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

AH-7-47-6 AIRFOIL (ah7476-il)

AH-7-47-6 AIRFOIL - Althaus AH 7-476 airfoil


Airfoil ah7476-il
Details Dat file Parser  
(ah7476-il) AH-7-47-6 AIRFOIL
Althaus AH 7-476 airfoil
Max thickness 5.9% at 20% chord.
Max camber 6.2% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
AH-7-47-6 AIRFOIL
       16.       16.

 0.0000000 0.0000000
 0.0124200 0.0180600
 0.0248800 0.0271100
 0.0498200 0.0392200
 0.0747800 0.0488400
 0.0997500 0.0564500
 0.1497000 0.0676700
 0.1996600 0.0759000
 0.2996100 0.0858500
 0.3996000 0.0878000
 0.4996100 0.0862500
 0.5996400 0.0807000
 0.6996800 0.0706500
 0.7997500 0.0546000
 0.8998500 0.0340500
 1.0000000 0.0035000

 0.0000000 0.0000000
 0.0125400 -.0079400
 0.0250300 -.0058900
 0.0500100 -.0032700
 0.0750000 0.0003400
 0.0999800 0.0034500
 0.1499500 0.0106700
 0.1999200 0.0169000
 0.2998800 0.0273500
 0.3998500 0.0343000
 0.4998300 0.0377500
 0.5998300 0.0387000
 0.6998400 0.0361500
 0.7998700 0.0291000
 0.8999299 0.0160500
 1.0000000 -.0035000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

E61 (5.64%)PreviewDetails
GOE 395 AIRFOILPreviewDetails
GOE 417 AIRFOILPreviewDetails
GOE 394 AIRFOILPreviewDetails
GOE 342 AIRFOILPreviewDetails
EPPLER 59 AIRFOILPreviewDetails
ARA-D 6% AIRFOILPreviewDetails
GOE 803 (HACKLINGER) AIRFOILPreviewDetails
GOE 483 AIRFOILPreviewDetails
SOKOLOV AIRFOILPreviewDetails

Polars for AH-7-47-6 AIRFOIL (ah7476-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ah7476-il50,000948.1 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah7476-il50,000548.9 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   ah7476-il100,000975.7 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah7476-il100,000574.4 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   ah7476-il200,0009107.2 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ah7476-il200,0005103.1 at α=2.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ah7476-il500,0009148.4 at α=2.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah7476-il500,0005110.4 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   ah7476-il1,000,0009138.1 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ah7476-il1,000,0005112.2 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit