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

E. Bambino (ebambino7-il)

E. Bambino - E. Bambino airfoil


Airfoil ebambino7-il
Details Dat file Parser  
(ebambino7-il) E. Bambino
E. Bambino airfoil
Max thickness 6% at 40% chord.
Max camber 1.9% at 20% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
E. Bambino
1.0000     0.0270
0.9500     0.0290
0.9000     0.0325
0.8000     0.0400
0.7000     0.0460
0.6000     0.0520
0.5000     0.0580
0.4000     0.0600
0.3000     0.0580
0.2000     0.0555
0.1500     0.0510
0.1000     0.0480
0.0750     0.0430
0.0500     0.0360
0.0250     0.0295
0.0125     0.0160
0.0000     0.0050
0.0125     0.0020
0.0250     0.0000
0.0500     0.0000
0.0750     0.0000
0.1000     0.0000
0.1500     0.0000
0.2000     0.0000
0.3000     0.0000
0.4000     0.0000
0.5000     0.0000
0.6000     0.0000
0.7000     0.0010
0.8000     0.0075
0.9000     0.0140
0.9500     0.0180
1.0000     0.0220
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

SIKORSKY SSC-A07 AIRFOILPreviewDetails
GOE 587 AIRFOILPreviewDetails
ONERA OA206 AIRFOILPreviewDetails
BOEING VERTOL V13006-.7 AIRFOILPreviewDetails
NACA M10 AIRFOILPreviewDetails
NACA M4 AIRFOILPreviewDetails
EH 2.0/7.0PreviewDetails
Coanda 2PreviewDetails
NASA/LANGLEY RC-08(N)1 AIRFOILPreviewDetails
BOEING-VERTOL VR-14 AIRFOILPreviewDetails

Polars for E. Bambino (ebambino7-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   ebambino7-il50,000926.3 at α=8.75°Mach=0 Ncrit=9Xfoil predictionDetails
   ebambino7-il50,000528 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ebambino7-il100,000935 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ebambino7-il100,000533 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ebambino7-il200,000946.3 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   ebambino7-il200,000537.5 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   ebambino7-il500,000953.6 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ebambino7-il500,000548.4 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   ebambino7-il1,000,000959.2 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   ebambino7-il1,000,000558.4 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit