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GOE 735 AIRFOIL (goe735-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 735 AIRFOIL (goe735-il)
Reynolds number: 500,000
Max Cl/Cd: 82.17 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe735-il-500000.txt
Download as CSV file: xf-goe735-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 735 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -0.9242   0.09342   0.08983  -0.0458   1.0000   0.0419
 -19.000  -0.9475   0.08623   0.08251  -0.0503   1.0000   0.0422
 -18.750  -0.9709   0.07913   0.07528  -0.0548   1.0000   0.0426
 -18.500  -0.9917   0.07269   0.06871  -0.0588   1.0000   0.0429
 -18.250  -1.0108   0.06650   0.06238  -0.0627   1.0000   0.0433
 -18.000  -1.0273   0.06080   0.05654  -0.0663   1.0000   0.0437
 -17.750  -1.0404   0.05565   0.05124  -0.0695   1.0000   0.0440
 -17.500  -1.0503   0.05115   0.04658  -0.0722   1.0000   0.0443
 -17.250  -1.0582   0.04735   0.04274  -0.0738   1.0000   0.0448
 -17.000  -1.0640   0.04387   0.03922  -0.0754   1.0000   0.0453
 -16.750  -1.0673   0.04081   0.03611  -0.0765   1.0000   0.0458
 -16.500  -1.0686   0.03816   0.03340  -0.0772   1.0000   0.0463
 -16.250  -1.0680   0.03587   0.03104  -0.0774   1.0000   0.0470
 -16.000  -1.0653   0.03389   0.02899  -0.0773   1.0000   0.0477
 -15.750  -1.0408   0.03185   0.02679  -0.0811   0.9312   0.0489
 -15.500  -1.0248   0.03016   0.02483  -0.0827   0.8750   0.0498
 -15.250  -1.0252   0.02886   0.02340  -0.0806   0.8502   0.0505
 -15.000  -1.0219   0.02778   0.02221  -0.0786   0.8344   0.0513
 -14.750  -1.0159   0.02688   0.02119  -0.0766   0.8222   0.0522
 -14.500  -1.0088   0.02600   0.02020  -0.0746   0.8115   0.0532
 -14.250  -0.9997   0.02526   0.01931  -0.0726   0.8024   0.0543
 -14.000  -0.9933   0.02435   0.01835  -0.0703   0.7936   0.0554
 -13.750  -0.9849   0.02365   0.01760  -0.0680   0.7858   0.0566
 -13.500  -0.9730   0.02306   0.01696  -0.0660   0.7782   0.0579
 -13.250  -0.9600   0.02252   0.01633  -0.0640   0.7708   0.0594
 -13.000  -0.9471   0.02199   0.01566  -0.0618   0.7641   0.0608
 -12.750  -0.9358   0.02136   0.01506  -0.0596   0.7573   0.0623
 -12.500  -0.9206   0.02096   0.01461  -0.0576   0.7503   0.0639
 -12.250  -0.9045   0.02061   0.01415  -0.0557   0.7437   0.0658
 -12.000  -0.8891   0.02012   0.01362  -0.0537   0.7370   0.0676
 -11.750  -0.8735   0.01974   0.01322  -0.0517   0.7304   0.0694
 -11.500  -0.8560   0.01950   0.01290  -0.0498   0.7240   0.0713
 -11.250  -0.8373   0.01922   0.01255  -0.0481   0.7171   0.0733
 -11.000  -0.8213   0.01875   0.01205  -0.0461   0.7101   0.0751
 -10.750  -0.8038   0.01855   0.01181  -0.0441   0.7034   0.0769
 -10.500  -0.7845   0.01834   0.01157  -0.0424   0.6966   0.0789
 -10.250  -0.7643   0.01816   0.01128  -0.0409   0.6892   0.0808
 -10.000  -0.7444   0.01776   0.01084  -0.0394   0.6822   0.0828
  -9.750  -0.7228   0.01751   0.01061  -0.0382   0.6744   0.0846
  -9.500  -0.7006   0.01736   0.01038  -0.0369   0.6665   0.0867
  -9.250  -0.6776   0.01718   0.01011  -0.0358   0.6588   0.0886
  -9.000  -0.6550   0.01680   0.00968  -0.0348   0.6502   0.0905
  -8.750  -0.6326   0.01651   0.00937  -0.0337   0.6420   0.0924
  -8.500  -0.6087   0.01631   0.00916  -0.0328   0.6326   0.0943
  -8.250  -0.5848   0.01616   0.00891  -0.0318   0.6238   0.0964
  -8.000  -0.5600   0.01602   0.00870  -0.0310   0.6148   0.0981
  -7.750  -0.5366   0.01559   0.00823  -0.0301   0.6056   0.1002
  -7.500  -0.5124   0.01534   0.00798  -0.0293   0.5965   0.1021
