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GOE 229 (MVA H.39) AIRFOIL (goe229-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 229 (MVA H.39) AIRFOIL (goe229-il)
Reynolds number: 200,000
Max Cl/Cd: 40.89 at α=-0.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe229-il-200000-n5.txt
Download as CSV file: xf-goe229-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 229 (MVA H.39) AIRFOIL                      
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.2657   0.08138   0.07768  -0.1070   0.9486   0.0196
 -12.750  -0.3119   0.06818   0.06415  -0.1175   0.9407   0.0193
 -12.500  -0.3338   0.06131   0.05706  -0.1229   0.9291   0.0194
 -12.250  -0.3478   0.05596   0.05149  -0.1270   0.9179   0.0195
 -12.000  -0.3577   0.05151   0.04681  -0.1302   0.9067   0.0198
 -11.750  -0.3648   0.04779   0.04288  -0.1327   0.8942   0.0201
 -11.500  -0.3692   0.04437   0.03922  -0.1351   0.8834   0.0206
 -11.250  -0.3716   0.04115   0.03573  -0.1373   0.8734   0.0213
 -11.000  -0.3732   0.03822   0.03248  -0.1395   0.8630   0.0219
 -10.750  -0.3679   0.03587   0.02987  -0.1414   0.8551   0.0225
 -10.500  -0.3533   0.03433   0.02829  -0.1426   0.8467   0.0230
 -10.250  -0.3360   0.03282   0.02666  -0.1443   0.8398   0.0236
 -10.000  -0.3181   0.03145   0.02516  -0.1453   0.8327   0.0243
  -9.750  -0.2991   0.03014   0.02369  -0.1460   0.8256   0.0251
  -9.500  -0.2783   0.02894   0.02229  -0.1467   0.8195   0.0263
  -9.250  -0.2572   0.02790   0.02104  -0.1474   0.8119   0.0276
  -9.000  -0.2350   0.02675   0.01972  -0.1477   0.8056   0.0287
  -8.750  -0.2137   0.02569   0.01867  -0.1475   0.7990   0.0297
  -8.500  -0.1909   0.02482   0.01776  -0.1477   0.7924   0.0307
  -8.000  -0.1427   0.02331   0.01608  -0.1482   0.7798   0.0337
  -7.750  -0.1176   0.02265   0.01529  -0.1485   0.7732   0.0350
  -7.500  -0.0920   0.02205   0.01457  -0.1488   0.7668   0.0359
  -7.250  -0.0698   0.02100   0.01355  -0.1488   0.7594   0.0375
  -7.000  -0.0440   0.02023   0.01273  -0.1495   0.7533   0.0393
  -6.750  -0.0182   0.01959   0.01205  -0.1501   0.7462   0.0409
  -6.500   0.0088   0.01897   0.01134  -0.1508   0.7395   0.0423
  -6.250   0.0366   0.01841   0.01068  -0.1515   0.7334   0.0438
  -6.000   0.0641   0.01796   0.01013  -0.1522   0.7261   0.0454
  -5.750   0.0926   0.01732   0.00935  -0.1532   0.7196   0.0474
  -5.500   0.1207   0.01681   0.00875  -0.1540   0.7119   0.0494
  -5.250   0.1492   0.01640   0.00821  -0.1546   0.7034   0.0517
  -5.000   0.1771   0.01608   0.00777  -0.1550   0.6938   0.0547
  -4.750   0.2055   0.01577   0.00732  -0.1554   0.6842   0.0603
  -4.500   0.2333   0.01517   0.00687  -0.1562   0.6732   0.0987
  -4.250   0.2617   0.01400   0.00619  -0.1578   0.6629   0.2432
  -4.000   0.2894   0.01379   0.00615  -0.1582   0.6523   0.3130
  -3.750   0.3173   0.01382   0.00615  -0.1583   0.6427   0.3445
  -3.500   0.3452   0.01390   0.00611  -0.1583   0.6333   0.3612
  -3.250   0.3726   0.01400   0.00615  -0.1582   0.6222   0.3753
  -3.000   0.3995   0.01412   0.00618  -0.1580   0.6104   0.3861
  -2.750   0.4264   0.01425   0.00614  -0.1579   0.5982   0.3969
  -2.500   0.4526   0.01437   0.00619  -0.1576   0.5851   0.4035
  -2.250   0.4787   0.01454   0.00618  -0.1573   0.5699   0.4134
  -2.000   0.5029   0.01478   0.00635  -0.1566   0.5524   0.4223
  -1.750   0.5280   0.01501   0.00637  -0.1562   0.5361   0.4309
  -1.500   0.5528   0.01516   0.00647  -0.1557   0.5229   0.4356
  -1.250   0.5773   0.01533   0.00652  -0.1552   0.5086   0.4393
  -1.000   0.6008   0.01551   0.00655  -0.1545   0.4893   0.4427
  -0.750   0.6235   0.01574   0.00659  -0.1538   0.4658   0.4464
  -0.500   0.6459   0.01598   0.00664  -0.1530   0.4424   0.4496
  -0.250   0.6661   0.01629   0.00678  -0.1519   0.4080   0.4520
   0.250   0.6672   0.01913   0.00837  -0.1436   0.1973   0.4564
   0.750   0.6878   0.02062   0.00940  -0.1384   0.1088   0.4626
   1.000   0.7075   0.02101   0.00972  -0.1374   0.1036   0.4659
   1.250   0.7289   0.02132   0.01004  -0.1367   0.1008   0.4684
   1.500   0.7500   0.02166   0.01039  -0.1359   0.0983   0.4711
   1.750   0.7707   0.02205   0.01078  -0.1351   0.0960   0.4744
   2.000   0.7904   0.02249   0.01121  -0.1343   0.0935   0.4781
   2.250   0.8092   0.02300   0.01168  -0.1333   0.0909   0.4818
   2.500   0.8298   0.02340   0.01206  -0.1326   0.0889   0.4850
   2.750   0.8498   0.02381   0.01251  -0.1319   0.0862   0.4878
   3.000   0.8691   0.02429   0.01301  -0.1310   0.0836   0.4910
   3.250   0.8883   0.02479   0.01352  -0.1302   0.0819   0.4947
   3.500   0.9064   0.02538   0.01411  -0.1293   0.0637   0.4988
   3.750   0.9199   0.02627   0.01490  -0.1280   0.0607   0.5027
   4.000   0.9370   0.02692   0.01562  -0.1270   0.0597   0.5062
   4.250   0.9537   0.02763   0.01637  -0.1261   0.0591   0.5100
   4.500   0.9703   0.02836   0.01716  -0.1251   0.0586   0.5141
   4.750   0.9866   0.02915   0.01798  -0.1242   0.0582   0.5184
   5.000   1.0022   0.02998   0.01888  -0.1233   0.0579   0.5223
   5.250   1.0172   0.03088   0.01987  -0.1223   0.0575   0.5264
   5.500   1.0315   0.03185   0.02091  -0.1213   0.0571   0.5314
   5.750   1.0453   0.03290   0.02203  -0.1204   0.0566   0.5368
   6.000   1.0583   0.03401   0.02324  -0.1194   0.0562   0.5417
   6.250   1.0706   0.03520   0.02453  -0.1183   0.0559   0.5471
   6.500   1.0825   0.03646   0.02587  -0.1173   0.0556   0.5531
   6.750   1.0952   0.03766   0.02716  -0.1165   0.0554   0.5587
   7.000   1.1077   0.03890   0.02849  -0.1156   0.0554   0.5649
   7.250   1.1196   0.04022   0.02990  -0.1148   0.0553   0.5719
   7.500   1.1311   0.04159   0.03137  -0.1140   0.0552   0.5790
