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GOE 243 (MVA PR.3) AIRFOIL (goe243-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 243 (MVA PR.3) AIRFOIL (goe243-il)
Reynolds number: 1,000,000
Max Cl/Cd: 107.89 at α=2.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe243-il-1000000-n5.txt
Download as CSV file: xf-goe243-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 243 (MVA PR.3) 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.3666   0.06122   0.05771  -0.1231   0.8013   0.0226
 -13.250  -0.3794   0.05544   0.05178  -0.1282   0.7951   0.0226
 -13.000  -0.3840   0.05101   0.04722  -0.1322   0.7880   0.0226
 -12.750  -0.3839   0.04734   0.04342  -0.1357   0.7812   0.0227
 -12.500  -0.3792   0.04424   0.04022  -0.1388   0.7762   0.0227
 -12.250  -0.3727   0.04137   0.03727  -0.1419   0.7705   0.0227
 -12.000  -0.3642   0.03880   0.03460  -0.1447   0.7642   0.0228
 -11.750  -0.3580   0.03626   0.03195  -0.1473   0.7582   0.0229
 -11.500  -0.3467   0.03371   0.02931  -0.1510   0.7530   0.0230
 -11.250  -0.3288   0.03156   0.02708  -0.1548   0.7475   0.0231
 -11.000  -0.3069   0.02972   0.02516  -0.1585   0.7422   0.0232
 -10.750  -0.2821   0.02804   0.02341  -0.1623   0.7372   0.0233
 -10.500  -0.2545   0.02655   0.02187  -0.1660   0.7327   0.0234
 -10.250  -0.2253   0.02516   0.02042  -0.1696   0.7274   0.0235
 -10.000  -0.1947   0.02393   0.01912  -0.1731   0.7222   0.0237
  -9.750  -0.1631   0.02277   0.01789  -0.1766   0.7167   0.0238
  -9.500  -0.1300   0.02171   0.01678  -0.1800   0.7110   0.0239
  -9.250  -0.0966   0.02074   0.01574  -0.1833   0.7026   0.0240
  -9.000  -0.0627   0.01986   0.01478  -0.1864   0.6946   0.0242
  -8.750  -0.0278   0.01902   0.01388  -0.1896   0.6878   0.0243
  -8.500   0.0073   0.01824   0.01303  -0.1926   0.6817   0.0245
  -8.250   0.0424   0.01754   0.01226  -0.1954   0.6757   0.0247
  -8.000   0.0785   0.01684   0.01152  -0.1984   0.6711   0.0248
  -7.750   0.1145   0.01620   0.01082  -0.2011   0.6655   0.0250
  -7.500   0.1504   0.01562   0.01017  -0.2038   0.6592   0.0252
  -7.250   0.1865   0.01506   0.00955  -0.2064   0.6537   0.0254
  -7.000   0.2229   0.01451   0.00896  -0.2090   0.6487   0.0256
  -6.750   0.2590   0.01402   0.00840  -0.2114   0.6426   0.0258
  -6.500   0.2946   0.01358   0.00789  -0.2137   0.6360   0.0259
  -6.250   0.3307   0.01314   0.00740  -0.2160   0.6305   0.0261
  -6.000   0.3663   0.01274   0.00695  -0.2181   0.6246   0.0263
  -5.750   0.4012   0.01241   0.00655  -0.2201   0.6181   0.0264
  -5.500   0.4379   0.01193   0.00601  -0.2225   0.6120   0.0268
  -5.250   0.4726   0.01161   0.00565  -0.2243   0.6051   0.0271
  -5.000   0.5057   0.01141   0.00538  -0.2256   0.5968   0.0275
  -4.750   0.5385   0.01122   0.00515  -0.2267   0.5887   0.0278
  -4.500   0.5704   0.01111   0.00496  -0.2276   0.5782   0.0282
  -4.250   0.6022   0.01100   0.00480  -0.2285   0.5691   0.0287
  -4.000   0.6337   0.01091   0.00465  -0.2293   0.5593   0.0292
