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GOE 550 AIRFOIL (goe550-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 550 AIRFOIL (goe550-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.47 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe550-il-1000000.txt
Download as CSV file: xf-goe550-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 550 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8537   0.08357   0.08081  -0.0640   1.0000   0.0222
 -16.000  -0.8686   0.07824   0.07543  -0.0668   1.0000   0.0225
 -15.750  -0.8836   0.07310   0.07024  -0.0695   1.0000   0.0227
 -15.500  -0.9008   0.06786   0.06494  -0.0722   1.0000   0.0231
 -15.250  -0.9277   0.06190   0.05892  -0.0753   1.0000   0.0231
 -15.000  -0.9669   0.05496   0.05191  -0.0789   1.0000   0.0230
 -14.750  -1.0772   0.04324   0.04005  -0.0823   1.0000   0.0217
 -14.500  -1.1488   0.02891   0.02529  -0.0923   1.0000   0.0209
 -14.250  -1.1520   0.02613   0.02239  -0.0916   1.0000   0.0215
 -14.000  -1.1325   0.02446   0.02064  -0.0929   0.9991   0.0223
 -13.750  -1.1030   0.02328   0.01938  -0.0951   0.9975   0.0233
 -13.500  -1.0722   0.02237   0.01837  -0.0971   0.9958   0.0241
 -13.250  -1.0420   0.02117   0.01708  -0.0993   0.9943   0.0251
 -13.000  -1.0130   0.02005   0.01590  -0.1011   0.9927   0.0262
 -12.750  -0.9842   0.01931   0.01510  -0.1022   0.9903   0.0272
 -12.500  -0.9533   0.01868   0.01441  -0.1035   0.9882   0.0282
 -12.250  -0.9209   0.01817   0.01382  -0.1049   0.9865   0.0290
 -12.000  -0.8899   0.01713   0.01273  -0.1067   0.9848   0.0306
 -11.750  -0.8561   0.01657   0.01214  -0.1085   0.9837   0.0318
 -11.500  -0.8215   0.01608   0.01160  -0.1103   0.9828   0.0330
 -11.250  -0.7951   0.01566   0.01111  -0.1102   0.9788   0.0337
 -11.000  -0.7654   0.01488   0.01028  -0.1113   0.9758   0.0352
 -10.750  -0.7324   0.01433   0.00971  -0.1127   0.9738   0.0367
 -10.500  -0.6980   0.01391   0.00925  -0.1143   0.9723   0.0381
 -10.250  -0.6625   0.01351   0.00880  -0.1160   0.9711   0.0392
 -10.000  -0.6315   0.01293   0.00816  -0.1169   0.9680   0.0407
  -9.750  -0.6033   0.01240   0.00761  -0.1172   0.9626   0.0425
  -9.500  -0.5683   0.01200   0.00718  -0.1188   0.9596   0.0443
  -9.250  -0.5322   0.01167   0.00680  -0.1206   0.9571   0.0457
  -9.000  -0.5050   0.01120   0.00628  -0.1206   0.9495   0.0479
  -8.750  -0.4713   0.01076   0.00582  -0.1219   0.9440   0.0504
  -8.500  -0.4393   0.01045   0.00547  -0.1228   0.9364   0.0525
  -8.250  -0.4060   0.01009   0.00505  -0.1239   0.9277   0.0552
  -8.000  -0.3760   0.00973   0.00466  -0.1244   0.9160   0.0587
  -7.750  -0.3458   0.00950   0.00436  -0.1248   0.9037   0.0616
  -7.500  -0.3175   0.00919   0.00402  -0.1249   0.8903   0.0672
  -7.250  -0.2899   0.00900   0.00377  -0.1247   0.8767   0.0724
  -7.000  -0.2633   0.00879   0.00354  -0.1244   0.8636   0.0801
  -6.750  -0.2367   0.00861   0.00334  -0.1241   0.8519   0.0877
  -6.500  -0.2095   0.00854   0.00320  -0.1238   0.8411   0.0931
  -6.250  -0.1831   0.00836   0.00301  -0.1234   0.8304   0.1005
  -6.000  -0.1560   0.00828   0.00287  -0.1230   0.8208   0.1050
