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GOE 222 (MVA H.33) AIRFOIL (goe222-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: GOE 222 (MVA H.33) AIRFOIL (goe222-il)
Reynolds number: 100,000
Max Cl/Cd: 47.49 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe222-il-100000-n5.txt
Download as CSV file: xf-goe222-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 222 (MVA H.33) AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.0742   0.10216   0.09660  -0.1196   0.9296   0.0522
 -11.500  -0.0863   0.09316   0.08758  -0.1253   0.9260   0.0526
 -11.250  -0.2070   0.06836   0.06253  -0.1401   0.9118   0.0513
 -11.000  -0.2586   0.05923   0.05313  -0.1468   0.8981   0.0507
 -10.750  -0.2865   0.05416   0.04786  -0.1499   0.8861   0.0507
 -10.500  -0.2976   0.04970   0.04315  -0.1545   0.8772   0.0510
 -10.250  -0.3058   0.04660   0.03982  -0.1571   0.8661   0.0515
 -10.000  -0.2920   0.04334   0.03621  -0.1618   0.8616   0.0523
  -9.750  -0.2864   0.04147   0.03411  -0.1622   0.8539   0.0528
  -9.500  -0.2700   0.03954   0.03191  -0.1635   0.8489   0.0535
  -9.250  -0.2449   0.03765   0.02972  -0.1658   0.8460   0.0543
  -9.000  -0.2166   0.03607   0.02805  -0.1673   0.8441   0.0554
  -8.750  -0.2105   0.03554   0.02755  -0.1647   0.8358   0.0563
  -8.500  -0.1864   0.03451   0.02648  -0.1652   0.8325   0.0577
  -8.250  -0.1585   0.03345   0.02534  -0.1663   0.8303   0.0591
  -8.000  -0.1286   0.03246   0.02424  -0.1674   0.8285   0.0604
  -7.750  -0.1178   0.03216   0.02389  -0.1654   0.8221   0.0613
  -7.500  -0.0951   0.03158   0.02322  -0.1653   0.8180   0.0624
  -7.250  -0.0670   0.03082   0.02249  -0.1661   0.8154   0.0642
  -7.000  -0.0353   0.03000   0.02165  -0.1679   0.8136   0.0668
  -6.750  -0.0010   0.02917   0.02073  -0.1702   0.8120   0.0697
  -6.500   0.0103   0.02911   0.02060  -0.1686   0.8053   0.0715
  -6.250   0.0389   0.02837   0.01985  -0.1702   0.8017   0.0745
  -6.000   0.0733   0.02755   0.01894  -0.1727   0.7993   0.0792
  -5.750   0.1128   0.02648   0.01783  -0.1760   0.7973   0.0893
  -5.500   0.1578   0.02504   0.01639  -0.1805   0.7954   0.1176
  -5.250   0.1774   0.02442   0.01598  -0.1805   0.7866   0.1609
  -5.000   0.2169   0.02373   0.01549  -0.1829   0.7823   0.2274
  -4.750   0.2588   0.02337   0.01505  -0.1851   0.7791   0.2649
  -4.500   0.2790   0.02368   0.01528  -0.1839   0.7723   0.2814
  -4.250   0.3068   0.02383   0.01529  -0.1840   0.7678   0.2964
  -4.000   0.3409   0.02381   0.01510  -0.1851   0.7647   0.3112
  -3.750   0.3767   0.02387   0.01509  -0.1862   0.7622   0.3243
  -3.500   0.3995   0.02430   0.01552  -0.1852   0.7573   0.3357
  -3.250   0.4212   0.02465   0.01577  -0.1843   0.7515   0.3477
  -3.000   0.4519   0.02475   0.01587  -0.1844   0.7477   0.3568
  -2.750   0.4899   0.02447   0.01541  -0.1863   0.7449   0.3661
