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GOE 229 (MVA H.39) AIRFOIL (goe229-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 229 (MVA H.39) AIRFOIL (goe229-il)
Reynolds number: 1,000,000
Max Cl/Cd: 59.19 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe229-il-1000000-n5.txt
Download as CSV file: xf-goe229-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.6328   0.11346   0.11105  -0.0722   1.0000   0.0070
 -18.500  -0.6606   0.10483   0.10228  -0.0768   1.0000   0.0070
 -18.250  -0.6810   0.09770   0.09504  -0.0807   1.0000   0.0070
 -18.000  -0.6963   0.09168   0.08892  -0.0840   1.0000   0.0071
 -17.750  -0.7087   0.08625   0.08340  -0.0869   1.0000   0.0071
 -17.500  -0.7171   0.08114   0.07819  -0.0901   0.9974   0.0072
 -17.250  -0.7208   0.07617   0.07313  -0.0941   0.9909   0.0072
 -17.000  -0.7214   0.07169   0.06856  -0.0978   0.9829   0.0073
 -16.750  -0.7210   0.06764   0.06441  -0.1010   0.9724   0.0074
 -16.500  -0.7212   0.06388   0.06055  -0.1036   0.9595   0.0074
 -16.250  -0.7228   0.06045   0.05702  -0.1054   0.9451   0.0075
 -16.000  -0.7226   0.05747   0.05393  -0.1067   0.9316   0.0076
 -15.750  -0.7222   0.05455   0.05088  -0.1081   0.9194   0.0076
 -15.500  -0.7223   0.05160   0.04782  -0.1095   0.9072   0.0077
 -15.250  -0.7222   0.04863   0.04475  -0.1111   0.8964   0.0079
 -15.000  -0.7210   0.04587   0.04188  -0.1126   0.8863   0.0081
 -14.750  -0.7181   0.04331   0.03924  -0.1140   0.8761   0.0083
 -14.500  -0.7142   0.04097   0.03681  -0.1153   0.8665   0.0085
 -14.250  -0.7100   0.03868   0.03443  -0.1166   0.8564   0.0086
 -14.000  -0.7039   0.03654   0.03221  -0.1179   0.8471   0.0088
 -13.750  -0.6971   0.03449   0.03006  -0.1192   0.8373   0.0090
 -13.500  -0.6894   0.03243   0.02793  -0.1206   0.8274   0.0092
 -13.250  -0.6806   0.03047   0.02587  -0.1221   0.8177   0.0094
 -13.000  -0.6709   0.02855   0.02387  -0.1236   0.8077   0.0096
 -12.750  -0.6597   0.02669   0.02192  -0.1255   0.7991   0.0098
 -12.500  -0.6422   0.02487   0.02001  -0.1283   0.7908   0.0100
 -12.250  -0.6213   0.02315   0.01819  -0.1313   0.7835   0.0102
 -12.000  -0.5977   0.02138   0.01634  -0.1349   0.7759   0.0107
 -11.750  -0.5714   0.01984   0.01471  -0.1384   0.7694   0.0112
 -11.500  -0.5429   0.01855   0.01336  -0.1416   0.7634   0.0117
 -11.250  -0.5146   0.01759   0.01232  -0.1439   0.7569   0.0122
 -11.000  -0.4872   0.01688   0.01154  -0.1454   0.7509   0.0128
 -10.750  -0.4595   0.01626   0.01084  -0.1466   0.7444   0.0133
 -10.500  -0.4321   0.01571   0.01022  -0.1477   0.7375   0.0140
 -10.250  -0.4040   0.01528   0.00977  -0.1485   0.7316   0.0148
 -10.000  -0.3758   0.01491   0.00937  -0.1493   0.7255   0.0157
  -9.750  -0.3478   0.01456   0.00895  -0.1500   0.7195   0.0165
  -9.500  -0.3193   0.01419   0.00853  -0.1507   0.7143   0.0171
  -9.250  -0.2911   0.01384   0.00811  -0.1514   0.7062   0.0177
  -9.000  -0.2630   0.01355   0.00778  -0.1520   0.6958   0.0185
  -8.750  -0.2351   0.01335   0.00752  -0.1524   0.6841   0.0193
  -8.500  -0.2065   0.01315   0.00728  -0.1529   0.6737   0.0202
  -8.250  -0.1782   0.01296   0.00702  -0.1533   0.6648   0.0211
  -8.000  -0.1496   0.01276   0.00676  -0.1538   0.6549   0.0217
  -7.750  -0.1211   0.01258   0.00651  -0.1542   0.6454   0.0221
  -7.500  -0.0929   0.01227   0.00612  -0.1547   0.6347   0.0229