  -5.500  -0.1023   0.00803   0.00256  -0.1224   0.8035   0.1156
  -5.000  -0.0482   0.00781   0.00229  -0.1217   0.7868   0.1270
  -4.750  -0.0212   0.00774   0.00217  -0.1214   0.7790   0.1325
  -4.500   0.0060   0.00760   0.00206  -0.1211   0.7715   0.1426
  -4.250   0.0329   0.00751   0.00197  -0.1208   0.7634   0.1540
  -4.000   0.0602   0.00743   0.00191  -0.1205   0.7551   0.1657
  -3.750   0.0873   0.00741   0.00185  -0.1201   0.7455   0.1754
  -3.500   0.1144   0.00736   0.00181  -0.1198   0.7352   0.1842
  -3.250   0.1416   0.00738   0.00177  -0.1194   0.7253   0.1904
  -3.000   0.1689   0.00734   0.00174  -0.1192   0.7159   0.1976
  -2.750   0.1964   0.00736   0.00173  -0.1189   0.7076   0.2040
  -2.500   0.2241   0.00737   0.00170  -0.1186   0.6989   0.2086
  -2.250   0.2513   0.00734   0.00166  -0.1183   0.6906   0.2134
  -2.000   0.2787   0.00734   0.00164  -0.1180   0.6813   0.2173
  -1.750   0.3061   0.00736   0.00162  -0.1177   0.6723   0.2205
  -1.500   0.3334   0.00740   0.00160  -0.1174   0.6629   0.2227
  -1.250   0.3606   0.00736   0.00156  -0.1171   0.6539   0.2271
  -1.000   0.3873   0.00738   0.00155  -0.1167   0.6437   0.2311
  -0.750   0.4148   0.00739   0.00155  -0.1164   0.6334   0.2348
  -0.500   0.4418   0.00744   0.00155  -0.1160   0.6234   0.2376
  -0.250   0.4688   0.00748   0.00155  -0.1157   0.6130   0.2398
   0.000   0.4958   0.00747   0.00154  -0.1153   0.6033   0.2445
   0.250   0.5223   0.00751   0.00156  -0.1149   0.5930   0.2487
   0.500   0.5494   0.00756   0.00159  -0.1146   0.5823   0.2526
   0.750   0.5762   0.00762   0.00162  -0.1142   0.5724   0.2557
   1.000   0.6026   0.00766   0.00164  -0.1137   0.5625   0.2611
   1.250   0.6296   0.00769   0.00168  -0.1134   0.5534   0.2669
   1.500   0.6559   0.00778   0.00173  -0.1129   0.5426   0.2715
   1.750   0.6823   0.00783   0.00177  -0.1125   0.5316   0.2764
   2.000   0.7088   0.00788   0.00182  -0.1121   0.5219   0.2822
   2.500   0.7616   0.00801   0.00194  -0.1112   0.5029   0.2941
   2.750   0.7875   0.00808   0.00201  -0.1107   0.4929   0.3020
   3.000   0.8135   0.00816   0.00208  -0.1102   0.4815   0.3110
   3.250   0.8394   0.00822   0.00216  -0.1097   0.4701   0.3230
   3.500   0.8647   0.00829   0.00225  -0.1092   0.4577   0.3415
   3.750   0.8894   0.00832   0.00238  -0.1085   0.4452   0.3880
   4.000   0.9139   0.00830   0.00253  -0.1078   0.4323   0.4763
   4.250   0.9381   0.00829   0.00266  -0.1071   0.4195   0.5424
   4.500   0.9531   0.00775   0.00289  -0.1044   0.4081   0.8449
   4.750   0.9994   0.00784   0.00310  -0.1084   0.3913   1.0000
   5.000   1.0231   0.00805   0.00325  -0.1075   0.3781   1.0000
   5.500   1.0710   0.00845   0.00356  -0.1058   0.3562   1.0000
   5.750   1.0945   0.00867   0.00373  -0.1048   0.3453   1.0000
   6.000   1.1171   0.00894   0.00393  -0.1038   0.3319   1.0000
   6.250   1.1401   0.00917   0.00412  -0.1028   0.3199   1.0000
   6.500   1.1635   0.00938   0.00430  -0.1019   0.3097   1.0000
   6.750   1.1860   0.00964   0.00451  -0.1008   0.2995   1.0000
   7.000   1.2084   0.00989   0.00471  -0.0998   0.2877   1.0000
