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LOCKHEED C-5A BL758.6 AIRFOIL (c5d-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: LOCKHEED C-5A BL758.6 AIRFOIL (c5d-il)
Reynolds number: 100,000
Max Cl/Cd: 48.12 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-c5d-il-100000.txt
Download as CSV file: xf-c5d-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: LOCKHEED C-5A BL758.6 AIRFOIL                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000  -0.4822   0.10913   0.10361  -0.0322   1.0000   0.1239
  -9.750  -0.4892   0.10587   0.10040  -0.0334   1.0000   0.1282
  -9.500  -0.5506   0.10192   0.09668  -0.0413   1.0000   0.1314
  -9.250  -0.5239   0.09768   0.09242  -0.0374   1.0000   0.1333
  -9.000  -0.5071   0.09507   0.08980  -0.0346   1.0000   0.1359
  -8.750  -0.5080   0.09219   0.08697  -0.0337   1.0000   0.1392
  -8.500  -0.5285   0.08879   0.08367  -0.0344   1.0000   0.1434
  -8.250  -0.5945   0.08531   0.08030  -0.0356   1.0000   0.1458
  -8.000  -0.6275   0.08122   0.07620  -0.0347   1.0000   0.1477
  -7.750  -0.5995   0.07817   0.07325  -0.0319   1.0000   0.1502
  -7.500  -0.6000   0.07550   0.07060  -0.0298   1.0000   0.1533
  -7.250  -0.6539   0.07258   0.06734  -0.0294   1.0000   0.1624
  -7.000  -0.6346   0.06843   0.06338  -0.0275   1.0000   0.1645
  -6.750  -0.6271   0.06571   0.06070  -0.0254   1.0000   0.1680
  -6.500  -0.6631   0.04554   0.03814  -0.0257   1.0000   0.0764
  -6.250  -0.6488   0.04229   0.03472  -0.0243   1.0000   0.0751
  -6.000  -0.6347   0.03917   0.03126  -0.0228   1.0000   0.0747
  -5.750  -0.6184   0.03632   0.02804  -0.0214   1.0000   0.0746
  -5.500  -0.5997   0.03368   0.02500  -0.0201   1.0000   0.0744
  -5.250  -0.5789   0.03127   0.02220  -0.0190   1.0000   0.0745
  -5.000  -0.5562   0.02931   0.01982  -0.0180   1.0000   0.0753
  -4.750  -0.5325   0.02724   0.01755  -0.0174   1.0000   0.0781
  -4.500  -0.5096   0.02618   0.01646  -0.0168   1.0000   0.0832
  -4.250  -0.4850   0.02503   0.01504  -0.0159   1.0000   0.0880
  -4.000  -0.4613   0.02384   0.01393  -0.0154   1.0000   0.0950
  -3.750  -0.4369   0.02301   0.01292  -0.0146   1.0000   0.1029
  -3.500  -0.4134   0.02210   0.01212  -0.0140   1.0000   0.1140
  -3.250  -0.3895   0.02117   0.01130  -0.0134   1.0000   0.1279
  -3.000  -0.3658   0.02022   0.01053  -0.0129   1.0000   0.1512
  -2.750  -0.3414   0.01895   0.00975  -0.0127   1.0000   0.2127
  -2.500  -0.3193   0.01645   0.00953  -0.0120   1.0000   0.6063
  -2.250  -0.3074   0.01643   0.01002  -0.0070   1.0000   0.7726
  -2.000  -0.2954   0.01662   0.01029  -0.0024   1.0000   0.8431
  -1.750  -0.2813   0.01689   0.01060   0.0019   1.0000   0.9060
  -1.500  -0.2145   0.01778   0.01130  -0.0039   1.0000   0.9781
  -1.250  -0.1388   0.01834   0.01158  -0.0138   1.0000   1.0000
  -1.000  -0.1421   0.01800   0.01118  -0.0098   1.0000   1.0000
  -0.750  -0.1406   0.01778   0.01088  -0.0065   1.0000   1.0000
  -0.500  -0.1301   0.01777   0.01075  -0.0047   1.0000   1.0000
  -0.250  -0.1139   0.01791   0.01078  -0.0038   1.0000   1.0000