  -2.500   0.5174   0.02451   0.01544  -0.1862   0.7406   0.3714
  -2.250   0.5355   0.02475   0.01562  -0.1848   0.7340   0.3764
  -2.000   0.5695   0.02448   0.01515  -0.1862   0.7299   0.3825
  -1.750   0.6065   0.02415   0.01477  -0.1877   0.7267   0.3864
  -1.500   0.6297   0.02425   0.01485  -0.1870   0.7209   0.3905
  -1.250   0.6519   0.02434   0.01488  -0.1862   0.7142   0.3951
  -1.000   0.6882   0.02404   0.01439  -0.1878   0.7100   0.4004
  -0.750   0.7271   0.02369   0.01399  -0.1897   0.7067   0.4044
  -0.500   0.7353   0.02419   0.01457  -0.1865   0.6978   0.4078
  -0.250   0.7661   0.02406   0.01438  -0.1871   0.6926   0.4128
   0.000   0.8055   0.02373   0.01388  -0.1892   0.6888   0.4184
   0.250   0.8142   0.02418   0.01441  -0.1860   0.6794   0.4212
   0.500   0.8438   0.02405   0.01427  -0.1863   0.6735   0.4255
   0.750   0.8716   0.02400   0.01419  -0.1863   0.6673   0.4308
   1.000   0.8859   0.02430   0.01448  -0.1842   0.6579   0.4357
   1.250   0.9212   0.02401   0.01415  -0.1854   0.6528   0.4407
   1.500   0.9248   0.02455   0.01479  -0.1814   0.6419   0.4440
   1.750   0.9573   0.02435   0.01454  -0.1822   0.6361   0.4496
   2.000   0.9628   0.02491   0.01513  -0.1786   0.6252   0.4544
   2.250   0.9934   0.02473   0.01494  -0.1790   0.6191   0.4602
   2.500   1.0031   0.02532   0.01561  -0.1763   0.6082   0.4650
   2.750   1.0349   0.02510   0.01533  -0.1768   0.6021   0.4721
   3.000   1.0474   0.02569   0.01596  -0.1747   0.5912   0.4773
   3.250   1.0778   0.02551   0.01577  -0.1750   0.5850   0.4838
   3.500   1.0942   0.02602   0.01630  -0.1735   0.5755   0.4908
   3.750   1.1259   0.02582   0.01605  -0.1740   0.5697   0.4989
   4.000   1.1420   0.02635   0.01662  -0.1724   0.5605   0.5064
   4.250   1.1723   0.02622   0.01642  -0.1727   0.5540   0.5158
   4.500   1.1894   0.02673   0.01696  -0.1713   0.5452   0.5238
   4.750   1.2174   0.02673   0.01690  -0.1713   0.5384   0.5346
   5.000   1.2362   0.02719   0.01740  -0.1701   0.5304   0.5453
   5.250   1.2602   0.02741   0.01761  -0.1696   0.5234   0.5575
   5.500   1.2852   0.02764   0.01783  -0.1693   0.5174   0.5714
   6.000   1.3299   0.02832   0.01856  -0.1680   0.5045   0.6036
   6.250   1.3464   0.02889   0.01923  -0.1666   0.4975   0.6224
   6.500   1.3650   0.02934   0.01977  -0.1655   0.4905   0.6466
   6.750   1.3930   0.02933   0.01983  -0.1655   0.4849   0.6867
   7.000   1.3916   0.02973   0.02070  -0.1609   0.4788   0.9430
   7.250   1.4111   0.03034   0.02131  -0.1601   0.4734   1.0000
   7.500   1.4393   0.03061   0.02148  -0.1603   0.4689   1.0000
   7.750   1.4529   0.03152   0.02244  -0.1588   0.4634   1.0000
   8.000   1.4660   0.03245   0.02341  -0.1572   0.4576   1.0000
   8.250   1.4882   0.03292   0.02385  -0.1567   0.4524   1.0000
   8.500   1.5054   0.03366   0.02461  -0.1556   0.4470   1.0000
