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MARSKE MONARCH AIRFOIL (NACA 43012A) (marske5-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MARSKE MONARCH AIRFOIL (NACA 43012A) (marske5-il)
Reynolds number: 500,000
Max Cl/Cd: 73.65 at α=10.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-marske5-il-500000-n5.txt
Download as CSV file: xf-marske5-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.5526   0.08671   0.08439  -0.0101   1.0000   0.0117
 -10.750  -0.5995   0.07224   0.06990  -0.0228   1.0000   0.0116
 -10.500  -0.9158   0.02653   0.02151  -0.0064   1.0000   0.0133
 -10.250  -0.9042   0.02483   0.01958  -0.0038   1.0000   0.0135
 -10.000  -0.8876   0.02406   0.01874  -0.0018   1.0000   0.0137
  -9.750  -0.8693   0.02348   0.01813   0.0000   1.0000   0.0138
  -9.500  -0.8507   0.02290   0.01750   0.0018   1.0000   0.0140
  -9.250  -0.8318   0.02232   0.01686   0.0036   1.0000   0.0143
  -9.000  -0.8129   0.02163   0.01610   0.0054   1.0000   0.0145
  -8.750  -0.7944   0.02076   0.01511   0.0072   1.0000   0.0148
  -8.500  -0.7751   0.01995   0.01419   0.0090   1.0000   0.0152
  -8.250  -0.7455   0.01879   0.01285   0.0086   0.9888   0.0158
  -8.000  -0.6989   0.01774   0.01164   0.0047   0.9556   0.0164
  -7.750  -0.6289   0.01728   0.01092  -0.0039   0.8292   0.0171
  -7.500  -0.6083   0.01719   0.01057  -0.0021   0.7705   0.0175
  -7.250  -0.5861   0.01690   0.01008  -0.0007   0.7414   0.0181
  -6.750  -0.5395   0.01586   0.00869   0.0017   0.7045   0.0193
  -6.500  -0.5161   0.01553   0.00828   0.0029   0.6854   0.0198
  -6.250  -0.4920   0.01530   0.00799   0.0039   0.6640   0.0202
  -6.000  -0.4678   0.01508   0.00768   0.0049   0.6395   0.0209
  -5.750  -0.4439   0.01481   0.00727   0.0060   0.6096   0.0217
  -5.500  -0.4200   0.01458   0.00684   0.0071   0.5738   0.0227
  -5.250  -0.3973   0.01435   0.00643   0.0084   0.5251   0.0233
  -5.000  -0.3742   0.01428   0.00617   0.0096   0.4675   0.0240
  -4.750  -0.3519   0.01429   0.00589   0.0108   0.3841   0.0247
  -4.500  -0.3284   0.01421   0.00560   0.0119   0.3365   0.0256
  -4.250  -0.3038   0.01413   0.00535   0.0128   0.3116   0.0267
  -4.000  -0.2802   0.01385   0.00504   0.0138   0.2965   0.0275
  -3.750  -0.2555   0.01370   0.00484   0.0147   0.2852   0.0285
  -3.500  -0.2308   0.01352   0.00461   0.0156   0.2759   0.0296
  -3.250  -0.2060   0.01337   0.00439   0.0165   0.2680   0.0307
  -3.000  -0.1815   0.01317   0.00415   0.0175   0.2609   0.0317
  -2.750  -0.1571   0.01301   0.00395   0.0184   0.2536   0.0328
  -2.500  -0.1320   0.01286   0.00378   0.0193   0.2483   0.0341
  -2.250  -0.1068   0.01274   0.00362   0.0201   0.2428   0.0355
  -2.000  -0.0817   0.01264   0.00347   0.0209   0.2376   0.0366
  -1.750  -0.0568   0.01249   0.00331   0.0218   0.2333   0.0381
  -1.500  -0.0313   0.01238   0.00319   0.0225   0.2294   0.0398
  -1.250  -0.0057   0.01232   0.00309   0.0233   0.2250   0.0418
  -1.000   0.0196   0.01225   0.00300   0.0241   0.2206   0.0443
  -0.750   0.0452   0.01219   0.00293   0.0248   0.2171   0.0475
  -0.500   0.0708   0.01212   0.00286   0.0255   0.2138   0.0541
  -0.250   0.0955   0.01198   0.00281   0.0264   0.2102   0.0820
   0.000   0.1049   0.01075   0.00262   0.0297   0.2073   0.3982
   0.250   0.0985   0.00928   0.00249   0.0368   0.2052   0.7581
   0.500   0.1206   0.00923   0.00263   0.0386   0.2018   0.8324
   0.750   0.1461   0.00929   0.00277   0.0397   0.1996   0.8697
   1.000   0.1737   0.00941   0.00291   0.0402   0.1969   0.8898
   1.250   0.2010   0.00954   0.00302   0.0408   0.1943   0.9032
   1.500   0.2314   0.00970   0.00315   0.0406   0.1915   0.9118
   1.750   0.2558   0.00984   0.00324   0.0417   0.1892   0.9215
   2.000   0.2885   0.01007   0.00342   0.0409   0.1864   0.9271
   2.250   0.3164   0.01019   0.00352   0.0412   0.1850   0.9326
   2.500   0.3417   0.01028   0.00359   0.0419   0.1835   0.9364
   2.750   0.3726   0.01041   0.00369   0.0414   0.1817   0.9378
   3.000   0.4029   0.01055   0.00380   0.0410   0.1800   0.9395
