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GOE 223 (MVA H.34) AIRFOIL (goe223-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 223 (MVA H.34) AIRFOIL (goe223-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.41 at α=0.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe223-il-1000000-n5.txt
Download as CSV file: xf-goe223-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 223 (MVA H.34) 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
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.7580   0.10450   0.10197  -0.0697   1.0000   0.0114
 -18.750  -0.7762   0.09765   0.09501  -0.0737   1.0000   0.0115
 -18.500  -0.7892   0.09162   0.08886  -0.0777   0.9880   0.0116
 -18.250  -0.7980   0.08627   0.08340  -0.0813   0.9784   0.0117
 -18.000  -0.8057   0.08153   0.07856  -0.0840   0.9692   0.0118
 -17.750  -0.8134   0.07725   0.07417  -0.0861   0.9599   0.0119
 -17.500  -0.8198   0.07315   0.06998  -0.0881   0.9516   0.0121
 -17.250  -0.8232   0.06965   0.06640  -0.0897   0.9431   0.0123
 -17.000  -0.8243   0.06627   0.06295  -0.0914   0.9349   0.0124
 -16.750  -0.8247   0.06308   0.05968  -0.0930   0.9269   0.0126
 -16.500  -0.8222   0.06024   0.05677  -0.0944   0.9176   0.0128
 -16.250  -0.8200   0.05739   0.05385  -0.0959   0.9075   0.0130
 -16.000  -0.8165   0.05479   0.05115  -0.0972   0.8951   0.0132
 -15.750  -0.8128   0.05222   0.04848  -0.0985   0.8811   0.0134
 -15.500  -0.8080   0.04977   0.04592  -0.0998   0.8677   0.0136
 -15.250  -0.8029   0.04740   0.04344  -0.1012   0.8564   0.0139
 -15.000  -0.7975   0.04507   0.04100  -0.1025   0.8468   0.0141
 -14.750  -0.7917   0.04286   0.03871  -0.1038   0.8386   0.0143
 -14.500  -0.7860   0.04066   0.03640  -0.1052   0.8310   0.0146
 -14.250  -0.7785   0.03860   0.03425  -0.1065   0.8241   0.0148
 -14.000  -0.7704   0.03656   0.03213  -0.1079   0.8166   0.0150
 -13.750  -0.7593   0.03474   0.03027  -0.1093   0.8100   0.0152
 -13.500  -0.7462   0.03309   0.02856  -0.1107   0.8034   0.0155
 -13.250  -0.7323   0.03148   0.02690  -0.1121   0.7980   0.0157
 -13.000  -0.7176   0.02989   0.02527  -0.1137   0.7939   0.0160
 -12.750  -0.7039   0.02835   0.02368  -0.1152   0.7894   0.0162
 -12.500  -0.6846   0.02684   0.02210  -0.1174   0.7850   0.0165
 -12.000  -0.6399   0.02394   0.01906  -0.1227   0.7758   0.0172
 -11.750  -0.6146   0.02260   0.01764  -0.1255   0.7711   0.0175
 -11.500  -0.5877   0.02140   0.01634  -0.1282   0.7666   0.0179
 -11.250  -0.5594   0.02033   0.01518  -0.1309   0.7622   0.0181
 -11.000  -0.5305   0.01916   0.01396  -0.1338   0.7577   0.0185
 -10.750  -0.5019   0.01847   0.01323  -0.1355   0.7527   0.0188
 -10.500  -0.4738   0.01794   0.01263  -0.1368   0.7477   0.0191
 -10.250  -0.4455   0.01744   0.01209  -0.1379   0.7432   0.0194
 -10.000  -0.4170   0.01699   0.01160  -0.1389   0.7381   0.0198
  -9.750  -0.3886   0.01657   0.01113  -0.1398   0.7331   0.0202
  -9.500  -0.3603   0.01613   0.01062  -0.1407   0.7286   0.0206
  -9.250  -0.3317   0.01566   0.01010  -0.1416   0.7237   0.0210
  -9.000  -0.3032   0.01525   0.00962  -0.1423   0.7175   0.0213
  -8.750  -0.2746   0.01493   0.00923  -0.1430   0.7113   0.0217
  -8.500  -0.2456   0.01462   0.00886  -0.1437   0.7044   0.0219
  -8.250  -0.2175   0.01399   0.00818  -0.1446   0.6971   0.0223
  -8.000  -0.1887   0.01356   0.00770  -0.1454   0.6898   0.0227
  -7.750  -0.1599   0.01325   0.00734  -0.1460   0.6806   0.0230
  -7.500  -0.1309   0.01298   0.00702  -0.1467   0.6707   0.0235
  -7.250  -0.1021   0.01272   0.00669  -0.1472   0.6589   0.0239
  -7.000  -0.0735   0.01247   0.00635  -0.1477   0.6438   0.0242
  -6.750  -0.0452   0.01226   0.00603  -0.1482   0.6233   0.0246
  -6.500  -0.0174   0.01212   0.00574  -0.1485   0.5971   0.0249
  -6.250   0.0102   0.01205   0.00552  -0.1488   0.5688   0.0254
  -6.000   0.0380   0.01198   0.00532  -0.1491   0.5483   0.0257
  -5.750   0.0666   0.01185   0.00509  -0.1495   0.5353   0.0260
  -5.500   0.0956   0.01170   0.00488  -0.1499   0.5271   0.0262
  -5.250   0.1245   0.01155   0.00466  -0.1504   0.5183   0.0264
  -5.000   0.1536   0.01131   0.00433  -0.1510   0.5101   0.0269
  -4.750   0.1826   0.01115   0.00411  -0.1514   0.5021   0.0274
  -4.500   0.2117   0.01103   0.00394  -0.1519   0.4963   0.0279
  -4.250   0.2412   0.01090   0.00378  -0.1523   0.4922   0.0285
  -4.000   0.2705   0.01080   0.00364  -0.1528   0.4878   0.0291
  -3.750   0.2996   0.01073   0.00353  -0.1532   0.4830   0.0296
  -3.500   0.3288   0.01066   0.00342  -0.1535   0.4785   0.0301
  -3.250   0.3583   0.01058   0.00331  -0.1540   0.4744   0.0306
  -3.000   0.3875   0.01053   0.00322  -0.1543   0.4697   0.0311
  -2.750   0.4164   0.01051   0.00316  -0.1547   0.4648   0.0316
  -2.500   0.4456   0.01046   0.00308  -0.1550   0.4608   0.0327
  -2.250   0.4750   0.01041   0.00301  -0.1554   0.4572   0.0341
  -2.000   0.5041   0.01038   0.00296  -0.1558   0.4529   0.0358
  -1.750   0.5329   0.01036   0.00292  -0.1561   0.4483   0.0408
  -1.500   0.5624   0.01011   0.00282  -0.1568   0.4445   0.1071
  -1.250   0.5929   0.00938   0.00257  -0.1581   0.4409   0.2804
  -1.000   0.6219   0.00930   0.00259  -0.1586   0.4363   0.3208
  -0.750   0.6505   0.00934   0.00264  -0.1588   0.4311   0.3361
  -0.500   0.6791   0.00940   0.00269  -0.1591   0.4266   0.3461
  -0.250   0.7077   0.00945   0.00274  -0.1593   0.4210   0.3555
   0.000   0.7357   0.00955   0.00280  -0.1595   0.4138   0.3623
   0.250   0.7637   0.00964   0.00288  -0.1596   0.4056   0.3707
   0.500   0.7904   0.00983   0.00298  -0.1596   0.3900   0.3768
   0.750   0.8149   0.01015   0.00316  -0.1592   0.3628   0.3820
   1.000   0.8248   0.01146   0.00390  -0.1564   0.2550   0.3858
   1.250   0.8463   0.01197   0.00424  -0.1556   0.2232   0.3911
   1.500   0.8712   0.01223   0.00445  -0.1552   0.2123   0.3969
   1.750   0.8967   0.01243   0.00462  -0.1550   0.2049   0.4015
   2.000   0.9223   0.01262   0.00479  -0.1547   0.1999   0.4041
   2.250   0.9472   0.01285   0.00498  -0.1544   0.1945   0.4067
   2.500   0.9724   0.01304   0.00515  -0.1541   0.1901   0.4093
   3.000   1.0217   0.01346   0.00553  -0.1533   0.1805   0.4149
   3.250   1.0450   0.01371   0.00575  -0.1528   0.1745   0.4179
   3.500   1.0635   0.01410   0.00606  -0.1513   0.1566   0.4208
   3.750   1.0726   0.01490   0.00667  -0.1484   0.1155   0.4233
