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

GOE 723 AIRFOIL (goe723-il)

GOE 723 AIRFOIL - Gottingen 723 airfoil


Airfoil goe723-il
Details Dat file Parser  
(goe723-il) GOE 723 AIRFOIL
Gottingen 723 airfoil
Max thickness 11.6% at 29.7% chord.
Max camber 4.5% at 49.7% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
GOE 723 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0118800 0.0218400
 0.0241100 0.0311900
 0.0487600 0.0433900
 0.0734700 0.0535900
 0.0982400 0.0618000
 0.1478300 0.0762100
 0.1975300 0.0866300
 0.2972400 0.0969700
 0.3972000 0.0983200
 0.4973900 0.0916800
 0.5977500 0.0790400
 0.6982200 0.0624000
 0.7987500 0.0437600
 0.8993300 0.0236300
 0.9496300 0.0130600
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0129900 -.0171300
 0.0255800 -.0202700
 0.0506700 -.0235600
 0.0757400 -.0258400
 0.1007700 -.0271300
 0.1507800 -.0272000
 0.2007200 -.0252800
 0.3005300 -.0184400
 0.4002700 -.0095900
 0.5000500 -.0017500
 0.5998800 0.0041000
 0.6998200 0.0064400
 0.7998300 0.0058000
 0.8999500 0.0016500
 0.9500300 -.0009200
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

FX 63-110 AIRFOILPreviewDetails
Curtis C-72PreviewDetails
EPPLER 393 AIRFOILPreviewDetails
FX 63-120 AIRFOILPreviewDetails
FX 83-W-108PreviewDetails
EPPLER 67 AIRFOILPreviewDetails
EPPLER 395 AIRFOILPreviewDetails
USA-35B AIRFOILPreviewDetails
S4022PreviewDetails
GOE 593 AIRFOILPreviewDetails

Polars for GOE 723 AIRFOIL (goe723-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   goe723-il50,000932 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe723-il50,000533.4 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   goe723-il100,000958.4 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   goe723-il100,000558.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   goe723-il200,000982.2 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe723-il200,000579.2 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   goe723-il500,0009114 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   goe723-il500,0005103.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   goe723-il1,000,0009136.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   goe723-il1,000,0005112 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit