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GOE 222 (MVA H.33) AIRFOIL (goe222-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 222 (MVA H.33) AIRFOIL (goe222-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.01 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe222-il-1000000-n5.txt
Download as CSV file: xf-goe222-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -0.5248   0.12101   0.11855  -0.1003   0.9683   0.0175
 -19.250  -0.5437   0.11402   0.11145  -0.1042   0.9656   0.0178
 -19.000  -0.5581   0.10798   0.10531  -0.1076   0.9624   0.0181
 -18.750  -0.5684   0.10275   0.09998  -0.1105   0.9591   0.0183
 -18.500  -0.5757   0.09812   0.09526  -0.1130   0.9561   0.0185
 -18.250  -0.5826   0.09348   0.09054  -0.1157   0.9532   0.0187
 -18.000  -0.5876   0.08928   0.08626  -0.1181   0.9495   0.0188
 -17.750  -0.5924   0.08521   0.08214  -0.1204   0.9456   0.0191
 -17.500  -0.5973   0.08116   0.07801  -0.1227   0.9419   0.0192
 -17.250  -0.5985   0.07760   0.07440  -0.1249   0.9385   0.0194
 -17.000  -0.6005   0.07391   0.07067  -0.1272   0.9343   0.0196
 -16.750  -0.6002   0.07065   0.06735  -0.1291   0.9298   0.0198
 -16.500  -0.6007   0.06734   0.06397  -0.1311   0.9257   0.0200
 -16.250  -0.5986   0.06428   0.06086  -0.1330   0.9219   0.0202
 -16.000  -0.5967   0.06123   0.05775  -0.1350   0.9172   0.0204
 -15.750  -0.5936   0.05841   0.05486  -0.1368   0.9119   0.0206
 -15.500  -0.5908   0.05557   0.05194  -0.1387   0.9068   0.0209
 -15.250  -0.5864   0.05290   0.04922  -0.1405   0.9007   0.0211
 -15.000  -0.5828   0.05022   0.04645  -0.1423   0.8936   0.0213
 -14.750  -0.5776   0.04772   0.04389  -0.1440   0.8862   0.0216
 -14.500  -0.5735   0.04518   0.04125  -0.1458   0.8768   0.0218
 -14.250  -0.5686   0.04277   0.03875  -0.1476   0.8661   0.0219
 -14.000  -0.5644   0.04036   0.03623  -0.1494   0.8530   0.0221
 -13.750  -0.5598   0.03800   0.03375  -0.1512   0.8361   0.0222
 -13.500  -0.5553   0.03569   0.03129  -0.1530   0.8142   0.0223
 -13.250  -0.5563   0.03304   0.02850  -0.1550   0.7904   0.0226
 -13.000  -0.5482   0.03040   0.02572  -0.1587   0.7726   0.0228
 -12.750  -0.5334   0.02793   0.02314  -0.1629   0.7604   0.0231
 -12.500  -0.5132   0.02562   0.02075  -0.1673   0.7523   0.0234
 -12.000  -0.4630   0.02162   0.01656  -0.1760   0.7402   0.0240
 -11.750  -0.4342   0.01999   0.01483  -0.1799   0.7359   0.0243
 -11.500  -0.4049   0.01876   0.01350  -0.1829   0.7318   0.0248
 -11.250  -0.3768   0.01795   0.01261  -0.1847   0.7281   0.0251
 -11.000  -0.3488   0.01726   0.01183  -0.1862   0.7247   0.0254
 -10.750  -0.3202   0.01664   0.01114  -0.1875   0.7224   0.0257
 -10.500  -0.2915   0.01614   0.01058  -0.1886   0.7201   0.0260
 -10.250  -0.2628   0.01560   0.00999  -0.1897   0.7177   0.0263
 -10.000  -0.2343   0.01493   0.00926  -0.1910   0.7148   0.0267
  -9.750  -0.2057   0.01445   0.00872  -0.1919   0.7113   0.0271
  -9.250  -0.1479   0.01371   0.00787  -0.1935   0.7050   0.0279
  -9.000  -0.1184   0.01338   0.00751  -0.1943   0.7029   0.0284
  -8.750  -0.0889   0.01306   0.00716  -0.1950   0.7004   0.0288
  -8.500  -0.0594   0.01275   0.00681  -0.1957   0.6979   0.0292
  -8.250  -0.0299   0.01247   0.00648  -0.1964   0.6954   0.0296
  -8.000  -0.0004   0.01222   0.00617  -0.1970   0.6930   0.0299
  -7.750   0.0290   0.01199   0.00589  -0.1976   0.6905   0.0303
  -7.500   0.0584   0.01178   0.00563  -0.1982   0.6879   0.0305
  -7.250   0.0886   0.01144   0.00527  -0.1990   0.6859   0.0312
  -7.000   0.1187   0.01119   0.00500  -0.1997   0.6834   0.0319
  -6.750   0.1485   0.01099   0.00478  -0.2003   0.6806   0.0326
  -6.500   0.1784   0.01081   0.00457  -0.2008   0.6780   0.0333
  -6.250   0.2080   0.01065   0.00437  -0.2014   0.6753   0.0340
  -6.000   0.2375   0.01051   0.00419  -0.2018   0.6724   0.0346
  -5.750   0.2670   0.01039   0.00403  -0.2023   0.6695   0.0352
  -5.500   0.2973   0.01021   0.00384  -0.2029   0.6675   0.0362
  -5.250   0.3274   0.01005   0.00368  -0.2035   0.6652   0.0375
  -5.000   0.3574   0.00992   0.00354  -0.2040   0.6628   0.0389
  -4.750   0.3872   0.00981   0.00342  -0.2045   0.6599   0.0404
  -4.500   0.4167   0.00970   0.00329  -0.2050   0.6567   0.0429
  -4.250   0.4460   0.00960   0.00317  -0.2053   0.6536   0.0463
  -4.000   0.4758   0.00949   0.00305  -0.2058   0.6510   0.0514
  -3.750   0.5066   0.00915   0.00285  -0.2068   0.6483   0.0911
  -3.500   0.5367   0.00895   0.00273  -0.2074   0.6449   0.1173
  -3.250   0.5666   0.00875   0.00260  -0.2081   0.6410   0.1472
  -3.000   0.5962   0.00847   0.00247  -0.2088   0.6368   0.2001
  -2.750   0.6257   0.00835   0.00244  -0.2093   0.6329   0.2327
  -2.500   0.6552   0.00830   0.00243  -0.2097   0.6278   0.2519
  -2.250   0.6837   0.00829   0.00244  -0.2099   0.6213   0.2655
  -2.000   0.7120   0.00832   0.00244  -0.2101   0.6146   0.2745
  -1.750   0.7393   0.00837   0.00246  -0.2100   0.6027   0.2824
  -1.500   0.7648   0.00849   0.00251  -0.2096   0.5831   0.2910
  -1.000   0.8094   0.00905   0.00279  -0.2075   0.5257   0.3051
  -0.750   0.8330   0.00929   0.00292  -0.2068   0.5070   0.3089
  -0.500   0.8574   0.00950   0.00305  -0.2062   0.4925   0.3122
  -0.250   0.8818   0.00969   0.00318  -0.2057   0.4798   0.3155
   0.000   0.9056   0.00991   0.00333  -0.2050   0.4671   0.3185
   0.250   0.9304   0.01007   0.00345  -0.2045   0.4569   0.3217
   0.500   0.9545   0.01026   0.00358  -0.2038   0.4488   0.3253
   0.750   0.9793   0.01038   0.00368  -0.2033   0.4435   0.3285
   1.000   1.0027   0.01050   0.00380  -0.2025   0.4381   0.3328
   1.250   1.0247   0.01066   0.00394  -0.2015   0.4329   0.3361
   1.500   1.0484   0.01078   0.00407  -0.2008   0.4292   0.3392
   1.750   1.0729   0.01092   0.00420  -0.2002   0.4254   0.3422
   2.000   1.0974   0.01108   0.00435  -0.1997   0.4216   0.3447
   2.250   1.1212   0.01128   0.00453  -0.1991   0.4173   0.3473
   2.500   1.1451   0.01148   0.00472  -0.1985   0.4126   0.3508
   2.750   1.1698   0.01164   0.00490  -0.1981   0.4083   0.3545
   3.000   1.1937   0.01184   0.00510  -0.1975   0.4041   0.3584
   3.250   1.2170   0.01206   0.00531  -0.1968   0.4006   0.3619
   3.500   1.2400   0.01229   0.00553  -0.1961   0.3974   0.3646
