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GOE 565 AIRFOIL (goe565-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 565 AIRFOIL (goe565-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.88 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe565-il-1000000-n5.txt
Download as CSV file: xf-goe565-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 565 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.6372   0.10388   0.10197  -0.0270   1.0000   0.0055
 -13.000  -0.9646   0.03782   0.03549  -0.0749   1.0000   0.0044
 -12.750  -0.9782   0.03304   0.03046  -0.0750   1.0000   0.0044
 -12.500  -0.9799   0.03004   0.02725  -0.0738   1.0000   0.0045
 -12.250  -0.9770   0.02772   0.02474  -0.0721   1.0000   0.0045
 -12.000  -0.9623   0.02575   0.02258  -0.0720   0.9993   0.0046
 -11.750  -0.9383   0.02384   0.02048  -0.0734   0.9974   0.0048
 -11.500  -0.9127   0.02223   0.01868  -0.0748   0.9954   0.0049
 -11.250  -0.8868   0.02088   0.01717  -0.0758   0.9932   0.0051
 -11.000  -0.8605   0.01969   0.01583  -0.0766   0.9907   0.0052
 -10.750  -0.8328   0.01864   0.01461  -0.0775   0.9886   0.0054
 -10.500  -0.8039   0.01770   0.01354  -0.0785   0.9870   0.0055
 -10.250  -0.7763   0.01664   0.01233  -0.0793   0.9848   0.0057
 -10.000  -0.7496   0.01568   0.01125  -0.0798   0.9818   0.0061
  -9.750  -0.7212   0.01492   0.01039  -0.0805   0.9799   0.0064
  -9.500  -0.6918   0.01425   0.00964  -0.0813   0.9783   0.0068
  -9.250  -0.6618   0.01365   0.00894  -0.0821   0.9769   0.0072
  -9.000  -0.6350   0.01315   0.00835  -0.0822   0.9734   0.0076
  -8.750  -0.6063   0.01269   0.00781  -0.0826   0.9706   0.0079
  -8.500  -0.5773   0.01204   0.00708  -0.0831   0.9684   0.0087
  -8.250  -0.5487   0.01154   0.00652  -0.0835   0.9658   0.0094
  -8.000  -0.5216   0.01112   0.00604  -0.0835   0.9617   0.0103
  -7.750  -0.4927   0.01075   0.00560  -0.0838   0.9584   0.0110
  -7.500  -0.4645   0.01034   0.00514  -0.0840   0.9551   0.0126
  -7.250  -0.4378   0.00997   0.00475  -0.0839   0.9506   0.0147
  -7.000  -0.4100   0.00965   0.00443  -0.0839   0.9468   0.0187
  -6.750  -0.3823   0.00941   0.00418  -0.0839   0.9431   0.0222
  -6.500  -0.3551   0.00925   0.00404  -0.0838   0.9383   0.0254
  -6.250  -0.3271   0.00910   0.00384  -0.0838   0.9340   0.0274
  -6.000  -0.2997   0.00895   0.00365  -0.0836   0.9295   0.0286
  -5.750  -0.2725   0.00878   0.00349  -0.0835   0.9246   0.0306
  -5.500  -0.2448   0.00865   0.00334  -0.0834   0.9198   0.0321
  -5.250  -0.2177   0.00854   0.00320  -0.0831   0.9134   0.0335
  -5.000  -0.1904   0.00843   0.00305  -0.0829   0.9063   0.0346
  -4.750  -0.1630   0.00836   0.00296  -0.0827   0.8992   0.0356
  -4.500  -0.1356   0.00830   0.00286  -0.0825   0.8917   0.0360
  -4.250  -0.1094   0.00798   0.00247  -0.0821   0.8835   0.0374
  -4.000  -0.0827   0.00779   0.00222  -0.0817   0.8748   0.0387