  -7.250  -0.4878   0.01519   0.00777  -0.0285   0.5869   0.1042
  -7.000  -0.4625   0.01506   0.00757  -0.0278   0.5783   0.1064
  -6.750  -0.4369   0.01498   0.00739  -0.0271   0.5695   0.1082
  -6.500  -0.4132   0.01459   0.00699  -0.0263   0.5615   0.1109
  -6.250  -0.3880   0.01442   0.00682  -0.0256   0.5533   0.1134
  -6.000  -0.3628   0.01431   0.00664  -0.0249   0.5452   0.1157
  -5.750  -0.3368   0.01417   0.00646  -0.0244   0.5380   0.1179
  -5.500  -0.3107   0.01407   0.00628  -0.0238   0.5307   0.1197
  -5.250  -0.2873   0.01374   0.00593  -0.0229   0.5241   0.1227
  -5.000  -0.2616   0.01355   0.00576  -0.0223   0.5180   0.1252
  -4.750  -0.2357   0.01343   0.00561  -0.0217   0.5113   0.1279
  -4.500  -0.2100   0.01339   0.00547  -0.0211   0.5048   0.1305
  -4.250  -0.1845   0.01316   0.00525  -0.0205   0.4995   0.1334
  -4.000  -0.1596   0.01296   0.00507  -0.0198   0.4939   0.1368
  -3.750  -0.1340   0.01288   0.00494  -0.0192   0.4884   0.1404
  -3.500  -0.1077   0.01283   0.00485  -0.0187   0.4834   0.1439
  -3.250  -0.0825   0.01262   0.00467  -0.0180   0.4784   0.1485
  -3.000  -0.0571   0.01250   0.00455  -0.0174   0.4731   0.1534
  -2.750  -0.0312   0.01247   0.00446  -0.0169   0.4678   0.1583
  -2.500  -0.0061   0.01232   0.00434  -0.0162   0.4636   0.1652
  -2.250   0.0199   0.01221   0.00426  -0.0157   0.4592   0.1729
  -2.000   0.0451   0.01208   0.00417  -0.0150   0.4547   0.1827
  -1.750   0.0703   0.01201   0.00409  -0.0144   0.4503   0.1949
  -1.500   0.0949   0.01191   0.00405  -0.0137   0.4460   0.2135
  -1.250   0.1195   0.01170   0.00400  -0.0130   0.4420   0.2442
  -1.000   0.1432   0.01149   0.00396  -0.0122   0.4379   0.2883
  -0.750   0.1661   0.01129   0.00393  -0.0112   0.4338   0.3381
  -0.500   0.1884   0.01116   0.00391  -0.0101   0.4297   0.3891
  -0.250   0.2089   0.01088   0.00390  -0.0087   0.4265   0.4564
   0.000   0.2243   0.01043   0.00390  -0.0062   0.4234   0.5681
   0.250   0.2390   0.01005   0.00390  -0.0034   0.4201   0.6674
   0.500   0.2563   0.00976   0.00399  -0.0009   0.4166   0.7722
   0.750   0.2862   0.00977   0.00415  -0.0009   0.4126   0.8369
   1.000   0.3249   0.00993   0.00437  -0.0028   0.4086   0.8762
   1.250   0.3671   0.01009   0.00456  -0.0055   0.4049   0.8979
   1.500   0.4015   0.01027   0.00473  -0.0065   0.4013   0.9139
   1.750   0.4464   0.01054   0.00494  -0.0098   0.3975   0.9223
   2.000   0.4756   0.01081   0.00513  -0.0098   0.3940   0.9324
   2.250   0.5201   0.01113   0.00541  -0.0130   0.3904   0.9363
   2.500   0.5591   0.01138   0.00565  -0.0151   0.3872   0.9417
   2.750   0.5954   0.01166   0.00591  -0.0165   0.3837   0.9495
   3.000   0.6494   0.01203   0.00622  -0.0215   0.3798   0.9534
   3.250   0.6916   0.01240   0.00650  -0.0243   0.3762   0.9597
   3.500   0.7267   0.01269   0.00675  -0.0257   0.3731   0.9650
   3.750   0.7690   0.01283   0.00689  -0.0287   0.3704   0.9671
   4.000   0.8118   0.01300   0.00706  -0.0317   0.3672   0.9705
   4.250   0.8483   0.01320   0.00724  -0.0336   0.3642   0.9756
   4.500   0.8833   0.01337   0.00736  -0.0352   0.3611   0.9794
   4.750   0.9202   0.01356   0.00747  -0.0373   0.3576   0.9812
   5.000   0.9558   0.01369   0.00761  -0.0391   0.3551   0.9834
   5.250   0.9904   0.01379   0.00773  -0.0407   0.3527   0.9862
   5.500   1.0246   0.01391   0.00786  -0.0423   0.3499   0.9898
   5.750   1.0613   0.01402   0.00796  -0.0444   0.3470   0.9928
   6.000   1.0992   0.01410   0.00801  -0.0468   0.3441   0.9953
