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NACA CYH (nacacyh-il)

NACA CYH - NACA CYH airfoil


Airfoil nacacyh-il
Details Dat file Parser  
(nacacyh-il) NACA CYH
NACA CYH airfoil
Max thickness 11.7% at 30% chord.
Max camber 2.8% at 40% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Selig format
NACA CYH
1.0000     0.0205
0.9500     0.0293
0.9000     0.0384
0.8000     0.0562
0.7000     0.0741
0.6000     0.0915
0.5000     0.1052
0.4000     0.1140
0.3000     0.1170
0.2000     0.1136
0.1500     0.1068
0.1000     0.0960
0.0750     0.0885
0.0500     0.0790
0.0250     0.0650
0.0125     0.0545
0.0000     0.0350
0.0125     0.0193
0.0250     0.0147
0.0500     0.0093
0.0750     0.0063
0.1000     0.0042
0.1500     0.0015
0.2000     0.0003
0.3000     0.0000
0.4000     0.0000
0.5000     0.0000
0.6000     0.0000
0.7000     0.0006
0.8000     0.0038
0.9000     0.0102
0.9500     0.0140
1.0000     0.0185
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Lednicer format dat file
Selig format dat file

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Polars for NACA CYH (nacacyh-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   nacacyh-il50,000925.7 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   nacacyh-il50,000533.3 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   nacacyh-il100,000947.8 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   nacacyh-il100,000549.4 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   nacacyh-il200,000965.4 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   nacacyh-il200,000564.7 at α=6.75°Mach=0 Ncrit=5Xfoil predictionDetails
   nacacyh-il500,000990.5 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   nacacyh-il500,000587 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
   nacacyh-il1,000,0009110.4 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   nacacyh-il1,000,0005101 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
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