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GOE 479 AIRFOIL (goe479-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 479 AIRFOIL (goe479-il)
Reynolds number: 1,000,000
Max Cl/Cd: 121.47 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe479-il-1000000.txt
Download as CSV file: xf-goe479-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 479 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.9373   0.03541   0.03277  -0.0926   1.0000   0.0206
 -13.500  -0.9674   0.03371   0.03098  -0.0865   1.0000   0.0207
 -13.250  -0.9784   0.03227   0.02945  -0.0824   1.0000   0.0208
 -13.000  -0.9692   0.03086   0.02793  -0.0814   0.9992   0.0211
 -12.750  -0.9441   0.02918   0.02609  -0.0835   0.9972   0.0215
 -12.500  -0.9191   0.02758   0.02431  -0.0853   0.9952   0.0219
 -12.250  -0.8920   0.02625   0.02283  -0.0869   0.9936   0.0223
 -12.000  -0.8672   0.02533   0.02177  -0.0875   0.9910   0.0226
 -11.750  -0.8481   0.02298   0.01918  -0.0884   0.9879   0.0232
 -11.500  -0.8193   0.02222   0.01839  -0.0895   0.9862   0.0236
 -11.250  -0.7882   0.02169   0.01783  -0.0907   0.9849   0.0240
 -11.000  -0.7565   0.02113   0.01722  -0.0921   0.9838   0.0244
 -10.750  -0.7247   0.02041   0.01641  -0.0935   0.9829   0.0249
 -10.500  -0.7022   0.01963   0.01552  -0.0930   0.9786   0.0253
 -10.250  -0.6727   0.01909   0.01488  -0.0938   0.9764   0.0259
 -10.000  -0.6415   0.01855   0.01424  -0.0948   0.9747   0.0263
  -9.750  -0.6096   0.01790   0.01347  -0.0960   0.9733   0.0266
  -9.500  -0.5808   0.01618   0.01161  -0.0973   0.9718   0.0274
  -9.250  -0.5480   0.01562   0.01103  -0.0986   0.9704   0.0279
  -9.000  -0.5229   0.01527   0.01065  -0.0982   0.9655   0.0284
  -8.750  -0.4934   0.01487   0.01020  -0.0986   0.9620   0.0290
  -8.500  -0.4631   0.01438   0.00964  -0.0992   0.9588   0.0296
  -8.250  -0.4316   0.01385   0.00903  -0.1001   0.9558   0.0301
  -8.000  -0.4082   0.01345   0.00856  -0.0992   0.9489   0.0305
  -7.750  -0.3794   0.01312   0.00815  -0.0993   0.9437   0.0309
  -7.500  -0.3552   0.01219   0.00713  -0.0988   0.9376   0.0317
  -7.250  -0.3302   0.01177   0.00669  -0.0982   0.9300   0.0324
  -7.000  -0.3032   0.01143   0.00630  -0.0979   0.9224   0.0329
  -6.750  -0.2778   0.01112   0.00595  -0.0973   0.9128   0.0335
  -6.500  -0.2519   0.01082   0.00559  -0.0967   0.9031   0.0341
  -6.250  -0.2256   0.01055   0.00524  -0.0962   0.8927   0.0348
  -6.000  -0.2003   0.01029   0.00492  -0.0955   0.8803   0.0354
  -5.750  -0.1740   0.01014   0.00470  -0.0950   0.8682   0.0359
  -5.500  -0.1502   0.00962   0.00410  -0.0941   0.8555   0.0369
  -5.250  -0.1251   0.00936   0.00379  -0.0934   0.8413   0.0378
  -5.000  -0.0996   0.00919   0.00356  -0.0927   0.8257   0.0387
  -4.750  -0.0741   0.00905   0.00334  -0.0920   0.8093   0.0397
  -4.500  -0.0487   0.00892   0.00313  -0.0913   0.7918   0.0407
  -4.250  -0.0232   0.00884   0.00296  -0.0907   0.7744   0.0415
  -4.000   0.0013   0.00861   0.00265  -0.0898   0.7578   0.0432
