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NACA 63-212 AIRFOIL (n63212-il)

NACA 63-212 AIRFOIL - NACA 63(1)-212 airfoil


Airfoil n63212-il
Details Dat file Parser  
(n63212-il) NACA 63-212 AIRFOIL
NACA 63(1)-212 airfoil
Max thickness 12% at 34.9% chord.
Max camber 1.1% at 55% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
NACA 63-212 AIRFOIL
      26.       26.

  0.000000  0.000000
  0.004170  0.010320
  0.006570  0.012600
  0.011450  0.016220
  0.023780  0.022840
  0.048630  0.032380
  0.073580  0.039630
  0.098590  0.045540
  0.148680  0.054700
  0.198820  0.061370
  0.249000  0.066060
  0.299200  0.069010
  0.349410  0.070300
  0.399620  0.069910
  0.449820  0.067990
  0.500000  0.064730
  0.550160  0.060300
  0.600290  0.054910
  0.650380  0.048700
  0.700430  0.041820
  0.750450  0.034510
  0.800420  0.026980
  0.850350  0.019470
  0.900250  0.012240
  0.950120  0.005660
  1.000000  0.000000

  0.000000  0.000000
  0.005380 -0.009320
  0.008430 -0.011200
  0.013550 -0.014080
  0.026220 -0.019120
  0.051370 -0.026060
  0.076420 -0.031150
  0.101410 -0.035200
  0.151320 -0.041240
  0.201180 -0.045450
  0.251000 -0.048160
  0.300800 -0.049570
  0.350590 -0.049700
  0.400380 -0.048490
  0.450180 -0.046090
  0.500000 -0.042670
  0.548480 -0.038400
  0.599710 -0.033490
  0.649620 -0.028100
  0.699570 -0.022380
  0.749550 -0.016610
  0.799580 -0.011060
  0.849650 -0.006010
  0.899750 -0.001900
  0.949880  0.000660
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for NACA 63-212 AIRFOIL (n63212-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n63212-il50,000933.5 at α=6.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n63212-il50,000532.8 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n63212-il100,000949.6 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   n63212-il100,000546.9 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n63212-il200,000965.6 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n63212-il200,000557.4 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n63212-il500,000981.7 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n63212-il500,000569.1 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n63212-il1,000,000991.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n63212-il1,000,000574.9 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
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