   6.250   1.1335   0.01428   0.00814  -0.0485   0.3411   0.9978
   6.500   1.1666   0.01448   0.00832  -0.0500   0.3384   0.9997
   6.750   1.1885   0.01460   0.00849  -0.0493   0.3362   1.0000
   7.000   1.2070   0.01475   0.00868  -0.0479   0.3339   1.0000
   7.250   1.2250   0.01493   0.00887  -0.0465   0.3314   1.0000
   7.500   1.2424   0.01512   0.00906  -0.0449   0.3290   1.0000
   7.750   1.2590   0.01535   0.00928  -0.0433   0.3267   1.0000
   8.000   1.2749   0.01566   0.00954  -0.0415   0.3239   1.0000
   8.250   1.2910   0.01596   0.00985  -0.0398   0.3218   1.0000
   8.500   1.3051   0.01618   0.01013  -0.0377   0.3201   1.0000
   8.750   1.3182   0.01642   0.01042  -0.0355   0.3181   1.0000
   9.000   1.3298   0.01667   0.01070  -0.0330   0.3159   1.0000
   9.250   1.3395   0.01693   0.01099  -0.0302   0.3137   1.0000
   9.500   1.3442   0.01720   0.01127  -0.0265   0.3117   1.0000
   9.750   1.3449   0.01750   0.01157  -0.0222   0.3098   1.0000
  10.000   1.3510   0.01790   0.01194  -0.0190   0.3076   1.0000
  10.250   1.3596   0.01832   0.01237  -0.0163   0.3055   1.0000
  10.500   1.3630   0.01878   0.01290  -0.0131   0.3039   1.0000
  10.750   1.3688   0.01929   0.01348  -0.0104   0.3020   1.0000
  11.000   1.3765   0.01985   0.01408  -0.0082   0.2998   1.0000
  11.250   1.3854   0.02043   0.01469  -0.0062   0.2976   1.0000
  11.500   1.3948   0.02105   0.01533  -0.0044   0.2953   1.0000
  11.750   1.4058   0.02168   0.01595  -0.0028   0.2929   1.0000
  12.000   1.4226   0.02219   0.01641  -0.0018   0.2901   1.0000
  12.250   1.4294   0.02305   0.01736  -0.0001   0.2885   1.0000
  12.500   1.4371   0.02393   0.01832   0.0014   0.2865   1.0000
  12.750   1.4457   0.02483   0.01928   0.0027   0.2841   1.0000
  13.000   1.4550   0.02574   0.02023   0.0038   0.2818   1.0000
  13.250   1.4643   0.02667   0.02119   0.0049   0.2794   1.0000
  13.500   1.4756   0.02753   0.02203   0.0058   0.2769   1.0000
  13.750   1.4911   0.02817   0.02264   0.0066   0.2741   1.0000
  14.000   1.4927   0.02970   0.02430   0.0077   0.2719   1.0000
  14.250   1.4969   0.03113   0.02582   0.0086   0.2692   1.0000
  14.500   1.5029   0.03248   0.02722   0.0094   0.2665   1.0000
  14.750   1.5083   0.03391   0.02867   0.0100   0.2635   1.0000
  15.000   1.5185   0.03497   0.02970   0.0106   0.2602   1.0000
  15.250   1.5202   0.03685   0.03166   0.0112   0.2571   1.0000
  15.500   1.5190   0.03908   0.03399   0.0116   0.2537   1.0000
  15.750   1.5195   0.04124   0.03621   0.0118   0.2501   1.0000
  16.000   1.5236   0.04306   0.03800   0.0121   0.2462   1.0000
  16.250   1.5258   0.04511   0.04009   0.0123   0.2427   1.0000
  16.500   1.5203   0.04809   0.04320   0.0122   0.2390   1.0000
  16.750   1.5189   0.05069   0.04584   0.0122   0.2354   1.0000
  17.000   1.5207   0.05290   0.04804   0.0122   0.2316   1.0000
  17.250   1.5195   0.05548   0.05066   0.0121   0.2281   1.0000
  17.500   1.5125   0.05883   0.05413   0.0117   0.2245   1.0000
  17.750   1.5082   0.06188   0.05722   0.0114   0.2204   1.0000
  18.000   1.5089   0.06433   0.05967   0.0112   0.2172   1.0000
  18.250   1.5062   0.06720   0.06259   0.0109   0.2137   1.0000
  18.500   1.4955   0.07117   0.06667   0.0102   0.2100   1.0000
  18.750   1.4896   0.07455   0.07008   0.0096   0.2060   1.0000
  19.000   1.4915   0.07693   0.07243   0.0093   0.2026   1.0000
  19.250   1.4813   0.08091   0.07651   0.0085   0.1990   1.0000
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