   8.750   1.5125   0.03490   0.02595  -0.1533   0.4409   1.0000
   9.000   1.5301   0.03560   0.02665  -0.1523   0.4355   1.0000
   9.250   1.5523   0.03609   0.02712  -0.1518   0.4306   1.0000
   9.500   1.5524   0.03777   0.02897  -0.1490   0.4243   1.0000
   9.750   1.5649   0.03876   0.03000  -0.1475   0.4185   1.0000
  10.000   1.5881   0.03912   0.03033  -0.1470   0.4133   1.0000
  10.250   1.5807   0.04136   0.03277  -0.1437   0.4061   1.0000
  10.500   1.5910   0.04248   0.03393  -0.1421   0.3995   1.0000
  10.750   1.5994   0.04376   0.03527  -0.1404   0.3930   1.0000
  11.000   1.5951   0.04599   0.03765  -0.1378   0.3851   1.0000
  11.250   1.6126   0.04659   0.03823  -0.1368   0.3790   1.0000
  11.500   1.5990   0.04978   0.04164  -0.1338   0.3704   1.0000
  11.750   1.6082   0.05107   0.04295  -0.1324   0.3632   1.0000
  12.000   1.5981   0.05423   0.04628  -0.1301   0.3541   1.0000
  12.250   1.6055   0.05574   0.04781  -0.1288   0.3465   1.0000
  12.500   1.5937   0.05935   0.05158  -0.1267   0.3367   1.0000
  12.750   1.6044   0.06058   0.05281  -0.1256   0.3296   1.0000
  13.000   1.5905   0.06465   0.05705  -0.1239   0.3197   1.0000
  13.250   1.5980   0.06632   0.05872  -0.1228   0.3127   1.0000
  13.500   1.5896   0.06995   0.06248  -0.1215   0.3042   1.0000
  13.750   1.6006   0.07125   0.06375  -0.1206   0.2982   1.0000
  14.000   1.5916   0.07512   0.06776  -0.1195   0.2906   1.0000
  14.250   1.6016   0.07655   0.06919  -0.1187   0.2851   1.0000
  14.500   1.5993   0.07964   0.07236  -0.1178   0.2790   1.0000
  14.750   1.5995   0.08243   0.07522  -0.1171   0.2730   1.0000
  15.000   1.6153   0.08306   0.07578  -0.1164   0.2677   1.0000
  15.250   1.6037   0.08754   0.08043  -0.1158   0.2617   1.0000
  15.500   1.6078   0.08981   0.08272  -0.1152   0.2556   1.0000
  15.750   1.6128   0.09194   0.08486  -0.1147   0.2498   1.0000
  16.000   1.6030   0.09627   0.08934  -0.1145   0.2438   1.0000
  16.250   1.6147   0.09740   0.09041  -0.1140   0.2375   1.0000
  16.500   1.6068   0.10156   0.09470  -0.1140   0.2321   1.0000
  16.750   1.5989   0.10578   0.09906  -0.1142   0.2265   1.0000
  17.000   1.6139   0.10636   0.09954  -0.1137   0.2205   1.0000
  17.250   1.6002   0.11160   0.10499  -0.1144   0.2156   1.0000
  17.500   1.5899   0.11634   0.10989  -0.1152   0.2103   1.0000
  17.750   1.6008   0.11757   0.11108  -0.1150   0.2046   1.0000
  18.000   1.5884   0.12278   0.11648  -0.1162   0.1999   1.0000
  18.250   1.5738   0.12844   0.12233  -0.1178   0.1949   1.0000
  18.500   1.5788   0.13075   0.12465  -0.1183   0.1890   1.0000
  18.750   1.5640   0.13658   0.13066  -0.1202   0.1841   1.0000
  19.000   1.5446   0.14337   0.13765  -0.1229   0.1789   1.0000
  19.250   1.5516   0.14539   0.13966  -0.1235   0.1724   1.0000
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