   0.000  -0.0953   0.01815   0.01091  -0.0033   1.0000   1.0000
   0.250  -0.0755   0.01846   0.01113  -0.0030   1.0000   1.0000
   0.500  -0.0376   0.01904   0.01161  -0.0061   0.9952   1.0000
   0.750   0.0061   0.01965   0.01215  -0.0103   0.9872   1.0000
   1.000   0.0487   0.02023   0.01267  -0.0141   0.9783   1.0000
   1.250   0.0908   0.02076   0.01316  -0.0177   0.9687   1.0000
   1.500   0.1340   0.02129   0.01366  -0.0215   0.9598   1.0000
   1.750   0.1742   0.02172   0.01409  -0.0246   0.9501   1.0000
   2.000   0.2092   0.02208   0.01447  -0.0267   0.9392   1.0000
   2.250   0.2505   0.02239   0.01481  -0.0297   0.9281   1.0000
   2.500   0.2986   0.02246   0.01494  -0.0335   0.9149   1.0000
   2.750   0.3498   0.02231   0.01487  -0.0376   0.9020   1.0000
   3.000   0.4013   0.02191   0.01457  -0.0414   0.8885   1.0000
   3.250   0.4456   0.02124   0.01402  -0.0434   0.8705   1.0000
   3.500   0.4948   0.02026   0.01317  -0.0458   0.8531   1.0000
   3.750   0.5479   0.01889   0.01198  -0.0483   0.8352   1.0000
   4.000   0.5987   0.01734   0.01059  -0.0501   0.8143   1.0000
   4.250   0.6332   0.01631   0.00967  -0.0493   0.7855   1.0000
   4.500   0.6665   0.01544   0.00887  -0.0483   0.7435   1.0000
   4.750   0.7043   0.01481   0.00813  -0.0482   0.6739   1.0000
   5.000   0.7280   0.01513   0.00776  -0.0457   0.5223   1.0000
   5.250   0.7241   0.01703   0.00825  -0.0395   0.3069   1.0000
   5.500   0.7284   0.01888   0.00924  -0.0355   0.2084   1.0000
   5.750   0.7411   0.02032   0.01027  -0.0329   0.1727   1.0000
   6.000   0.7600   0.02162   0.01133  -0.0313   0.1538   1.0000
   6.250   0.7833   0.02268   0.01231  -0.0304   0.1419   1.0000
   6.500   0.8091   0.02379   0.01343  -0.0300   0.1330   1.0000
   6.750   0.8371   0.02520   0.01466  -0.0302   0.1256   1.0000
   7.000   0.8647   0.02640   0.01602  -0.0300   0.1203   1.0000
   7.250   0.8927   0.02778   0.01743  -0.0300   0.1154   1.0000
   7.500   0.9214   0.02965   0.01932  -0.0303   0.1107   1.0000
   7.750   0.9457   0.03113   0.02110  -0.0295   0.1071   1.0000
   8.000   0.9699   0.03270   0.02283  -0.0289   0.1031   1.0000
   8.250   0.9953   0.03509   0.02520  -0.0290   0.0988   1.0000
   8.500   1.0122   0.03700   0.02759  -0.0270   0.0964   1.0000
   8.750   1.0274   0.03901   0.03004  -0.0249   0.0931   1.0000
   9.000   1.0430   0.04130   0.03264  -0.0230   0.0902   1.0000
   9.250   1.0631   0.04351   0.03486  -0.0224   0.0868   1.0000
   9.500   1.0716   0.04722   0.03889  -0.0202   0.0844   1.0000
   9.750   1.0734   0.05030   0.04252  -0.0166   0.0834   1.0000
  10.000   1.0722   0.05397   0.04665  -0.0131   0.0828   1.0000
  10.250   1.0661   0.05778   0.05090  -0.0094   0.0823   1.0000
  10.500   1.0551   0.06176   0.05526  -0.0056   0.0820   1.0000
  10.750   1.0400   0.06592   0.05972  -0.0020   0.0822   1.0000
  11.000   1.0221   0.07004   0.06408   0.0015   0.0828   1.0000
  11.250   1.0079   0.07450   0.06868   0.0040   0.0837   1.0000
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