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NASA/LANGLEY RC-08(B)3 AIRFOIL (rc08b3-il)

NASA/LANGLEY RC-08(B)3 AIRFOIL - NASA/Langley RC-08(B)3 rotorcraft airfoil


Airfoil rc08b3-il
Details Dat file Parser  
(rc08b3-il) NASA/LANGLEY RC-08(B)3 AIRFOIL
NASA/Langley RC-08(B)3 rotorcraft airfoil
Max thickness 8% at 37.8% chord.
Max camber 1.1% at 34.1% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 NASA/LANGLEY RC-08(B)3 AIRFOIL
 33.      33.
 
 0.000000  0.000000
 0.003140  0.006710
 0.011700  0.013120
 0.025340  0.019000
 0.043690  0.024550
 0.065080  0.029520
 0.088890  0.033890
 0.114710  0.037700
 0.142390  0.040960
 0.171860  0.043760
 0.202980  0.046060
 0.235600  0.047890
 0.269590  0.049280
 0.304840  0.050230
 0.341210  0.050750
 0.378400  0.050870
 0.416120  0.050570
 0.454040  0.049860
 0.491990  0.048760
 0.529830  0.047250
 0.567660  0.045330
 0.605530  0.043000
 0.643670  0.040240
 0.682380  0.037040
 0.721500  0.033420
 0.760570  0.029440
 0.798420  0.025280
 0.834570  0.021070
 0.869270  0.016860
 0.902800  0.012710
 0.935430  0.008640
 0.967820  0.004900
 1.000000  0.001300
 
 0.000000  0.000000
 0.003140  -.006560
 0.011700  -.010960
 0.025340  -.014450
 0.043690  -.017290
 0.065080  -.019510
 0.088890  -.021290
 0.114710  -.022780
 0.142390  -.024030
 0.171860  -.025130
 0.202980  -.026090
 0.235600  -.026930
 0.269590  -.027910
 0.304840  -.028530
 0.341210  -.028770
 0.378400  -.029130
 0.416120  -.029340
 0.454040  -.029390
 0.491990  -.029290
 0.529830  -.029020
 0.567660  -.028580
 0.605530  -.027960
 0.643670  -.027130
 0.682380  -.026050
 0.721500  -.024690
 0.760570  -.023000
 0.798420  -.020990
 0.834570  -.018670
 0.869270  -.015990
 0.902800  -.012930
 0.935430  -.009420
 0.967820  -.005130
 1.000000  -.000500
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Lednicer format dat file
Selig format dat file

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Polars for NASA/LANGLEY RC-08(B)3 AIRFOIL (rc08b3-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   rc08b3-il50,000932.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   rc08b3-il50,000531.2 at α=4.5°Mach=0 Ncrit=5Xfoil predictionDetails
   rc08b3-il100,000945.5 at α=4.5°Mach=0 Ncrit=9Xfoil predictionDetails
   rc08b3-il100,000541.5 at α=3.75°Mach=0 Ncrit=5Xfoil predictionDetails
   rc08b3-il200,000957.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   rc08b3-il200,000549.3 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   rc08b3-il500,000967.8 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   rc08b3-il500,000560 at α=6°Mach=0 Ncrit=5Xfoil predictionDetails
   rc08b3-il1,000,000971.5 at α=5.5°Mach=0 Ncrit=9Xfoil predictionDetails
   rc08b3-il1,000,000573.8 at α=7.75°Mach=0 Ncrit=5Xfoil predictionDetails
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