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GOE 655 AIRFOIL (goe655-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 655 AIRFOIL (goe655-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.99 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe655-il-1000000-n5.txt
Download as CSV file: xf-goe655-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 655 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.0022   0.05271   0.04977  -0.0860   1.0000   0.0127
 -16.250  -1.0624   0.03957   0.03635  -0.0965   1.0000   0.0125
 -16.000  -1.0891   0.03246   0.02903  -0.1029   1.0000   0.0126
 -15.750  -1.1086   0.02945   0.02590  -0.1024   1.0000   0.0126
 -15.500  -1.1289   0.02800   0.02435  -0.0977   1.0000   0.0126
 -15.250  -1.1145   0.02655   0.02282  -0.0982   0.9977   0.0130
 -15.000  -1.0926   0.02520   0.02137  -0.0994   0.9946   0.0134
 -14.750  -1.0721   0.02407   0.02015  -0.0998   0.9914   0.0138
 -14.500  -1.0493   0.02305   0.01905  -0.1003   0.9881   0.0142
 -14.250  -1.0241   0.02209   0.01799  -0.1012   0.9855   0.0146
 -14.000  -0.9972   0.02122   0.01708  -0.1021   0.9837   0.0151
 -13.750  -0.9750   0.02053   0.01634  -0.1018   0.9799   0.0156
 -13.500  -0.9499   0.01986   0.01561  -0.1021   0.9769   0.0161
 -13.250  -0.9222   0.01924   0.01494  -0.1027   0.9746   0.0167
 -13.000  -0.8924   0.01861   0.01424  -0.1037   0.9729   0.0173
 -12.750  -0.8636   0.01801   0.01356  -0.1044   0.9708   0.0177
 -12.500  -0.8385   0.01746   0.01299  -0.1044   0.9664   0.0182
 -12.250  -0.8090   0.01697   0.01246  -0.1051   0.9632   0.0187
 -12.000  -0.7779   0.01652   0.01197  -0.1061   0.9604   0.0192
 -11.750  -0.7488   0.01609   0.01149  -0.1066   0.9566   0.0198
 -11.500  -0.7220   0.01568   0.01102  -0.1066   0.9511   0.0203
 -11.250  -0.6923   0.01529   0.01056  -0.1072   0.9462   0.0208
 -11.000  -0.6650   0.01491   0.01011  -0.1072   0.9404   0.0211
 -10.750  -0.6399   0.01443   0.00958  -0.1069   0.9330   0.0216
 -10.500  -0.6130   0.01406   0.00917  -0.1068   0.9258   0.0221
 -10.250  -0.5877   0.01375   0.00881  -0.1063   0.9166   0.0225
 -10.000  -0.5616   0.01349   0.00850  -0.1060   0.9076   0.0231
  -9.750  -0.5362   0.01322   0.00816  -0.1054   0.8975   0.0236
  -9.500  -0.5112   0.01294   0.00781  -0.1048   0.8874   0.0240
  -9.250  -0.4863   0.01267   0.00746  -0.1042   0.8765   0.0244
  -9.000  -0.4612   0.01245   0.00716  -0.1035   0.8636   0.0248
  -8.750  -0.4364   0.01225   0.00686  -0.1028   0.8488   0.0251
  -8.500  -0.4139   0.01188   0.00638  -0.1017   0.8287   0.0257
  -8.250  -0.3907   0.01165   0.00606  -0.1007   0.8047   0.0263
  -8.000  -0.3673   0.01150   0.00579  -0.0996   0.7812   0.0268
  -7.750  -0.3433   0.01136   0.00554  -0.0987   0.7609   0.0273
  -7.500  -0.3189   0.01121   0.00529  -0.0979   0.7435   0.0278
  -7.250  -0.2943   0.01107   0.00505  -0.0971   0.7267   0.0283
  -7.000  -0.2696   0.01091   0.00480  -0.0963   0.7116   0.0288
  -6.750  -0.2442   0.01075   0.00456  -0.0957   0.6991   0.0291
  -6.500  -0.2181   0.01058   0.00433  -0.0952   0.6913   0.0295
  -6.250  -0.1923   0.01040   0.00409  -0.0947   0.6828   0.0299
  -6.000  -0.1665   0.01017   0.00382  -0.0941   0.6749   0.0307
