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GOE 222 (MVA H.33) AIRFOIL (goe222-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 222 (MVA H.33) AIRFOIL (goe222-il)
Reynolds number: 500,000
Max Cl/Cd: 99.22 at α=2°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe222-il-500000.txt
Download as CSV file: xf-goe222-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.3324   0.06863   0.06541  -0.1476   0.9712   0.0312
 -14.000  -0.3593   0.06050   0.05708  -0.1554   0.9668   0.0312
 -13.750  -0.3813   0.05457   0.05096  -0.1606   0.9589   0.0312
 -13.250  -0.4126   0.04465   0.04070  -0.1684   0.9429   0.0316
 -13.000  -0.4090   0.04208   0.03806  -0.1697   0.9369   0.0319
 -12.750  -0.4039   0.04001   0.03596  -0.1707   0.9282   0.0323
 -12.500  -0.3930   0.03826   0.03416  -0.1718   0.9220   0.0327
 -12.250  -0.3880   0.03613   0.03197  -0.1733   0.9116   0.0330
 -12.000  -0.3808   0.03371   0.02941  -0.1764   0.9024   0.0334
 -11.750  -0.3659   0.03109   0.02661  -0.1811   0.8920   0.0339
 -11.500  -0.3485   0.02909   0.02441  -0.1841   0.8816   0.0344
 -11.250  -0.3283   0.02740   0.02250  -0.1861   0.8730   0.0349
 -11.000  -0.3077   0.02607   0.02097  -0.1876   0.8616   0.0355
 -10.750  -0.2839   0.02510   0.01974  -0.1892   0.8520   0.0360
 -10.500  -0.2626   0.02343   0.01794  -0.1897   0.8428   0.0367
 -10.250  -0.2392   0.02237   0.01685  -0.1899   0.8343   0.0373
 -10.000  -0.2143   0.02154   0.01594  -0.1904   0.8264   0.0378
  -9.750  -0.1887   0.02079   0.01511  -0.1910   0.8194   0.0384
  -9.500  -0.1628   0.02008   0.01433  -0.1915   0.8126   0.0391
  -9.000  -0.1092   0.01887   0.01291  -0.1928   0.8014   0.0407
  -8.750  -0.0817   0.01834   0.01227  -0.1933   0.7960   0.0413
  -8.500  -0.0535   0.01791   0.01170  -0.1940   0.7912   0.0417
  -8.250  -0.0286   0.01688   0.01070  -0.1943   0.7863   0.0425
  -8.000  -0.0015   0.01625   0.01005  -0.1949   0.7814   0.0433
  -7.750   0.0269   0.01576   0.00951  -0.1956   0.7772   0.0443
  -7.500   0.0563   0.01535   0.00902  -0.1965   0.7732   0.0454
  -7.250   0.0847   0.01493   0.00857  -0.1971   0.7692   0.0464
  -7.000   0.1136   0.01454   0.00813  -0.1978   0.7651   0.0473
  -6.750   0.1431   0.01422   0.00773  -0.1984   0.7613   0.0480
  -6.500   0.1734   0.01356   0.00700  -0.1998   0.7578   0.0496
  -6.250   0.2036   0.01317   0.00656  -0.2007   0.7543   0.0511
  -6.000   0.2330   0.01284   0.00620  -0.2014   0.7507   0.0530
  -5.750   0.2627   0.01258   0.00588  -0.2020   0.7468   0.0548
  -5.500   0.2931   0.01218   0.00542  -0.2029   0.7431   0.0579
  -5.250   0.3240   0.01193   0.00508  -0.2038   0.7397   0.0618
  -4.750   0.3859   0.01056   0.00423  -0.2067   0.7340   0.1941
  -4.500   0.4159   0.01036   0.00420  -0.2074   0.7311   0.2523
  -4.250   0.4456   0.01037   0.00421  -0.2078   0.7282   0.2725
