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LOCKHEED C-5A BL576 AIRFOIL (c5c-il)

LOCKHEED C-5A BL576 AIRFOIL - Lockheed-Georgia C-5A transonic wing airfoils


Airfoil c5c-il
Details Dat file Parser  
(c5c-il) LOCKHEED C-5A BL576 AIRFOIL
Lockheed-Georgia C-5A transonic wing airfoils
Max thickness 11.1% at 40% chord.
Max camber 1.4% at 65% chord
Source UIUC Airfoil Coordinates Database
Source dat file
The dat file is in Lednicer format
 LOCKHEED C-5A BL576 AIRFOIL
      31.0      31.0

 0.0000000 0.0000000
 0.0024665 0.0057808
 0.0049467 0.0091929
 0.0074317 0.0117761
 0.0099194 0.0138925
 0.0198817 0.0203895
 0.0398357 0.0283071
 0.0598001 0.0344414
 0.0797739 0.0389598
 0.0997523 0.0426758
 0.1197313 0.0463014
 0.1397135 0.0493739
 0.1596981 0.0520273
 0.1796848 0.0543211
 0.1996717 0.0565757
 0.2496462 0.0609693
 0.2996276 0.0641777
 0.3496152 0.0663089
 0.3996078 0.0675769
 0.4496055 0.0679757
 0.4996090 0.0673765
 0.5496180 0.0658186
 0.5996321 0.0633915
 0.6496519 0.0599930
 0.6996760 0.0558376
 0.7497076 0.0503954
 0.7997473 0.0435528
 0.8497962 0.0351239
 0.8998530 0.0253346
 0.9499219 0.0134639
 1.0000000 0.0010949

 0.0000000 0.0000000
 0.0025568 -.0097839
 0.0050744 -.0128176
 0.0075854 -.0147139
 0.0100947 -.0163164
 0.0201199 -.0206592
 0.0401519 -.0261763
 0.0601756 -.0302537
 0.0801933 -.0333143
 0.1002064 -.0355666
 0.1202155 -.0371439
 0.1402243 -.0386578
 0.1602316 -.0399016
 0.1802367 -.0407856
 0.2002418 -.0416695
 0.2502506 -.0431830
 0.3002547 -.0438881
 0.3502550 -.0439497
 0.4002521 -.0434500
 0.4502460 -.0423942
 0.5002362 -.0406954
 0.5502223 -.0383040
 0.6002061 -.0355139
 0.6501851 -.0318928
 0.7001613 -.0277984
 0.7501358 -.0233957
 0.8001096 -.0188861
 0.8500839 -.0144657
 0.9000583 -.0100437
 0.9500320 -.0055153
 1.0000000 -.0010949
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Lednicer format dat file
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Polars for LOCKHEED C-5A BL576 AIRFOIL (c5c-il)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   c5c-il50,000931.7 at α=5.75°Mach=0 Ncrit=9Xfoil predictionDetails
   c5c-il50,000530.5 at α=5.5°Mach=0 Ncrit=5Xfoil predictionDetails
   c5c-il100,000948.2 at α=5°Mach=0 Ncrit=9Xfoil predictionDetails
   c5c-il100,000544.1 at α=4.25°Mach=0 Ncrit=5Xfoil predictionDetails
   c5c-il200,000967.3 at α=4°Mach=0 Ncrit=9Xfoil predictionDetails
   c5c-il200,000555.2 at α=3.25°Mach=0 Ncrit=5Xfoil predictionDetails
   c5c-il500,000978.4 at α=3°Mach=0 Ncrit=9Xfoil predictionDetails
   c5c-il500,000562.3 at α=7.25°Mach=0 Ncrit=5Xfoil predictionDetails
   c5c-il1,000,000982.7 at α=1.75°Mach=0 Ncrit=9Xfoil predictionDetails
   c5c-il1,000,000577.6 at α=9°Mach=0 Ncrit=5Xfoil predictionDetails
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