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GOE 510 AIRFOIL (goe510-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 510 AIRFOIL (goe510-il)
Reynolds number: 1,000,000
Max Cl/Cd: 99.46 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe510-il-1000000-n5.txt
Download as CSV file: xf-goe510-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 510 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  -0.7022   0.02808   0.02499  -0.1404   0.9610   0.0278
 -13.000  -0.6861   0.02560   0.02228  -0.1414   0.9591   0.0279
 -12.750  -0.6652   0.02355   0.02005  -0.1426   0.9577   0.0282
 -12.500  -0.6608   0.02265   0.01906  -0.1389   0.9511   0.0284
 -12.250  -0.6385   0.02166   0.01798  -0.1389   0.9481   0.0286
 -12.000  -0.6101   0.02088   0.01712  -0.1398   0.9461   0.0288
 -11.750  -0.5797   0.02003   0.01617  -0.1412   0.9441   0.0289
 -11.500  -0.5634   0.01939   0.01546  -0.1394   0.9388   0.0291
 -11.250  -0.5430   0.01886   0.01486  -0.1383   0.9339   0.0293
 -11.000  -0.5155   0.01822   0.01413  -0.1387   0.9308   0.0295
 -10.750  -0.4849   0.01763   0.01346  -0.1397   0.9281   0.0297
 -10.500  -0.4703   0.01714   0.01289  -0.1373   0.9210   0.0299
 -10.250  -0.4440   0.01657   0.01223  -0.1373   0.9152   0.0301
 -10.000  -0.4196   0.01605   0.01161  -0.1369   0.9087   0.0304
  -9.750  -0.3949   0.01554   0.01101  -0.1364   0.8997   0.0306
  -9.500  -0.3706   0.01503   0.01039  -0.1359   0.8904   0.0309
  -9.250  -0.3445   0.01456   0.00980  -0.1357   0.8805   0.0312
  -9.000  -0.3209   0.01419   0.00933  -0.1349   0.8700   0.0315
  -8.750  -0.2966   0.01386   0.00889  -0.1343   0.8604   0.0317
  -8.500  -0.2731   0.01351   0.00841  -0.1334   0.8491   0.0320
  -8.250  -0.2508   0.01321   0.00800  -0.1322   0.8361   0.0321
  -8.000  -0.2289   0.01292   0.00760  -0.1310   0.8236   0.0322
  -7.750  -0.2082   0.01250   0.00708  -0.1296   0.8132   0.0326
  -7.500  -0.1865   0.01222   0.00672  -0.1283   0.8026   0.0329
  -7.250  -0.1644   0.01201   0.00644  -0.1270   0.7913   0.0332
  -7.000  -0.1426   0.01185   0.00621  -0.1256   0.7790   0.0335
  -6.750  -0.1215   0.01172   0.00599  -0.1241   0.7641   0.0338
  -6.500  -0.1003   0.01157   0.00576  -0.1226   0.7497   0.0340
  -6.250  -0.0784   0.01145   0.00557  -0.1213   0.7360   0.0344
  -6.000  -0.0570   0.01131   0.00536  -0.1198   0.7219   0.0347
  -5.750  -0.0363   0.01119   0.00515  -0.1182   0.7063   0.0350
  -5.500  -0.0161   0.01107   0.00494  -0.1164   0.6897   0.0354
  -5.250   0.0039   0.01097   0.00474  -0.1147   0.6728   0.0357
  -5.000   0.0246   0.01087   0.00455  -0.1130   0.6582   0.0361
  -4.750   0.0456   0.01078   0.00438  -0.1115   0.6456   0.0364
  -4.500   0.0681   0.01071   0.00425  -0.1102   0.6346   0.0368
  -4.250   0.0902   0.01061   0.00409  -0.1089   0.6248   0.0371
  -4.000   0.1113   0.01050   0.00390  -0.1074   0.6137   0.0374
  -3.750   0.1335   0.01032   0.00368  -0.1061   0.6044   0.0379
  -3.500   0.1548   0.01024   0.00356  -0.1046   0.5939   0.0384
  -3.250   0.1774   0.01016   0.00344  -0.1034   0.5840   0.0389
  -3.000   0.1986   0.01010   0.00334  -0.1018   0.5747   0.0393
  -2.750   0.2188   0.01006   0.00325  -0.1001   0.5626   0.0398
  -2.500   0.2394   0.01001   0.00315  -0.0984   0.5505   0.0403
  -2.250   0.2588   0.00998   0.00306  -0.0965   0.5350   0.0408
  -2.000   0.2782   0.00998   0.00298  -0.0946   0.5179   0.0413
  -1.750   0.2972   0.01001   0.00292  -0.0927   0.4986   0.0418
  -1.500   0.3160   0.01006   0.00288  -0.0907   0.4784   0.0423
  -1.250   0.3356   0.01013   0.00286  -0.0889   0.4617   0.0428
  -1.000   0.3561   0.01013   0.00280  -0.0873   0.4499   0.0432
  -0.750   0.3764   0.01010   0.00272  -0.0856   0.4404   0.0440
  -0.500   0.3975   0.01009   0.00269  -0.0841   0.4314   0.0448
  -0.250   0.4187   0.01011   0.00268  -0.0826   0.4238   0.0454
   0.000   0.4409   0.01013   0.00267  -0.0814   0.4174   0.0463
   0.250   0.4623   0.01017   0.00268  -0.0800   0.4108   0.0471
   0.500   0.4845   0.01019   0.00269  -0.0788   0.4055   0.0479
   0.750   0.5067   0.01022   0.00271  -0.0775   0.4005   0.0488
   1.000   0.5282   0.01028   0.00274  -0.0762   0.3950   0.0494
   1.250   0.5497   0.01032   0.00276  -0.0748   0.3903   0.0502
   1.500   0.5719   0.01032   0.00276  -0.0736   0.3862   0.0516
   1.750   0.5940   0.01035   0.00279  -0.0724   0.3820   0.0529
   2.000   0.6156   0.01040   0.00283  -0.0711   0.3778   0.0544
   2.250   0.6369   0.01047   0.00288  -0.0697   0.3733   0.0559
   2.500   0.6593   0.01051   0.00293  -0.0686   0.3698   0.0574
   2.750   0.6812   0.01055   0.00298  -0.0673   0.3663   0.0600
   3.000   0.7025   0.01061   0.00305  -0.0660   0.3626   0.0648
   3.250   0.7227   0.01064   0.00312  -0.0645   0.3589   0.0843
   3.500   0.7407   0.01054   0.00324  -0.0625   0.3556   0.1709
   3.750   0.7620   0.01056   0.00335  -0.0613   0.3520   0.2050
   4.000   0.7830   0.01063   0.00347  -0.0599   0.3482   0.2304
   4.250   0.8035   0.01073   0.00359  -0.0585   0.3439   0.2450
   4.500   0.8237   0.01085   0.00373  -0.0571   0.3402   0.2599
   4.750   0.8458   0.01093   0.00384  -0.0560   0.3373   0.2708
   5.000   0.8674   0.01103   0.00397  -0.0548   0.3338   0.2804
   5.250   0.8882   0.01116   0.00411  -0.0535   0.3294   0.2910
   5.750   0.9283   0.01143   0.00442  -0.0507   0.3208   0.3174
   6.000   0.9488   0.01154   0.00457  -0.0494   0.3168   0.3324
   6.250   0.9685   0.01168   0.00475  -0.0480   0.3124   0.3510
   6.500   0.9851   0.01174   0.00496  -0.0460   0.3080   0.4329
   7.000   1.1518   0.01158   0.00596  -0.0718   0.2797   0.9888
   7.250   1.1729   0.01194   0.00628  -0.0708   0.2711   0.9970
   7.500   1.2035   0.01239   0.00664  -0.0721   0.2577   0.9993
   7.750   1.2251   0.01286   0.00701  -0.0715   0.2418   1.0000