  -3.750  -0.0557   0.00763   0.00205  -0.0815   0.8658   0.0398
  -3.500  -0.0286   0.00752   0.00189  -0.0812   0.8578   0.0410
  -3.250  -0.0015   0.00741   0.00175  -0.0809   0.8480   0.0424
  -3.000   0.0251   0.00733   0.00161  -0.0805   0.8328   0.0435
  -2.750   0.0512   0.00728   0.00146  -0.0800   0.8118   0.0445
  -2.500   0.0770   0.00727   0.00134  -0.0794   0.7873   0.0453
  -2.250   0.1029   0.00727   0.00124  -0.0789   0.7637   0.0459
  -2.000   0.1291   0.00726   0.00114  -0.0784   0.7446   0.0468
  -1.750   0.1559   0.00721   0.00104  -0.0781   0.7324   0.0495
  -1.500   0.1826   0.00717   0.00097  -0.0777   0.7187   0.0525
  -1.250   0.2093   0.00716   0.00091  -0.0774   0.7037   0.0554
  -1.000   0.2361   0.00715   0.00086  -0.0770   0.6898   0.0585
  -0.750   0.2628   0.00711   0.00083  -0.0767   0.6763   0.0705
  -0.500   0.2893   0.00706   0.00082  -0.0764   0.6598   0.1001
  -0.250   0.3154   0.00708   0.00080  -0.0760   0.6361   0.1128
   0.000   0.3409   0.00713   0.00079  -0.0754   0.6041   0.1281
   0.250   0.3653   0.00697   0.00080  -0.0748   0.5730   0.2295
   0.500   0.3904   0.00703   0.00085  -0.0743   0.5423   0.2699
   0.750   0.4158   0.00709   0.00090  -0.0738   0.5150   0.3055
   1.000   0.4414   0.00710   0.00096  -0.0734   0.4913   0.3480
   1.250   0.4660   0.00711   0.00104  -0.0728   0.4586   0.4193
   1.500   0.4901   0.00719   0.00114  -0.0721   0.4178   0.4858
   1.750   0.5137   0.00735   0.00126  -0.0714   0.3703   0.5456
   2.000   0.5370   0.00755   0.00141  -0.0706   0.3232   0.6032
   2.250   0.5617   0.00761   0.00153  -0.0700   0.3006   0.6605
   2.500   0.5816   0.00733   0.00166  -0.0683   0.2787   0.8110
   3.000   0.6566   0.00785   0.00207  -0.0729   0.1817   1.0000
   3.250   0.6814   0.00805   0.00221  -0.0723   0.1692   1.0000
   3.500   0.7065   0.00823   0.00234  -0.0717   0.1608   1.0000
   3.750   0.7318   0.00840   0.00248  -0.0711   0.1520   1.0000
   4.000   0.7568   0.00860   0.00263  -0.0705   0.1428   1.0000
   4.250   0.7823   0.00875   0.00277  -0.0700   0.1363   1.0000
   4.500   0.8071   0.00898   0.00294  -0.0694   0.1232   1.0000
   4.750   0.8297   0.00943   0.00318  -0.0685   0.0865   1.0000
   5.000   0.8537   0.00973   0.00343  -0.0678   0.0717   1.0000
   5.250   0.8761   0.01022   0.00377  -0.0668   0.0441   1.0000
   5.500   0.9001   0.01052   0.00403  -0.0661   0.0364   1.0000
   5.750   0.9244   0.01081   0.00430  -0.0654   0.0327   1.0000
   6.000   0.9488   0.01109   0.00459  -0.0648   0.0297   1.0000
   6.250   0.9736   0.01131   0.00483  -0.0642   0.0288   1.0000
   6.500   0.9982   0.01154   0.00509  -0.0636   0.0278   1.0000
   6.750   1.0226   0.01180   0.00537  -0.0630   0.0262   1.0000
   7.000   1.0464   0.01211   0.00569  -0.0623   0.0241   1.0000
   7.250   1.0698   0.01245   0.00604  -0.0616   0.0218   1.0000
