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GOE 775 AIRFOIL (goe775-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 775 AIRFOIL (goe775-il)
Reynolds number: 100,000
Max Cl/Cd: 35.78 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe775-il-100000-n5.txt
Download as CSV file: xf-goe775-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 775 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.9509   0.10686   0.09916  -0.0386   1.0000   0.1002
 -17.750  -0.9552   0.10280   0.09506  -0.0403   1.0000   0.1021
 -17.500  -0.9508   0.10021   0.09248  -0.0413   1.0000   0.1041
 -17.250  -0.9693   0.09398   0.08610  -0.0440   1.0000   0.1065
 -17.000  -0.9958   0.08672   0.07859  -0.0472   1.0000   0.1089
 -16.750  -1.0048   0.08229   0.07404  -0.0488   1.0000   0.1110
 -16.500  -0.9998   0.07998   0.07176  -0.0493   1.0000   0.1133
 -16.250  -1.0044   0.07632   0.06802  -0.0504   1.0000   0.1157
 -16.000  -1.0147   0.07194   0.06346  -0.0517   1.0000   0.1184
 -15.750  -1.0200   0.06836   0.05976  -0.0526   1.0000   0.1209
 -15.500  -1.0152   0.06620   0.05764  -0.0528   1.0000   0.1233
 -15.250  -1.0163   0.06333   0.05470  -0.0533   1.0000   0.1261
 -15.000  -1.0205   0.06011   0.05134  -0.0538   1.0000   0.1291
 -14.750  -1.0198   0.05757   0.04873  -0.0539   1.0000   0.1319
 -14.500  -1.0162   0.05549   0.04666  -0.0538   1.0000   0.1347
 -14.250  -1.0154   0.05311   0.04421  -0.0537   1.0000   0.1379
 -14.000  -1.0161   0.05062   0.04157  -0.0535   1.0000   0.1414
 -13.750  -1.0113   0.04881   0.03980  -0.0531   1.0000   0.1445
 -13.500  -1.0079   0.04693   0.03790  -0.0525   1.0000   0.1478
 -13.250  -1.0053   0.04499   0.03586  -0.0519   1.0000   0.1517
 -13.000  -1.0013   0.04325   0.03407  -0.0511   1.0000   0.1554
 -12.750  -0.9965   0.04171   0.03255  -0.0501   1.0000   0.1590
 -12.500  -0.9924   0.04015   0.03094  -0.0490   1.0000   0.1633
 -12.250  -0.9878   0.03869   0.02939  -0.0477   1.0000   0.1677
 -12.000  -0.9826   0.03743   0.02817  -0.0462   1.0000   0.1716
 -11.750  -0.9781   0.03619   0.02689  -0.0444   1.0000   0.1763
 -11.500  -0.9734   0.03503   0.02566  -0.0425   1.0000   0.1814
 -11.250  -0.9693   0.03401   0.02471  -0.0403   1.0000   0.1857
 -11.000  -0.9661   0.03305   0.02372  -0.0377   1.0000   0.1909
 -10.750  -0.9632   0.03218   0.02278  -0.0349   1.0000   0.1962
 -10.500  -0.9622   0.03140   0.02208  -0.0316   1.0000   0.2008
 -10.250  -0.9620   0.03071   0.02136  -0.0280   1.0000   0.2062
 -10.000  -0.9623   0.03008   0.02069  -0.0241   1.0000   0.2116
  -9.750  -0.9656   0.02953   0.02021  -0.0196   1.0000   0.2162
  -9.500  -0.9702   0.02906   0.01974  -0.0147   1.0000   0.2214
  -9.250  -0.9754   0.02867   0.01926  -0.0095   1.0000   0.2268
  -9.000  -0.9816   0.02827   0.01895  -0.0041   1.0000   0.2313
  -8.750  -0.9830   0.02787   0.01856   0.0005   1.0000   0.2370
  -8.500  -0.9812   0.02749   0.01810   0.0046   1.0000   0.2435
  -8.250  -0.9622   0.02696   0.01767   0.0053   0.9965   0.2510
  -8.000  -0.9296   0.02646   0.01708   0.0036   0.9910   0.2615
  -7.750  -0.9003   0.02592   0.01663   0.0025   0.9840   0.2705
  -7.500  -0.8657   0.02545   0.01611   0.0005   0.9783   0.2811
  -7.250  -0.8375   0.02497   0.01570  -0.0002   0.9702   0.2908
  -7.000  -0.8026   0.02452   0.01525  -0.0021   0.9642   0.3015
  -6.750  -0.7739   0.02411   0.01484  -0.0027   0.9557   0.3119
  -6.500  -0.7396   0.02368   0.01446  -0.0044   0.9491   0.3227
  -6.250  -0.7084   0.02330   0.01404  -0.0054   0.9411   0.3343
  -6.000  -0.6757   0.02291   0.01373  -0.0066   0.9333   0.3451
  -5.750  -0.6386   0.02250   0.01331  -0.0086   0.9275   0.3577
  -5.500  -0.6141   0.02217   0.01303  -0.0080   0.9160   0.3691
  -5.250  -0.5780   0.02177   0.01267  -0.0097   0.9097   0.3822
  -4.750  -0.5209   0.02111   0.01207  -0.0098   0.8898   0.4074
  -4.500  -0.4983   0.02085   0.01181  -0.0088   0.8766   0.4187
  -4.250  -0.4653   0.02049   0.01148  -0.0096   0.8686   0.4310
  -4.000  -0.4431   0.02026   0.01128  -0.0083   0.8546   0.4414
  -3.750  -0.4131   0.01995   0.01097  -0.0085   0.8449   0.4537
  -3.500  -0.3886   0.01972   0.01079  -0.0076   0.8315   0.4644
  -3.250  -0.3625   0.01948   0.01053  -0.0071   0.8193   0.4766
  -3.000  -0.3338   0.01922   0.01032  -0.0069   0.8078   0.4877
  -2.750  -0.3091   0.01903   0.01010  -0.0061   0.7942   0.5001
  -2.500  -0.2791   0.01879   0.00990  -0.0061   0.7831   0.5117
  -2.250  -0.2535   0.01862   0.00972  -0.0054   0.7695   0.5240
  -2.000  -0.2261   0.01846   0.00957  -0.0050   0.7570   0.5364
  -1.750  -0.1975   0.01829   0.00939  -0.0047   0.7447   0.5486
  -1.500  -0.1724   0.01820   0.00927  -0.0040   0.7312   0.5621
  -1.250  -0.1430   0.01808   0.00916  -0.0038   0.7195   0.5743
  -1.000  -0.1186   0.01802   0.00909  -0.0029   0.7055   0.5877
  -0.750  -0.0912   0.01797   0.00904  -0.0025   0.6931   0.6007
  -0.500  -0.0650   0.01794   0.00901  -0.0018   0.6798   0.6136
  -0.250  -0.0399   0.01792   0.00897  -0.0010   0.6669   0.6276
   0.000  -0.0120   0.01790   0.00896  -0.0006   0.6543   0.6399
   0.250   0.0119   0.01790   0.00896   0.0003   0.6406   0.6537
   0.500   0.0402   0.01792   0.00896   0.0007   0.6284   0.6662
   0.750   0.0649   0.01793   0.00901   0.0015   0.6144   0.6793
   1.000   0.0914   0.01797   0.00904   0.0021   0.6016   0.6925
   1.250   0.1185   0.01802   0.00910   0.0026   0.5885   0.7051
   1.500   0.1432   0.01808   0.00916   0.0034   0.5752   0.7190
   1.750   0.1726   0.01819   0.00926   0.0036   0.5631   0.7308
   2.000   0.1974   0.01829   0.00939   0.0044   0.5495   0.7444
   2.250   0.2262   0.01845   0.00956   0.0046   0.5374   0.7566
   2.500   0.2534   0.01861   0.00972   0.0051   0.5249   0.7693
   2.750   0.2793   0.01878   0.00989   0.0057   0.5128   0.7829
   3.000   0.3090   0.01902   0.01010   0.0058   0.5010   0.7940
   3.250   0.3338   0.01921   0.01032   0.0066   0.4888   0.8077
   3.500   0.3627   0.01947   0.01051   0.0067   0.4778   0.8192
   3.750   0.3887   0.01971   0.01079   0.0073   0.4655   0.8315
   4.000   0.4133   0.01994   0.01095   0.0081   0.4550   0.8449
   4.250   0.4432   0.02024   0.01128   0.0080   0.4425   0.8547
   4.500   0.4655   0.02048   0.01146   0.0092   0.4323   0.8686
   4.750   0.4984   0.02083   0.01181   0.0084   0.4198   0.8767
   5.000   0.5213   0.02109   0.01205   0.0094   0.4086   0.8899
   5.250   0.5556   0.02147   0.01235   0.0083   0.3960   0.8972
   5.500   0.5785   0.02176   0.01266   0.0092   0.3834   0.9098
   5.750   0.6145   0.02216   0.01300   0.0076   0.3705   0.9162
