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FAUVEL 14% AIRFOIL (fauvel-il)

FAUVEL 14% AIRFOIL - Fauvel 14% flying wing airfoil


Airfoil fauvel-il
Details Dat file Parser  
(fauvel-il) FAUVEL 14% AIRFOIL
Fauvel 14% flying wing airfoil
Max thickness 14% at 25.2% chord.
Max camber 2.5% at 25.2% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
FAUVEL 14% AIRFOIL
       18.       18.

 0.0000000 0.0000000
 0.0011073 0.0073763
 0.0139486 0.0314635
 0.0265991 0.0425664
 0.0518005 0.0579806
 0.0769359 0.0689001
 0.1020302 0.0770231
 0.1521485 0.0884749
 0.2021831 0.0942337
 0.2521488 0.0952981
 0.3020616 0.0927669
 0.4017920 0.0812125
 0.5014448 0.0643644
 0.6010416 0.0437210
 0.7007105 0.0279716
 0.8004306 0.0157180
 0.9002036 0.0070599
 1.0000000 -.0000000

 0.0000000 0.0000000
 0.0009064 -.0063070
 0.0131976 -.0196743
 0.0256179 -.0242523
 0.0505054 -.0302122
 0.0754237 -.0340747
 0.1003567 -.0369383
 0.1502402 -.0414671
 0.2001560 -.0437985
 0.2500953 -.0445319
 0.3000346 -.0452652
 0.3999131 -.0467320
 0.4997917 -.0481987
 0.5997362 -.0451710
 0.6997366 -.0383478
 0.7997838 -.0283285
 0.8998751 -.0153129
 1.0000000 -.0000000
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Lednicer format dat file
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Polars for FAUVEL 14% AIRFOIL (fauvel-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   fauvel-il50,00099.9 at α=0.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fauvel-il50,000518.3 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fauvel-il100,000922.7 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   fauvel-il100,000539.5 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   fauvel-il200,000957.7 at α=10.5°Mach=0 Ncrit=9Xfoil predictionDetails
   fauvel-il200,000560.5 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
   fauvel-il500,000989.8 at α=9.25°Mach=0 Ncrit=9Xfoil predictionDetails
   fauvel-il500,000582.6 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   fauvel-il1,000,0009106.3 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   fauvel-il1,000,000596 at α=8.25°Mach=0 Ncrit=5Xfoil predictionDetails
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