   7.500   1.0936   0.01275   0.00636  -0.0609   0.0204   1.0000
   7.750   1.1175   0.01302   0.00665  -0.0602   0.0189   1.0000
   8.000   1.1407   0.01335   0.00697  -0.0595   0.0164   1.0000
   8.250   1.1633   0.01374   0.00735  -0.0586   0.0140   1.0000
   8.500   1.1858   0.01411   0.00774  -0.0578   0.0125   1.0000
   8.750   1.2075   0.01456   0.00818  -0.0568   0.0104   1.0000
   9.000   1.2295   0.01496   0.00861  -0.0559   0.0097   1.0000
   9.250   1.2510   0.01540   0.00908  -0.0549   0.0088   1.0000
   9.500   1.2718   0.01588   0.00958  -0.0538   0.0081   1.0000
   9.750   1.2916   0.01643   0.01017  -0.0526   0.0073   1.0000
  10.000   1.3120   0.01690   0.01071  -0.0514   0.0070   1.0000
  10.250   1.3317   0.01740   0.01126  -0.0502   0.0066   1.0000
  10.500   1.3507   0.01793   0.01184  -0.0489   0.0062   1.0000
  10.750   1.3688   0.01849   0.01245  -0.0474   0.0059   1.0000
  11.000   1.3857   0.01913   0.01314  -0.0458   0.0056   1.0000
  11.250   1.3999   0.01985   0.01391  -0.0438   0.0052   1.0000
  11.500   1.4134   0.02048   0.01461  -0.0416   0.0050   1.0000
  11.750   1.4266   0.02110   0.01532  -0.0393   0.0049   1.0000
  12.000   1.4395   0.02174   0.01602  -0.0372   0.0046   1.0000
  12.250   1.4511   0.02248   0.01684  -0.0349   0.0045   1.0000
  12.500   1.4620   0.02327   0.01770  -0.0327   0.0043   1.0000
  12.750   1.4722   0.02411   0.01862  -0.0305   0.0042   1.0000
  13.000   1.4813   0.02506   0.01964  -0.0283   0.0041   1.0000
  13.250   1.4896   0.02607   0.02074  -0.0261   0.0040   1.0000
  13.500   1.4970   0.02719   0.02193  -0.0240   0.0039   1.0000
  13.750   1.5028   0.02847   0.02330  -0.0219   0.0037   1.0000
  14.000   1.5060   0.02998   0.02492  -0.0198   0.0037   1.0000
  14.250   1.5052   0.03191   0.02697  -0.0176   0.0035   1.0000
  14.500   1.5063   0.03378   0.02895  -0.0159   0.0034   1.0000
  14.750   1.5074   0.03575   0.03103  -0.0145   0.0034   1.0000
  15.000   1.5077   0.03791   0.03331  -0.0133   0.0034   1.0000
  15.250   1.5067   0.04035   0.03587  -0.0125   0.0033   1.0000
  15.500   1.5046   0.04305   0.03869  -0.0119   0.0033   1.0000
  15.750   1.5027   0.04590   0.04164  -0.0117   0.0033   1.0000
  16.000   1.4931   0.04984   0.04574  -0.0120   0.0033   1.0000
  16.250   1.4885   0.05344   0.04945  -0.0127   0.0032   1.0000
  16.500   1.4751   0.05855   0.05472  -0.0142   0.0032   1.0000
  16.750   1.4667   0.06326   0.05956  -0.0160   0.0031   1.0000
  17.000   1.4504   0.06958   0.06603  -0.0188   0.0031   1.0000
  17.250   1.4374   0.07566   0.07225  -0.0217   0.0031   1.0000
  17.500   1.4148   0.08378   0.08053  -0.0259   0.0031   1.0000
  17.750   1.3923   0.09227   0.08918  -0.0305   0.0031   1.0000
  18.000   1.3649   0.10199   0.09906  -0.0358   0.0031   1.0000
  18.250   1.3387   0.11177   0.10899  -0.0412   0.0031   1.0000
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