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CLARK YM-18 AIRFOIL (clarym18-il)

CLARK YM-18 AIRFOIL - CLARK YM18 airfoil


Airfoil clarym18-il
Details Dat file Parser  
(clarym18-il) CLARK YM-18 AIRFOIL
CLARK YM18 airfoil
Max thickness 18% 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-18 AIRFOIL
       17.       17.

 0.0000000 0.0000000
 0.0114900 0.0294000
 0.0234700 0.0444100
 0.0477800 0.0644400
 0.0723100 0.0780900
 0.0969400 0.0890300
 0.1463800 0.1052400
 0.1960200 0.1158400
 0.2957500 0.1236700
 0.3957600 0.1233100
 0.4960200 0.1155600
 0.5965000 0.1016200
 0.6971700 0.0822800
 0.7979800 0.0586500
 0.8989200 0.0315200
 0.9494300 0.0166600
 1.0000000 0.0009000

 0.0000000 0.0000000
 0.0133500 -.0247400
 0.0261400 -.0330000
 0.0514700 -.0426300
 0.0766600 -.0481600
 0.1017900 -.0520000
 0.1519500 -.0566700
 0.2020000 -.0582500
 0.3019300 -.0561100
 0.4017800 -.0518800
 0.5015800 -.0460500
 0.6013400 -.0389100
 0.7010601 -.0306800
 0.8007400 -.0214500
 0.9004000 -.0115300
 0.9502200 -.0063100
 1.0000000 -.0009000
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Lednicer format dat file
Selig format dat file

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Polars for CLARK YM-18 AIRFOIL (clarym18-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   clarym18-il50,00097.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   clarym18-il50,000525.7 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   clarym18-il100,000943.4 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   clarym18-il100,000543.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   clarym18-il200,000960.9 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   clarym18-il200,000556 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   clarym18-il500,000977.6 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   clarym18-il500,000573.5 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   clarym18-il1,000,000996.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   clarym18-il1,000,000593.9 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
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