  -7.250  -0.0644   0.01203   0.00583  -0.1552   0.6238   0.0239
  -7.000  -0.0361   0.01187   0.00561  -0.1556   0.6121   0.0247
  -6.750  -0.0080   0.01173   0.00539  -0.1559   0.5985   0.0254
  -6.500   0.0204   0.01160   0.00519  -0.1563   0.5857   0.0263
  -6.250   0.0484   0.01151   0.00500  -0.1566   0.5706   0.0270
  -6.000   0.0760   0.01144   0.00483  -0.1568   0.5530   0.0276
  -5.750   0.1035   0.01143   0.00470  -0.1569   0.5346   0.0280
  -5.500   0.1313   0.01136   0.00454  -0.1571   0.5192   0.0285
  -5.250   0.1588   0.01124   0.00428  -0.1574   0.5019   0.0294
  -5.000   0.1867   0.01115   0.00409  -0.1576   0.4879   0.0305
  -4.750   0.2145   0.01110   0.00396  -0.1578   0.4728   0.0316
  -4.500   0.2417   0.01112   0.00386  -0.1579   0.4511   0.0324
  -4.250   0.2673   0.01127   0.00381  -0.1577   0.4161   0.0332
  -4.000   0.2734   0.01283   0.00444  -0.1543   0.2057   0.0338
  -3.750   0.2989   0.01300   0.00446  -0.1541   0.1767   0.0346
  -3.250   0.3494   0.01339   0.00458  -0.1536   0.0999   0.0367
  -3.000   0.3771   0.01339   0.00455  -0.1537   0.0976   0.0406
  -2.750   0.4047   0.01341   0.00454  -0.1538   0.0951   0.0453
  -2.500   0.4326   0.01322   0.00447  -0.1543   0.0916   0.0993
  -2.250   0.4604   0.01315   0.00444  -0.1545   0.0899   0.1244
  -2.000   0.4894   0.01251   0.00423  -0.1557   0.0874   0.2732
  -1.750   0.5163   0.01253   0.00430  -0.1558   0.0817   0.3098
  -1.250   0.5685   0.01282   0.00457  -0.1555   0.0535   0.3415
  -1.000   0.5951   0.01294   0.00470  -0.1554   0.0517   0.3526
  -0.750   0.6215   0.01308   0.00484  -0.1553   0.0504   0.3646
  -0.500   0.6476   0.01322   0.00498  -0.1552   0.0493   0.3718
  -0.250   0.6734   0.01339   0.00513  -0.1549   0.0483   0.3764
   0.000   0.6989   0.01357   0.00529  -0.1547   0.0475   0.3800
   0.250   0.7243   0.01373   0.00546  -0.1544   0.0468   0.3857
   0.500   0.7492   0.01392   0.00564  -0.1540   0.0461   0.3928
   0.750   0.7737   0.01412   0.00583  -0.1536   0.0454   0.3967
   1.000   0.7978   0.01431   0.00602  -0.1531   0.0448   0.3995
   1.250   0.8200   0.01452   0.00623  -0.1522   0.0442   0.4022
   1.500   0.8410   0.01474   0.00646  -0.1511   0.0436   0.4052
   1.750   0.8627   0.01496   0.00668  -0.1502   0.0432   0.4086
   2.000   0.8851   0.01522   0.00693  -0.1494   0.0427   0.4119
   2.250   0.9076   0.01550   0.00722  -0.1487   0.0422   0.4152
   2.500   0.9298   0.01579   0.00752  -0.1480   0.0418   0.4187
   2.750   0.9517   0.01611   0.00784  -0.1473   0.0414   0.4214
   3.000   0.9731   0.01644   0.00819  -0.1465   0.0410   0.4243
   3.250   0.9941   0.01680   0.00855  -0.1457   0.0407   0.4273
   3.500   1.0147   0.01718   0.00894  -0.1448   0.0404   0.4297
   3.750   1.0347   0.01759   0.00936  -0.1439   0.0401   0.4318
   4.000   1.0544   0.01803   0.00982  -0.1429   0.0399   0.4348
   4.250   1.0732   0.01852   0.01035  -0.1419   0.0396   0.4377
   4.500   1.0921   0.01902   0.01087  -0.1409   0.0394   0.4406
   4.750   1.1106   0.01955   0.01141  -0.1399   0.0393   0.4435
   5.000   1.1288   0.02011   0.01200  -0.1389   0.0392   0.4464
   5.500   1.1637   0.02135   0.01330  -0.1369   0.0389   0.4527
   5.750   1.1805   0.02204   0.01402  -0.1358   0.0388   0.4563
   6.000   1.1978   0.02271   0.01472  -0.1349   0.0384   0.4598