   6.000   0.6381   0.02247   0.01330   0.0083   0.3589   0.9281
   6.250   0.6762   0.02288   0.01370   0.0061   0.3463   0.9334
   6.500   0.7085   0.02328   0.01400   0.0049   0.3356   0.9414
   6.750   0.7403   0.02366   0.01444   0.0038   0.3239   0.9492
   7.000   0.7744   0.02408   0.01481   0.0022   0.3132   0.9559
   7.250   0.8034   0.02449   0.01522   0.0015   0.3025   0.9643
   7.500   0.8381   0.02494   0.01566  -0.0004   0.2920   0.9705
   7.750   0.8667   0.02541   0.01609  -0.0011   0.2821   0.9784
   8.000   0.9011   0.02588   0.01659  -0.0031   0.2716   0.9842
   8.250   0.9304   0.02642   0.01705  -0.0042   0.2624   0.9913
   8.500   0.9632   0.02692   0.01762  -0.0060   0.2520   0.9967
   8.750   0.9810   0.02744   0.01806  -0.0050   0.2446   1.0000
   9.000   0.9830   0.02782   0.01850  -0.0010   0.2381   1.0000
   9.250   0.9819   0.02822   0.01890   0.0036   0.2323   1.0000
   9.500   0.9756   0.02861   0.01921   0.0090   0.2278   1.0000
   9.750   0.9706   0.02901   0.01967   0.0142   0.2224   1.0000
  10.000   0.9662   0.02947   0.02016   0.0191   0.2172   1.0000
  10.250   0.9629   0.03002   0.02064   0.0236   0.2125   1.0000
  10.500   0.9626   0.03064   0.02128   0.0275   0.2072   1.0000
  10.750   0.9631   0.03134   0.02201   0.0311   0.2017   1.0000
  11.000   0.9642   0.03211   0.02272   0.0343   0.1970   1.0000
  11.250   0.9673   0.03297   0.02362   0.0372   0.1919   1.0000
  11.500   0.9707   0.03393   0.02462   0.0397   0.1865   1.0000
  11.750   0.9748   0.03495   0.02559   0.0419   0.1821   1.0000
  12.000   0.9799   0.03609   0.02678   0.0438   0.1772   1.0000
  12.250   0.9846   0.03733   0.02807   0.0455   0.1724   1.0000
  12.500   0.9896   0.03859   0.02931   0.0470   0.1684   1.0000
  12.750   0.9947   0.04002   0.03079   0.0483   0.1641   1.0000
  13.000   0.9990   0.04158   0.03242   0.0494   0.1597   1.0000
  13.250   1.0036   0.04313   0.03396   0.0504   0.1561   1.0000
  13.500   1.0083   0.04480   0.03566   0.0512   0.1525   1.0000
  13.750   1.0109   0.04675   0.03771   0.0519   0.1485   1.0000
  14.000   1.0142   0.04866   0.03964   0.0524   0.1451   1.0000
  14.250   1.0199   0.05035   0.04127   0.0529   0.1421   1.0000
  14.500   1.0192   0.05286   0.04395   0.0530   0.1386   1.0000
  14.750   1.0197   0.05527   0.04644   0.0531   0.1353   1.0000
  15.000   1.0228   0.05742   0.04859   0.0532   0.1325   1.0000
  15.250   1.0252   0.05974   0.05094   0.0531   0.1297   1.0000
  15.500   1.0206   0.06302   0.05437   0.0526   0.1267   1.0000
  15.750   1.0190   0.06597   0.05740   0.0521   0.1238   1.0000
  16.000   1.0228   0.06826   0.05967   0.0518   0.1213   1.0000
  16.250   1.0206   0.07141   0.06290   0.0512   0.1189   1.0000
  16.500   1.0097   0.07588   0.06756   0.0498   0.1163   1.0000
  16.750   1.0039   0.07970   0.07147   0.0486   0.1137   1.0000
  17.000   1.0074   0.08224   0.07400   0.0479   0.1115   1.0000
  17.250   1.0038   0.08586   0.07769   0.0468   0.1093   1.0000
  17.500   0.9767   0.09320   0.08529   0.0436   0.1069   1.0000
  17.750   0.9561   0.09975   0.09201   0.0407   0.1045   1.0000
  18.000   0.9571   0.10291   0.09518   0.0395   0.1025   1.0000
  18.250   0.9676   0.10451   0.09673   0.0391   0.1007   1.0000
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