  -5.750  -0.1406   0.01001   0.00362  -0.0936   0.6650   0.0315
  -5.500  -0.1143   0.00987   0.00344  -0.0931   0.6551   0.0322
  -5.250  -0.0882   0.00975   0.00326  -0.0926   0.6445   0.0329
  -5.000  -0.0618   0.00963   0.00309  -0.0921   0.6333   0.0335
  -4.750  -0.0354   0.00953   0.00294  -0.0917   0.6225   0.0342
  -4.500  -0.0091   0.00945   0.00279  -0.0912   0.6102   0.0348
  -4.000   0.0429   0.00928   0.00251  -0.0901   0.5818   0.0375
  -3.750   0.0688   0.00923   0.00241  -0.0896   0.5658   0.0392
  -3.500   0.0947   0.00922   0.00231  -0.0890   0.5484   0.0407
  -3.250   0.1205   0.00918   0.00222  -0.0884   0.5321   0.0432
  -3.000   0.1465   0.00915   0.00214  -0.0879   0.5169   0.0464
  -2.750   0.1727   0.00914   0.00207  -0.0874   0.5023   0.0495
  -2.500   0.1987   0.00911   0.00201  -0.0869   0.4882   0.0546
  -2.250   0.2246   0.00909   0.00195  -0.0864   0.4740   0.0609
  -2.000   0.2505   0.00907   0.00191  -0.0859   0.4598   0.0706
  -1.750   0.2759   0.00902   0.00186  -0.0853   0.4456   0.0893
  -1.500   0.3009   0.00892   0.00182  -0.0847   0.4314   0.1236
  -1.250   0.3262   0.00889   0.00181  -0.0841   0.4162   0.1514
  -1.000   0.3515   0.00889   0.00181  -0.0836   0.4008   0.1745
  -0.500   0.4021   0.00893   0.00185  -0.0824   0.3713   0.2203
  -0.250   0.4276   0.00892   0.00188  -0.0819   0.3617   0.2527
   0.000   0.4524   0.00889   0.00193  -0.0813   0.3510   0.2946
   0.250   0.4781   0.00886   0.00196  -0.0808   0.3436   0.3305
   0.500   0.5034   0.00884   0.00201  -0.0802   0.3368   0.3686
   0.750   0.5290   0.00883   0.00207  -0.0797   0.3317   0.4050
   1.000   0.5550   0.00881   0.00212  -0.0792   0.3277   0.4334
   1.250   0.5810   0.00883   0.00217  -0.0788   0.3235   0.4586
   1.500   0.6064   0.00884   0.00224  -0.0782   0.3193   0.4909
   1.750   0.6316   0.00883   0.00231  -0.0777   0.3157   0.5275
   2.000   0.6566   0.00877   0.00238  -0.0770   0.3126   0.5774
   2.250   0.6795   0.00864   0.00247  -0.0760   0.3090   0.6626
   2.500   0.6998   0.00849   0.00258  -0.0743   0.3039   0.7640
   2.750   0.7190   0.00831   0.00269  -0.0723   0.2996   0.8703
   3.000   0.7985   0.00840   0.00292  -0.0836   0.2950   0.9726
   3.250   0.8394   0.00855   0.00303  -0.0864   0.2912   0.9881
   3.500   0.8707   0.00870   0.00315  -0.0872   0.2875   0.9981
   3.750   0.9004   0.00885   0.00326  -0.0877   0.2837   1.0000
   4.000   0.9240   0.00895   0.00335  -0.0868   0.2807   1.0000
   4.250   0.9473   0.00907   0.00345  -0.0858   0.2769   1.0000
   4.500   0.9703   0.00921   0.00356  -0.0848   0.2728   1.0000
   4.750   0.9930   0.00936   0.00369  -0.0838   0.2686   1.0000
   5.000   1.0166   0.00948   0.00380  -0.0829   0.2653   1.0000
   5.250   1.0395   0.00962   0.00392  -0.0819   0.2596   1.0000
   5.500   1.0615   0.00981   0.00407  -0.0808   0.2536   1.0000
   5.750   1.0844   0.00995   0.00421  -0.0798   0.2484   1.0000
   6.000   1.1061   0.01016   0.00436  -0.0787   0.2408   1.0000
   6.250   1.1279   0.01035   0.00453  -0.0775   0.2328   1.0000
   6.500   1.1484   0.01061   0.00473  -0.0762   0.2217   1.0000
   6.750   1.1668   0.01096   0.00498  -0.0745   0.2045   1.0000
