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HQ 3.0/10 AIRFOIL (hq3010-il)

HQ 3.0/10 AIRFOIL - Quabeck HQ 3.0/10 R/C sailplane airfoil


Airfoil hq3010-il
Details Dat file Parser  
(hq3010-il) HQ 3.0/10 AIRFOIL
Quabeck HQ 3.0/10 R/C sailplane airfoil
Max thickness 10% at 35% chord.
Max camber 3% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
HQ 3.0/10 AIRFOIL
       39.       39.

 0.0000000 0.0000000
 0.0025000 0.0069700
 0.0050000 0.0108100
 0.0087500 0.0149600
 0.0125000 0.0181900
 0.0187500 0.0227300
 0.0250000 0.0265800
 0.0375000 0.0330900
 0.0500000 0.0385200
 0.0750000 0.0472600
 0.1000000 0.0540000
 0.1250000 0.0593600
 0.1500000 0.0637000
 0.1750000 0.0673000
 0.2000000 0.0702600
 0.2250000 0.0726500
 0.2500000 0.0745500
 0.2750000 0.0760800
 0.3000000 0.0772700
 0.3250000 0.0781200
 0.3500000 0.0785900
 0.3750000 0.0787300
 0.4000000 0.0785900
 0.4500000 0.0774800
 0.5000000 0.0752200
 0.5500000 0.0717300
 0.6000000 0.0670100
 0.6500000 0.0611500
 0.7000000 0.0543700
 0.7500000 0.0466800
 0.8000000 0.0381700
 0.8250000 0.0335600
 0.8500000 0.0287800
 0.8750000 0.0239300
 0.9000000 0.0191400
 0.9250000 0.0144700
 0.9500000 0.0096000
 0.9750000 0.0047400
 1.0000000 0.0000000

 0.0000000 0.0000000
 0.0025000 -.0034200
 0.0050000 -.0049700
 0.0087500 -.0068300
 0.0125000 -.0083200
 0.0187500 -.0102400
 0.0250000 -.0115600
 0.0375000 -.0135400
 0.0500000 -.0149300
 0.0750000 -.0169100
 0.1000000 -.0183100
 0.1250000 -.0193900
 0.1500000 -.0202300
 0.1750000 -.0208200
 0.2000000 -.0212200
 0.2250000 -.0214800
 0.2500000 -.0216100
 0.2750000 -.0216200
 0.3000000 -.0215700
 0.3250000 -.0214700
 0.3500000 -.0212600
 0.3750000 -.0207900
 0.4000000 -.0200600
 0.4500000 -.0180600
 0.5000000 -.0154000
 0.5500000 -.0122700
 0.6000000 -.0087700
 0.6500000 -.0051400
 0.7000000 -.0017200
 0.7500000 0.0012800
 0.8000000 0.0034900
 0.8250000 0.0041600
 0.8500000 0.0045100
 0.8750000 0.0044400
 0.9000000 0.0041000
 0.9250000 0.0033300
 0.9500000 0.0025700
 0.9750000 0.0014400
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for HQ 3.0/10 AIRFOIL (hq3010-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   hq3010-il50,000937.7 at α=7°Mach=0 Ncrit=9Xfoil predictionDetails
   hq3010-il50,000539.8 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   hq3010-il100,000960 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   hq3010-il100,000558.9 at α=5°Mach=0 Ncrit=5Xfoil predictionDetails
   hq3010-il200,000983.5 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   hq3010-il200,000577.3 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   hq3010-il500,0009113.6 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   hq3010-il500,000592.8 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   hq3010-il1,000,0009126 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   hq3010-il1,000,000599.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
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