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GOE 619 AIRFOIL (goe619-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 619 AIRFOIL (goe619-il)
Reynolds number: 1,000,000
Max Cl/Cd: 99.6 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe619-il-1000000-n5.txt
Download as CSV file: xf-goe619-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 619 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.6664   0.12698   0.12477  -0.0452   1.0000   0.0198
 -17.500  -0.6934   0.11808   0.11578  -0.0499   1.0000   0.0203
 -17.250  -0.7160   0.11030   0.10792  -0.0540   1.0000   0.0205
 -17.000  -0.7354   0.10334   0.10088  -0.0576   1.0000   0.0208
 -16.750  -0.7565   0.09630   0.09376  -0.0614   1.0000   0.0209
 -16.500  -0.7768   0.08959   0.08697  -0.0650   1.0000   0.0211
 -16.250  -0.7958   0.08329   0.08059  -0.0683   1.0000   0.0212
 -16.000  -0.8152   0.07718   0.07441  -0.0716   1.0000   0.0213
 -15.750  -0.8375   0.07097   0.06812  -0.0750   1.0000   0.0214
 -15.500  -0.8650   0.06455   0.06162  -0.0784   1.0000   0.0214
 -15.250  -0.8981   0.05779   0.05477  -0.0820   1.0000   0.0214
 -15.000  -0.9428   0.05012   0.04701  -0.0857   1.0000   0.0214
 -14.750  -1.0061   0.03912   0.03585  -0.0935   0.9991   0.0212
 -14.500  -1.0066   0.02917   0.02557  -0.1098   0.9934   0.0214
 -14.250  -0.9912   0.02708   0.02336  -0.1116   0.9886   0.0216
 -14.000  -0.9677   0.02566   0.02183  -0.1135   0.9852   0.0218
 -13.750  -0.9423   0.02438   0.02045  -0.1153   0.9828   0.0219
 -13.500  -0.9238   0.02343   0.01942  -0.1150   0.9769   0.0221
 -13.250  -0.9002   0.02231   0.01821  -0.1160   0.9729   0.0223
 -13.000  -0.8802   0.02102   0.01683  -0.1163   0.9672   0.0227
 -12.750  -0.8555   0.02007   0.01581  -0.1170   0.9617   0.0230
 -12.250  -0.7943   0.01855   0.01418  -0.1199   0.9524   0.0236
 -12.000  -0.7603   0.01783   0.01339  -0.1219   0.9468   0.0239
 -11.750  -0.7258   0.01720   0.01269  -0.1239   0.9407   0.0243
 -11.500  -0.6927   0.01659   0.01200  -0.1256   0.9316   0.0246
 -11.250  -0.6617   0.01601   0.01133  -0.1268   0.9206   0.0249
 -11.000  -0.6336   0.01549   0.01071  -0.1272   0.9084   0.0251
 -10.750  -0.6083   0.01504   0.01015  -0.1270   0.8960   0.0254
 -10.500  -0.5843   0.01465   0.00967  -0.1265   0.8846   0.0256
 -10.250  -0.5603   0.01429   0.00922  -0.1259   0.8739   0.0259
 -10.000  -0.5365   0.01397   0.00880  -0.1252   0.8627   0.0261
  -9.750  -0.5128   0.01363   0.00837  -0.1245   0.8524   0.0262
  -9.500  -0.4889   0.01332   0.00797  -0.1237   0.8427   0.0264
  -9.250  -0.4645   0.01303   0.00760  -0.1231   0.8334   0.0265
  -9.000  -0.4413   0.01261   0.00710  -0.1223   0.8246   0.0268
  -8.750  -0.4177   0.01222   0.00663  -0.1215   0.8151   0.0272
  -8.500  -0.3935   0.01188   0.00622  -0.1208   0.8063   0.0276
  -8.250  -0.3688   0.01160   0.00587  -0.1201   0.7972   0.0279
  -8.000  -0.3437   0.01133   0.00554  -0.1196   0.7893   0.0283
  -7.750  -0.3183   0.01109   0.00524  -0.1190   0.7810   0.0286
  -7.500  -0.2928   0.01087   0.00496  -0.1184   0.7731   0.0291
  -7.250  -0.2670   0.01066   0.00470  -0.1179   0.7643   0.0295
  -7.000  -0.2411   0.01047   0.00445  -0.1174   0.7566   0.0300
