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NACA 63-210 AIRFOIL (n63210-il)

NACA 63-210 AIRFOIL - NACA 63-210 airfoil


Airfoil n63210-il
Details Dat file Parser  
(n63210-il) NACA 63-210 AIRFOIL
NACA 63-210 airfoil
Max thickness 10% at 35% chord.
Max camber 1.1% at 60% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
NACA 63-210 AIRFOIL
      26.       26.

  0.000000  0.000000
  0.004300  0.008760
  0.006690  0.011070
  0.011620  0.013790
  0.023980  0.019390
  0.048860  0.027530
  0.073820  0.033720
  0.098820  0.038770
  0.148900  0.046650
  0.199020  0.052400
  0.249170  0.056470
  0.299330  0.059100
  0.349510  0.060300
  0.399680  0.060090
  0.449850  0.058610
  0.500000  0.055990
  0.550130  0.052350
  0.600240  0.047860
  0.650320  0.042640
  0.700360  0.036840
  0.750380  0.030610
  0.800360  0.024140
  0.850300  0.017610
  0.900210  0.012120
  0.950100  0.005300
  1.000000  0.000000

  0.000000  0.000000
  0.005700 -0.007760
  0.008310 -0.009670
  0.013380 -0.011650
  0.026020 -0.015670
  0.051140 -0.021210
  0.076180 -0.025240
  0.101180 -0.028430
  0.151100 -0.033190
  0.200980 -0.036480
  0.250830 -0.038570
  0.300670 -0.039660
  0.350490 -0.039700
  0.400320 -0.038670
  0.450150 -0.036710
  0.500000 -0.033930
  0.549870 -0.030450
  0.589760 -0.026440
  0.649680 -0.022040
  0.699640 -0.017400
  0.749620 -0.012710
  0.799640 -0.008220
  0.849700 -0.004150
  0.899790 -0.000870
  0.949900  0.001200
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for NACA 63-210 AIRFOIL (n63210-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n63210-il50,000933.5 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n63210-il50,000532 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n63210-il100,000946.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n63210-il100,000542.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   n63210-il200,000959.4 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   n63210-il200,000548.7 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n63210-il500,000967.7 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   n63210-il500,000555.8 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n63210-il1,000,000969 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   n63210-il1,000,000566.3 at α=11°Mach=0 Ncrit=5Xfoil predictionDetails
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