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GOE 190 (MVA MK.18) AIRFOIL (goe190-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 190 (MVA MK.18) AIRFOIL (goe190-il)
Reynolds number: 1,000,000
Max Cl/Cd: 121.32 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe190-il-1000000.txt
Download as CSV file: xf-goe190-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7401   0.08525   0.08307  -0.0552   1.0000   0.0169
 -14.500  -0.7750   0.07698   0.07467  -0.0593   1.0000   0.0169
 -14.250  -0.7942   0.07021   0.06779  -0.0640   0.9995   0.0170
 -14.000  -0.8021   0.06433   0.06180  -0.0693   0.9984   0.0171
 -13.750  -0.8084   0.05889   0.05624  -0.0746   0.9969   0.0173
 -13.500  -0.8092   0.05437   0.05162  -0.0794   0.9953   0.0174
 -13.250  -0.8179   0.04918   0.04633  -0.0852   0.9932   0.0175
 -13.000  -0.8305   0.04449   0.04157  -0.0895   0.9883   0.0179
 -12.750  -0.8156   0.04006   0.03707  -0.0974   0.9855   0.0182
 -12.500  -0.7896   0.03660   0.03354  -0.1050   0.9840   0.0187
 -12.250  -0.7607   0.03368   0.03055  -0.1118   0.9829   0.0192
 -12.000  -0.7445   0.03090   0.02768  -0.1156   0.9800   0.0195
 -11.750  -0.7222   0.02841   0.02508  -0.1196   0.9772   0.0200
 -11.500  -0.6904   0.02634   0.02289  -0.1243   0.9753   0.0206
 -11.250  -0.6550   0.02432   0.02074  -0.1293   0.9737   0.0211
 -11.000  -0.6200   0.02199   0.01832  -0.1345   0.9724   0.0220
 -10.750  -0.5846   0.02079   0.01707  -0.1379   0.9716   0.0226
 -10.500  -0.5492   0.01976   0.01598  -0.1409   0.9709   0.0233
 -10.250  -0.5130   0.01884   0.01497  -0.1437   0.9703   0.0240
 -10.000  -0.4756   0.01813   0.01416  -0.1464   0.9697   0.0247
  -9.750  -0.4556   0.01778   0.01375  -0.1451   0.9658   0.0250
  -9.500  -0.4290   0.01647   0.01238  -0.1461   0.9627   0.0262
  -9.250  -0.3946   0.01592   0.01181  -0.1479   0.9611   0.0269
  -9.000  -0.3589   0.01543   0.01127  -0.1498   0.9599   0.0277
  -8.750  -0.3225   0.01491   0.01069  -0.1518   0.9590   0.0286
  -8.500  -0.2843   0.01450   0.01023  -0.1540   0.9583   0.0294
  -8.250  -0.2476   0.01368   0.00933  -0.1563   0.9572   0.0303
  -8.000  -0.2114   0.01301   0.00865  -0.1583   0.9561   0.0314
  -7.750  -0.1766   0.01260   0.00821  -0.1598   0.9544   0.0322
  -7.500  -0.1582   0.01230   0.00789  -0.1577   0.9488   0.0330
  -7.250  -0.1269   0.01190   0.00745  -0.1583   0.9452   0.0340
  -7.000  -0.0931   0.01150   0.00700  -0.1594   0.9422   0.0347
  -6.750  -0.0609   0.01111   0.00656  -0.1602   0.9391   0.0353
  -6.500  -0.0422   0.01046   0.00587  -0.1585   0.9316   0.0367
  -6.250  -0.0122   0.01008   0.00547  -0.1588   0.9259   0.0378
  -6.000   0.0112   0.00979   0.00516  -0.1577   0.9157   0.0387
  -5.750   0.0387   0.00947   0.00479  -0.1573   0.8999   0.0397
  -5.500   0.0739   0.00918   0.00433  -0.1585   0.8563   0.0409
  -5.250   0.0986   0.00929   0.00410  -0.1575   0.7982   0.0415
  -5.000   0.1213   0.00900   0.00362  -0.1564   0.7721   0.0433
  -4.750   0.1461   0.00888   0.00339  -0.1556   0.7550   0.0448
  -4.500   0.1716   0.00879   0.00322  -0.1549   0.7412   0.0462
