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GOE 222 (MVA H.33) AIRFOIL (goe222-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 222 (MVA H.33) AIRFOIL (goe222-il)
Reynolds number: 500,000
Max Cl/Cd: 84.81 at α=0.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe222-il-500000-n5.txt
Download as CSV file: xf-goe222-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.4238   0.09710   0.09385  -0.1189   0.9672   0.0224
 -16.750  -0.4357   0.09129   0.08795  -0.1223   0.9631   0.0226
 -16.500  -0.4436   0.08611   0.08269  -0.1255   0.9594   0.0228
 -16.250  -0.4491   0.08140   0.07790  -0.1286   0.9562   0.0230
 -16.000  -0.4544   0.07704   0.07347  -0.1313   0.9520   0.0232
 -15.750  -0.4587   0.07288   0.06923  -0.1339   0.9476   0.0234
 -15.500  -0.4623   0.06886   0.06512  -0.1364   0.9433   0.0236
 -15.250  -0.4644   0.06514   0.06132  -0.1388   0.9392   0.0239
 -15.000  -0.4659   0.06159   0.05768  -0.1412   0.9340   0.0241
 -14.750  -0.4674   0.05812   0.05411  -0.1434   0.9286   0.0244
 -14.500  -0.4679   0.05484   0.05073  -0.1456   0.9235   0.0247
 -14.250  -0.4674   0.05178   0.04757  -0.1477   0.9171   0.0250
 -14.000  -0.4668   0.04884   0.04451  -0.1497   0.9105   0.0253
 -13.750  -0.4654   0.04609   0.04165  -0.1516   0.9036   0.0256
 -13.500  -0.4625   0.04356   0.03900  -0.1533   0.8954   0.0258
 -13.250  -0.4583   0.04113   0.03645  -0.1550   0.8870   0.0260
 -13.000  -0.4528   0.03890   0.03411  -0.1565   0.8773   0.0263
 -12.750  -0.4450   0.03700   0.03217  -0.1577   0.8666   0.0266
 -12.500  -0.4364   0.03509   0.03018  -0.1591   0.8546   0.0268
 -12.250  -0.4275   0.03324   0.02824  -0.1605   0.8407   0.0271
 -12.000  -0.4180   0.03146   0.02635  -0.1622   0.8256   0.0274
 -11.750  -0.4028   0.02965   0.02442  -0.1648   0.8113   0.0277
 -11.500  -0.3844   0.02789   0.02254  -0.1678   0.7985   0.0280
 -11.250  -0.3632   0.02620   0.02072  -0.1710   0.7880   0.0284
 -11.000  -0.3393   0.02461   0.01899  -0.1744   0.7790   0.0289
 -10.750  -0.3131   0.02314   0.01739  -0.1778   0.7718   0.0294
 -10.500  -0.2859   0.02189   0.01599  -0.1806   0.7655   0.0299
 -10.250  -0.2592   0.02095   0.01490  -0.1826   0.7603   0.0302
 -10.000  -0.2324   0.02012   0.01398  -0.1842   0.7559   0.0306
  -9.750  -0.2061   0.01920   0.01301  -0.1857   0.7517   0.0310
  -9.500  -0.1788   0.01849   0.01224  -0.1870   0.7479   0.0315
  -9.250  -0.1509   0.01791   0.01158  -0.1882   0.7443   0.0321
  -9.000  -0.1227   0.01736   0.01098  -0.1893   0.7410   0.0326
  -8.750  -0.0943   0.01684   0.01039  -0.1903   0.7374   0.0331
  -8.500  -0.0658   0.01635   0.00983  -0.1912   0.7335   0.0337
  -8.250  -0.0372   0.01590   0.00930  -0.1921   0.7296   0.0342
  -8.000  -0.0084   0.01550   0.00881  -0.1929   0.7262   0.0347
  -7.750   0.0209   0.01512   0.00836  -0.1937   0.7234   0.0352
  -7.500   0.0503   0.01465   0.00785  -0.1947   0.7206   0.0359
  -7.250   0.0797   0.01422   0.00739  -0.1956   0.7173   0.0367
