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LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL (lg10sc-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL (lg10sc-il)
Reynolds number: 1,000,000
Max Cl/Cd: 90.76 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-lg10sc-il-1000000-n5.txt
Download as CSV file: xf-lg10sc-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: LOCKHEED-GEORGIA SUPERCRITICAL AIRFOIL          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.6000   0.10911   0.10742   0.0035   1.0000   0.0052
 -10.750  -0.6028   0.10378   0.10210   0.0010   1.0000   0.0052
 -10.250  -0.9084   0.03095   0.02778  -0.0251   1.0000   0.0048
 -10.000  -0.9078   0.02705   0.02346  -0.0224   1.0000   0.0049
  -9.750  -0.8967   0.02482   0.02096  -0.0205   1.0000   0.0050
  -9.500  -0.8828   0.02307   0.01898  -0.0187   1.0000   0.0050
  -9.250  -0.8678   0.02152   0.01722  -0.0168   1.0000   0.0050
  -9.000  -0.8517   0.02024   0.01576  -0.0150   1.0000   0.0051
  -8.750  -0.8345   0.01915   0.01453  -0.0133   1.0000   0.0051
  -8.500  -0.8169   0.01822   0.01347  -0.0115   1.0000   0.0052
  -8.250  -0.7938   0.01733   0.01246  -0.0109   0.9993   0.0053
  -8.000  -0.7655   0.01646   0.01146  -0.0114   0.9976   0.0054
  -7.750  -0.7363   0.01565   0.01056  -0.0120   0.9960   0.0055
  -7.500  -0.7063   0.01491   0.00972  -0.0127   0.9946   0.0056
  -7.250  -0.6773   0.01422   0.00895  -0.0132   0.9923   0.0057
  -7.000  -0.6476   0.01359   0.00824  -0.0137   0.9899   0.0059
  -6.750  -0.6175   0.01300   0.00757  -0.0144   0.9875   0.0061
  -6.500  -0.5870   0.01246   0.00696  -0.0151   0.9852   0.0063
  -6.250  -0.5585   0.01199   0.00644  -0.0153   0.9812   0.0065
  -6.000  -0.5296   0.01157   0.00597  -0.0156   0.9767   0.0067
  -5.750  -0.4996   0.01114   0.00550  -0.0161   0.9730   0.0068
  -5.500  -0.4731   0.01064   0.00496  -0.0159   0.9666   0.0072
  -5.250  -0.4449   0.01031   0.00462  -0.0159   0.9605   0.0075
  -5.000  -0.4178   0.01003   0.00430  -0.0157   0.9528   0.0078
  -4.750  -0.3910   0.00975   0.00400  -0.0154   0.9442   0.0082
  -4.500  -0.3648   0.00949   0.00371  -0.0149   0.9334   0.0086
  -4.250  -0.3395   0.00928   0.00342  -0.0142   0.9152   0.0090
  -4.000  -0.3150   0.00911   0.00313  -0.0132   0.8843   0.0095
  -3.750  -0.2900   0.00895   0.00287  -0.0124   0.8528   0.0105
  -3.500  -0.2634   0.00881   0.00266  -0.0120   0.8316   0.0114
  -3.250  -0.2367   0.00870   0.00246  -0.0117   0.8097   0.0122
  -3.000  -0.2101   0.00856   0.00224  -0.0113   0.7871   0.0137
  -2.500  -0.1565   0.00842   0.00192  -0.0107   0.7327   0.0181
  -2.250  -0.1297   0.00835   0.00178  -0.0104   0.7029   0.0246
  -2.000  -0.1031   0.00830   0.00166  -0.0101   0.6678   0.0384
  -1.750  -0.0766   0.00821   0.00155  -0.0098   0.6326   0.0628
  -1.500  -0.0506   0.00808   0.00145  -0.0096   0.5935   0.1112
  -1.250  -0.0250   0.00793   0.00135  -0.0093   0.5497   0.1778
  -1.000  -0.0002   0.00761   0.00126  -0.0089   0.5086   0.2881
  -0.750   0.0227   0.00705   0.00115  -0.0083   0.4674   0.4700
  -0.500   0.0459   0.00666   0.00111  -0.0076   0.4243   0.6169
  -0.250   0.0694   0.00641   0.00112  -0.0068   0.3895   0.7299
   0.000   0.0944   0.00635   0.00116  -0.0061   0.3606   0.7931
   0.250   0.1202   0.00639   0.00121  -0.0056   0.3332   0.8311
   0.500   0.1467   0.00647   0.00126  -0.0052   0.3084   0.8555
   0.750   0.1736   0.00655   0.00130  -0.0049   0.2899   0.8732
   1.000   0.2007   0.00665   0.00135  -0.0046   0.2723   0.8871
   1.250   0.2279   0.00677   0.00140  -0.0044   0.2563   0.8989
   1.500   0.2551   0.00685   0.00146  -0.0042   0.2448   0.9100
   1.750   0.2824   0.00695   0.00152  -0.0040   0.2344   0.9197
   2.000   0.3096   0.00707   0.00158  -0.0038   0.2232   0.9292
   2.250   0.3369   0.00717   0.00166  -0.0036   0.2143   0.9378
   2.500   0.3645   0.00728   0.00173  -0.0035   0.2071   0.9456
   2.750   0.3924   0.00739   0.00181  -0.0034   0.1993   0.9526