  -4.000   0.4754   0.01041   0.00423  -0.2082   0.7253   0.2855
  -3.750   0.5058   0.01049   0.00425  -0.2087   0.7224   0.2949
  -3.500   0.5357   0.01059   0.00432  -0.2091   0.7195   0.3037
  -3.250   0.5643   0.01062   0.00434  -0.2093   0.7164   0.3111
  -3.000   0.5932   0.01067   0.00440  -0.2095   0.7130   0.3183
  -2.750   0.6224   0.01074   0.00440  -0.2097   0.7094   0.3240
  -2.500   0.6519   0.01077   0.00441  -0.2101   0.7059   0.3299
  -2.250   0.6821   0.01093   0.00452  -0.2105   0.7023   0.3367
  -2.000   0.7099   0.01103   0.00461  -0.2105   0.6990   0.3435
  -1.750   0.7380   0.01099   0.00462  -0.2106   0.6951   0.3495
  -1.500   0.7667   0.01101   0.00462  -0.2108   0.6911   0.3532
  -1.250   0.7958   0.01106   0.00463  -0.2110   0.6873   0.3578
  -1.000   0.8249   0.01117   0.00467  -0.2113   0.6833   0.3619
  -0.750   0.8519   0.01107   0.00463  -0.2112   0.6788   0.3661
  -0.500   0.8795   0.01105   0.00462  -0.2112   0.6739   0.3694
  -0.250   0.9077   0.01106   0.00460  -0.2113   0.6690   0.3729
   0.000   0.9346   0.01107   0.00461  -0.2111   0.6632   0.3765
   0.250   0.9606   0.01107   0.00459  -0.2108   0.6563   0.3799
   0.500   0.9876   0.01105   0.00453  -0.2107   0.6497   0.3839
   0.750   1.0126   0.01101   0.00456  -0.2101   0.6414   0.3876
   1.000   1.0377   0.01104   0.00454  -0.2096   0.6327   0.3913
   1.250   1.0617   0.01106   0.00457  -0.2089   0.6211   0.3951
   1.500   1.0849   0.01113   0.00460  -0.2080   0.6080   0.3987
   1.750   1.1066   0.01119   0.00463  -0.2068   0.5924   0.4027
   2.000   1.1261   0.01135   0.00473  -0.2053   0.5739   0.4069
   2.250   1.1434   0.01162   0.00490  -0.2033   0.5549   0.4112
   2.500   1.1584   0.01193   0.00510  -0.2008   0.5379   0.4153
   2.750   1.1737   0.01225   0.00534  -0.1985   0.5238   0.4190
   3.000   1.1916   0.01257   0.00562  -0.1968   0.5119   0.4237
   3.250   1.2110   0.01292   0.00592  -0.1954   0.5015   0.4285
   3.500   1.2321   0.01323   0.00621  -0.1943   0.4932   0.4336
   3.750   1.2527   0.01356   0.00650  -0.1932   0.4855   0.4388
   4.000   1.2738   0.01387   0.00682  -0.1922   0.4791   0.4449
   4.250   1.2960   0.01415   0.00711  -0.1914   0.4731   0.4516
   4.500   1.3166   0.01449   0.00744  -0.1903   0.4672   0.4580
   4.750   1.3378   0.01482   0.00779  -0.1894   0.4622   0.4652
   5.000   1.3604   0.01508   0.00809  -0.1887   0.4578   0.4733
   5.250   1.3818   0.01538   0.00844  -0.1879   0.4531   0.4820
   5.500   1.4016   0.01579   0.00883  -0.1867   0.4482   0.4924
   5.750   1.4231   0.01610   0.00921  -0.1859   0.4441   0.5044
   6.000   1.4450   0.01639   0.00958  -0.1852   0.4402   0.5181
   6.250   1.4661   0.01672   0.00997  -0.1843   0.4363   0.5336
   6.500   1.4863   0.01712   0.01040  -0.1833   0.4325   0.5510
   6.750   1.5066   0.01754   0.01085  -0.1824   0.4287   0.5702
   7.000   1.5277   0.01784   0.01128  -0.1816   0.4254   0.5920
