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MARSKE MONARCH AIRFOIL (NACA 43012A) (marske5-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MARSKE MONARCH AIRFOIL (NACA 43012A) (marske5-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.53 at α=12°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-marske5-il-1000000-n5.txt
Download as CSV file: xf-marske5-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MARSKE MONARCH AIRFOIL (NACA 43012A)            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.1652   0.04952   0.04656  -0.0473   1.0000   0.0086
 -16.250  -1.1893   0.04440   0.04124  -0.0481   1.0000   0.0086
 -16.000  -1.2091   0.04039   0.03704  -0.0471   1.0000   0.0087
 -15.750  -1.2175   0.03772   0.03421  -0.0454   1.0000   0.0087
 -15.500  -1.2270   0.03514   0.03148  -0.0430   1.0000   0.0088
 -15.250  -1.2275   0.03338   0.02960  -0.0406   1.0000   0.0089
 -15.000  -1.2269   0.03174   0.02783  -0.0380   1.0000   0.0089
 -14.750  -1.2236   0.03035   0.02634  -0.0353   1.0000   0.0090
 -14.500  -1.2190   0.02906   0.02494  -0.0325   1.0000   0.0091
 -14.250  -1.2122   0.02795   0.02374  -0.0297   1.0000   0.0092
 -14.000  -1.2041   0.02695   0.02265  -0.0269   1.0000   0.0093
 -13.750  -1.1946   0.02607   0.02169  -0.0241   1.0000   0.0094
 -13.500  -1.1854   0.02519   0.02072  -0.0212   1.0000   0.0094
 -13.250  -1.1742   0.02439   0.01985  -0.0184   1.0000   0.0096
 -13.000  -1.1606   0.02360   0.01898  -0.0160   1.0000   0.0096
 -12.750  -1.1461   0.02279   0.01808  -0.0138   1.0000   0.0097
 -12.500  -1.1299   0.02208   0.01729  -0.0117   1.0000   0.0099
 -12.250  -1.1129   0.02142   0.01656  -0.0098   1.0000   0.0100
 -12.000  -1.0960   0.02070   0.01576  -0.0078   1.0000   0.0102
 -11.750  -1.0780   0.02006   0.01505  -0.0059   1.0000   0.0103
 -11.500  -1.0597   0.01943   0.01435  -0.0040   1.0000   0.0105
 -11.250  -1.0410   0.01883   0.01368  -0.0022   1.0000   0.0106
 -11.000  -1.0217   0.01827   0.01305  -0.0004   1.0000   0.0107
 -10.750  -1.0020   0.01775   0.01247   0.0013   1.0000   0.0108
 -10.500  -0.9827   0.01717   0.01185   0.0031   1.0000   0.0111
 -10.250  -0.9627   0.01667   0.01132   0.0048   1.0000   0.0114
 -10.000  -0.9422   0.01622   0.01084   0.0064   1.0000   0.0116
  -9.750  -0.9214   0.01582   0.01042   0.0080   1.0000   0.0118
  -9.500  -0.8938   0.01536   0.00994   0.0082   0.9965   0.0120
  -9.250  -0.8624   0.01489   0.00944   0.0076   0.9817   0.0124
  -9.000  -0.7769   0.01433   0.00844  -0.0044   0.8104   0.0130
  -8.750  -0.7575   0.01415   0.00802  -0.0024   0.7589   0.0131
  -8.500  -0.7350   0.01391   0.00765  -0.0011   0.7368   0.0134
  -8.250  -0.7124   0.01359   0.00725   0.0002   0.7183   0.0138
  -8.000  -0.6887   0.01335   0.00696   0.0014   0.7026   0.0141
  -7.750  -0.6644   0.01311   0.00667   0.0024   0.6910   0.0145
  -7.500  -0.6402   0.01288   0.00639   0.0034   0.6760   0.0150
  -7.250  -0.6159   0.01266   0.00610   0.0044   0.6597   0.0154
  -7.000  -0.5917   0.01245   0.00580   0.0055   0.6379   0.0160
  -6.750  -0.5677   0.01227   0.00551   0.0066   0.6077   0.0164
  -6.500  -0.5441   0.01216   0.00527   0.0077   0.5626   0.0170
  -6.250  -0.5201   0.01210   0.00507   0.0088   0.5166   0.0175
  -6.000  -0.4962   0.01207   0.00487   0.0099   0.4639   0.0182
  -5.750  -0.4731   0.01211   0.00465   0.0110   0.3886   0.0187
  -5.500  -0.4492   0.01212   0.00445   0.0121   0.3329   0.0193
  -5.250  -0.4247   0.01201   0.00426   0.0130   0.3069   0.0199
  -4.750  -0.3734   0.01185   0.00401   0.0145   0.2798   0.0214
  -4.500  -0.3478   0.01175   0.00385   0.0153   0.2701   0.0222
  -4.250  -0.3220   0.01164   0.00369   0.0160   0.2633   0.0228
  -4.000  -0.2969   0.01149   0.00351   0.0169   0.2550   0.0235
  -3.750  -0.2709   0.01138   0.00339   0.0176   0.2493   0.0243
  -3.500  -0.2449   0.01129   0.00327   0.0183   0.2433   0.0252
  -3.250  -0.2189   0.01122   0.00316   0.0190   0.2375   0.0261
  -3.000  -0.1927   0.01114   0.00304   0.0196   0.2332   0.0267
  -2.750  -0.1672   0.01098   0.00288   0.0204   0.2291   0.0276
  -2.500  -0.1412   0.01090   0.00278   0.0211   0.2244   0.0287
  -2.250  -0.1151   0.01084   0.00268   0.0217   0.2194   0.0297
  -2.000  -0.0888   0.01076   0.00259   0.0224   0.2161   0.0305
  -1.750  -0.0625   0.01069   0.00250   0.0230   0.2126   0.0314
  -1.500  -0.0366   0.01060   0.00240   0.0237   0.2087   0.0327
  -1.250  -0.0105   0.01056   0.00233   0.0243   0.2036   0.0339
  -1.000   0.0159   0.01052   0.00227   0.0249   0.2003   0.0351
  -0.750   0.0425   0.01048   0.00222   0.0255   0.1974   0.0365
  -0.500   0.0687   0.01043   0.00217   0.0261   0.1942   0.0390
  -0.250   0.0951   0.01041   0.00214   0.0266   0.1908   0.0418
   0.000   0.1213   0.01039   0.00211   0.0272   0.1874   0.0485
   0.250   0.1464   0.01026   0.00210   0.0280   0.1854   0.0850
   0.500   0.1621   0.00946   0.00201   0.0304   0.1839   0.3260
   0.750   0.1700   0.00840   0.00185   0.0343   0.1824   0.6036
   1.000   0.1768   0.00769   0.00186   0.0391   0.1808   0.8031
   1.250   0.2002   0.00766   0.00194   0.0404   0.1787   0.8441
   1.500   0.2261   0.00771   0.00201   0.0411   0.1763   0.8617
   1.750   0.2525   0.00779   0.00208   0.0417   0.1740   0.8745
   2.000   0.2789   0.00788   0.00216   0.0423   0.1715   0.8850
   2.250   0.3063   0.00795   0.00224   0.0427   0.1706   0.8940
   2.500   0.3330   0.00803   0.00232   0.0432   0.1696   0.9028
   2.750   0.3607   0.00811   0.00241   0.0435   0.1683   0.9103
   3.000   0.3881   0.00820   0.00249   0.0438   0.1669   0.9159
   3.250   0.4150   0.00830   0.00256   0.0442   0.1653   0.9192
   3.500   0.4424   0.00840   0.00264   0.0444   0.1637   0.9221
   3.750   0.4708   0.00851   0.00273   0.0444   0.1622   0.9248
   4.000   0.4988   0.00863   0.00284   0.0445   0.1607   0.9279
   4.250   0.5261   0.00876   0.00296   0.0447   0.1591   0.9315
   4.500   0.5522   0.00890   0.00309   0.0452   0.1576   0.9353
   4.750   0.5810   0.00902   0.00321   0.0451   0.1570   0.9381
   5.000   0.6102   0.00914   0.00334   0.0448   0.1564   0.9409
   5.250   0.6387   0.00926   0.00346   0.0447   0.1557   0.9443
   5.500   0.6656   0.00938   0.00359   0.0450   0.1549   0.9484
   5.750   0.6950   0.00951   0.00373   0.0447   0.1537   0.9512
   6.000   0.7255   0.00966   0.00388   0.0441   0.1525   0.9536
   6.250   0.7553   0.00981   0.00403   0.0437   0.1513   0.9563
   6.500   0.7833   0.00996   0.00418   0.0436   0.1501   0.9597
   6.750   0.8115   0.01012   0.00434   0.0434   0.1489   0.9628
   7.000   0.8430   0.01031   0.00453   0.0426   0.1476   0.9643
   7.250   0.8740   0.01052   0.00473   0.0418   0.1461   0.9660
   7.500   0.9037   0.01076   0.00497   0.0412   0.1445   0.9681
   7.750   0.9325   0.01093   0.00517   0.0409   0.1438   0.9707
   8.000   0.9600   0.01108   0.00534   0.0408   0.1431   0.9737
   8.250   0.9922   0.01126   0.00554   0.0397   0.1423   0.9746
   8.500   1.0238   0.01144   0.00575   0.0387   0.1414   0.9757
   8.750   1.0547   0.01164   0.00597   0.0379   0.1405   0.9770
   9.000   1.0847   0.01185   0.00620   0.0372   0.1396   0.9786
   9.250   1.1136   0.01205   0.00643   0.0367   0.1385   0.9805
   9.500   1.1403   0.01227   0.00666   0.0367   0.1374   0.9832
   9.750   1.1692   0.01249   0.00691   0.0362   0.1363   0.9847
  10.000   1.1994   0.01274   0.00717   0.0353   0.1351   0.9857
  10.250   1.2290   0.01301   0.00745   0.0346   0.1337   0.9870
  10.500   1.2577   0.01332   0.00779   0.0340   0.1322   0.9885
  10.750   1.2865   0.01354   0.00806   0.0334   0.1316   0.9901
  11.000   1.3148   0.01377   0.00834   0.0329   0.1308   0.9919
  11.250   1.3421   0.01402   0.00863   0.0326   0.1299   0.9937
  11.500   1.3716   0.01427   0.00893   0.0318   0.1286   0.9950
  11.750   1.4008   0.01453   0.00923   0.0310   0.1272   0.9964
  12.000   1.4296   0.01481   0.00953   0.0303   0.1252   0.9977
  12.250   1.4578   0.01513   0.00987   0.0296   0.1232   0.9989
  12.500   1.4856   0.01550   0.01026   0.0289   0.1209   0.9998
  12.750   1.5046   0.01576   0.01057   0.0301   0.1197   1.0000
  13.000   1.5205   0.01603   0.01089   0.0320   0.1180   1.0000
  13.250   1.5360   0.01633   0.01123   0.0338   0.1160   1.0000
  13.500   1.5507   0.01667   0.01159   0.0357   0.1136   1.0000
  13.750   1.5638   0.01710   0.01202   0.0378   0.1099   1.0000
  14.000   1.5775   0.01750   0.01245   0.0398   0.1066   1.0000
  14.250   1.5843   0.01802   0.01296   0.0429   0.1020   1.0000
  14.500   1.5907   0.01855   0.01351   0.0459   0.0985   1.0000
  14.750   1.5978   0.01917   0.01416   0.0485   0.0953   1.0000
  15.000   1.6041   0.01995   0.01496   0.0509   0.0923   1.0000
  15.250   1.6126   0.02070   0.01577   0.0527   0.0902   1.0000
  15.500   1.6204   0.02159   0.01671   0.0544   0.0881   1.0000
  15.750   1.6256   0.02274   0.01791   0.0558   0.0856   1.0000
  16.000   1.6293   0.02416   0.01938   0.0569   0.0835   1.0000
  16.250   1.6337   0.02570   0.02099   0.0575   0.0810   1.0000
  16.500   1.6395   0.02727   0.02264   0.0577   0.0799   1.0000
  16.750   1.6404   0.02938   0.02483   0.0576   0.0776   1.0000
  17.000   1.6361   0.03213   0.02764   0.0573   0.0752   1.0000
  17.250   1.6303   0.03517   0.03077   0.0566   0.0732   1.0000
  17.500   1.6268   0.03812   0.03382   0.0557   0.0718   1.0000
  17.750   1.6160   0.04202   0.03784   0.0543   0.0700   1.0000
  18.000   1.5987   0.04695   0.04289   0.0522   0.0688   1.0000
  18.250   1.5597   0.05501   0.05111   0.0484   0.0672   1.0000
  18.500   1.5152   0.06432   0.06063   0.0439   0.0677   1.0000
  18.750   1.4660   0.07445   0.07099   0.0391   0.0696   1.0000
  19.000   1.3947   0.08772   0.08446   0.0327   0.0707   1.0000
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