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DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il)

DELFT DU84-132V3 AIRFOIL (MEASURED) - Airfoil measured from an ASW22 wing


Airfoil du84132v-il
Details Dat file Parser  
(du84132v-il) DELFT DU84-132V3 AIRFOIL (MEASURED)
Airfoil measured from an ASW22 wing
Max thickness 13.6% at 33.9% chord.
Max camber 3.1% at 45.3% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
DELFT DU84-132V3 AIRFOIL (MEASURED)
       49.       49.

  0.000000  0.000000
  0.002280  0.010020
  0.006830  0.017310
  0.015950  0.026420
  0.025060  0.033710
  0.034170  0.039180
  0.043280  0.044650
  0.066060  0.054670
  0.088840  0.062870
  0.111620  0.070160
  0.134400  0.075630
  0.157180  0.081090
  0.179950  0.085200
  0.202730  0.088600
  0.225510  0.091120
  0.248290  0.092940
  0.271070  0.094760
  0.293850  0.095900
  0.316630  0.096900
  0.339410  0.097400
  0.362190  0.097490
  0.384970  0.097490
  0.407740  0.097400
  0.430520  0.096580
  0.453300  0.095670
  0.476080  0.093900
  0.498860  0.092030
  0.521640  0.090210
  0.544420  0.088000
  0.567200  0.085650
  0.589980  0.083200
  0.612760  0.080180
  0.635540  0.077300
  0.658310  0.073800
  0.681090  0.070500
  0.703870  0.066510
  0.726650  0.062870
  0.749430  0.058500
  0.772210  0.054670
  0.794990  0.050000
  0.817770  0.045200
  0.840550  0.040090
  0.863330  0.035200
  0.886100  0.030070
  0.908880  0.024700
  0.931660  0.019200
  0.954440  0.013100
  0.977220  0.006800
  1.000000  0.000000

  0.000000  0.000000
  0.002280  -.005470
  0.006830  -.011850
  0.015950  -.016700
  0.025060  -.020050
  0.034170  -.022780
  0.043280  -.024400
  0.066060  -.028800
  0.088840  -.031890
  0.111620  -.034620
  0.134400  -.036200
  0.157180  -.037360
  0.179950  -.038400
  0.202730  -.039180
  0.225510  -.039400
  0.248290  -.039600
  0.271070  -.039600
  0.293850  -.039500
  0.316630  -.039300
  0.339410  -.038900
  0.362190  -.038270
  0.384970  -.037360
  0.407740  -.036450
  0.430520  -.035540
  0.453300  -.034620
  0.476080  -.033710
  0.498860  -.032500
  0.521640  -.031200
  0.544420  -.030000
  0.567200  -.028400
  0.589980  -.026900
  0.612760  -.025100
  0.635540  -.022900
  0.658310  -.020500
  0.681090  -.017500
  0.703870  -.014400
  0.726650  -.010930
  0.749430  -.007290
  0.772210  -.003640
  0.794990  0.000000
  0.817770  0.002730
  0.840550  0.004560
  0.863330  0.005470
  0.886100  0.005470
  0.908880  0.005470
  0.931660  0.004800
  0.954440  0.003640
  0.977220  0.001800
  1.000000  0.000000

Dat file parser warnings
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Polars for DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   du84132v-il50,000931.4 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   du84132v-il50,000534.3 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   du84132v-il100,000953.6 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   du84132v-il100,000552.5 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   du84132v-il200,000971.7 at α=6.25°Mach=0 Ncrit=9Xfoil predictionDetails
   du84132v-il200,000562.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   du84132v-il500,000982 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   du84132v-il500,000575.3 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   du84132v-il1,000,000992.6 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   du84132v-il1,000,000582.1 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
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