  -6.750  -0.2150   0.01028   0.00421  -0.1169   0.7486   0.0304
  -6.500  -0.1889   0.01012   0.00399  -0.1164   0.7412   0.0307
  -6.250  -0.1624   0.00996   0.00378  -0.1160   0.7330   0.0311
  -6.000  -0.1362   0.00982   0.00358  -0.1155   0.7256   0.0314
  -5.750  -0.1095   0.00964   0.00337  -0.1151   0.7182   0.0321
  -5.250  -0.0566   0.00933   0.00299  -0.1143   0.7034   0.0343
  -5.000  -0.0301   0.00921   0.00283  -0.1138   0.6956   0.0356
  -4.750  -0.0033   0.00909   0.00267  -0.1134   0.6885   0.0371
  -4.500   0.0231   0.00893   0.00251  -0.1130   0.6805   0.0422
  -4.250   0.0486   0.00868   0.00234  -0.1125   0.6732   0.0635
  -4.000   0.0753   0.00857   0.00225  -0.1121   0.6646   0.0733
  -3.750   0.1019   0.00853   0.00217  -0.1116   0.6539   0.0782
  -3.500   0.1277   0.00848   0.00209  -0.1110   0.6401   0.0832
  -3.000   0.1805   0.00846   0.00196  -0.1100   0.6138   0.0891
  -2.750   0.2071   0.00842   0.00189  -0.1096   0.6034   0.0933
  -2.500   0.2338   0.00838   0.00184  -0.1092   0.5950   0.0972
  -2.250   0.2610   0.00835   0.00179  -0.1089   0.5887   0.1006
  -2.000   0.2883   0.00833   0.00174  -0.1086   0.5815   0.1030
  -1.750   0.3150   0.00829   0.00170  -0.1081   0.5744   0.1084
  -1.500   0.3420   0.00824   0.00166  -0.1078   0.5663   0.1153
  -1.250   0.3682   0.00821   0.00162  -0.1073   0.5562   0.1264
  -1.000   0.3942   0.00815   0.00160  -0.1068   0.5447   0.1461
  -0.750   0.4201   0.00808   0.00159  -0.1063   0.5337   0.1743
  -0.500   0.4461   0.00808   0.00160  -0.1058   0.5220   0.1919
  -0.250   0.4718   0.00811   0.00162  -0.1052   0.5082   0.2076
   0.000   0.4973   0.00816   0.00165  -0.1046   0.4924   0.2209
   0.250   0.5226   0.00825   0.00169  -0.1040   0.4746   0.2306
   0.500   0.5475   0.00835   0.00174  -0.1032   0.4556   0.2416
   0.750   0.5720   0.00848   0.00181  -0.1025   0.4352   0.2520
   1.000   0.5960   0.00864   0.00190  -0.1016   0.4133   0.2617
   1.250   0.6199   0.00881   0.00200  -0.1007   0.3916   0.2706
   1.500   0.6438   0.00900   0.00210  -0.0999   0.3697   0.2786
   1.750   0.6664   0.00922   0.00223  -0.0988   0.3447   0.2895
   2.000   0.6899   0.00940   0.00235  -0.0979   0.3247   0.3013
   2.250   0.7137   0.00956   0.00247  -0.0970   0.3088   0.3150
   2.500   0.7377   0.00969   0.00258  -0.0961   0.2968   0.3280
   2.750   0.7621   0.00980   0.00269  -0.0954   0.2863   0.3437
   3.250   0.8085   0.01007   0.00297  -0.0935   0.2628   0.3923
   3.500   0.8322   0.01019   0.00311  -0.0926   0.2534   0.4125
   3.750   0.8552   0.01034   0.00326  -0.0916   0.2437   0.4338
   4.000   0.8785   0.01045   0.00340  -0.0907   0.2364   0.4593
   4.250   0.9011   0.01058   0.00355  -0.0896   0.2291   0.4845
   4.500   0.9242   0.01065   0.00369  -0.0887   0.2245   0.5166
   4.750   0.9409   0.01036   0.00390  -0.0865   0.2199   0.7207
   5.250   1.0249   0.01036   0.00442  -0.0928   0.2097   1.0000
   5.500   1.0466   0.01055   0.00458  -0.0915   0.2050   1.0000
   5.750   1.0675   0.01077   0.00476  -0.0901   0.1998   1.0000
   6.000   1.0888   0.01094   0.00492  -0.0888   0.1965   1.0000
   6.250   1.1086   0.01113   0.00510  -0.0872   0.1919   1.0000
   6.500   1.1261   0.01139   0.00531  -0.0852   0.1845   1.0000