  -3.750   0.0267   0.00850   0.00248  -0.0892   0.7430   0.0449
  -3.500   0.0527   0.00841   0.00234  -0.0886   0.7298   0.0466
  -3.250   0.0791   0.00835   0.00223  -0.0881   0.7179   0.0482
  -3.000   0.1046   0.00819   0.00202  -0.0875   0.7069   0.0513
  -2.750   0.1308   0.00812   0.00191  -0.0870   0.6962   0.0544
  -2.500   0.1573   0.00801   0.00179  -0.0865   0.6871   0.0585
  -2.250   0.1835   0.00794   0.00170  -0.0861   0.6782   0.0640
  -2.000   0.2101   0.00782   0.00160  -0.0857   0.6703   0.0728
  -1.750   0.2361   0.00771   0.00152  -0.0852   0.6620   0.0896
  -1.500   0.2623   0.00755   0.00147  -0.0847   0.6543   0.1234
  -1.250   0.2884   0.00745   0.00144  -0.0843   0.6464   0.1530
  -1.000   0.3150   0.00736   0.00141  -0.0839   0.6395   0.1801
  -0.750   0.3414   0.00727   0.00139  -0.0835   0.6319   0.2118
  -0.500   0.3673   0.00717   0.00139  -0.0831   0.6243   0.2524
  -0.250   0.3932   0.00704   0.00138  -0.0826   0.6151   0.3012
   0.000   0.4181   0.00686   0.00138  -0.0819   0.6055   0.3762
   0.250   0.4404   0.00652   0.00141  -0.0809   0.5946   0.5210
   0.500   0.4623   0.00617   0.00145  -0.0796   0.5843   0.6593
   0.750   0.4819   0.00588   0.00150  -0.0776   0.5751   0.7874
   1.000   0.5411   0.00566   0.00167  -0.0841   0.5626   0.9655
   1.250   0.5893   0.00580   0.00175  -0.0884   0.5492   0.9853
   1.500   0.6289   0.00592   0.00179  -0.0909   0.5362   0.9923
   1.750   0.6703   0.00604   0.00183  -0.0938   0.5209   0.9972
   2.000   0.7090   0.00616   0.00187  -0.0962   0.5039   1.0000
   2.250   0.7315   0.00629   0.00192  -0.0950   0.4882   1.0000
   2.500   0.7538   0.00644   0.00198  -0.0938   0.4720   1.0000
   2.750   0.7759   0.00661   0.00206  -0.0925   0.4548   1.0000
   3.000   0.7984   0.00677   0.00215  -0.0914   0.4418   1.0000
   3.250   0.8208   0.00693   0.00225  -0.0902   0.4295   1.0000
   3.500   0.8439   0.00707   0.00234  -0.0891   0.4179   1.0000
   3.750   0.8669   0.00722   0.00245  -0.0881   0.4065   1.0000
   4.000   0.8897   0.00739   0.00256  -0.0870   0.3961   1.0000
   4.250   0.9128   0.00754   0.00267  -0.0860   0.3844   1.0000
   4.500   0.9356   0.00771   0.00279  -0.0849   0.3703   1.0000
   4.750   0.9584   0.00789   0.00292  -0.0838   0.3572   1.0000
   5.000   0.9806   0.00810   0.00307  -0.0827   0.3403   1.0000
   5.250   1.0019   0.00837   0.00323  -0.0814   0.3196   1.0000
   5.500   1.0222   0.00869   0.00343  -0.0799   0.2926   1.0000
   5.750   1.0417   0.00907   0.00367  -0.0783   0.2668   1.0000
   6.000   1.0608   0.00946   0.00393  -0.0767   0.2425   1.0000
   6.250   1.0803   0.00983   0.00420  -0.0751   0.2218   1.0000
   6.500   1.0993   0.01023   0.00449  -0.0735   0.2001   1.0000
   6.750   1.1165   0.01072   0.00483  -0.0715   0.1721   1.0000
   7.000   1.1278   0.01154   0.00535  -0.0686   0.1247   1.0000
   7.250   1.1291   0.01290   0.00626  -0.0641   0.0545   1.0000
   7.500   1.1459   0.01337   0.00670  -0.0621   0.0466   1.0000