   4.000   1.0939   0.01524   0.00700  -0.1475   0.1119   0.4262
   4.250   1.1153   0.01559   0.00733  -0.1467   0.1088   0.4289
   4.500   1.1368   0.01592   0.00768  -0.1459   0.1061   0.4329
   4.750   1.1585   0.01624   0.00802  -0.1452   0.1046   0.4367
   5.000   1.1800   0.01657   0.00837  -0.1445   0.1040   0.4404
   5.250   1.2012   0.01692   0.00874  -0.1437   0.1035   0.4438
   5.750   1.2424   0.01770   0.00956  -0.1421   0.1024   0.4511
   6.000   1.2625   0.01812   0.01002  -0.1413   0.1020   0.4556
   6.250   1.2823   0.01856   0.01049  -0.1404   0.1016   0.4603
   6.500   1.3014   0.01905   0.01100  -0.1395   0.1010   0.4647
   6.750   1.3194   0.01962   0.01160  -0.1385   0.0997   0.4703
   7.000   1.3367   0.02024   0.01225  -0.1374   0.0983   0.4757
   7.250   1.3540   0.02087   0.01290  -0.1364   0.0973   0.4807
   7.500   1.3708   0.02154   0.01362  -0.1354   0.0961   0.4861
   7.750   1.3877   0.02223   0.01435  -0.1344   0.0952   0.4923
   8.000   1.4036   0.02300   0.01516  -0.1333   0.0941   0.4983
   8.250   1.4193   0.02379   0.01600  -0.1323   0.0930   0.5049
   8.500   1.4367   0.02448   0.01675  -0.1315   0.0928   0.5129
   8.750   1.4542   0.02518   0.01750  -0.1308   0.0922   0.5216
   9.000   1.4709   0.02595   0.01833  -0.1300   0.0914   0.5320
   9.250   1.4868   0.02677   0.01922  -0.1291   0.0902   0.5430
   9.500   1.5016   0.02770   0.02020  -0.1282   0.0887   0.5544
   9.750   1.5150   0.02874   0.02129  -0.1272   0.0867   0.5673
  10.000   1.5262   0.02997   0.02256  -0.1260   0.0838   0.5811
  10.250   1.5387   0.03111   0.02376  -0.1250   0.0813   0.5961
  10.500   1.5324   0.03378   0.02627  -0.1226   0.0519   0.6080
  10.750   1.5099   0.03806   0.03050  -0.1192   0.0185   0.6172
  11.000   1.5135   0.04017   0.03267  -0.1178   0.0143   0.6311
  11.250   1.5205   0.04202   0.03460  -0.1169   0.0130   0.6455
  11.500   1.5268   0.04400   0.03665  -0.1159   0.0122   0.6597
  11.750   1.5327   0.04605   0.03878  -0.1150   0.0115   0.6733
  12.000   1.5380   0.04820   0.04101  -0.1141   0.0108   0.6867
  12.250   1.5438   0.05034   0.04324  -0.1134   0.0105   0.7007
  12.500   1.5491   0.05257   0.04558  -0.1127   0.0101   0.7176
  12.750   1.5541   0.05489   0.04802  -0.1121   0.0096   0.7456
  13.000   1.5561   0.05693   0.05049  -0.1110   0.0092   1.0000
  13.250   1.5582   0.05962   0.05324  -0.1104   0.0088   1.0000
  13.500   1.5592   0.06246   0.05614  -0.1098   0.0085   1.0000
  13.750   1.5621   0.06514   0.05888  -0.1093   0.0083   1.0000
  14.000   1.5649   0.06785   0.06165  -0.1089   0.0081   1.0000
  14.250   1.5667   0.07071   0.06457  -0.1086   0.0079   1.0000
  14.500   1.5680   0.07361   0.06753  -0.1082   0.0077   1.0000
  14.750   1.5694   0.07651   0.07049  -0.1079   0.0074   1.0000
  15.000   1.5698   0.07956   0.07360  -0.1077   0.0072   1.0000
  15.250   1.5700   0.08266   0.07676  -0.1075   0.0071   1.0000
  15.500   1.5703   0.08575   0.07990  -0.1073   0.0069   1.0000
  15.750   1.5691   0.08906   0.08328  -0.1072   0.0067   1.0000
  16.000   1.5679   0.09231   0.08658  -0.1071   0.0065   1.0000
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