   6.250   1.2155   0.02336   0.01539  -0.1340   0.0377   0.4631
   6.500   1.2329   0.02405   0.01609  -0.1332   0.0371   0.4660
   6.750   1.2495   0.02480   0.01687  -0.1323   0.0367   0.4695
   7.000   1.2665   0.02554   0.01764  -0.1315   0.0362   0.4734
   7.250   1.2828   0.02635   0.01846  -0.1306   0.0358   0.4774
   7.500   1.2973   0.02729   0.01944  -0.1296   0.0354   0.4811
   8.000   1.3287   0.02905   0.02128  -0.1280   0.0341   0.4899
   8.250   1.3445   0.02994   0.02221  -0.1273   0.0332   0.4952
   8.500   1.3600   0.03088   0.02316  -0.1266   0.0323   0.5000
   8.750   1.3753   0.03182   0.02413  -0.1258   0.0309   0.5047
   9.000   1.3894   0.03288   0.02522  -0.1251   0.0276   0.5102
   9.250   1.3975   0.03445   0.02673  -0.1239   0.0124   0.5155
   9.750   1.4146   0.03769   0.03012  -0.1217   0.0103   0.5270
  10.000   1.4237   0.03929   0.03178  -0.1207   0.0097   0.5340
  10.250   1.4319   0.04102   0.03359  -0.1198   0.0092   0.5419
  10.500   1.4391   0.04289   0.03554  -0.1189   0.0087   0.5520
  10.750   1.4457   0.04485   0.03758  -0.1180   0.0082   0.5628
  11.000   1.4535   0.04671   0.03952  -0.1172   0.0079   0.5754
  11.250   1.4606   0.04867   0.04157  -0.1164   0.0075   0.5896
  11.500   1.4677   0.05066   0.04365  -0.1157   0.0072   0.6041
  11.750   1.4736   0.05282   0.04588  -0.1151   0.0069   0.6182
  12.000   1.4795   0.05498   0.04812  -0.1144   0.0066   0.6315
  12.250   1.4847   0.05727   0.05048  -0.1138   0.0064   0.6441
  12.500   1.4886   0.05970   0.05298  -0.1132   0.0061   0.6557
  12.750   1.4938   0.06202   0.05538  -0.1127   0.0060   0.6675
  13.000   1.4977   0.06453   0.05797  -0.1122   0.0059   0.6795
  13.250   1.5014   0.06709   0.06063  -0.1118   0.0057   0.6922
  13.500   1.5046   0.06973   0.06336  -0.1114   0.0055   0.7058
  13.750   1.5068   0.07253   0.06626  -0.1110   0.0054   0.7243
  14.000   1.5106   0.07509   0.06915  -0.1109   0.0052   0.8404
  14.250   1.5095   0.07771   0.07200  -0.1100   0.0051   1.0000
  14.500   1.5104   0.08070   0.07505  -0.1098   0.0049   1.0000
  14.750   1.5110   0.08375   0.07815  -0.1095   0.0048   1.0000
  15.000   1.5100   0.08705   0.08151  -0.1094   0.0046   1.0000
  15.250   1.5086   0.09036   0.08490  -0.1093   0.0045   1.0000
  15.500   1.5065   0.09383   0.08843  -0.1092   0.0044   1.0000
  15.750   1.5063   0.09704   0.09171  -0.1093   0.0043   1.0000
  16.000   1.5043   0.10057   0.09531  -0.1094   0.0043   1.0000
  16.250   1.5033   0.10395   0.09875  -0.1095   0.0042   1.0000
  16.500   1.5005   0.10762   0.10250  -0.1098   0.0041   1.0000
  16.750   1.4983   0.11117   0.10612  -0.1101   0.0040   1.0000
  17.000   1.4952   0.11492   0.10994  -0.1106   0.0040   1.0000
  17.250   1.4921   0.11869   0.11379  -0.1111   0.0039   1.0000
  17.500   1.4892   0.12247   0.11764  -0.1118   0.0038   1.0000
  17.750   1.4852   0.12646   0.12170  -0.1126   0.0038   1.0000
  18.000   1.4826   0.13025   0.12555  -0.1134   0.0037   1.0000
  18.250   1.4780   0.13438   0.12976  -0.1145   0.0036   1.0000
  18.500   1.4745   0.13835   0.13381  -0.1155   0.0036   1.0000
  18.750   1.4704   0.14246   0.13799  -0.1168   0.0035   1.0000
  19.000   1.4660   0.14670   0.14230  -0.1182   0.0035   1.0000
  19.250   1.4627   0.15076   0.14643  -0.1197   0.0034   1.0000
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