   7.750   1.1423   0.04302   0.03290  -0.1132   0.0552   0.5874
   8.000   1.1530   0.04453   0.03451  -0.1124   0.0551   0.5963
   8.250   1.1636   0.04608   0.03616  -0.1117   0.0551   0.6064
   8.500   1.1736   0.04771   0.03791  -0.1110   0.0551   0.6167
   8.750   1.1832   0.04940   0.03970  -0.1104   0.0551   0.6282
   9.000   1.1925   0.05115   0.04156  -0.1097   0.0550   0.6396
   9.250   1.2008   0.05304   0.04356  -0.1091   0.0546   0.6517
   9.500   1.2073   0.05515   0.04579  -0.1084   0.0538   0.6646
   9.750   1.2109   0.05761   0.04838  -0.1077   0.0528   0.6782
  10.000   1.2105   0.06056   0.05150  -0.1069   0.0520   0.6921
  10.250   1.2184   0.06260   0.05368  -0.1064   0.0512   0.7107
  10.500   1.2254   0.06473   0.05599  -0.1060   0.0505   0.7362
  10.750   1.2258   0.06661   0.05826  -0.1045   0.0498   0.9172
  11.000   1.2280   0.06930   0.06104  -0.1040   0.0490   1.0000
  11.250   1.2276   0.07253   0.06436  -0.1037   0.0481   1.0000
  11.500   1.2345   0.07489   0.06681  -0.1035   0.0468   1.0000
  11.750   1.2403   0.07739   0.06939  -0.1034   0.0456   1.0000
  12.000   1.2434   0.08027   0.07235  -0.1033   0.0447   1.0000
  12.250   1.2442   0.08348   0.07565  -0.1032   0.0439   1.0000
  12.500   1.2530   0.08562   0.07787  -0.1032   0.0426   1.0000
  12.750   1.2601   0.08799   0.08031  -0.1032   0.0410   1.0000
  13.000   1.2639   0.09084   0.08324  -0.1032   0.0396   1.0000
  13.250   1.2757   0.09258   0.08506  -0.1033   0.0376   1.0000
  13.500   1.2839   0.09483   0.08738  -0.1034   0.0357   1.0000
  13.750   1.2934   0.09690   0.08952  -0.1035   0.0333   1.0000
  14.000   1.3017   0.09913   0.09186  -0.1036   0.0296   1.0000
  14.250   1.3132   0.10089   0.09355  -0.1038   0.0172   1.0000
  14.500   1.3169   0.10375   0.09637  -0.1041   0.0155   1.0000
  14.750   1.3181   0.10697   0.09966  -0.1044   0.0148   1.0000
  15.000   1.3185   0.11035   0.10314  -0.1048   0.0143   1.0000
  15.250   1.3188   0.11378   0.10665  -0.1053   0.0139   1.0000
  15.500   1.3180   0.11741   0.11036  -0.1059   0.0135   1.0000
  15.750   1.3170   0.12110   0.11415  -0.1066   0.0132   1.0000
  16.000   1.3160   0.12483   0.11797  -0.1075   0.0129   1.0000
  16.250   1.3152   0.12857   0.12182  -0.1084   0.0126   1.0000
  16.500   1.3136   0.13245   0.12581  -0.1095   0.0124   1.0000
  16.750   1.3110   0.13659   0.13006  -0.1107   0.0120   1.0000
  17.000   1.3078   0.14087   0.13446  -0.1122   0.0117   1.0000
  17.250   1.3037   0.14536   0.13906  -0.1138   0.0115   1.0000
  17.500   1.2985   0.15012   0.14393  -0.1157   0.0112   1.0000
  17.750   1.2935   0.15495   0.14889  -0.1178   0.0111   1.0000
  18.000   1.2875   0.16000   0.15404  -0.1200   0.0109   1.0000
  18.250   1.2817   0.16508   0.15923  -0.1225   0.0108   1.0000
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