   3.000   0.4203   0.00751   0.00190  -0.0034   0.1916   0.9595
   3.250   0.4496   0.00764   0.00199  -0.0037   0.1837   0.9648
   3.500   0.4781   0.00776   0.00208  -0.0039   0.1780   0.9705
   3.750   0.5082   0.00789   0.00218  -0.0044   0.1721   0.9744
   4.000   0.5390   0.00804   0.00230  -0.0051   0.1653   0.9779
   4.250   0.5689   0.00818   0.00241  -0.0056   0.1594   0.9820
   4.500   0.5991   0.00834   0.00253  -0.0062   0.1532   0.9853
   4.750   0.6314   0.00848   0.00267  -0.0073   0.1489   0.9873
   5.000   0.6635   0.00864   0.00280  -0.0083   0.1437   0.9893
   5.250   0.6948   0.00882   0.00295  -0.0092   0.1376   0.9913
   5.500   0.7258   0.00897   0.00311  -0.0100   0.1333   0.9935
   5.750   0.7570   0.00915   0.00327  -0.0109   0.1285   0.9950
   6.000   0.7888   0.00934   0.00344  -0.0119   0.1239   0.9963
   6.250   0.8204   0.00950   0.00362  -0.0129   0.1207   0.9977
   6.500   0.8515   0.00971   0.00381  -0.0138   0.1160   0.9991
   6.750   0.8801   0.00993   0.00401  -0.0142   0.1103   1.0000
   7.000   0.9034   0.01011   0.00420  -0.0133   0.1057   1.0000
   7.250   0.9265   0.01034   0.00440  -0.0125   0.1006   1.0000
   7.500   0.9502   0.01054   0.00461  -0.0118   0.0973   1.0000
   7.750   0.9739   0.01075   0.00484  -0.0111   0.0928   1.0000
   8.000   0.9971   0.01103   0.00509  -0.0103   0.0869   1.0000
   8.250   1.0211   0.01125   0.00532  -0.0097   0.0835   1.0000
   8.500   1.0449   0.01152   0.00559  -0.0091   0.0786   1.0000
   8.750   1.0689   0.01181   0.00588  -0.0085   0.0743   1.0000
   9.000   1.0930   0.01210   0.00618  -0.0080   0.0691   1.0000
   9.250   1.1167   0.01246   0.00651  -0.0074   0.0630   1.0000
   9.500   1.1400   0.01287   0.00690  -0.0068   0.0556   1.0000
   9.750   1.1627   0.01335   0.00735  -0.0062   0.0466   1.0000
  10.000   1.1846   0.01393   0.00787  -0.0055   0.0374   1.0000
  10.250   1.2071   0.01444   0.00838  -0.0048   0.0323   1.0000
  10.500   1.2297   0.01494   0.00889  -0.0042   0.0285   1.0000
  10.750   1.2516   0.01548   0.00945  -0.0035   0.0251   1.0000
  11.000   1.2740   0.01596   0.00997  -0.0029   0.0229   1.0000
  11.250   1.2959   0.01649   0.01052  -0.0022   0.0207   1.0000
  11.500   1.3171   0.01707   0.01113  -0.0015   0.0186   1.0000
  11.750   1.3384   0.01760   0.01170  -0.0007   0.0171   1.0000
  12.000   1.3585   0.01823   0.01237   0.0001   0.0154   1.0000
  12.250   1.3788   0.01881   0.01300   0.0009   0.0143   1.0000
  12.500   1.3985   0.01942   0.01366   0.0018   0.0133   1.0000
  12.750   1.4170   0.02010   0.01439   0.0028   0.0123   1.0000
  13.000   1.4343   0.02085   0.01519   0.0040   0.0114   1.0000
  13.250   1.4521   0.02150   0.01592   0.0051   0.0110   1.0000
  13.500   1.4684   0.02222   0.01672   0.0063   0.0104   1.0000
  13.750   1.4825   0.02301   0.01757   0.0079   0.0098   1.0000
  14.000   1.4927   0.02388   0.01851   0.0100   0.0093   1.0000
  14.250   1.5009   0.02489   0.01959   0.0122   0.0087   1.0000
  14.500   1.5105   0.02584   0.02063   0.0141   0.0084   1.0000
  14.750   1.5189   0.02692   0.02180   0.0158   0.0081   1.0000
  15.000   1.5256   0.02817   0.02314   0.0174   0.0077   1.0000
  15.250   1.5306   0.02964   0.02470   0.0189   0.0074   1.0000
  15.500   1.5337   0.03138   0.02653   0.0201   0.0071   1.0000
  15.750   1.5345   0.03345   0.02871   0.0210   0.0068   1.0000
  16.000   1.5327   0.03599   0.03136   0.0215   0.0066   1.0000
  16.250   1.5290   0.03898   0.03447   0.0213   0.0064   1.0000
  16.500   1.5245   0.04241   0.03803   0.0205   0.0063   1.0000
  16.750   1.5159   0.04669   0.04246   0.0188   0.0062   1.0000
  17.000   1.5017   0.05226   0.04819   0.0160   0.0061   1.0000
  17.250   1.4787   0.05978   0.05590   0.0118   0.0061   1.0000
  17.500   1.4413   0.07023   0.06656   0.0059   0.0062   1.0000
  17.750   1.3819   0.08432   0.08089  -0.0013   0.0064   1.0000
  18.000   1.3263   0.09746   0.09423  -0.0076   0.0067   1.0000
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