   7.250   1.5482   0.01818   0.01173  -0.1807   0.4214   0.6167
   7.500   1.5679   0.01857   0.01222  -0.1798   0.4173   0.6469
   7.750   1.5871   0.01896   0.01279  -0.1788   0.4131   0.7146
   8.000   1.5996   0.01900   0.01321  -0.1762   0.4098   1.0000
   8.250   1.6189   0.01945   0.01371  -0.1752   0.4061   1.0000
   8.500   1.6370   0.01997   0.01426  -0.1741   0.4019   1.0000
   8.750   1.6533   0.02059   0.01487  -0.1727   0.3975   1.0000
   9.000   1.6695   0.02123   0.01551  -0.1713   0.3925   1.0000
   9.250   1.6853   0.02187   0.01622  -0.1700   0.3864   1.0000
   9.500   1.6970   0.02275   0.01707  -0.1681   0.3790   1.0000
   9.750   1.7109   0.02355   0.01792  -0.1665   0.3712   1.0000
  10.000   1.7212   0.02457   0.01893  -0.1646   0.3621   1.0000
  10.250   1.7339   0.02551   0.01991  -0.1631   0.3526   1.0000
  10.500   1.7423   0.02676   0.02114  -0.1611   0.3418   1.0000
  10.750   1.7498   0.02814   0.02249  -0.1591   0.3280   1.0000
  11.000   1.7551   0.02974   0.02405  -0.1570   0.3118   1.0000
  11.250   1.7573   0.03163   0.02588  -0.1547   0.2932   1.0000
  11.500   1.7564   0.03383   0.02799  -0.1522   0.2753   1.0000
  11.750   1.7559   0.03605   0.03016  -0.1498   0.2619   1.0000
  12.000   1.7571   0.03819   0.03226  -0.1477   0.2516   1.0000
  12.250   1.7618   0.04007   0.03414  -0.1460   0.2439   1.0000
  12.500   1.7637   0.04223   0.03629  -0.1442   0.2367   1.0000
  12.750   1.7686   0.04414   0.03822  -0.1426   0.2307   1.0000
  13.000   1.7739   0.04604   0.04015  -0.1412   0.2253   1.0000
  13.250   1.7755   0.04831   0.04242  -0.1395   0.2201   1.0000
  13.500   1.7823   0.05012   0.04428  -0.1383   0.2157   1.0000
  13.750   1.7890   0.05196   0.04618  -0.1371   0.2114   1.0000
  14.000   1.7922   0.05415   0.04838  -0.1358   0.2073   1.0000
  14.250   1.7921   0.05668   0.05093  -0.1343   0.2027   1.0000
  14.500   1.8014   0.05834   0.05268  -0.1334   0.1988   1.0000
  14.750   1.8059   0.06048   0.05487  -0.1324   0.1940   1.0000
  15.000   1.8041   0.06332   0.05772  -0.1311   0.1888   1.0000
  15.250   1.8103   0.06536   0.05983  -0.1302   0.1836   1.0000
  15.500   1.8115   0.06796   0.06247  -0.1292   0.1775   1.0000
  15.750   1.8096   0.07091   0.06546  -0.1282   0.1718   1.0000
  16.000   1.8117   0.07348   0.06808  -0.1274   0.1640   1.0000
  16.250   1.8067   0.07693   0.07153  -0.1265   0.1553   1.0000
  16.500   1.7976   0.08091   0.07550  -0.1256   0.1439   1.0000
  16.750   1.7832   0.08558   0.08014  -0.1247   0.1300   1.0000
  17.000   1.7642   0.09090   0.08542  -0.1240   0.1157   1.0000
  17.250   1.7427   0.09666   0.09114  -0.1235   0.1008   1.0000
  17.500   1.7144   0.10341   0.09780  -0.1232   0.0776   1.0000
  17.750   1.6839   0.11058   0.10488  -0.1234   0.0586   1.0000
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