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GOE 422 AIRFOIL (goe422-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 422 AIRFOIL (goe422-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.84 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe422-il-1000000-n5.txt
Download as CSV file: xf-goe422-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 422 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.6758   0.03260   0.02903  -0.1478   0.8737   0.0231
 -14.000  -0.6819   0.02913   0.02523  -0.1509   0.8410   0.0231
 -13.750  -0.6796   0.02737   0.02325  -0.1506   0.8251   0.0231
 -13.500  -0.6682   0.02594   0.02165  -0.1506   0.8152   0.0232
 -13.250  -0.6536   0.02473   0.02029  -0.1504   0.8077   0.0233
 -13.000  -0.6366   0.02366   0.01909  -0.1502   0.8012   0.0234
 -12.750  -0.6181   0.02272   0.01801  -0.1499   0.7950   0.0234
 -12.500  -0.5983   0.02187   0.01704  -0.1496   0.7896   0.0235
 -12.250  -0.5770   0.02107   0.01615  -0.1494   0.7852   0.0235
 -12.000  -0.5551   0.02035   0.01533  -0.1491   0.7803   0.0236
 -11.750  -0.5325   0.01969   0.01457  -0.1488   0.7753   0.0237
 -11.500  -0.5095   0.01910   0.01387  -0.1485   0.7699   0.0237
 -11.250  -0.4879   0.01820   0.01288  -0.1482   0.7659   0.0239
 -11.000  -0.4648   0.01750   0.01210  -0.1479   0.7611   0.0240
 -10.750  -0.4407   0.01692   0.01145  -0.1476   0.7564   0.0242
 -10.500  -0.4162   0.01641   0.01087  -0.1474   0.7519   0.0243
 -10.250  -0.3909   0.01595   0.01036  -0.1472   0.7481   0.0244
 -10.000  -0.3650   0.01552   0.00987  -0.1470   0.7445   0.0246
  -9.750  -0.3389   0.01512   0.00943  -0.1469   0.7404   0.0247
  -9.500  -0.3127   0.01475   0.00900  -0.1467   0.7362   0.0249
  -9.250  -0.2866   0.01441   0.00859  -0.1465   0.7319   0.0250
  -9.000  -0.2600   0.01407   0.00820  -0.1463   0.7281   0.0252
  -8.750  -0.2330   0.01374   0.00784  -0.1463   0.7244   0.0254
  -8.500  -0.2060   0.01343   0.00749  -0.1462   0.7204   0.0256
  -8.250  -0.1790   0.01315   0.00715  -0.1460   0.7159   0.0258
  -8.000  -0.1522   0.01289   0.00684  -0.1458   0.7112   0.0261
  -7.750  -0.1248   0.01261   0.00652  -0.1458   0.7074   0.0263
  -7.500  -0.0973   0.01234   0.00621  -0.1457   0.7034   0.0265
  -7.250  -0.0700   0.01209   0.00591  -0.1456   0.6987   0.0267
  -7.000  -0.0428   0.01187   0.00563  -0.1454   0.6936   0.0268
  -6.750  -0.0153   0.01166   0.00538  -0.1453   0.6892   0.0270
  -6.500   0.0125   0.01145   0.00514  -0.1453   0.6847   0.0271
  -6.250   0.0399   0.01122   0.00486  -0.1452   0.6796   0.0274
  -6.000   0.0667   0.01098   0.00458  -0.1449   0.6739   0.0277
  -5.750   0.0943   0.01078   0.00435  -0.1448   0.6677   0.0280
  -5.500   0.1216   0.01062   0.00415  -0.1447   0.6597   0.0283
  -5.250   0.1487   0.01049   0.00398  -0.1444   0.6516   0.0287
  -5.000   0.1759   0.01036   0.00381  -0.1443   0.6415   0.0290
  -4.750   0.2028   0.01027   0.00366  -0.1440   0.6315   0.0294
  -4.500   0.2297   0.01019   0.00352  -0.1437   0.6206   0.0298
  -4.250   0.2571   0.01010   0.00339  -0.1436   0.6130   0.0303
  -4.000   0.2847   0.01001   0.00327  -0.1434   0.6053   0.0307
  -3.750   0.3116   0.00995   0.00317  -0.1432   0.5973   0.0311
  -3.500   0.3389   0.00985   0.00304  -0.1430   0.5885   0.0318
  -3.250   0.3655   0.00981   0.00296  -0.1427   0.5792   0.0326
  -3.000   0.3928   0.00976   0.00288  -0.1426   0.5705   0.0335
  -2.500   0.4469   0.00970   0.00276  -0.1421   0.5549   0.0356
  -2.250   0.4736   0.00968   0.00272  -0.1419   0.5467   0.0373
  -2.000   0.5006   0.00967   0.00268  -0.1416   0.5394   0.0392
  -1.750   0.5274   0.00965   0.00265  -0.1414   0.5309   0.0425
  -1.500   0.5536   0.00966   0.00264  -0.1411   0.5226   0.0475
  -1.250   0.5803   0.00965   0.00263  -0.1408   0.5137   0.0550
  -1.000   0.6059   0.00968   0.00265  -0.1404   0.5034   0.0650
  -0.750   0.6320   0.00971   0.00269  -0.1400   0.4931   0.0755
  -0.500   0.6579   0.00977   0.00273  -0.1397   0.4846   0.0841
  -0.250   0.6844   0.00981   0.00277  -0.1394   0.4769   0.0904
   0.000   0.7098   0.00990   0.00282  -0.1389   0.4686   0.0951
   0.250   0.7361   0.00995   0.00286  -0.1386   0.4600   0.0996
   0.500   0.7607   0.01008   0.00293  -0.1380   0.4493   0.1033
   0.750   0.7857   0.01016   0.00300  -0.1375   0.4381   0.1097
   1.000   0.8098   0.01028   0.00308  -0.1368   0.4264   0.1180
   1.250   0.8329   0.01042   0.00319  -0.1360   0.4126   0.1312
   1.500   0.8562   0.01040   0.00332  -0.1353   0.4000   0.2064
   1.750   0.8790   0.01044   0.00345  -0.1345   0.3902   0.2636
   2.000   0.9003   0.01054   0.00360  -0.1333   0.3797   0.3034
   2.250   0.9231   0.01061   0.00374  -0.1325   0.3710   0.3483
   2.500   0.9448   0.01071   0.00393  -0.1315   0.3615   0.4094
   2.750   0.9692   0.01066   0.00413  -0.1312   0.3541   0.5245
   3.000   0.9924   0.01053   0.00444  -0.1306   0.3458   0.7160
   3.250   1.0156   0.01065   0.00466  -0.1298   0.3396   0.7770
   3.500   1.0386   0.01082   0.00486  -0.1290   0.3331   0.8021
   3.750   1.0600   0.01103   0.00510  -0.1280   0.3259   0.8305
   4.000   1.0823   0.01095   0.00530  -0.1268   0.3208   1.0000
   4.250   1.1043   0.01121   0.00553  -0.1259   0.3145   1.0000
   4.500   1.1254   0.01153   0.00578  -0.1249   0.3083   1.0000
   4.750   1.1486   0.01176   0.00599  -0.1243   0.3042   1.0000
   5.000   1.1707   0.01203   0.00623  -0.1234   0.2992   1.0000
   5.250   1.1917   0.01235   0.00652  -0.1225   0.2942   1.0000
   5.500   1.2133   0.01266   0.00680  -0.1216   0.2899   1.0000
   5.750   1.2359   0.01293   0.00705  -0.1209   0.2864   1.0000
   6.000   1.2564   0.01328   0.00737  -0.1199   0.2803   1.0000
   6.250   1.2756   0.01371   0.00775  -0.1188   0.2742   1.0000
   6.500   1.2972   0.01402   0.00806  -0.1180   0.2701   1.0000
   6.750   1.3171   0.01443   0.00844  -0.1170   0.2639   1.0000
   7.000   1.3352   0.01492   0.00888  -0.1158   0.2575   1.0000
   7.250   1.3546   0.01535   0.00930  -0.1148   0.2504   1.0000
   7.500   1.3706   0.01597   0.00985  -0.1133   0.2410   1.0000
   7.750   1.3847   0.01670   0.01051  -0.1116   0.2277   1.0000
   8.000   1.3775   0.01863   0.01214  -0.1072   0.1800   1.0000
   8.250   1.3515   0.02189   0.01501  -0.1008   0.1120   1.0000
   8.500   1.3545   0.02352   0.01652  -0.0983   0.0899   1.0000
   8.750   1.3666   0.02459   0.01758  -0.0969   0.0848   1.0000
   9.000   1.3813   0.02550   0.01849  -0.0959   0.0826   1.0000
   9.250   1.3957   0.02645   0.01946  -0.0948   0.0814   1.0000
   9.500   1.4102   0.02740   0.02042  -0.0938   0.0803   1.0000
   9.750   1.4237   0.02846   0.02149  -0.0928   0.0793   1.0000
  10.000   1.4373   0.02952   0.02257  -0.0918   0.0784   1.0000
  10.250   1.4500   0.03067   0.02373  -0.0908   0.0775   1.0000
  10.500   1.4624   0.03184   0.02493  -0.0898   0.0766   1.0000
  10.750   1.4744   0.03307   0.02618  -0.0888   0.0757   1.0000
  11.000   1.4863   0.03433   0.02747  -0.0879   0.0751   1.0000
  11.250   1.4993   0.03551   0.02868  -0.0870   0.0748   1.0000
  11.500   1.5108   0.03684   0.03005  -0.0862   0.0746   1.0000
  11.750   1.5227   0.03815   0.03140  -0.0853   0.0743   1.0000
  12.000   1.5331   0.03959   0.03288  -0.0845   0.0740   1.0000
  12.250   1.5436   0.04105   0.03438  -0.0836   0.0738   1.0000
  12.500   1.5532   0.04261   0.03599  -0.0828   0.0735   1.0000
  12.750   1.5625   0.04423   0.03765  -0.0820   0.0732   1.0000
  13.000   1.5711   0.04594   0.03941  -0.0812   0.0729   1.0000
  13.250   1.5791   0.04773   0.04124  -0.0805   0.0726   1.0000
  13.500   1.5863   0.04960   0.04316  -0.0797   0.0723   1.0000
  13.750   1.5930   0.05155   0.04517  -0.0790   0.0720   1.0000
  14.000   1.5989   0.05363   0.04730  -0.0783   0.0718   1.0000
  14.250   1.6045   0.05574   0.04947  -0.0777   0.0715   1.0000
  14.500   1.6087   0.05805   0.05184  -0.0771   0.0712   1.0000
  14.750   1.6133   0.06032   0.05416  -0.0765   0.0710   1.0000
  15.000   1.6155   0.06288   0.05678  -0.0759   0.0707   1.0000
  15.250   1.6182   0.06540   0.05937  -0.0754   0.0704   1.0000
  15.500   1.6192   0.06817   0.06219  -0.0749   0.0700   1.0000
  15.750   1.6191   0.07110   0.06518  -0.0745   0.0695   1.0000
  16.000   1.6184   0.07409   0.06824  -0.0742   0.0689   1.0000
  16.250   1.6151   0.07745   0.07167  -0.0738   0.0683   1.0000
  16.500   1.6104   0.08100   0.07530  -0.0736   0.0678   1.0000
  16.750   1.6068   0.08445   0.07882  -0.0734   0.0674   1.0000
  17.000   1.6072   0.08745   0.08189  -0.0734   0.0672   1.0000
  17.250   1.6081   0.09038   0.08489  -0.0734   0.0670   1.0000
  17.500   1.6080   0.09343   0.08801  -0.0734   0.0668   1.0000
  17.750   1.6083   0.09643   0.09108  -0.0735   0.0665   1.0000
  18.000   1.6073   0.09963   0.09436  -0.0737   0.0662   1.0000
  18.250   1.6054   0.10298   0.09777  -0.0740   0.0659   1.0000
  18.500   1.6042   0.10623   0.10110  -0.0743   0.0657   1.0000
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