  -3.750   0.6651   0.01083   0.00451  -0.2300   0.5502   0.0296
  -3.500   0.6959   0.01079   0.00440  -0.2306   0.5388   0.0300
  -3.250   0.7266   0.01076   0.00429  -0.2312   0.5273   0.0304
  -3.000   0.7570   0.01074   0.00419  -0.2318   0.5145   0.0311
  -2.750   0.7873   0.01073   0.00412  -0.2323   0.5022   0.0318
  -2.500   0.8168   0.01078   0.00410  -0.2326   0.4890   0.0326
  -2.250   0.8456   0.01088   0.00409  -0.2328   0.4748   0.0334
  -2.000   0.8747   0.01094   0.00409  -0.2331   0.4624   0.0343
  -1.750   0.9040   0.01100   0.00409  -0.2333   0.4527   0.0359
  -1.500   0.9329   0.01107   0.00412  -0.2335   0.4425   0.0380
  -1.250   0.9617   0.01115   0.00415  -0.2337   0.4334   0.0417
  -1.000   0.9906   0.01121   0.00419  -0.2339   0.4240   0.0508
  -0.750   1.0192   0.01128   0.00425  -0.2341   0.4156   0.0679
  -0.500   1.0482   0.01132   0.00430  -0.2344   0.4082   0.0853
  -0.250   1.0768   0.01138   0.00436  -0.2346   0.4000   0.1142
   0.000   1.1097   0.01107   0.00433  -0.2361   0.3940   0.2600
   0.250   1.1377   0.01116   0.00444  -0.2361   0.3881   0.2771
   0.500   1.1648   0.01132   0.00458  -0.2360   0.3812   0.2931
   0.750   1.1921   0.01145   0.00471  -0.2359   0.3757   0.3044
   1.000   1.2193   0.01159   0.00484  -0.2357   0.3698   0.3142
   1.250   1.2453   0.01179   0.00500  -0.2353   0.3631   0.3205
   1.500   1.2715   0.01196   0.00516  -0.2350   0.3568   0.3305
   1.750   1.2977   0.01213   0.00531  -0.2347   0.3507   0.3384
   2.000   1.3228   0.01235   0.00549  -0.2342   0.3446   0.3417
   2.250   1.3480   0.01255   0.00566  -0.2337   0.3392   0.3469
   2.500   1.3734   0.01273   0.00583  -0.2333   0.3341   0.3520
   2.750   1.3973   0.01297   0.00605  -0.2326   0.3273   0.3568
   3.000   1.4202   0.01324   0.00628  -0.2317   0.3207   0.3608
   3.250   1.4432   0.01348   0.00649  -0.2308   0.3139   0.3643
   3.500   1.4611   0.01380   0.00678  -0.2290   0.3062   0.3698
   3.750   1.4806   0.01408   0.00704  -0.2275   0.3003   0.3752
   4.000   1.5008   0.01443   0.00736  -0.2263   0.2925   0.3803
   4.250   1.5198   0.01487   0.00775  -0.2248   0.2834   0.3847
   4.500   1.5367   0.01541   0.00823  -0.2231   0.2711   0.3899
   4.750   1.5545   0.01592   0.00870  -0.2216   0.2597   0.3963
   5.000   1.5693   0.01659   0.00930  -0.2197   0.2456   0.4026
   5.250   1.5805   0.01748   0.01007  -0.2172   0.2267   0.4080
   5.500   1.5810   0.01899   0.01138  -0.2134   0.1925   0.4138
   5.750   1.5918   0.01998   0.01230  -0.2111   0.1787   0.4211
   6.000   1.6066   0.02075   0.01305  -0.2094   0.1724   0.4279
   6.250   1.6210   0.02156   0.01385  -0.2077   0.1668   0.4341
   6.500   1.6381   0.02222   0.01454  -0.2065   0.1644   0.4424
   6.750   1.6545   0.02294   0.01528  -0.2051   0.1624   0.4503
   7.000   1.6706   0.02369   0.01604  -0.2038   0.1605   0.4574
   7.250   1.6858   0.02452   0.01691  -0.2024   0.1587   0.4661
   7.500   1.7008   0.02537   0.01778  -0.2010   0.1568   0.4747
   7.750   1.7153   0.02629   0.01873  -0.1997   0.1550   0.4829
