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NACA 64-110 AIRFOIL (n64110-il)

NACA 64-110 AIRFOIL - NACA 64-110 airfoil


Airfoil n64110-il
Details Dat file Parser  
(n64110-il) NACA 64-110 AIRFOIL
NACA 64-110 airfoil
Max thickness 10% at 40% chord.
Max camber 0.6% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
NACA 64-110 AIRFOIL
       26.       26.

  0.000000  0.000000
  0.004650  0.008440
  0.007120  0.010230
  0.012070  0.013030
  0.024500  0.017930
  0.049450  0.025000
  0.074430  0.030370
  0.099440  0.034790
  0.149470  0.041780
  0.199530  0.047000
  0.249590  0.050870
  0.299670  0.053500
  0.349750  0.054950
  0.399840  0.055240
  0.449920  0.053910
  0.500000  0.051380
  0.550070  0.047860
  0.600120  0.043560
  0.650160  0.038600
  0.700190  0.033130
  0.750200  0.027290
  0.800190  0.021200
  0.850160  0.015120
  0.900120  0.009290
  0.950060  0.004060
  1.000000  0.000000

  0.000000  0.000000
  0.005350 -0.007940
  0.007880 -0.009530
  0.012930 -0.011950
  0.025500 -0.016070
  0.050550 -0.021840
  0.075570 -0.026130
  0.100560 -0.029630
  0.150530 -0.035060
  0.200470 -0.039040
  0.250410 -0.041910
  0.300330 -0.043780
  0.350250 -0.044650
  0.400160 -0.044520
  0.450080 -0.042950
  0.500000 -0.040340
  0.549930 -0.036900
  0.599880 -0.032840
  0.649840 -0.028300
  0.699810 -0.023410
  0.749800 -0.018330
  0.799810 -0.013240
  0.849840 -0.008400
  0.899880 -0.004130
  0.949940 -0.000900
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for NACA 64-110 AIRFOIL (n64110-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n64110-il50,000929.9 at α=4.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n64110-il50,000528.7 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n64110-il100,000941.6 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n64110-il100,000539 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   n64110-il200,000954.5 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n64110-il200,000544.6 at α=3.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n64110-il500,000963.5 at α=3.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n64110-il500,000554.1 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n64110-il1,000,000969.3 at α=2.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n64110-il1,000,000568.1 at α=7.5°Mach=0 Ncrit=5Xfoil predictionDetails
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