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GOE 190 (MVA MK.18) AIRFOIL (goe190-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 190 (MVA MK.18) AIRFOIL (goe190-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.59 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe190-il-1000000-n5.txt
Download as CSV file: xf-goe190-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 190 (MVA MK.18) 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.6847   0.08797   0.08556  -0.0752   0.9931   0.0119
 -15.500  -0.7213   0.07790   0.07534  -0.0821   0.9918   0.0118
 -15.250  -0.7426   0.07044   0.06777  -0.0877   0.9903   0.0119
 -15.000  -0.7539   0.06449   0.06171  -0.0927   0.9888   0.0121
 -14.750  -0.7609   0.05922   0.05635  -0.0975   0.9873   0.0122
 -14.500  -0.7620   0.05461   0.05165  -0.1023   0.9859   0.0124
 -14.250  -0.7607   0.05012   0.04707  -0.1076   0.9845   0.0126
 -14.000  -0.7592   0.04627   0.04315  -0.1118   0.9823   0.0128
 -13.750  -0.7648   0.04280   0.03960  -0.1145   0.9783   0.0129
 -13.500  -0.7588   0.03836   0.03508  -0.1213   0.9753   0.0133
 -13.250  -0.7404   0.03429   0.03091  -0.1295   0.9736   0.0137
 -13.000  -0.7155   0.03066   0.02720  -0.1376   0.9724   0.0143
 -12.750  -0.6966   0.02777   0.02422  -0.1426   0.9700   0.0149
 -12.500  -0.6778   0.02539   0.02174  -0.1460   0.9670   0.0154
 -12.250  -0.6528   0.02330   0.01954  -0.1497   0.9649   0.0159
 -12.000  -0.6248   0.02141   0.01758  -0.1531   0.9629   0.0168
 -11.750  -0.5959   0.01993   0.01604  -0.1559   0.9613   0.0177
 -11.500  -0.5670   0.01868   0.01472  -0.1580   0.9600   0.0185
 -11.250  -0.5372   0.01755   0.01349  -0.1600   0.9588   0.0192
 -11.000  -0.5129   0.01656   0.01243  -0.1606   0.9566   0.0199
 -10.750  -0.4895   0.01575   0.01158  -0.1607   0.9534   0.0205
 -10.500  -0.4631   0.01513   0.01092  -0.1611   0.9506   0.0213
 -10.250  -0.4355   0.01462   0.01036  -0.1615   0.9483   0.0221
 -10.000  -0.4071   0.01413   0.00980  -0.1620   0.9462   0.0229
  -9.750  -0.3771   0.01369   0.00930  -0.1627   0.9442   0.0234
  -9.500  -0.3523   0.01317   0.00873  -0.1624   0.9413   0.0242
  -9.250  -0.3286   0.01276   0.00830  -0.1618   0.9373   0.0248
  -9.000  -0.3023   0.01240   0.00790  -0.1616   0.9332   0.0255
  -8.750  -0.2733   0.01207   0.00753  -0.1619   0.9296   0.0263
  -8.500  -0.2475   0.01175   0.00717  -0.1615   0.9243   0.0270
  -8.250  -0.2216   0.01143   0.00681  -0.1611   0.9157   0.0276
  -8.000  -0.1943   0.01115   0.00645  -0.1609   0.9025   0.0281
  -7.750  -0.1650   0.01086   0.00578  -0.1611   0.8169   0.0289
  -7.500  -0.1442   0.01083   0.00552  -0.1595   0.7732   0.0297
  -7.250  -0.1200   0.01072   0.00528  -0.1587   0.7526   0.0305
  -7.000  -0.0950   0.01057   0.00504  -0.1581   0.7378   0.0311
  -6.750  -0.0688   0.01041   0.00481  -0.1577   0.7277   0.0319
  -6.500  -0.0426   0.01025   0.00457  -0.1572   0.7193   0.0325
  -6.250  -0.0161   0.01008   0.00432  -0.1568   0.7108   0.0330
  -6.000   0.0103   0.00993   0.00410  -0.1564   0.7027   0.0334
  -5.750   0.0368   0.00971   0.00382  -0.1560   0.6940   0.0344
  -5.500   0.0631   0.00954   0.00359  -0.1556   0.6861   0.0356
  -5.250   0.0901   0.00939   0.00341  -0.1553   0.6776   0.0365
  -5.000   0.1166   0.00928   0.00323  -0.1548   0.6678   0.0375
  -4.750   0.1431   0.00918   0.00307  -0.1543   0.6552   0.0384
  -4.500   0.1693   0.00911   0.00291  -0.1538   0.6391   0.0393
  -4.250   0.1944   0.00910   0.00278  -0.1530   0.6097   0.0400
  -4.000   0.2176   0.00916   0.00262  -0.1520   0.5674   0.0420
  -3.750   0.2426   0.00919   0.00254  -0.1512   0.5427   0.0441
  -3.500   0.2689   0.00917   0.00244  -0.1507   0.5302   0.0458
  -3.250   0.2956   0.00916   0.00236  -0.1503   0.5215   0.0474
  -3.000   0.3227   0.00909   0.00226  -0.1499   0.5155   0.0500
  -2.750   0.3496   0.00904   0.00218  -0.1495   0.5094   0.0532
  -2.500   0.3765   0.00901   0.00211  -0.1491   0.5041   0.0564
  -2.250   0.4039   0.00895   0.00204  -0.1488   0.4995   0.0611
  -2.000   0.4310   0.00888   0.00197  -0.1485   0.4952   0.0689
  -1.750   0.4568   0.00848   0.00178  -0.1481   0.4911   0.1504
  -1.500   0.4827   0.00822   0.00169  -0.1477   0.4870   0.2189
  -1.250   0.5101   0.00817   0.00170  -0.1474   0.4833   0.2417
  -1.000   0.5374   0.00817   0.00171  -0.1471   0.4790   0.2550
  -0.750   0.5645   0.00820   0.00173  -0.1467   0.4748   0.2642
  -0.500   0.5915   0.00824   0.00177  -0.1463   0.4709   0.2739
  -0.250   0.6188   0.00826   0.00180  -0.1460   0.4677   0.2814
   0.000   0.6462   0.00829   0.00183  -0.1457   0.4638   0.2866
   0.250   0.6733   0.00834   0.00186  -0.1453   0.4590   0.2909
   0.500   0.7000   0.00839   0.00190  -0.1449   0.4542   0.2952
   0.750   0.7270   0.00843   0.00195  -0.1445   0.4504   0.3002
   1.000   0.7542   0.00847   0.00199  -0.1442   0.4462   0.3044
   1.250   0.7810   0.00853   0.00203  -0.1437   0.4412   0.3069
   1.500   0.8074   0.00861   0.00208  -0.1433   0.4352   0.3084
   1.750   0.8342   0.00865   0.00213  -0.1429   0.4290   0.3112
   2.000   0.8601   0.00874   0.00219  -0.1423   0.4201   0.3139
   2.250   0.8865   0.00881   0.00226  -0.1418   0.4113   0.3167
   2.500   0.9123   0.00892   0.00233  -0.1413   0.4016   0.3196
   2.750   0.9381   0.00903   0.00241  -0.1407   0.3917   0.3226
   3.000   0.9637   0.00915   0.00250  -0.1401   0.3825   0.3250
   3.500   1.0139   0.00943   0.00272  -0.1388   0.3603   0.3313
   3.750   1.0389   0.00957   0.00285  -0.1381   0.3512   0.3348
   4.000   1.0637   0.00973   0.00298  -0.1374   0.3421   0.3380
   4.250   1.0887   0.00986   0.00311  -0.1367   0.3352   0.3410
   4.500   1.1134   0.01001   0.00324  -0.1360   0.3276   0.3439
   4.750   1.1379   0.01016   0.00340  -0.1352   0.3204   0.3480
   5.000   1.1625   0.01031   0.00355  -0.1345   0.3138   0.3521
   5.250   1.1864   0.01050   0.00372  -0.1336   0.3056   0.3566
   5.750   1.2341   0.01084   0.00407  -0.1319   0.2919   0.3652
   6.000   1.2581   0.01098   0.00424  -0.1311   0.2855   0.3698
   6.250   1.2807   0.01122   0.00445  -0.1300   0.2759   0.3742
   6.500   1.3040   0.01138   0.00462  -0.1291   0.2689   0.3781
   6.750   1.3253   0.01162   0.00485  -0.1278   0.2596   0.3829
   7.000   1.3464   0.01185   0.00506  -0.1264   0.2483   0.3879
   7.250   1.3667   0.01210   0.00529  -0.1249   0.2373   0.3929
   7.500   1.3855   0.01244   0.00559  -0.1232   0.2214   0.3978
   7.750   1.4036   0.01281   0.00591  -0.1214   0.2058   0.4032
   8.000   1.4209   0.01322   0.00626  -0.1194   0.1906   0.4082
   8.250   1.4373   0.01369   0.00666  -0.1173   0.1751   0.4122
   8.500   1.4540   0.01411   0.00705  -0.1154   0.1636   0.4171
   8.750   1.4702   0.01456   0.00747  -0.1133   0.1525   0.4222
   9.000   1.4855   0.01505   0.00791  -0.1111   0.1405   0.4266
   9.250   1.5028   0.01542   0.00830  -0.1093   0.1327   0.4318
   9.500   1.5187   0.01586   0.00873  -0.1072   0.1246   0.4374
   9.750   1.5321   0.01644   0.00925  -0.1049   0.1111   0.4427
  10.000   1.5424   0.01716   0.00989  -0.1020   0.0946   0.4469
  10.250   1.5518   0.01793   0.01060  -0.0992   0.0811   0.4514
  10.500   1.5641   0.01854   0.01121  -0.0968   0.0742   0.4565
  11.000   1.5873   0.01988   0.01256  -0.0920   0.0617   0.4672
  11.250   1.5974   0.02064   0.01333  -0.0895   0.0563   0.4726
  11.500   1.6089   0.02134   0.01405  -0.0872   0.0521   0.4783
  11.750   1.6174   0.02222   0.01494  -0.0847   0.0470   0.4839
  12.000   1.6252   0.02317   0.01590  -0.0822   0.0416   0.4897
  12.250   1.6306   0.02429   0.01704  -0.0795   0.0356   0.4959
  12.500   1.6371   0.02540   0.01818  -0.0771   0.0319   0.5034
  12.750   1.6404   0.02678   0.01957  -0.0746   0.0268   0.5122
  13.250   1.6441   0.02998   0.02286  -0.0700   0.0185   0.5400
  13.500   1.6461   0.03162   0.02468  -0.0680   0.0162   0.6181
  14.000   1.7044   0.03617   0.02987  -0.0766   0.0122   1.0000
  14.250   1.7081   0.03825   0.03202  -0.0756   0.0115   1.0000
  14.500   1.7105   0.04052   0.03436  -0.0747   0.0110   1.0000
  14.750   1.7107   0.04310   0.03700  -0.0738   0.0104   1.0000
  15.000   1.7103   0.04581   0.03979  -0.0731   0.0099   1.0000
  15.250   1.7097   0.04860   0.04265  -0.0725   0.0096   1.0000
  15.500   1.7091   0.05144   0.04559  -0.0720   0.0093   1.0000
  15.750   1.7072   0.05452   0.04876  -0.0717   0.0090   1.0000
  16.000   1.7043   0.05782   0.05214  -0.0715   0.0088   1.0000
  16.250   1.6999   0.06137   0.05577  -0.0715   0.0086   1.0000
  16.500   1.6948   0.06507   0.05956  -0.0715   0.0083   1.0000
  16.750   1.6886   0.06899   0.06357  -0.0718   0.0081   1.0000
  17.000   1.6811   0.07313   0.06779  -0.0721   0.0078   1.0000
  17.250   1.6731   0.07734   0.07210  -0.0726   0.0077   1.0000
  17.500   1.6637   0.08181   0.07665  -0.0731   0.0075   1.0000
  17.750   1.6566   0.08600   0.08093  -0.0737   0.0074   1.0000
  18.000   1.6487   0.09034   0.08537  -0.0744   0.0073   1.0000
  18.250   1.6401   0.09483   0.08995  -0.0752   0.0072   1.0000
  18.500   1.6312   0.09944   0.09467  -0.0762   0.0070   1.0000
  18.750   1.6226   0.10409   0.09941  -0.0773   0.0069   1.0000
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