   7.250   1.2307   0.01013   0.00492  -0.0987   0.2751   1.0000
   7.500   1.2522   0.01041   0.00515  -0.0974   0.2618   1.0000
   7.750   1.2728   0.01072   0.00541  -0.0961   0.2471   1.0000
   8.000   1.2911   0.01114   0.00571  -0.0943   0.2263   1.0000
   8.250   1.3040   0.01172   0.00612  -0.0916   0.1952   1.0000
   8.500   1.3080   0.01264   0.00676  -0.0874   0.1499   1.0000
   8.750   1.3176   0.01332   0.00731  -0.0842   0.1276   1.0000
   9.000   1.3322   0.01381   0.00775  -0.0819   0.1173   1.0000
   9.250   1.3469   0.01429   0.00820  -0.0796   0.1087   1.0000
   9.500   1.3620   0.01476   0.00865  -0.0775   0.1009   1.0000
   9.750   1.3775   0.01521   0.00910  -0.0755   0.0936   1.0000
  10.000   1.3908   0.01578   0.00962  -0.0732   0.0833   1.0000
  10.250   1.4019   0.01647   0.01022  -0.0707   0.0697   1.0000
  10.500   1.4112   0.01725   0.01093  -0.0680   0.0580   1.0000
  10.750   1.4211   0.01804   0.01168  -0.0655   0.0499   1.0000
  11.000   1.4313   0.01884   0.01247  -0.0631   0.0442   1.0000
  11.250   1.4405   0.01972   0.01334  -0.0607   0.0391   1.0000
  11.500   1.4511   0.02055   0.01418  -0.0587   0.0355   1.0000
  11.750   1.4607   0.02149   0.01513  -0.0566   0.0323   1.0000
  12.000   1.4698   0.02249   0.01614  -0.0546   0.0296   1.0000
  12.250   1.4784   0.02358   0.01726  -0.0526   0.0273   1.0000
  12.500   1.4873   0.02469   0.01839  -0.0509   0.0254   1.0000
  12.750   1.4927   0.02610   0.01983  -0.0489   0.0236   1.0000
  13.000   1.5027   0.02725   0.02103  -0.0475   0.0225   1.0000
  13.250   1.5101   0.02862   0.02244  -0.0460   0.0213   1.0000
  13.500   1.5146   0.03028   0.02413  -0.0445   0.0201   1.0000
  13.750   1.5203   0.03191   0.02582  -0.0431   0.0193   1.0000
  14.000   1.5272   0.03349   0.02747  -0.0420   0.0187   1.0000
  14.250   1.5327   0.03523   0.02927  -0.0409   0.0180   1.0000
  14.500   1.5362   0.03722   0.03130  -0.0399   0.0174   1.0000
  14.750   1.5370   0.03955   0.03369  -0.0389   0.0168   1.0000
  15.000   1.5357   0.04216   0.03638  -0.0380   0.0162   1.0000
  15.250   1.5393   0.04436   0.03865  -0.0374   0.0159   1.0000
  15.500   1.5418   0.04674   0.04112  -0.0369   0.0155   1.0000
  15.750   1.5436   0.04927   0.04371  -0.0366   0.0152   1.0000
  16.000   1.5435   0.05207   0.04659  -0.0363   0.0149   1.0000
  16.250   1.5425   0.05505   0.04964  -0.0362   0.0146   1.0000
  16.500   1.5408   0.05821   0.05288  -0.0362   0.0143   1.0000
  16.750   1.5354   0.06192   0.05666  -0.0365   0.0140   1.0000
  17.000   1.5262   0.06619   0.06102  -0.0369   0.0136   1.0000
  17.250   1.5151   0.07087   0.06581  -0.0377   0.0134   1.0000
  17.500   1.5141   0.07428   0.06930  -0.0382   0.0132   1.0000
  17.750   1.5111   0.07801   0.07312  -0.0390   0.0131   1.0000
  18.000   1.5081   0.08180   0.07700  -0.0398   0.0128   1.0000
  18.250   1.5034   0.08592   0.08121  -0.0409   0.0126   1.0000
  18.500   1.4980   0.09022   0.08560  -0.0421   0.0125   1.0000
  18.750   1.4911   0.09483   0.09030  -0.0435   0.0124   1.0000
  19.000   1.4862   0.09916   0.09472  -0.0449   0.0121   1.0000
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