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EPPLER 297 AIRFOIL (e297-il)

EPPLER 297 AIRFOIL - Eppler E297 tailplane airfoil


Airfoil e297-il
Details Dat file Parser  
(e297-il) EPPLER 297 AIRFOIL
Eppler E297 tailplane airfoil
Max thickness 11.4% at 37.7% chord.
Max camber 0% at 0% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
EPPLER 297 AIRFOIL
       35.       36.

 0.0000500 0.0004900
 0.0001800 0.0010200
 0.0003800 0.0015600
 0.0009600 0.0026900
 0.0017500 0.0038700
 0.0033200 0.0057200
 0.0117700 0.0121700
 0.0250700 0.0187900
 0.0430500 0.0252500
 0.0655800 0.0313700
 0.0924900 0.0370100
 0.1235400 0.0420600
 0.1584200 0.0464700
 0.1967900 0.0501700
 0.2382500 0.0531000
 0.2823900 0.0552300
 0.3287500 0.0565200
 0.3768400 0.0569400
 0.4261800 0.0564900
 0.4762400 0.0551500
 0.5265100 0.0529200
 0.5765100 0.0497900
 0.6257400 0.0457600
 0.6737500 0.0408000
 0.7203200 0.0348400
 0.7654700 0.0282500
 0.8087700 0.0217700
 0.8494000 0.0159300
 0.8865500 0.0109600
 0.9194400 0.0070000
 0.9473900 0.0040400
 0.9698400 0.0019700
 0.9863700 0.0007000
 0.9965500 0.0001300
 1.0000000 0.0000000

 0.0000500 0.0004900
 0.0000500 -.0004900
 0.0001800 -.0010200
 0.0003800 -.0015600
 0.0009600 -.0026900
 0.0017500 -.0038700
 0.0033200 -.0057200
 0.0117700 -.0121700
 0.0250700 -.0187900
 0.0430500 -.0252500
 0.0655800 -.0313700
 0.0924900 -.0370100
 0.1235400 -.0420600
 0.1584200 -.0464700
 0.1967900 -.0501700
 0.2382500 -.0531000
 0.2823900 -.0552300
 0.3287500 -.0565200
 0.3768400 -.0569400
 0.4261800 -.0564900
 0.4762400 -.0551500
 0.5265100 -.0529200
 0.5765100 -.0497900
 0.6257400 -.0457600
 0.6737500 -.0408000
 0.7203200 -.0348400
 0.7654700 -.0282500
 0.8087700 -.0217700
 0.8494000 -.0159300
 0.8865500 -.0109600
 0.9194400 -.0070000
 0.9473900 -.0040400
 0.9698400 -.0019700
 0.9863700 -.0007000
 0.9965500 -.0001300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for EPPLER 297 AIRFOIL (e297-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   e297-il50,000929.3 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e297-il50,000528.8 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   e297-il100,000943.1 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e297-il100,000534.9 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e297-il200,000946.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   e297-il200,000539.6 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   e297-il500,000956 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   e297-il500,000551.1 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   e297-il1,000,000961.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   e297-il1,000,000560.4 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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