   8.000   1.2370   0.01327   0.00736  -0.0688   0.2298   1.0000
   8.250   1.2483   0.01373   0.00774  -0.0660   0.2165   1.0000
   8.500   1.2629   0.01410   0.00808  -0.0639   0.2086   1.0000
   8.750   1.2743   0.01464   0.00853  -0.0613   0.1946   1.0000
   9.000   1.2858   0.01520   0.00903  -0.0588   0.1822   1.0000
   9.250   1.2961   0.01586   0.00960  -0.0562   0.1666   1.0000
   9.500   1.3023   0.01673   0.01035  -0.0531   0.1460   1.0000
   9.750   1.3075   0.01772   0.01121  -0.0500   0.1254   1.0000
  10.250   1.3084   0.02033   0.01355  -0.0430   0.0803   1.0000
  10.500   1.2903   0.02284   0.01583  -0.0376   0.0326   1.0000
  10.750   1.2942   0.02417   0.01716  -0.0351   0.0192   1.0000
  11.000   1.3052   0.02511   0.01811  -0.0335   0.0170   1.0000
  11.250   1.3161   0.02608   0.01911  -0.0319   0.0158   1.0000
  11.500   1.3264   0.02713   0.02018  -0.0304   0.0147   1.0000
  11.750   1.3363   0.02822   0.02132  -0.0290   0.0140   1.0000
  12.000   1.3466   0.02934   0.02248  -0.0277   0.0135   1.0000
  12.250   1.3562   0.03055   0.02373  -0.0264   0.0130   1.0000
  12.500   1.3651   0.03184   0.02505  -0.0252   0.0124   1.0000
  12.750   1.3729   0.03327   0.02652  -0.0239   0.0121   1.0000
  13.000   1.3795   0.03483   0.02813  -0.0227   0.0116   1.0000
  13.250   1.3846   0.03659   0.02994  -0.0216   0.0111   1.0000
  13.500   1.3916   0.03822   0.03162  -0.0207   0.0108   1.0000
  13.750   1.3981   0.03996   0.03342  -0.0198   0.0107   1.0000
  14.000   1.4031   0.04187   0.03538  -0.0190   0.0104   1.0000
  14.250   1.4073   0.04391   0.03748  -0.0183   0.0101   1.0000
  14.500   1.4106   0.04611   0.03974  -0.0176   0.0099   1.0000
  14.750   1.4133   0.04843   0.04212  -0.0171   0.0096   1.0000
  15.000   1.4150   0.05089   0.04464  -0.0166   0.0094   1.0000
  15.250   1.4151   0.05355   0.04737  -0.0162   0.0092   1.0000
  15.500   1.4146   0.05636   0.05025  -0.0159   0.0091   1.0000
  15.750   1.4112   0.05957   0.05353  -0.0157   0.0088   1.0000
  16.000   1.4081   0.06281   0.05685  -0.0156   0.0087   1.0000
  16.250   1.4055   0.06602   0.06013  -0.0156   0.0085   1.0000
  16.500   1.4019   0.06943   0.06363  -0.0158   0.0085   1.0000
  16.750   1.3977   0.07298   0.06727  -0.0161   0.0083   1.0000
  17.000   1.3943   0.07649   0.07085  -0.0164   0.0082   1.0000
  17.250   1.3874   0.08050   0.07495  -0.0169   0.0082   1.0000
  17.500   1.3829   0.08421   0.07873  -0.0174   0.0080   1.0000
  17.750   1.3782   0.08798   0.08258  -0.0180   0.0078   1.0000
  18.000   1.3706   0.09221   0.08690  -0.0188   0.0077   1.0000
  18.250   1.3632   0.09642   0.09120  -0.0196   0.0077   1.0000
  18.500   1.3566   0.10053   0.09539  -0.0205   0.0076   1.0000
  18.750   1.3487   0.10487   0.09981  -0.0215   0.0075   1.0000
  19.000   1.3437   0.10882   0.10383  -0.0225   0.0073   1.0000
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