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NASA/LANGLEY RC10-64C AIRFOIL (rc1064c-il)

NASA/LANGLEY RC10-64C AIRFOIL - NASA/Langley 10-64C rotorcraft airfoil


Airfoil rc1064c-il
Details Dat file Parser  
(rc1064c-il) NASA/LANGLEY RC10-64C AIRFOIL
NASA/Langley 10-64C rotorcraft airfoil
Max thickness 10% 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 RC10-64C AIRFOIL
       33.       33.
 
 0.0       0.0
 0.00355   0.00910
 0.01128   0.01611
 0.02363   0.02241
 0.03836   0.02754
 0.04864   0.03053
 0.05766   0.03282
 0.07357   0.03632
 0.08022   0.03759
 0.09859   0.04091
 0.13226   0.04569
 0.14879   0.04779
 0.16115   0.04907
 0.19908   0.05271
 0.22385   0.05448
 0.24940   0.05614
 0.29970   0.05842
 0.32544   0.05909
 0.34999   0.05964
 0.40024   0.05986
 0.46674   0.05860
 0.50060   0.05747
 0.53964   0.05551
 0.60073   0.05164
 0.65212   0.04745
 0.70066   0.04288
 0.76700   0.03556
 0.80050   0.03144
 0.84428   0.02560
 0.90028   0.01742
 0.92202   0.01045
 0.95014   0.00949
 1.00000   0.00100
 
 0.0       0.0
 0.00355   -.00737
 0.01373   -.01391
 0.02637   -.01835
 0.03836   -.02132
 0.05136   -.02383
 0.05766   -.02478
 0.07643   -.02726
 0.08022   -.02769
 0.10141   -.02971
 0.13226   -.03205
 0.15121   -.03317
 0.16115   -.03373
 0.20092   -.03356
 0.22385   -.03648
 0.25060   -.03737
 0.30030   -.03872
 0.32544   -.03925
 0.35001   -.03964
 0.39976   -.04014
 0.46674   -.04004
 0.49940   -.03965
 0.53964   -.03884
 0.59927   -.03695
 0.65212   -.03450
 0.69934   -.03172
 0.76700   -.02676
 0.79950   -.02396
 0.84428   -.01970
 0.89972   -.01372
 0.92202   -.01112
 0.94986   -.00767
 1.00000   -.00100
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Lednicer format dat file
Selig format dat file

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Polars for NASA/LANGLEY RC10-64C AIRFOIL (rc1064c-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   rc1064c-il50,000931.7 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   rc1064c-il50,000530.6 at α=4.75°Mach=0 Ncrit=5Xfoil predictionDetails
   rc1064c-il100,000945.4 at α=4.25°Mach=0 Ncrit=9Xfoil predictionDetails
   rc1064c-il100,000541.9 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   rc1064c-il200,000957.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   rc1064c-il200,000546.6 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   rc1064c-il500,000962.4 at α=3.25°Mach=0 Ncrit=9Xfoil predictionDetails
   rc1064c-il500,000559.4 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
   rc1064c-il1,000,000971.2 at α=7.75°Mach=0 Ncrit=9Xfoil predictionDetails
   rc1064c-il1,000,000573.2 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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