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HQ 2.1/9.5 AIRFOIL (hq2195-il)

HQ 2.1/9.5 AIRFOIL - Quabeck HQ 2.1/9.5 R/C sailplane airfoil


Airfoil hq2195-il
Details Dat file Parser  
(hq2195-il) HQ 2.1/9.5 AIRFOIL
Quabeck HQ 2.1/9.5 R/C sailplane airfoil
Max thickness 9.5% at 35% chord.
Max camber 2.1% at 55% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
HQ 2.1/9.5 AIRFOIL
       27.       27.

 0.0000000 0.0000000
 0.0050000 0.0117500
 0.0125000 0.0178400
 0.0250000 0.0249200
 0.0500000 0.0345800
 0.1000000 0.0472500
 0.1500000 0.0557200
 0.2000000 0.0613200
 0.2500000 0.0646100
 0.3000000 0.0662300
 0.3500000 0.0667800
 0.4000000 0.0665200
 0.4500100 0.0655500
 0.5000000 0.0638400
 0.5500000 0.0613000
 0.6000000 0.0575100
 0.6500000 0.0522600
 0.7000000 0.0459300
 0.7500000 0.0390600
 0.8000000 0.0317200
 0.8500000 0.0240100
 0.9000000 0.0161500
 0.9269800 0.0118500
 0.9500000 0.0081300
 0.9775701 0.0036700
 0.9943600 0.0009300
 1.0000000 0.0000100

 0.0000000 0.0000000
 0.0050000 -.0068500
 0.0125000 -.0105400
 0.0250000 -.0139600
 0.0500000 -.0179800
 0.1000000 -.0224300
 0.1500000 -.0251000
 0.2000000 -.0269600
 0.2500000 -.0280900
 0.3000000 -.0284700
 0.3500000 -.0281400
 0.4000000 -.0270200
 0.4500100 -.0249900
 0.5000000 -.0223400
 0.5500000 -.0193200
 0.6000000 -.0158500
 0.6500000 -.0119200
 0.7000000 -.0079900
 0.7500000 -.0045600
 0.8000000 -.0016000
 0.8500000 0.0008900
 0.9000000 0.0022700
 0.9269800 0.0022700
 0.9500000 0.0018300
 0.9775701 0.0009100
 0.9943600 0.0002300
 1.0000000 0.0000000
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Lednicer format dat file
Selig format dat file

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Polars for HQ 2.1/9.5 AIRFOIL (hq2195-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   hq2195-il50,000937.3 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   hq2195-il50,000537.6 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   hq2195-il100,000955.4 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   hq2195-il100,000552.6 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   hq2195-il200,000974.5 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   hq2195-il200,000567.5 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   hq2195-il500,000996.2 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   hq2195-il500,000579 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   hq2195-il1,000,0009101 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   hq2195-il1,000,000587 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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