  -7.000   0.1090   0.01389   0.00701  -0.1964   0.7138   0.0375
  -6.750   0.1385   0.01361   0.00666  -0.1971   0.7106   0.0383
  -6.500   0.1682   0.01335   0.00633  -0.1978   0.7077   0.0392
  -6.250   0.1979   0.01311   0.00603  -0.1985   0.7052   0.0400
  -6.000   0.2276   0.01287   0.00576  -0.1991   0.7023   0.0409
  -5.750   0.2573   0.01257   0.00544  -0.1998   0.6989   0.0422
  -5.500   0.2868   0.01235   0.00517  -0.2004   0.6952   0.0438
  -5.250   0.3163   0.01219   0.00495  -0.2009   0.6917   0.0457
  -5.000   0.3459   0.01205   0.00475  -0.2014   0.6887   0.0480
  -4.750   0.3759   0.01184   0.00452  -0.2021   0.6865   0.0516
  -4.500   0.4058   0.01164   0.00432  -0.2027   0.6841   0.0575
  -4.250   0.4364   0.01117   0.00403  -0.2038   0.6815   0.1053
  -4.000   0.4666   0.01081   0.00379  -0.2047   0.6787   0.1458
  -3.750   0.4968   0.01045   0.00362  -0.2056   0.6758   0.2066
  -3.500   0.5263   0.01034   0.00358  -0.2061   0.6727   0.2408
  -3.250   0.5555   0.01034   0.00356  -0.2065   0.6697   0.2583
  -3.000   0.5846   0.01030   0.00356  -0.2068   0.6664   0.2699
  -2.750   0.6135   0.01029   0.00356  -0.2070   0.6625   0.2793
  -2.500   0.6422   0.01030   0.00357  -0.2073   0.6587   0.2894
  -2.250   0.6707   0.01032   0.00357  -0.2074   0.6549   0.2971
  -2.000   0.6991   0.01037   0.00361  -0.2076   0.6512   0.3075
  -1.750   0.7276   0.01038   0.00364  -0.2077   0.6468   0.3154
  -1.500   0.7556   0.01040   0.00367  -0.2078   0.6416   0.3203
  -1.250   0.7830   0.01045   0.00367  -0.2078   0.6362   0.3247
  -1.000   0.8108   0.01049   0.00367  -0.2078   0.6305   0.3282
  -0.750   0.8380   0.01050   0.00370  -0.2077   0.6230   0.3317
  -0.500   0.8643   0.01055   0.00373  -0.2074   0.6141   0.3356
  -0.250   0.8889   0.01064   0.00376  -0.2068   0.6008   0.3394
   0.000   0.9119   0.01077   0.00381  -0.2059   0.5823   0.3427
   0.250   0.9321   0.01099   0.00389  -0.2045   0.5596   0.3456
   0.500   0.9513   0.01126   0.00404  -0.2029   0.5390   0.3486
   0.750   0.9709   0.01154   0.00423  -0.2014   0.5219   0.3516
   1.000   0.9892   0.01182   0.00443  -0.1996   0.5065   0.3545
   1.250   1.0072   0.01209   0.00463  -0.1978   0.4933   0.3576
   1.500   1.0258   0.01238   0.00485  -0.1961   0.4822   0.3606
   1.750   1.0472   0.01264   0.00506  -0.1951   0.4731   0.3635
   2.000   1.0691   0.01291   0.00530  -0.1941   0.4662   0.3667
   2.250   1.0928   0.01312   0.00552  -0.1935   0.4601   0.3706
   2.500   1.1151   0.01338   0.00577  -0.1927   0.4543   0.3746
   2.750   1.1369   0.01367   0.00604  -0.1918   0.4493   0.3784
   3.000   1.1605   0.01389   0.00626  -0.1912   0.4447   0.3817
   3.250   1.1829   0.01416   0.00653  -0.1904   0.4393   0.3852
   3.500   1.2036   0.01449   0.00685  -0.1894   0.4339   0.3891
   3.750   1.2258   0.01476   0.00714  -0.1886   0.4298   0.3933
   4.000   1.2487   0.01502   0.00741  -0.1879   0.4259   0.3979
   4.250   1.2706   0.01531   0.00772  -0.1871   0.4218   0.4023
   4.500   1.2914   0.01565   0.00808  -0.1862   0.4177   0.4072
