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LOCKHEED C-5A BL758.6 AIRFOIL (c5d-il)

LOCKHEED C-5A BL758.6 AIRFOIL - Lockheed-Georgia C-5A transonic wing airfoils


Airfoil c5d-il
Details Dat file Parser  
(c5d-il) LOCKHEED C-5A BL758.6 AIRFOIL
Lockheed-Georgia C-5A transonic wing airfoils
Max thickness 11.1% at 40% chord.
Max camber 1.4% at 60% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 LOCKHEED C-5A BL758.6 AIRFOIL
      31.0      31.0

 0.0000000 0.0000000
 0.0024610 0.0064710
 0.0049413 0.0097248
 0.0074258 0.0122976
 0.0099127 0.0144718
 0.0198729 0.0210659
 0.0398255 0.0289355
 0.0597888 0.0350162
 0.0797614 0.0395488
 0.0997378 0.0434693
 0.1197177 0.0467899
 0.1396989 0.0499139
 0.1596841 0.0523648
 0.1796701 0.0546853
 0.1996564 0.0569638
 0.2496304 0.0612662
 0.2996117 0.0643632
 0.3495989 0.0664940
 0.3995927 0.0675273
 0.4495916 0.0677056
 0.4995971 0.0667876
 0.5496085 0.0648978
 0.5996250 0.0621620
 0.6496472 0.0584854
 0.6996740 0.0540367
 0.7497074 0.0485036
 0.7997488 0.0416457
 0.8497980 0.0334945
 0.8998541 0.0241860
 0.9499198 0.0132869
 1.0000000 0.0011080

 0.0000000 0.0000000
 0.0025593 -.0098344
 0.0050797 -.0132109
 0.0075913 -.0151284
 0.0101008 -.0167084
 0.0201274 -.0211238
 0.0401593 -.0264133
 0.0601824 -.0302367
 0.0801988 -.0329635
 0.1002112 -.0350103
 0.1202195 -.0363927
 0.1402274 -.0377041
 0.1602342 -.0388282
 0.1802394 -.0396831
 0.2002445 -.0405381
 0.2502527 -.0418983
 0.3002585 -.0428580
 0.3502612 -.0432958
 0.4002595 -.0430121
 0.4502540 -.0421064
 0.5002440 -.0404444
 0.5502297 -.0380722
 0.6002113 -.0350287
 0.6501904 -.0315566
 0.7001644 -.0272602
 0.7501376 -.0228124
 0.8001102 -.0182612
 0.8500827 -.0137126
 0.9000559 -.0092695
 0.9500306 -.0050679
 1.0000000 -.0011080
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Lednicer format dat file
Selig format dat file

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Polars for LOCKHEED C-5A BL758.6 AIRFOIL (c5d-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   c5d-il50,000930.7 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   c5d-il50,000531 at α=5.25°Mach=0 Ncrit=5Xfoil predictionDetails
   c5d-il100,000948.1 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   c5d-il100,000544.3 at α=4°Mach=0 Ncrit=5Xfoil predictionDetails
   c5d-il200,000966.7 at α=3.75°Mach=0 Ncrit=9Xfoil predictionDetails
   c5d-il200,000553.6 at α=3°Mach=0 Ncrit=5Xfoil predictionDetails
   c5d-il500,000975.9 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   c5d-il500,000562.3 at α=6.5°Mach=0 Ncrit=5Xfoil predictionDetails
   c5d-il1,000,000979.9 at α=2°Mach=0 Ncrit=9Xfoil predictionDetails
   c5d-il1,000,000578.3 at α=8.5°Mach=0 Ncrit=5Xfoil predictionDetails
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