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NASA/LANGLEY RC08-64C AIRFOIL (rc0864c-il)

NASA/LANGLEY RC08-64C AIRFOIL - NASA/Langley 08-64C rotorcraft airfoil


Airfoil rc0864c-il
Details Dat file Parser  
(rc0864c-il) NASA/LANGLEY RC08-64C AIRFOIL
NASA/Langley 08-64C rotorcraft airfoil
Max thickness 8% at 40% chord.
Max camber 1% at 35% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 NASA/LANGLEY RC08-64C AIRFOIL
       35.       35.
 
 0.0       0.0
 0.00034   0.00700
 0.01016   0.01245
 0.01152   0.01308
 0.02391   0.01830
 0.03808   0.02245
 0.04891   0.02506
 0.05744   0.02689
 0.07386   0.02993
 0.08010   0.03099
 0.09887   0.03383
 0.13206   0.03791
 0.14904   0.03968
 0.19927   0.04387
 0.22293   0.04538
 0.24952   0.04679
 0.28937   0.04838
 0.29976   0.04870
 0.32348   0.04929
 0.35000   0.04971
 0.40002   0.04986
 0.46380   0.04887
 0.50048   0.04776
 0.57368   0.04437
 0.60058   0.04278
 0.64943   0.03947
 0.70053   0.03543
 0.76516   0.02950
 0.80040   0.02590
 0.84332   0.02116
 0.90022   0.01430
 0.92185   0.01153
 0.95011   0.00778
 0.96105   0.00629
 1.00000   0.00080
 
 0.0       0.0
 0.00034   -.00585
 0.01016   -.00975
 0.01348   -.01088
 0.02609   -.01424
 0.03808   -.01666
 0.05109   -.01836
 0.05744   -.01912
 0.07614   -.02087
 0.08010   -.02120
 0.10113   -.02263
 0.13206   -.02424
 0.15096   -.02506
 0.20073   -.02672
 0.22293   -.02734
 0.25048   -.02801
 0.28937   -.02881
 0.30024   -.02900
 0.32348   -.02937
 0.35000   -.02971
 0.39980   -.03014
 0.46380   -.03019
 0.49952   -.02994
 0.53656   -.02946
 0.59941   -.02809
 0.64943   -.02642
 0.69947   -.02427
 0.76516   -.02065
 0.79960   -.01842
 0.84332   -.01524
 0.89978   -.01060
 0.92185   -.00861
 0.94989   -.00596
 0.96105   -.00485
 1.00000   -.00080
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Lednicer format dat file
Selig format dat file

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Polars for NASA/LANGLEY RC08-64C AIRFOIL (rc0864c-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   rc0864c-il50,000923.4 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   rc0864c-il50,000525.4 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   rc0864c-il100,000937.2 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   rc0864c-il100,000531.8 at α=2.25°Mach=0 Ncrit=5Xfoil predictionDetails
   rc0864c-il200,000944 at α=2.25°Mach=0 Ncrit=9Xfoil predictionDetails
   rc0864c-il200,000533.8 at α=1.25°Mach=0 Ncrit=5Xfoil predictionDetails
   rc0864c-il500,000942.7 at α=1.25°Mach=0 Ncrit=9Xfoil predictionDetails
   rc0864c-il500,000540.3 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   rc0864c-il1,000,000945.6 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   rc0864c-il1,000,000546.8 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
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