goe229-il) GOE 229 (MVA H.39) AIRFOIL
Gottingen 229 (MVA H.39) airfoil
Max thickness 19.3% at 29% chord.
Max camber 5.9% at 49.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 229 (MVA H.39) AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0109600 0.0232300
 0.0224100 0.0389900
 0.0557500 0.0640400
 0.0695400 0.0821200
 0.0936100 0.0962200
 0.1421600 0.1179500
 0.1913000 0.1309200
 0.2903100 0.1458000
 0.3901300 0.1484400
 0.4907500 0.1391300
 0.5918500 0.1226600
 0.6934000 0.0992100
 0.7953200 0.0703900
 0.8975300 0.0371900
 0.9487000 0.0195900
 1.0000000 0.0010000

 0.0000000 0.0000000
 0.0134400 -.0141100
 0.0262900 -.0192500
 0.0518000 -.0270600
 0.0772600 -.0338600
 0.1025400 -.0381800
 0.1530200 -.0453200
 0.2032600 -.0489800
 0.3031500 -.0473400
 0.4023500 -.0352400
 0.5012800 -.0191700
 0.6003100 -.0045800
 0.6995300 0.0070200
 0.7992900 0.0106500
 0.8994500 0.0083100
 0.9497600 0.0036600
 1.0000000 -.0010000
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Lednicer format dat file
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Polars for GOE 229 (MVA H.39) AIRFOIL (goe229-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe229-il50,000910.8 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe229-il50,000521.5 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe229-il100,000945.2 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe229-il100,000538.5 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe229-il200,000953.8 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe229-il200,000540.9 at α=-0.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe229-il500,000954.8 at α=-0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe229-il500,000547.1 at α=2.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe229-il1,000,000959.6 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   goe229-il1,000,000559.2 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
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