   8.000   1.7296   0.02723   0.01970  -0.1983   0.1532   0.4916
   8.250   1.7441   0.02816   0.02066  -0.1970   0.1521   0.4984
   8.500   1.7591   0.02908   0.02163  -0.1958   0.1516   0.5044
   8.750   1.7741   0.03000   0.02260  -0.1946   0.1512   0.5108
   9.000   1.7879   0.03105   0.02368  -0.1934   0.1507   0.5163
   9.250   1.8017   0.03208   0.02476  -0.1922   0.1502   0.5208
   9.500   1.8148   0.03320   0.02593  -0.1909   0.1497   0.5256
   9.750   1.8275   0.03438   0.02715  -0.1897   0.1491   0.5310
  10.000   1.8402   0.03557   0.02838  -0.1885   0.1486   0.5357
  10.250   1.8517   0.03690   0.02976  -0.1873   0.1481   0.5395
  10.500   1.8636   0.03820   0.03109  -0.1861   0.1475   0.5422
  10.750   1.8741   0.03964   0.03259  -0.1849   0.1470   0.5455
  11.000   1.8845   0.04110   0.03410  -0.1837   0.1465   0.5491
  11.250   1.8946   0.04261   0.03566  -0.1826   0.1460   0.5529
  11.500   1.9036   0.04427   0.03737  -0.1814   0.1455   0.5564
  11.750   1.9130   0.04588   0.03902  -0.1802   0.1450   0.5595
  12.000   1.9204   0.04773   0.04092  -0.1791   0.1445   0.5620
  12.250   1.9286   0.04949   0.04274  -0.1780   0.1440   0.5650
  12.500   1.9350   0.05147   0.04478  -0.1768   0.1436   0.5681
  12.750   1.9419   0.05340   0.04678  -0.1757   0.1431   0.5712
  13.000   1.9473   0.05553   0.04897  -0.1747   0.1426   0.5739
  13.250   1.9526   0.05769   0.05118  -0.1736   0.1421   0.5765
  13.500   1.9570   0.05996   0.05351  -0.1726   0.1417   0.5789
  13.750   1.9604   0.06235   0.05596  -0.1715   0.1412   0.5809
  14.000   1.9634   0.06481   0.05849  -0.1706   0.1408   0.5831
  14.250   1.9655   0.06740   0.06115  -0.1696   0.1403   0.5853
  14.500   1.9672   0.07006   0.06389  -0.1687   0.1398   0.5876
  14.750   1.9674   0.07291   0.06681  -0.1678   0.1392   0.5899
  15.000   1.9714   0.07530   0.06927  -0.1671   0.1388   0.5925
  15.250   1.9751   0.07776   0.07181  -0.1664   0.1386   0.5951
  15.500   1.9810   0.07993   0.07405  -0.1658   0.1382   0.5977
  15.750   1.9832   0.08260   0.07679  -0.1652   0.1379   0.5999
  16.000   1.9879   0.08494   0.07920  -0.1647   0.1374   0.6022
  16.250   1.9911   0.08749   0.08182  -0.1642   0.1368   0.6046
  16.500   1.9929   0.09022   0.08463  -0.1637   0.1363   0.6066
  16.750   1.9957   0.09278   0.08726  -0.1633   0.1359   0.6090
  17.000   1.9956   0.09576   0.09032  -0.1629   0.1353   0.6113
  17.250   1.9982   0.09836   0.09299  -0.1625   0.1347   0.6138
  17.500   1.9978   0.10137   0.09607  -0.1623   0.1340   0.6159
  17.750   1.9989   0.10419   0.09895  -0.1621   0.1331   0.6178
  18.000   1.9992   0.10713   0.10195  -0.1619   0.1326   0.6194
  18.250   1.9984   0.11020   0.10510  -0.1619   0.1320   0.6215
  18.500   1.9992   0.11303   0.10799  -0.1619   0.1313   0.6239
  18.750   1.9965   0.11639   0.11141  -0.1620   0.1305   0.6263
  19.000   1.9962   0.11938   0.11446  -0.1621   0.1295   0.6292
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