   7.000   1.1844   0.01134   0.00528  -0.0727   0.1896   1.0000
   7.250   1.2025   0.01166   0.00555  -0.0709   0.1806   1.0000
   7.500   1.2196   0.01196   0.00582  -0.0690   0.1741   1.0000
   7.750   1.2368   0.01225   0.00609  -0.0670   0.1687   1.0000
   8.000   1.2536   0.01256   0.00638  -0.0651   0.1628   1.0000
   8.250   1.2706   0.01290   0.00669  -0.0632   0.1580   1.0000
   8.500   1.2889   0.01318   0.00698  -0.0616   0.1545   1.0000
   8.750   1.3080   0.01344   0.00726  -0.0602   0.1517   1.0000
   9.000   1.3269   0.01372   0.00755  -0.0588   0.1495   1.0000
   9.250   1.3444   0.01408   0.00790  -0.0572   0.1458   1.0000
   9.500   1.3620   0.01444   0.00827  -0.0557   0.1428   1.0000
   9.750   1.3803   0.01478   0.00863  -0.0543   0.1404   1.0000
  10.000   1.3992   0.01509   0.00896  -0.0530   0.1380   1.0000
  10.250   1.4171   0.01546   0.00935  -0.0517   0.1352   1.0000
  10.500   1.4335   0.01591   0.00979  -0.0502   0.1310   1.0000
  10.750   1.4495   0.01640   0.01029  -0.0486   0.1274   1.0000
  11.000   1.4672   0.01681   0.01073  -0.0474   0.1239   1.0000
  11.250   1.4817   0.01740   0.01129  -0.0458   0.1178   1.0000
  11.500   1.4950   0.01808   0.01195  -0.0442   0.1096   1.0000
  11.750   1.5045   0.01900   0.01280  -0.0421   0.0979   1.0000
  12.000   1.4934   0.02120   0.01478  -0.0381   0.0661   1.0000
  12.250   1.4678   0.02463   0.01801  -0.0334   0.0296   1.0000
  12.500   1.4644   0.02680   0.02016  -0.0312   0.0177   1.0000
  12.750   1.4709   0.02832   0.02172  -0.0300   0.0154   1.0000
  13.000   1.4773   0.02990   0.02335  -0.0290   0.0138   1.0000
  13.250   1.4850   0.03145   0.02495  -0.0281   0.0130   1.0000
  13.500   1.4917   0.03313   0.02669  -0.0273   0.0124   1.0000
  13.750   1.4958   0.03510   0.02872  -0.0266   0.0115   1.0000
  14.000   1.5001   0.03712   0.03080  -0.0260   0.0111   1.0000
  14.250   1.5049   0.03913   0.03288  -0.0255   0.0107   1.0000
  14.500   1.5085   0.04135   0.03516  -0.0251   0.0104   1.0000
  14.750   1.5107   0.04373   0.03761  -0.0248   0.0101   1.0000
  15.000   1.5108   0.04641   0.04037  -0.0246   0.0097   1.0000
  15.250   1.5099   0.04930   0.04334  -0.0246   0.0094   1.0000
  15.500   1.5073   0.05246   0.04657  -0.0247   0.0091   1.0000
  15.750   1.5034   0.05583   0.05002  -0.0249   0.0087   1.0000
  16.000   1.4993   0.05934   0.05363  -0.0252   0.0086   1.0000
  16.250   1.4946   0.06301   0.05739  -0.0257   0.0085   1.0000
  16.500   1.4894   0.06676   0.06123  -0.0263   0.0082   1.0000
  16.750   1.4825   0.07079   0.06534  -0.0270   0.0081   1.0000
  17.000   1.4731   0.07524   0.06990  -0.0279   0.0081   1.0000
  17.250   1.4641   0.07968   0.07443  -0.0289   0.0078   1.0000
  17.500   1.4532   0.08439   0.07924  -0.0299   0.0077   1.0000
  17.750   1.4421   0.08920   0.08414  -0.0311   0.0076   1.0000
  18.000   1.4294   0.09432   0.08936  -0.0324   0.0075   1.0000
  18.250   1.4180   0.09926   0.09439  -0.0337   0.0073   1.0000
  18.500   1.4057   0.10436   0.09959  -0.0352   0.0073   1.0000
  18.750   1.3928   0.10964   0.10495  -0.0368   0.0071   1.0000
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