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NACA 63(2)-215 MOD B (n63215b-il)

NACA 63(2)-215 MOD B - NACA-NASA/AMES/Hicks 63(2)-215 MOD B airfoil


Airfoil n63215b-il
Details Dat file Parser  
(n63215b-il) NACA 63(2)-215 MOD B
NACA-NASA/AMES/Hicks 63(2)-215 MOD B airfoil
Max thickness 15% at 30% chord.
Max camber 1.5% at 10% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
  NACA 63(2)-215 MOD B
 60.0000   60.0000

  0.0       0.0
  0.0002    0.0034
  0.0004    0.0051
  0.0006    0.0064
  0.0008    0.0075
  0.0010    0.0085
  0.0020    0.0125
  0.0030    0.0156
  0.0040    0.0182
  0.0050    0.0205
  0.0100    0.0293
  0.0200    0.0408
  0.0300    0.0489
  0.0400    0.0550
  0.0500    0.0599
  0.0600    0.0640
  0.0700    0.0673
  0.0800    0.0702
  0.0900    0.0727
  0.1000    0.0748
  0.1250    0.0788
  0.1500    0.0816
  0.1750    0.0835
  0.2000    0.0847
  0.2250    0.0855
  0.2500    0.0859
  0.2750    0.0860
  0.3000    0.0859
  0.3250    0.0856
  0.3500    0.0853
  0.3750    0.0852
  0.4000    0.0845
  0.4250    0.0835
  0.4500    0.0819
  0.4750    0.0800
  0.5000    0.0777
  0.5250    0.0750
  0.5500    0.0720
  0.5750    0.0688
  0.6000    0.0653
  0.6250    0.0615
  0.6500    0.0576
  0.6750    0.0534
  0.7000    0.0491
  0.7250    0.0447
  0.7500    0.0402
  0.7750    0.0357
  0.8000    0.0311
  0.8250    0.0266
  0.8500    0.0222
  0.8750    0.0179
  0.9000    0.0137
  0.9250    0.0098
  0.9500    0.0062
  0.9600    0.0048
  0.9700    0.0036
  0.9800    0.0023
  0.9900    0.0012
  0.9950    0.0006
  1.0000    0.0000

  0.0       0.0
  0.0002    -.0011
  0.0004    -.0022
  0.0006    -.0031
  0.0008    -.0037
  0.0010    -.0042
  0.0020    -.0063
  0.0030    -.0079
  0.0040    -.0093
  0.0050    -.0104
  0.0100    -.0150
  0.0200    -.0211
  0.0300    -.0256
  0.0400    -.0294
  0.0500    -.0328
  0.0600    -.0357
  0.0700    -.0384
  0.0800    -.0408
  0.0900    -.0430
  0.1000    -.0450
  0.1250    -.0494
  0.1500    -.0531
  0.1750    -.0562
  0.2000    -.0588
  0.2250    -.0609
  0.2500    -.0625
  0.2750    -.0637
  0.3000    -.0645
  0.3250    -.0648
  0.3500    -.0647
  0.3750    -.0641
  0.4000    -.0632
  0.4250    -.0618
  0.4500    -.0601
  0.4750    -.0580
  0.5000    -.0556
  0.5250    -.0530
  0.5500    -.0501
  0.5750    -.0470
  0.6000    -.0438
  0.6250    -.0404
  0.6500    -.0368
  0.6750    -.0332
  0.7000    -.0295
  0.7250    -.0258
  0.7500    -.0221
  0.7750    -.0185
  0.8000    -.0150
  0.8250    -.0117
  0.8500    -.0086
  0.8750    -.0058
  0.9000    -.0033
  0.9250    -.0013
  0.9500    0.0001
  0.9600    0.0005
  0.9700    0.0007
  0.9800    0.0008
  0.9900    0.0006
  0.9950    0.0003
  1.0000    0.0000
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Lednicer format dat file
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Polars for NACA 63(2)-215 MOD B (n63215b-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   n63215b-il50,000925.9 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n63215b-il50,000524.5 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   n63215b-il100,000932.8 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n63215b-il100,000535.3 at α=8°Mach=0 Ncrit=5Xfoil predictionDetails
   n63215b-il200,000944.4 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   n63215b-il200,000547.9 at α=8.75°Mach=0 Ncrit=5Xfoil predictionDetails
   n63215b-il500,000966.4 at α=8.5°Mach=0 Ncrit=9Xfoil predictionDetails
   n63215b-il500,000568.3 at α=9.25°Mach=0 Ncrit=5Xfoil predictionDetails
   n63215b-il1,000,000986.3 at α=9°Mach=0 Ncrit=9Xfoil predictionDetails
   n63215b-il1,000,000583.9 at α=10°Mach=0 Ncrit=5Xfoil predictionDetails
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