  -4.250   0.1973   0.00873   0.00307  -0.1543   0.7278   0.0479
  -4.000   0.2229   0.00872   0.00297  -0.1536   0.7140   0.0491
  -3.750   0.2484   0.00850   0.00266  -0.1529   0.7007   0.0524
  -3.500   0.2748   0.00838   0.00250  -0.1524   0.6889   0.0551
  -3.250   0.3011   0.00833   0.00237  -0.1518   0.6768   0.0577
  -3.000   0.3269   0.00821   0.00219  -0.1512   0.6620   0.0628
  -2.750   0.3526   0.00813   0.00205  -0.1506   0.6447   0.0687
  -2.500   0.3769   0.00780   0.00179  -0.1498   0.6211   0.1234
  -2.250   0.3994   0.00739   0.00162  -0.1489   0.5924   0.2414
  -2.000   0.4242   0.00750   0.00164  -0.1480   0.5687   0.2605
  -1.750   0.4501   0.00761   0.00168  -0.1474   0.5536   0.2724
  -1.500   0.4766   0.00768   0.00172  -0.1469   0.5433   0.2809
  -1.250   0.5031   0.00779   0.00176  -0.1464   0.5345   0.2874
  -1.000   0.5301   0.00785   0.00179  -0.1460   0.5276   0.2923
  -0.750   0.5570   0.00792   0.00184  -0.1455   0.5210   0.2985
  -0.500   0.5835   0.00803   0.00190  -0.1450   0.5148   0.3037
  -0.250   0.6111   0.00808   0.00193  -0.1447   0.5104   0.3083
   0.000   0.6380   0.00811   0.00198  -0.1443   0.5057   0.3134
   0.250   0.6647   0.00820   0.00204  -0.1439   0.5007   0.3173
   0.500   0.6917   0.00828   0.00210  -0.1435   0.4962   0.3212
   0.750   0.7190   0.00832   0.00213  -0.1431   0.4918   0.3246
   1.000   0.7457   0.00835   0.00217  -0.1427   0.4870   0.3288
   1.250   0.7720   0.00843   0.00223  -0.1422   0.4821   0.3315
   1.500   0.7991   0.00847   0.00228  -0.1418   0.4781   0.3342
   1.750   0.8262   0.00851   0.00232  -0.1415   0.4731   0.3369
   2.000   0.8524   0.00860   0.00237  -0.1409   0.4668   0.3392
   2.250   0.8789   0.00865   0.00242  -0.1405   0.4612   0.3424
   2.500   0.9056   0.00867   0.00248  -0.1401   0.4555   0.3462
   2.750   0.9315   0.00876   0.00255  -0.1395   0.4494   0.3498
   3.000   0.9580   0.00882   0.00262  -0.1390   0.4430   0.3532
   3.250   0.9842   0.00890   0.00269  -0.1385   0.4355   0.3560
   3.500   1.0098   0.00898   0.00277  -0.1379   0.4285   0.3599
   3.750   1.0358   0.00904   0.00285  -0.1374   0.4202   0.3641
   4.000   1.0611   0.00916   0.00295  -0.1367   0.4121   0.3681
   4.250   1.0867   0.00925   0.00305  -0.1362   0.4036   0.3719
   4.500   1.1117   0.00938   0.00316  -0.1355   0.3949   0.3759
   4.750   1.1364   0.00951   0.00329  -0.1347   0.3851   0.3807
   5.000   1.1611   0.00965   0.00343  -0.1340   0.3753   0.3858
   5.250   1.1849   0.00984   0.00358  -0.1331   0.3641   0.3901
   5.500   1.2090   0.01000   0.00374  -0.1323   0.3546   0.3952
   5.750   1.2328   0.01017   0.00391  -0.1314   0.3459   0.4004
   6.000   1.2561   0.01038   0.00409  -0.1304   0.3364   0.4054
   6.250   1.2798   0.01055   0.00427  -0.1295   0.3277   0.4104
   6.500   1.3024   0.01077   0.00448  -0.1285   0.3195   0.4158
   6.750   1.3260   0.01093   0.00467  -0.1276   0.3119   0.4212
   7.000   1.3473   0.01119   0.00490  -0.1262   0.3025   0.4265
   7.250   1.3700   0.01133   0.00508  -0.1252   0.2956   0.4326
   7.500   1.3902   0.01159   0.00532  -0.1236   0.2867   0.4381
   7.750   1.4120   0.01175   0.00551  -0.1224   0.2784   0.4437
   8.000   1.4320   0.01202   0.00577  -0.1209   0.2672   0.4492
   8.250   1.4511   0.01234   0.00605  -0.1192   0.2535   0.4549
   8.500   1.4692   0.01270   0.00636  -0.1174   0.2369   0.4602
   8.750   1.4864   0.01311   0.00671  -0.1155   0.2190   0.4661
   9.000   1.5014   0.01364   0.00714  -0.1132   0.1987   0.4719
   9.250   1.5150   0.01421   0.00762  -0.1107   0.1801   0.4780
   9.500   1.5295   0.01473   0.00810  -0.1084   0.1666   0.4844
   9.750   1.5455   0.01516   0.00852  -0.1064   0.1571   0.4905
  10.000   1.5609   0.01561   0.00898  -0.1043   0.1483   0.4975
  10.250   1.5747   0.01615   0.00949  -0.1019   0.1383   0.5047
  10.500   1.5894   0.01662   0.00998  -0.0998   0.1284   0.5142
  10.750   1.6011   0.01725   0.01057  -0.0972   0.1156   0.5244
  11.000   1.6102   0.01801   0.01128  -0.0944   0.1007   0.5392
  11.250   1.6175   0.01882   0.01209  -0.0913   0.0878   0.5718
  11.500   1.6696   0.01969   0.01351  -0.0983   0.0724   1.0000
  11.750   1.6786   0.02060   0.01439  -0.0957   0.0657   1.0000
  12.000   1.6899   0.02141   0.01521  -0.0935   0.0604   1.0000
  12.250   1.6976   0.02244   0.01623  -0.0910   0.0542   1.0000
  12.500   1.7038   0.02361   0.01738  -0.0884   0.0474   1.0000
  12.750   1.7089   0.02490   0.01866  -0.0859   0.0407   1.0000
  13.000   1.7122   0.02639   0.02014  -0.0834   0.0343   1.0000
  13.250   1.7133   0.02812   0.02186  -0.0809   0.0285   1.0000
  13.500   1.7144   0.02998   0.02374  -0.0788   0.0242   1.0000
  13.750   1.7162   0.03193   0.02573  -0.0769   0.0215   1.0000
  14.000   1.7165   0.03413   0.02797  -0.0753   0.0195   1.0000
  14.250   1.7186   0.03628   0.03019  -0.0740   0.0183   1.0000
  14.500   1.7193   0.03867   0.03265  -0.0729   0.0172   1.0000
  14.750   1.7175   0.04140   0.03544  -0.0719   0.0162   1.0000
  15.000   1.7142   0.04439   0.03851  -0.0710   0.0155   1.0000
  15.250   1.7142   0.04710   0.04131  -0.0704   0.0151   1.0000
  15.500   1.7127   0.05003   0.04433  -0.0699   0.0146   1.0000
  15.750   1.7091   0.05327   0.04766  -0.0695   0.0142   1.0000
  16.000   1.7039   0.05682   0.05129  -0.0693   0.0138   1.0000
  16.250   1.6965   0.06076   0.05532  -0.0694   0.0134   1.0000
  16.500   1.6852   0.06528   0.05995  -0.0696   0.0130   1.0000
  16.750   1.6724   0.07014   0.06491  -0.0700   0.0126   1.0000
  17.000   1.6666   0.07409   0.06896  -0.0704   0.0125   1.0000
  17.250   1.6592   0.07826   0.07322  -0.0709   0.0123   1.0000
  17.500   1.6511   0.08256   0.07762  -0.0714   0.0122   1.0000
  17.750   1.6419   0.08707   0.08223  -0.0721   0.0119   1.0000
  18.000   1.6322   0.09172   0.08698  -0.0730   0.0118   1.0000
  18.250   1.6215   0.09656   0.09191  -0.0739   0.0116   1.0000
  18.500   1.6109   0.10147   0.09692  -0.0751   0.0114   1.0000
  18.750   1.6006   0.10647   0.10201  -0.0764   0.0112   1.0000
  19.000   1.5896   0.11165   0.10729  -0.0779   0.0111   1.0000
  19.250   1.5780   0.11700   0.11272  -0.0796   0.0109   1.0000
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