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

EPPLER 332 AIRFOIL (e332-il)

EPPLER 332 AIRFOIL - Eppler E332 flying wing airfoil


Airfoil e332-il
Details Dat file Parser  
(e332-il) EPPLER 332 AIRFOIL
Eppler E332 flying wing airfoil
Max thickness 11.5% at 32.3% chord.
Max camber 3.1% at 22.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 332 AIRFOIL
       34.       39.

 0.0000100 -.0005000
 0.0000300 0.0009000
 0.0003800 0.0031700
 0.0026400 0.0089500
 0.0093800 0.0183400
 0.0201200 0.0283200
 0.0348300 0.0384300
 0.0534100 0.0483200
 0.0757300 0.0576900
 0.1015900 0.0662400
 0.1308000 0.0737100
 0.1631200 0.0798200
 0.1983700 0.0843100
 0.2364000 0.0869500
 0.2671000 0.0876000
 0.3204200 0.0862900
 0.3662000 0.0832600
 0.4140600 0.0787900
 0.4635900 0.0731400
 0.5142900 0.0666000
 0.5656100 0.0594500
 0.6169700 0.0519900
 0.6677000 0.0445000
 0.7171400 0.0372500
 0.7645700 0.0304400
 0.8092900 0.0242500
 0.8505900 0.0188000
 0.8878100 0.0141200
 0.9203300 0.0102000
 0.9476200 0.0068900
 0.9694600 0.0039600
 0.9858600 0.0016200
 0.9963500 0.0003300
 1.0000000 0.0000000

 0.0000100 -.0005000
 0.0001600 -.0017800
 0.0003000 -.0023700
 0.0004900 -.0029200
 0.0007400 -.0034200
 0.0010900 -.0038600
 0.0015400 -.0043000
 0.0020800 -.0047200
 0.0033700 -.0055500
 0.0049300 -.0063600
 0.0077500 -.0075400
 0.0112300 -.0087400
 0.0263200 -.0121700
 0.0471800 -.0150100
 0.0735600 -.0173700
 0.1052000 -.0194200
 0.1416300 -.0214000
 0.1822100 -.0234100
 0.2263000 -.0254300
 0.2732600 -.0273600
 0.3225000 -.0290700
 0.3734900 -.0304700
 0.4256600 -.0315200
 0.4784300 -.0321800
 0.5312300 -.0324200
 0.5834700 -.0322000
 0.6345700 -.0315200
 0.6839600 -.0303600
 0.7310900 -.0286700
 0.7754400 -.0264300
 0.8164900 -.0234800
 0.8541400 -.0195100
 0.8886400 -.0148400
 0.9197600 -.0102800
 0.9467400 -.0063600
 0.9689100 -.0032600
 0.9856900 -.0011800
 0.9963300 -.0002100
 1.0000000 0.0000000
No parser warnings Send to airfoil plotter
Add to comparison
Lednicer format dat file
Selig format dat file

Similar airfoils

EPPLER 333 AIRFOILPreviewDetails
EH 3.0/12PreviewDetails
EPPLER 331 AIRFOILPreviewDetails
BOEING-VERTOL VR-7 AIRFOIL WITH TABPreviewDetails
USA 45 M AIRFOILPreviewDetails
EPPLER 636 AIRFOILPreviewDetails
EPPLER 635 AIRFOILPreviewDetails
SIKORSKY SC1012R8 AIRFOILPreviewDetails
GOE 559 AIRFOILPreviewDetails
GOE 285 AIRFOILPreviewDetails

Polars for EPPLER 332 AIRFOIL (e332-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e332-il50,000917.4 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e332-il50,000527.7 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e332-il100,000940.7 at α=10.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e332-il100,000547.1 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e332-il200,000964.3 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e332-il200,000567.2 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
   e332-il500,000995.6 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e332-il500,000586 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e332-il1,000,0009107.9 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   e332-il1,000,0005101.8 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
Reynolds number calculator
Set Reynolds number and Ncrit rangeLowHigh
Reynolds Number
NCrit