   3.750   1.2641   0.01247   0.00574  -0.1957   0.3950   0.3685
   4.000   1.2883   0.01265   0.00595  -0.1952   0.3927   0.3724
   4.250   1.3119   0.01286   0.00618  -0.1946   0.3896   0.3762
   4.500   1.3347   0.01310   0.00643  -0.1939   0.3861   0.3798
   4.750   1.3569   0.01336   0.00670  -0.1932   0.3829   0.3833
   5.000   1.3782   0.01367   0.00702  -0.1923   0.3793   0.3882
   5.250   1.4012   0.01390   0.00729  -0.1917   0.3764   0.3932
   5.500   1.4239   0.01416   0.00757  -0.1910   0.3728   0.3974
   6.000   1.4664   0.01480   0.00824  -0.1893   0.3649   0.4063
   6.250   1.4866   0.01517   0.00863  -0.1883   0.3614   0.4116
   6.500   1.5087   0.01545   0.00896  -0.1876   0.3579   0.4174
   6.750   1.5297   0.01580   0.00933  -0.1868   0.3527   0.4243
   7.000   1.5471   0.01632   0.00984  -0.1854   0.3459   0.4317
   7.500   1.5838   0.01730   0.01085  -0.1830   0.3304   0.4475
   7.750   1.5981   0.01801   0.01152  -0.1813   0.3161   0.4564
   8.000   1.6065   0.01906   0.01248  -0.1787   0.2929   0.4672
   8.250   1.6086   0.02050   0.01379  -0.1754   0.2661   0.4788
   8.500   1.6136   0.02184   0.01506  -0.1725   0.2461   0.4936
   8.750   1.6204   0.02310   0.01628  -0.1700   0.2310   0.5105
   9.000   1.6281   0.02436   0.01752  -0.1678   0.2194   0.5264
   9.250   1.6413   0.02530   0.01849  -0.1663   0.2130   0.5418
   9.500   1.6520   0.02645   0.01964  -0.1645   0.2063   0.5558
   9.750   1.6653   0.02744   0.02067  -0.1632   0.2012   0.5702
  10.000   1.6789   0.02843   0.02170  -0.1619   0.1970   0.5856
  10.250   1.6914   0.02951   0.02283  -0.1605   0.1928   0.6028
  10.500   1.7029   0.03072   0.02409  -0.1592   0.1884   0.6220
  10.750   1.7180   0.03167   0.02514  -0.1583   0.1858   0.6522
  11.000   1.7309   0.03227   0.02630  -0.1569   0.1826   1.0000
  11.250   1.7426   0.03351   0.02754  -0.1557   0.1782   1.0000
  11.500   1.7510   0.03504   0.02907  -0.1541   0.1731   1.0000
  11.750   1.7628   0.03629   0.03034  -0.1530   0.1687   1.0000
  12.000   1.7701   0.03796   0.03199  -0.1515   0.1613   1.0000
  12.250   1.7774   0.03964   0.03367  -0.1500   0.1544   1.0000
  12.500   1.7804   0.04172   0.03571  -0.1482   0.1440   1.0000
  12.750   1.7782   0.04429   0.03822  -0.1462   0.1308   1.0000
  13.000   1.7742   0.04708   0.04095  -0.1441   0.1182   1.0000
  13.250   1.7692   0.05002   0.04385  -0.1420   0.1060   1.0000
  13.500   1.7595   0.05348   0.04726  -0.1398   0.0910   1.0000
  13.750   1.7321   0.05879   0.05243  -0.1366   0.0620   1.0000
  14.000   1.7198   0.06278   0.05640  -0.1347   0.0505   1.0000
  14.250   1.7164   0.06593   0.05959  -0.1334   0.0459   1.0000
  14.500   1.7171   0.06863   0.06233  -0.1323   0.0424   1.0000
  14.750   1.7140   0.07182   0.06556  -0.1312   0.0383   1.0000
  15.000   1.7113   0.07503   0.06880  -0.1303   0.0337   1.0000
  15.250   1.7041   0.07882   0.07260  -0.1293   0.0259   1.0000
  15.500   1.6915   0.08333   0.07710  -0.1283   0.0173   1.0000
  15.750   1.6877   0.08682   0.08063  -0.1276   0.0151   1.0000
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