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HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED) (hq17-il)

HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED) - Airfoil measured from an ASW22 wing


Airfoil hq17-il
Details Dat file Parser  
(hq17-il) HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED)
Airfoil measured from an ASW22 wing
Max thickness 15.2% at 42% chord.
Max camber 4.5% at 42% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED)
       48.       48.

  0.000000  0.000000
  0.002350  0.006570
  0.007040  0.014080
  0.016420  0.023460
  0.025810  0.031300
  0.035190  0.037540
  0.044580  0.043170
  0.053970  0.047860
  0.063350  0.052560
  0.082120  0.061000
  0.100890  0.068510
  0.129050  0.077900
  0.157200  0.086200
  0.185360  0.093300
  0.213510  0.099200
  0.241670  0.104300
  0.269830  0.108870
  0.297980  0.112620
  0.326140  0.115440
  0.349600  0.117600
  0.373060  0.119190
  0.396530  0.120500
  0.419990  0.121200
  0.443450  0.121200
  0.466920  0.121000
  0.490380  0.120300
  0.513840  0.119100
  0.537310  0.117320
  0.560770  0.114900
  0.584230  0.112000
  0.607700  0.108870
  0.631160  0.105110
  0.654620  0.100420
  0.678090  0.095730
  0.701550  0.090100
  0.725010  0.084500
  0.748470  0.077900
  0.771940  0.071330
  0.795400  0.063820
  0.818860  0.056310
  0.842330  0.048500
  0.865790  0.041300
  0.889250  0.033500
  0.912720  0.025700
  0.936180  0.018770
  0.959640  0.011500
  0.983110  0.004690
  1.000000  0.000000

  0.000000  0.000000
  0.002350  -.004690
  0.007040  -.008450
  0.016420  -.011800
  0.025810  -.014080
  0.035190  -.015950
  0.044580  -.017500
  0.053970  -.018900
  0.063350  -.020200
  0.082120  -.022100
  0.100890  -.023600
  0.129050  -.025200
  0.157200  -.026400
  0.185360  -.027400
  0.213510  -.028200
  0.241670  -.029000
  0.269830  -.029700
  0.297980  -.030200
  0.326140  -.030700
  0.349600  -.030900
  0.373060  -.030900
  0.396530  -.030970
  0.419990  -.030970
  0.443450  -.030970
  0.466920  -.030900
  0.490380  -.030600
  0.513840  -.030030
  0.537310  -.029300
  0.560770  -.028500
  0.584230  -.027500
  0.607700  -.026400
  0.631160  -.025000
  0.654620  -.023600
  0.678090  -.021800
  0.701550  -.019800
  0.725010  -.017500
  0.748470  -.014800
  0.771940  -.011500
  0.795400  -.008450
  0.818860  -.004690
  0.842330  -.001400
  0.865790  0.001880
  0.889250  0.003750
  0.912720  0.004200
  0.936180  0.003700
  0.959640  0.002500
  0.983110  0.001000
  1.000000  0.000000

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Lednicer format dat file
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Polars for HORSTMANN AND QUAST HQ-17/14.38 AIRFOIL (MEASURED) (hq17-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   hq17-il50,000922.5 at α=12.75°Mach=0 Ncrit=9Xfoil predictionDetails
   hq17-il50,000518.3 at α=12.5°Mach=0 Ncrit=5Xfoil predictionDetails
   hq17-il100,000934.2 at α=11.25°Mach=0 Ncrit=9Xfoil predictionDetails
   hq17-il100,000532.5 at α=10.25°Mach=0 Ncrit=5Xfoil predictionDetails
   hq17-il200,000968.9 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   hq17-il200,000566.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   hq17-il500,0009113.5 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   hq17-il500,0005103.3 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   hq17-il1,000,0009139.5 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   hq17-il1,000,0005122.5 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
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