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CLARK YM-15 AIRFOIL (clarym15-il)

CLARK YM-15 AIRFOIL - CLARK YM15 airfoil


Airfoil clarym15-il
Details Dat file Parser  
(clarym15-il) CLARK YM-15 AIRFOIL
CLARK YM15 airfoil
Max thickness 15% at 29.6% chord.
Max camber 3.6% at 39.6% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
CLARK YM-15 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0116400 0.0249000
 0.0237000 0.0379200
 0.0480900 0.0554500
 0.0726700 0.0676000
 0.0973400 0.0772500
 0.1468400 0.0917500
 0.1965100 0.1013600
 0.2962600 0.1086900
 0.3962600 0.1087300
 0.4964900 0.1020800
 0.5969100 0.0899300
 0.6974900 0.0728900
 0.7982100 0.0519600
 0.8990400 0.0279300
 0.9495000 0.0146600
 1.0000000 0.0008000

 0.0000000 0.0000000
 0.0132000 -.0202500
 0.0259100 -.0265100
 0.0511600 -.0337400
 0.0763000 -.0376800
 0.1013800 -.0402100
 0.1514900 -.0431900
 0.2015000 -.0436700
 0.3014200 -.0411300
 0.4012800 -.0373000
 0.5011200 -.0325600
 0.6009400 -.0272300
 0.7007300 -.0212900
 0.8005100 -.0148600
 0.9002800 -.0080300
 0.9501500 -.0044100
 1.0000000 -.0008000
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Lednicer format dat file
Selig format dat file

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Polars for CLARK YM-15 AIRFOIL (clarym15-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   clarym15-il50,000912.3 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   clarym15-il50,000531 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   clarym15-il100,000947.6 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   clarym15-il100,000548.7 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   clarym15-il200,000966.2 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   clarym15-il200,000562.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   clarym15-il500,000988.9 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   clarym15-il500,000584.4 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   clarym15-il1,000,0009109.5 at α=8°Mach=0 Ncrit=9Xfoil predictionDetails
   clarym15-il1,000,0005105.1 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
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