   4.750   1.3113   0.01603   0.00846  -0.1851   0.4137   0.4121
   5.000   1.3342   0.01629   0.00877  -0.1845   0.4104   0.4171
   5.250   1.3561   0.01660   0.00912  -0.1837   0.4071   0.4221
   5.500   1.3770   0.01695   0.00951  -0.1828   0.4035   0.4282
   5.750   1.3965   0.01737   0.00994  -0.1818   0.3993   0.4350
   6.000   1.4157   0.01781   0.01041  -0.1807   0.3955   0.4422
   6.250   1.4374   0.01813   0.01081  -0.1800   0.3923   0.4510
   6.500   1.4582   0.01851   0.01124  -0.1791   0.3888   0.4595
   6.750   1.4782   0.01892   0.01172  -0.1782   0.3853   0.4699
   7.000   1.4969   0.01942   0.01225  -0.1771   0.3817   0.4811
   7.500   1.5356   0.02034   0.01332  -0.1752   0.3747   0.5124
   7.750   1.5549   0.02082   0.01388  -0.1743   0.3702   0.5299
   8.000   1.5715   0.02144   0.01455  -0.1730   0.3652   0.5467
   8.250   1.5881   0.02208   0.01524  -0.1718   0.3607   0.5626
   8.500   1.6073   0.02259   0.01585  -0.1709   0.3559   0.5792
   8.750   1.6231   0.02329   0.01661  -0.1696   0.3497   0.5968
   9.000   1.6375   0.02409   0.01746  -0.1682   0.3416   0.6173
   9.250   1.6483   0.02513   0.01854  -0.1664   0.3298   0.6429
   9.500   1.6583   0.02626   0.01982  -0.1647   0.3123   0.7176
   9.750   1.6544   0.02764   0.02139  -0.1607   0.2880   1.0000
  10.000   1.6505   0.02990   0.02350  -0.1576   0.2632   1.0000
  10.250   1.6509   0.03195   0.02546  -0.1550   0.2463   1.0000
  10.500   1.6538   0.03388   0.02733  -0.1529   0.2344   1.0000
  10.750   1.6606   0.03553   0.02897  -0.1512   0.2262   1.0000
  11.000   1.6660   0.03733   0.03076  -0.1494   0.2192   1.0000
  11.250   1.6761   0.03878   0.03223  -0.1482   0.2141   1.0000
  11.500   1.6840   0.04043   0.03390  -0.1468   0.2092   1.0000
  11.750   1.6899   0.04228   0.03574  -0.1453   0.2043   1.0000
  12.000   1.6998   0.04378   0.03730  -0.1441   0.2007   1.0000
  12.250   1.7095   0.04532   0.03888  -0.1430   0.1969   1.0000
  12.500   1.7164   0.04713   0.04072  -0.1417   0.1927   1.0000
  12.750   1.7210   0.04918   0.04278  -0.1403   0.1885   1.0000
  13.000   1.7301   0.05081   0.04447  -0.1393   0.1847   1.0000
  13.250   1.7378   0.05261   0.04632  -0.1382   0.1801   1.0000
  13.500   1.7424   0.05470   0.04843  -0.1370   0.1753   1.0000
  13.750   1.7465   0.05688   0.05065  -0.1358   0.1708   1.0000
  14.000   1.7522   0.05891   0.05271  -0.1348   0.1643   1.0000
  14.250   1.7522   0.06158   0.05539  -0.1335   0.1575   1.0000
  14.500   1.7535   0.06414   0.05797  -0.1324   0.1486   1.0000
  14.750   1.7481   0.06747   0.06127  -0.1311   0.1371   1.0000
  15.000   1.7384   0.07134   0.06510  -0.1297   0.1245   1.0000
  15.250   1.7275   0.07545   0.06918  -0.1285   0.1128   1.0000
  15.500   1.7151   0.07983   0.07355  -0.1274   0.1012   1.0000
  15.750   1.6957   0.08513   0.07880  -0.1263   0.0834   1.0000
  16.000   1.6678   0.09163   0.08520  -0.1254   0.0596   1.0000
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