   3.250   0.4326   0.01069   0.00391   0.0407   0.1782   0.9415
   3.500   0.4615   0.01083   0.00402   0.0406   0.1764   0.9439
   3.750   0.4884   0.01099   0.00414   0.0408   0.1747   0.9470
   4.000   0.5145   0.01116   0.00427   0.0412   0.1727   0.9502
   4.250   0.5455   0.01137   0.00445   0.0406   0.1711   0.9515
   4.500   0.5767   0.01153   0.00462   0.0399   0.1702   0.9530
   4.750   0.6075   0.01170   0.00479   0.0393   0.1692   0.9548
   5.000   0.6372   0.01187   0.00498   0.0389   0.1682   0.9571
   5.250   0.6641   0.01204   0.00515   0.0391   0.1671   0.9604
   5.500   0.6927   0.01223   0.00534   0.0389   0.1660   0.9628
   5.750   0.7248   0.01243   0.00555   0.0379   0.1648   0.9638
   6.000   0.7564   0.01264   0.00576   0.0370   0.1636   0.9650
   6.250   0.7872   0.01286   0.00598   0.0363   0.1623   0.9664
   6.500   0.8170   0.01309   0.00620   0.0357   0.1610   0.9683
   6.750   0.8449   0.01334   0.00643   0.0355   0.1593   0.9708
   7.000   0.8706   0.01366   0.00674   0.0358   0.1573   0.9739
   7.250   0.9024   0.01383   0.00695   0.0348   0.1563   0.9750
   7.500   0.9336   0.01404   0.00720   0.0339   0.1553   0.9763
   7.750   0.9641   0.01428   0.00748   0.0331   0.1544   0.9780
   8.000   0.9936   0.01451   0.00775   0.0325   0.1532   0.9801
   8.250   1.0211   0.01475   0.00803   0.0323   0.1521   0.9829
   8.500   1.0500   0.01500   0.00832   0.0318   0.1510   0.9848
   8.750   1.0806   0.01527   0.00862   0.0309   0.1498   0.9862
   9.000   1.1105   0.01554   0.00891   0.0301   0.1486   0.9878
   9.250   1.1396   0.01582   0.00921   0.0295   0.1472   0.9897
   9.500   1.1675   0.01615   0.00956   0.0290   0.1458   0.9919
   9.750   1.1943   0.01656   0.00999   0.0287   0.1444   0.9940
  10.000   1.2241   0.01687   0.01036   0.0278   0.1436   0.9956
  10.250   1.2540   0.01716   0.01073   0.0269   0.1427   0.9974
  10.500   1.2837   0.01747   0.01112   0.0260   0.1416   0.9990
  10.750   1.3102   0.01779   0.01151   0.0257   0.1404   1.0000
  11.000   1.3259   0.01807   0.01185   0.0277   0.1394   1.0000
  11.250   1.3413   0.01837   0.01221   0.0296   0.1383   1.0000
  11.500   1.3564   0.01867   0.01257   0.0316   0.1372   1.0000
  11.750   1.3713   0.01900   0.01293   0.0336   0.1360   1.0000
  12.000   1.3856   0.01934   0.01332   0.0356   0.1349   1.0000
  12.250   1.3991   0.01973   0.01374   0.0377   0.1338   1.0000
  12.500   1.4113   0.02018   0.01422   0.0399   0.1325   1.0000
  12.750   1.4244   0.02062   0.01473   0.0420   0.1315   1.0000
  13.000   1.4359   0.02101   0.01522   0.0443   0.1306   1.0000
  13.250   1.4455   0.02142   0.01571   0.0469   0.1295   1.0000
  13.500   1.4556   0.02187   0.01625   0.0493   0.1282   1.0000
  13.750   1.4661   0.02236   0.01681   0.0514   0.1265   1.0000
  14.000   1.4765   0.02290   0.01740   0.0532   0.1247   1.0000
  14.250   1.4859   0.02356   0.01812   0.0549   0.1230   1.0000
  14.500   1.4938   0.02442   0.01902   0.0564   0.1216   1.0000
  14.750   1.5034   0.02531   0.02001   0.0576   0.1200   1.0000
  15.000   1.5131   0.02629   0.02110   0.0585   0.1185   1.0000
  15.250   1.5223   0.02739   0.02228   0.0591   0.1162   1.0000
  15.500   1.5294   0.02874   0.02371   0.0594   0.1137   1.0000
  15.750   1.5332   0.03048   0.02549   0.0595   0.1111   1.0000
  16.000   1.5390   0.03217   0.02728   0.0595   0.1086   1.0000
  16.250   1.5420   0.03421   0.02941   0.0592   0.1054   1.0000
  16.500   1.5408   0.03676   0.03203   0.0586   0.1031   1.0000
  16.750   1.5337   0.04007   0.03541   0.0575   0.1008   1.0000
  17.000   1.5285   0.04330   0.03877   0.0564   0.0996   1.0000
  17.250   1.5172   0.04743   0.04303   0.0547   0.0976   1.0000
  17.500   1.4980   0.05276   0.04849   0.0523   0.0960   1.0000
  17.750   1.4714   0.05928   0.05515   0.0491   0.0950   1.0000
  18.000   1.4310   0.06807   0.06409   0.0447   0.0940   1.0000
  18.250   1.3810   0.07844   0.07461   0.0395   0.0933   1.0000
  18.500   1.3259   0.08968   0.08596   0.0339   0.0920   1.0000
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