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NACA 63-415 AIRFOIL (n63415-il)

NACA 63-415 AIRFOIL - NACA 63(2)-415 airfoil


Airfoil n63415-il
Details Dat file Parser  
(n63415-il) NACA 63-415 AIRFOIL
NACA 63(2)-415 airfoil
Max thickness 15% at 34.9% chord.
Max camber 2.2% at 50% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
NACA 63-415 AIRFOIL
      26.       26.

  0.000000  0.000000
  0.003000  0.012870
  0.005250  0.015850
  0.009910  0.020740
  0.021980  0.029640
  0.046600  0.042640
  0.071470  0.052610
  0.096470  0.060770
  0.146690  0.073480
  0.197050  0.082790
  0.247500  0.089410
  0.298000  0.093620
  0.348520  0.095590
  0.399050  0.095270
  0.449550  0.092890
  0.500000  0.088710
  0.550390  0.082980
  0.600700  0.075950
  0.650930  0.067800
  0.701060  0.058770
  0.751090  0.049070
  0.801020  0.039000
  0.850850  0.028850
  0.900590  0.018840
  0.950280  0.009310
  1.000000  0.000000

  0.000000  0.000000
  0.007000 -0.010870
  0.009750 -0.013050
  0.015090 -0.016460
  0.028020 -0.022200
  0.053400 -0.030000
  0.078530 -0.035650
  0.103530 -0.040090
  0.153310 -0.046560
  0.202950 -0.050950
  0.252500 -0.053610
  0.302000 -0.054740
  0.351480 -0.054390
  0.400950 -0.052430
  0.450450 -0.049090
  0.500000 -0.044590
  0.549610 -0.039180
  0.599300 -0.033110
  0.649070 -0.026600
  0.698940 -0.019890
  0.748910 -0.013270
  0.799890 -0.007160
  0.849150 -0.001930
  0.899410  0.001840
  0.949720  0.003330
  1.000000  0.000000
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Lednicer format dat file
Selig format dat file

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Polars for NACA 63-415 AIRFOIL (n63415-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n63415-il50,000930 at α=9.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n63415-il50,000527.8 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
   n63415-il100,000953.1 at α=8.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n63415-il100,000552.3 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n63415-il200,000975.6 at α=7.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n63415-il200,000570 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   n63415-il500,0009100.9 at α=6°Mach=0 Ncrit=9Xfoil predictionDetails
   n63415-il500,000590.7 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n63415-il1,000,0009118.7 at α=5.25°Mach=0 Ncrit=9Xfoil predictionDetails
   n63415-il1,000,0005103 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
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