   7.750   1.1629   0.01381   0.00712  -0.0601   0.0427   1.0000
   8.000   1.1806   0.01412   0.00746  -0.0583   0.0413   1.0000
   8.250   1.1968   0.01446   0.00781  -0.0562   0.0401   1.0000
   8.500   1.2123   0.01484   0.00820  -0.0540   0.0389   1.0000
   8.750   1.2267   0.01529   0.00867  -0.0516   0.0374   1.0000
   9.000   1.2394   0.01585   0.00926  -0.0491   0.0360   1.0000
   9.250   1.2558   0.01624   0.00969  -0.0473   0.0356   1.0000
   9.500   1.2719   0.01667   0.01015  -0.0454   0.0351   1.0000
   9.750   1.2870   0.01715   0.01067  -0.0435   0.0345   1.0000
  10.000   1.3017   0.01768   0.01124  -0.0416   0.0339   1.0000
  10.250   1.3161   0.01823   0.01182  -0.0398   0.0332   1.0000
  10.500   1.3294   0.01886   0.01248  -0.0378   0.0325   1.0000
  10.750   1.3411   0.01960   0.01326  -0.0358   0.0318   1.0000
  11.000   1.3501   0.02053   0.01423  -0.0335   0.0312   1.0000
  11.250   1.3529   0.02187   0.01566  -0.0307   0.0304   1.0000
  11.500   1.3663   0.02262   0.01645  -0.0292   0.0302   1.0000
  11.750   1.3800   0.02337   0.01726  -0.0279   0.0298   1.0000
  12.000   1.3911   0.02434   0.01828  -0.0264   0.0294   1.0000
  12.250   1.4015   0.02539   0.01938  -0.0250   0.0290   1.0000
  12.500   1.4111   0.02655   0.02060  -0.0236   0.0286   1.0000
  12.750   1.4219   0.02766   0.02176  -0.0224   0.0280   1.0000
  13.000   1.4302   0.02903   0.02317  -0.0213   0.0276   1.0000
  13.250   1.4376   0.03051   0.02470  -0.0202   0.0272   1.0000
  13.500   1.4432   0.03223   0.02647  -0.0191   0.0267   1.0000
  13.750   1.4438   0.03446   0.02877  -0.0181   0.0262   1.0000
  14.000   1.4383   0.03736   0.03176  -0.0170   0.0258   1.0000
  14.250   1.4415   0.03952   0.03400  -0.0164   0.0255   1.0000
  14.500   1.4507   0.04116   0.03571  -0.0161   0.0252   1.0000
  14.750   1.4563   0.04318   0.03780  -0.0157   0.0249   1.0000
  15.000   1.4609   0.04535   0.04005  -0.0155   0.0246   1.0000
  15.250   1.4646   0.04766   0.04243  -0.0153   0.0243   1.0000
  15.500   1.4681   0.05006   0.04490  -0.0152   0.0239   1.0000
  15.750   1.4697   0.05269   0.04760  -0.0152   0.0236   1.0000
  16.000   1.4720   0.05528   0.05026  -0.0153   0.0232   1.0000
  16.250   1.4733   0.05806   0.05309  -0.0155   0.0229   1.0000
  16.500   1.4742   0.06094   0.05602  -0.0158   0.0225   1.0000
  16.750   1.4719   0.06423   0.05938  -0.0162   0.0223   1.0000
  17.000   1.4656   0.06803   0.06325  -0.0167   0.0220   1.0000
  17.250   1.4521   0.07272   0.06802  -0.0173   0.0215   1.0000
  17.500   1.4512   0.07604   0.07143  -0.0179   0.0213   1.0000
  17.750   1.4510   0.07931   0.07478  -0.0187   0.0211   1.0000
  18.000   1.4499   0.08276   0.07832  -0.0195   0.0209   1.0000
  18.250   1.4495   0.08618   0.08183  -0.0205   0.0206   1.0000
  18.500   1.4450   0.09009   0.08582  -0.0215   0.0204   1.0000
  18.750   1.4415   0.09393   0.08974  -0.0226   0.0201   1.0000
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