Airfoil Tools
Search 1636 airfoils Google+
You have 0 airfoils loaded.
Your Reynold number range is 50,000 to 1,000,000. (set)

GOE 29B AIRFOIL (goe29b-il)

GOE 29B AIRFOIL - Gottingen 29B airfoil


Airfoil goe29b-il
Details Dat file Parser  
(goe29b-il) GOE 29B AIRFOIL
Gottingen 29B airfoil
Max thickness 9.4% at 19.8% chord.
Max camber 6.5% at 29.8% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 29B AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0120400 0.0248200
 0.0242800 0.0389500
 0.0488800 0.0600100
 0.0736200 0.0743700
 0.0984300 0.0843300
 0.1481700 0.0986600
 0.1980300 0.1056800
 0.2979200 0.1120400
 0.3980100 0.1072000
 0.4982100 0.0962700
 0.5985100 0.0802300
 0.6988300 0.0630000
 0.7992000 0.0428700
 0.8995900 0.0218300
 0.9497800 0.0115700
 1.0000000 0.0014000

 0.0000000 0.0000000
 0.0128200 -.0169600
 0.0253600 -.0195300
 0.0503000 -.0162600
 0.0751800 -.0096000
 0.1000800 -.0042400
 0.1499100 0.0050900
 0.1997800 0.0116200
 0.2996500 0.0189700
 0.3996100 0.0208300
 0.4996200 0.0204900
 0.5996500 0.0186500
 0.6997200 0.0153100
 0.7998000 0.0108800
 0.8999200 0.0042400
 0.9499800 0.0011700
 1.0000000 -.0014000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

GOE 207 (AVIATIK V8) AIRFOILPreviewDetails
GOE 164 (MVA MK.10) AIRFOILPreviewDetails
NACA M9 AIRFOILPreviewDetails
GOE 311 (MVA H.43) AIRFOILPreviewDetails
GOE 63 AIRFOILPreviewDetails
GOE 14 AIRFOILPreviewDetails
GOE 174 (ALBATROS 5020) AIRFOILPreviewDetails
GOE 182 (MVA H.27) AIRFOILPreviewDetails
GOE 360 AIRFOILPreviewDetails
GOE 176 (ALBATROS 7020) AIRFOILPreviewDetails

Polars for GOE 29B AIRFOIL (goe29b-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe29b-il50,000922.9 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe29b-il50,000537.7 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe29b-il100,000952.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe29b-il100,000557.8 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe29b-il200,000977.2 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe29b-il200,000575 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe29b-il500,000999.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe29b-il500,000594.8 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe29b-il1,000,0009118.1 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   goe29b-il1,000,0005116.5 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit