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GOE 433 AIRFOIL (goe433-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 433 AIRFOIL (goe433-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.92 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe433-il-1000000.txt
Download as CSV file: xf-goe433-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 433 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
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -0.9639   0.10400   0.10120  -0.0533   1.0000   0.0437
 -19.000  -0.9781   0.09819   0.09532  -0.0569   1.0000   0.0443
 -18.750  -0.9917   0.09254   0.08959  -0.0603   1.0000   0.0449
 -18.500  -1.0064   0.08680   0.08375  -0.0639   1.0000   0.0453
 -18.250  -1.0207   0.08115   0.07799  -0.0674   1.0000   0.0457
 -18.000  -1.0330   0.07613   0.07295  -0.0706   1.0000   0.0465
 -17.750  -1.0462   0.07093   0.06770  -0.0740   1.0000   0.0471
 -17.500  -1.0600   0.06567   0.06237  -0.0774   1.0000   0.0476
 -17.250  -1.0726   0.06061   0.05725  -0.0808   1.0000   0.0481
 -17.000  -1.0837   0.05581   0.05237  -0.0841   1.0000   0.0486
 -16.750  -1.0944   0.05120   0.04769  -0.0873   1.0000   0.0491
 -16.500  -1.1025   0.04696   0.04336  -0.0903   1.0000   0.0496
 -16.250  -1.1075   0.04312   0.03944  -0.0930   1.0000   0.0501
 -16.000  -1.1101   0.03960   0.03583  -0.0957   1.0000   0.0505
 -15.750  -1.1093   0.03651   0.03265  -0.0981   1.0000   0.0508
 -15.500  -1.1174   0.03267   0.02876  -0.1009   1.0000   0.0515
 -15.250  -1.1245   0.02922   0.02526  -0.1035   0.9970   0.0521
 -15.000  -1.0966   0.02637   0.02236  -0.1102   0.9901   0.0531
 -14.750  -1.0668   0.02423   0.02017  -0.1155   0.9816   0.0541
 -14.500  -1.0376   0.02234   0.01819  -0.1203   0.9720   0.0550
 -14.250  -1.0109   0.02114   0.01689  -0.1229   0.9623   0.0559
 -14.000  -0.9874   0.02045   0.01609  -0.1236   0.9508   0.0565
 -13.750  -0.9668   0.01918   0.01477  -0.1248   0.9380   0.0578
 -13.500  -0.9430   0.01846   0.01400  -0.1253   0.9272   0.0588
 -13.250  -0.9180   0.01792   0.01339  -0.1256   0.9156   0.0597
 -13.000  -0.8921   0.01744   0.01285  -0.1260   0.9041   0.0607
 -12.750  -0.8660   0.01702   0.01234  -0.1262   0.8929   0.0616
 -12.500  -0.8390   0.01665   0.01188  -0.1264   0.8821   0.0623
 -12.250  -0.8128   0.01609   0.01123  -0.1268   0.8729   0.0633
 -12.000  -0.7862   0.01548   0.01058  -0.1274   0.8643   0.0646
 -11.750  -0.7589   0.01511   0.01015  -0.1276   0.8564   0.0657
 -11.500  -0.7307   0.01477   0.00977  -0.1280   0.8500   0.0667
 -11.250  -0.7026   0.01446   0.00940  -0.1283   0.8432   0.0677
 -11.000  -0.6744   0.01420   0.00905  -0.1285   0.8366   0.0687
 -10.750  -0.6454   0.01397   0.00877  -0.1288   0.8312   0.0693
 -10.500  -0.6178   0.01338   0.00815  -0.1293   0.8249   0.0711
 -10.250  -0.5895   0.01306   0.00778  -0.1296   0.8182   0.0724
 -10.000  -0.5606   0.01278   0.00748  -0.1299   0.8127   0.0735
  -9.750  -0.5316   0.01252   0.00718  -0.1302   0.8065   0.0747
  -9.500  -0.5026   0.01232   0.00691  -0.1303   0.8002   0.0758
  -9.250  -0.4733   0.01216   0.00669  -0.1306   0.7944   0.0766
  -9.000  -0.4446   0.01169   0.00621  -0.1310   0.7879   0.0787
  -8.750  -0.4156   0.01142   0.00590  -0.1313   0.7804   0.0802
  -8.500  -0.3863   0.01119   0.00564  -0.1315   0.7730   0.0816
  -8.250  -0.3570   0.01100   0.00540  -0.1318   0.7642   0.0831
  -8.000  -0.3277   0.01086   0.00519  -0.1319   0.7551   0.0843
  -7.750  -0.2984   0.01057   0.00487  -0.1322   0.7429   0.0863
  -7.500  -0.2693   0.01034   0.00459  -0.1324   0.7276   0.0884
  -7.250  -0.2403   0.01018   0.00436  -0.1326   0.7092   0.0903
  -7.000  -0.2113   0.01008   0.00416  -0.1327   0.6908   0.0922
  -6.750  -0.1822   0.00998   0.00397  -0.1328   0.6760   0.0941
  -6.500  -0.1530   0.00981   0.00375  -0.1330   0.6638   0.0974
  -6.250  -0.1235   0.00968   0.00359  -0.1333   0.6549   0.1003
  -6.000  -0.0940   0.00960   0.00346  -0.1335   0.6471   0.1029
  -5.750  -0.0645   0.00945   0.00330  -0.1337   0.6400   0.1083
  -5.500  -0.0346   0.00935   0.00319  -0.1340   0.6348   0.1128
  -5.250  -0.0049   0.00922   0.00307  -0.1342   0.6296   0.1194
  -5.000   0.0247   0.00917   0.00299  -0.1344   0.6244   0.1252
  -4.750   0.0545   0.00907   0.00291  -0.1347   0.6200   0.1329
  -4.500   0.0846   0.00901   0.00284  -0.1349   0.6162   0.1381
  -4.250   0.1145   0.00890   0.00276  -0.1352   0.6122   0.1446
  -4.000   0.1443   0.00888   0.00271  -0.1354   0.6082   0.1492
  -3.750   0.1739   0.00885   0.00265  -0.1356   0.6037   0.1543
  -3.500   0.2039   0.00877   0.00259  -0.1358   0.6002   0.1600
  -3.250   0.2341   0.00871   0.00254  -0.1361   0.5970   0.1641
  -3.000   0.2641   0.00864   0.00247  -0.1363   0.5935   0.1693
  -2.750   0.2940   0.00858   0.00242  -0.1366   0.5898   0.1754
  -2.500   0.3236   0.00857   0.00239  -0.1368   0.5857   0.1804
  -2.250   0.3534   0.00853   0.00236  -0.1370   0.5814   0.1893
  -1.750   0.4137   0.00835   0.00228  -0.1376   0.5748   0.2116
  -1.500   0.4436   0.00828   0.00225  -0.1378   0.5709   0.2291
  -1.250   0.4732   0.00824   0.00225  -0.1381   0.5666   0.2483
  -1.000   0.5027   0.00823   0.00227  -0.1383   0.5618   0.2657
  -0.750   0.5329   0.00815   0.00226  -0.1385   0.5582   0.2806
  -0.500   0.5628   0.00811   0.00225  -0.1388   0.5539   0.2951
   0.000   0.6217   0.00812   0.00228  -0.1391   0.5436   0.3247
   0.250   0.6517   0.00806   0.00229  -0.1394   0.5392   0.3409
   0.500   0.6814   0.00803   0.00231  -0.1396   0.5325   0.3586
   0.750   0.7104   0.00805   0.00234  -0.1397   0.5249   0.3799
   1.000   0.7401   0.00802   0.00239  -0.1399   0.5182   0.4035
   1.250   0.7692   0.00806   0.00244  -0.1400   0.5095   0.4238
   1.500   0.7982   0.00812   0.00250  -0.1401   0.4997   0.4402
   1.750   0.8265   0.00824   0.00257  -0.1400   0.4866   0.4527
   2.000   0.8551   0.00835   0.00265  -0.1400   0.4738   0.4639
   2.250   0.8834   0.00847   0.00275  -0.1400   0.4629   0.4733
   2.500   0.9111   0.00865   0.00287  -0.1398   0.4506   0.4826
   2.750   0.9394   0.00877   0.00297  -0.1398   0.4401   0.4903
   3.000   0.9671   0.00893   0.00310  -0.1397   0.4305   0.4981
   3.250   0.9951   0.00909   0.00323  -0.1396   0.4208   0.5053
   3.500   1.0227   0.00925   0.00336  -0.1395   0.4122   0.5120
   3.750   1.0506   0.00939   0.00350  -0.1394   0.4037   0.5189
   4.000   1.0777   0.00959   0.00365  -0.1392   0.3942   0.5254
   4.250   1.1053   0.00974   0.00379  -0.1391   0.3849   0.5316
   4.500   1.1322   0.00993   0.00396  -0.1389   0.3757   0.5384
   4.750   1.1595   0.01010   0.00411  -0.1387   0.3667   0.5446
   5.000   1.1861   0.01031   0.00428  -0.1384   0.3573   0.5496
   5.250   1.2129   0.01049   0.00445  -0.1382   0.3477   0.5551
   5.500   1.2392   0.01069   0.00463  -0.1379   0.3383   0.5606
   5.750   1.2648   0.01096   0.00484  -0.1375   0.3266   0.5657
   6.000   1.2906   0.01118   0.00505  -0.1372   0.3146   0.5723
   6.250   1.3150   0.01149   0.00531  -0.1366   0.2995   0.5793
   6.500   1.3375   0.01194   0.00564  -0.1358   0.2781   0.5859
   6.750   1.3580   0.01247   0.00605  -0.1347   0.2529   0.5947
   7.000   1.3742   0.01326   0.00664  -0.1329   0.2164   0.6046
   7.250   1.3864   0.01424   0.00740  -0.1306   0.1784   0.6166
   7.500   1.4018   0.01495   0.00802  -0.1288   0.1570   0.6323
   7.750   1.4161   0.01549   0.00857  -0.1266   0.1435   0.6580
   8.000   1.4319   0.01599   0.00917  -0.1248   0.1318   0.7215
   8.250   1.4427   0.01619   0.00978  -0.1220   0.1208   1.0000
   8.500   1.4550   0.01701   0.01049  -0.1199   0.1068   1.0000
   8.750   1.4537   0.01863   0.01187  -0.1162   0.0700   1.0000
   9.000   1.4610   0.01984   0.01302  -0.1138   0.0597   1.0000
   9.250   1.4738   0.02078   0.01395  -0.1122   0.0572   1.0000
   9.500   1.4875   0.02169   0.01487  -0.1108   0.0555   1.0000
   9.750   1.5023   0.02257   0.01577  -0.1095   0.0548   1.0000
  10.000   1.5164   0.02351   0.01674  -0.1083   0.0542   1.0000
  10.250   1.5298   0.02454   0.01780  -0.1071   0.0537   1.0000
  10.500   1.5423   0.02567   0.01896  -0.1058   0.0531   1.0000
  10.750   1.5539   0.02689   0.02022  -0.1046   0.0527   1.0000
  11.000   1.5645   0.02821   0.02157  -0.1034   0.0522   1.0000
  11.250   1.5743   0.02964   0.02304  -0.1022   0.0518   1.0000
  11.500   1.5830   0.03119   0.02463  -0.1010   0.0514   1.0000
  11.750   1.5908   0.03284   0.02632  -0.0998   0.0510   1.0000
  12.000   1.5977   0.03460   0.02813  -0.0986   0.0506   1.0000
  12.250   1.6031   0.03655   0.03014  -0.0975   0.0502   1.0000
  12.500   1.6073   0.03865   0.03230  -0.0964   0.0499   1.0000
  12.750   1.6104   0.04094   0.03465  -0.0955   0.0496   1.0000
  13.000   1.6132   0.04335   0.03713  -0.0946   0.0493   1.0000
  13.250   1.6183   0.04557   0.03941  -0.0939   0.0493   1.0000
  13.500   1.6226   0.04789   0.04179  -0.0932   0.0491   1.0000
  13.750   1.6264   0.05031   0.04428  -0.0926   0.0490   1.0000
  14.000   1.6296   0.05285   0.04688  -0.0921   0.0489   1.0000
  14.250   1.6325   0.05545   0.04955  -0.0916   0.0487   1.0000
  14.500   1.6354   0.05803   0.05218  -0.0912   0.0484   1.0000
  14.750   1.6362   0.06090   0.05512  -0.0908   0.0482   1.0000
  15.000   1.6372   0.06375   0.05804  -0.0904   0.0479   1.0000
  15.250   1.6373   0.06676   0.06111  -0.0901   0.0477   1.0000
  15.500   1.6363   0.06993   0.06434  -0.0899   0.0474   1.0000
  15.750   1.6358   0.07302   0.06750  -0.0896   0.0472   1.0000
  16.000   1.6333   0.07645   0.07100  -0.0896   0.0470   1.0000
  16.250   1.6316   0.07980   0.07442  -0.0895   0.0467   1.0000
  16.500   1.6294   0.08325   0.07793  -0.0895   0.0465   1.0000
  16.750   1.6260   0.08687   0.08162  -0.0897   0.0464   1.0000
  17.000   1.6239   0.09033   0.08515  -0.0898   0.0462   1.0000
  17.250   1.6202   0.09408   0.08897  -0.0901   0.0460   1.0000
  17.500   1.6174   0.09772   0.09267  -0.0904   0.0458   1.0000
  17.750   1.6143   0.10139   0.09640  -0.0908   0.0456   1.0000
  18.000   1.6103   0.10519   0.10026  -0.0913   0.0454   1.0000
  18.250   1.6075   0.10884   0.10397  -0.0919   0.0451   1.0000
  18.500   1.6026   0.11280   0.10799  -0.0926   0.0448   1.0000
  18.750   1.5998   0.11645   0.11169  -0.0932   0.0445   1.0000
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