   6.750   1.1447   0.01163   0.00551  -0.0834   0.1762   1.0000
   7.000   1.1615   0.01196   0.00577  -0.0813   0.1657   1.0000
   7.250   1.1768   0.01236   0.00608  -0.0791   0.1505   1.0000
   7.500   1.1863   0.01302   0.00656  -0.0759   0.1242   1.0000
   7.750   1.1795   0.01447   0.00767  -0.0703   0.0672   1.0000
   8.000   1.1934   0.01502   0.00817  -0.0681   0.0579   1.0000
   8.250   1.2097   0.01547   0.00861  -0.0663   0.0542   1.0000
   8.500   1.2269   0.01589   0.00902  -0.0647   0.0514   1.0000
   8.750   1.2450   0.01627   0.00941  -0.0632   0.0504   1.0000
   9.000   1.2622   0.01670   0.00985  -0.0617   0.0489   1.0000
   9.250   1.2790   0.01718   0.01034  -0.0602   0.0473   1.0000
   9.500   1.2947   0.01772   0.01087  -0.0586   0.0453   1.0000
   9.750   1.3106   0.01827   0.01143  -0.0571   0.0432   1.0000
  10.000   1.3275   0.01878   0.01196  -0.0558   0.0422   1.0000
  10.250   1.3432   0.01938   0.01255  -0.0544   0.0397   1.0000
  10.500   1.3570   0.02010   0.01326  -0.0528   0.0363   1.0000
  11.000   1.3708   0.02256   0.01563  -0.0485   0.0130   1.0000
  11.250   1.3839   0.02344   0.01654  -0.0471   0.0120   1.0000
  11.500   1.3968   0.02436   0.01750  -0.0458   0.0112   1.0000
  11.750   1.4092   0.02533   0.01851  -0.0446   0.0108   1.0000
  12.000   1.4199   0.02646   0.01969  -0.0433   0.0101   1.0000
  12.250   1.4318   0.02754   0.02081  -0.0422   0.0098   1.0000
  12.500   1.4431   0.02867   0.02199  -0.0411   0.0095   1.0000
  12.750   1.4536   0.02990   0.02327  -0.0400   0.0091   1.0000
  13.000   1.4635   0.03121   0.02463  -0.0390   0.0088   1.0000
  13.250   1.4722   0.03266   0.02613  -0.0380   0.0085   1.0000
  13.500   1.4797   0.03424   0.02776  -0.0370   0.0082   1.0000
  13.750   1.4850   0.03606   0.02964  -0.0360   0.0079   1.0000
  14.000   1.4921   0.03776   0.03140  -0.0352   0.0078   1.0000
  14.250   1.4988   0.03955   0.03325  -0.0346   0.0076   1.0000
  14.500   1.5041   0.04151   0.03527  -0.0339   0.0075   1.0000
  14.750   1.5090   0.04355   0.03737  -0.0333   0.0073   1.0000
  15.000   1.5126   0.04577   0.03966  -0.0328   0.0071   1.0000
  15.250   1.5153   0.04815   0.04210  -0.0324   0.0070   1.0000
  15.500   1.5172   0.05065   0.04468  -0.0320   0.0069   1.0000
  15.750   1.5181   0.05331   0.04740  -0.0318   0.0067   1.0000
  16.000   1.5172   0.05623   0.05040  -0.0317   0.0066   1.0000
  16.250   1.5153   0.05935   0.05359  -0.0316   0.0065   1.0000
  16.500   1.5120   0.06270   0.05703  -0.0317   0.0063   1.0000
  16.750   1.5065   0.06636   0.06077  -0.0320   0.0062   1.0000
  17.000   1.4982   0.07050   0.06501  -0.0324   0.0061   1.0000
  17.250   1.4926   0.07435   0.06895  -0.0329   0.0060   1.0000
  17.500   1.4849   0.07855   0.07325  -0.0336   0.0060   1.0000
  17.750   1.4750   0.08310   0.07790  -0.0344   0.0060   1.0000
  18.000   1.4664   0.08757   0.08247  -0.0354   0.0059   1.0000
  18.250   1.4551   0.09253   0.08753  -0.0366   0.0059   1.0000
  18.500   1.4448   0.09737   0.09247  -0.0378   0.0058   1.0000
  18.750   1.4311   0.10279   0.09800  -0.0394   0.0058   1.0000
  19.000   1.4195   0.10800   0.10332  -0.0410   0.0057   1.0000
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