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MARSKE MONARCH AIRFOIL (NACA 43012A) (marske5-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MARSKE MONARCH AIRFOIL (NACA 43012A) (marske5-il)
Reynolds number: 1,000,000
Max Cl/Cd: 92.85 at α=12.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-marske5-il-1000000.txt
Download as CSV file: xf-marske5-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.5352   0.10391   0.10227   0.0045   1.0000   0.0177
 -11.000  -0.5381   0.09885   0.09721   0.0018   1.0000   0.0181
 -10.250  -0.9436   0.02495   0.02069   0.0031   1.0000   0.0156
 -10.000  -0.9325   0.02310   0.01858   0.0059   1.0000   0.0158
  -9.750  -0.9164   0.02200   0.01730   0.0081   1.0000   0.0160
  -9.500  -0.9032   0.02015   0.01521   0.0107   1.0000   0.0164
  -9.250  -0.8843   0.01947   0.01450   0.0125   1.0000   0.0167
  -9.000  -0.8643   0.01899   0.01399   0.0142   1.0000   0.0169
  -8.750  -0.8436   0.01866   0.01365   0.0158   1.0000   0.0171
  -8.500  -0.8232   0.01824   0.01319   0.0174   1.0000   0.0174
  -8.250  -0.8027   0.01774   0.01265   0.0191   1.0000   0.0177
  -8.000  -0.7820   0.01735   0.01222   0.0208   1.0000   0.0182
  -7.750  -0.7558   0.01675   0.01154   0.0213   0.9990   0.0187
  -7.500  -0.7187   0.01605   0.01073   0.0195   0.9850   0.0191
  -7.250  -0.6444   0.01455   0.00914   0.0095   0.9393   0.0200
  -7.000  -0.6065   0.01458   0.00870   0.0078   0.7856   0.0204
  -6.750  -0.5848   0.01443   0.00837   0.0094   0.7463   0.0209
  -6.500  -0.5612   0.01420   0.00803   0.0105   0.7244   0.0215
  -6.250  -0.5369   0.01387   0.00759   0.0116   0.7079   0.0221
  -5.750  -0.4887   0.01299   0.00654   0.0137   0.6753   0.0233
  -5.500  -0.4640   0.01277   0.00630   0.0146   0.6579   0.0239
  -5.250  -0.4390   0.01262   0.00609   0.0155   0.6369   0.0247
  -5.000  -0.4145   0.01239   0.00576   0.0165   0.6074   0.0254
  -4.750  -0.3906   0.01227   0.00547   0.0176   0.5608   0.0261
  -4.500  -0.3671   0.01229   0.00524   0.0188   0.4950   0.0266
  -4.250  -0.3474   0.01195   0.00464   0.0205   0.4103   0.0276
  -4.000  -0.3244   0.01202   0.00448   0.0216   0.3386   0.0284
  -3.750  -0.3000   0.01193   0.00429   0.0226   0.3094   0.0293
  -3.500  -0.2747   0.01186   0.00414   0.0234   0.2928   0.0304
  -3.250  -0.2499   0.01171   0.00392   0.0243   0.2811   0.0311
  -3.000  -0.2272   0.01137   0.00354   0.0256   0.2718   0.0322
  -2.750  -0.2019   0.01123   0.00339   0.0264   0.2645   0.0333
  -2.500  -0.1764   0.01113   0.00325   0.0272   0.2575   0.0346
  -2.250  -0.1508   0.01106   0.00313   0.0280   0.2504   0.0356
  -2.000  -0.1263   0.01082   0.00288   0.0290   0.2458   0.0369
  -1.750  -0.1011   0.01070   0.00273   0.0298   0.2398   0.0384
  -1.500  -0.0754   0.01064   0.00264   0.0305   0.2335   0.0402
  -1.250  -0.0491   0.01056   0.00255   0.0312   0.2300   0.0415
  -1.000  -0.0239   0.01043   0.00240   0.0320   0.2255   0.0444
  -0.750   0.0020   0.01039   0.00233   0.0327   0.2203   0.0472
  -0.500   0.0276   0.01031   0.00227   0.0334   0.2163   0.0538
  -0.250   0.0506   0.01000   0.00219   0.0346   0.2135   0.1218
   0.000   0.0443   0.00804   0.00186   0.0411   0.2117   0.6056
   0.250   0.0477   0.00728   0.00186   0.0467   0.2092   0.8176
   0.500   0.0715   0.00731   0.00195   0.0480   0.2052   0.8512
   0.750   0.0962   0.00740   0.00205   0.0491   0.2013   0.8718
   1.000   0.1221   0.00746   0.00214   0.0500   0.1994   0.8885
   1.250   0.1488   0.00755   0.00225   0.0507   0.1971   0.9022
   1.500   0.1753   0.00765   0.00232   0.0514   0.1944   0.9104
   1.750   0.2026   0.00778   0.00243   0.0519   0.1914   0.9184
   2.000   0.2273   0.00794   0.00254   0.0528   0.1879   0.9251
   2.250   0.2571   0.00807   0.00268   0.0527   0.1859   0.9304
   2.500   0.2843   0.00819   0.00280   0.0532   0.1846   0.9369
   2.750   0.3107   0.00829   0.00288   0.0538   0.1831   0.9417
   3.000   0.3408   0.00839   0.00297   0.0535   0.1814   0.9438
   3.250   0.3704   0.00851   0.00306   0.0533   0.1796   0.9459
   3.500   0.3994   0.00864   0.00316   0.0532   0.1777   0.9483
   3.750   0.4272   0.00879   0.00328   0.0533   0.1758   0.9512
   4.000   0.4506   0.00897   0.00344   0.0543   0.1735   0.9551
   4.250   0.4804   0.00915   0.00361   0.0540   0.1721   0.9572
   4.500   0.5121   0.00928   0.00374   0.0532   0.1714   0.9586
   4.750   0.5440   0.00941   0.00388   0.0525   0.1705   0.9601
   5.000   0.5758   0.00957   0.00403   0.0517   0.1695   0.9617
   5.250   0.6072   0.00972   0.00419   0.0509   0.1684   0.9635
   5.500   0.6372   0.00987   0.00433   0.0505   0.1670   0.9657
   5.750   0.6601   0.00997   0.00443   0.0516   0.1656   0.9701
   6.000   0.6936   0.01014   0.00458   0.0504   0.1641   0.9708
   6.250   0.7272   0.01035   0.00478   0.0491   0.1626   0.9715
   6.500   0.7602   0.01064   0.00506   0.0478   0.1605   0.9721
   6.750   0.7924   0.01097   0.00539   0.0467   0.1586   0.9729
   7.000   0.8255   0.01110   0.00554   0.0455   0.1580   0.9738
   7.250   0.8583   0.01123   0.00569   0.0444   0.1572   0.9748
   7.500   0.8902   0.01140   0.00588   0.0435   0.1562   0.9760
   7.750   0.9212   0.01158   0.00608   0.0427   0.1553   0.9776
   8.000   0.9506   0.01177   0.00628   0.0422   0.1542   0.9797
   8.250   0.9761   0.01196   0.00649   0.0426   0.1532   0.9829
   8.500   1.0094   0.01215   0.00670   0.0412   0.1521   0.9836
   8.750   1.0423   0.01234   0.00691   0.0399   0.1509   0.9843
   9.000   1.0747   0.01258   0.00716   0.0387   0.1497   0.9853
   9.250   1.1059   0.01290   0.00748   0.0376   0.1480   0.9865
   9.500   1.1350   0.01342   0.00802   0.0368   0.1460   0.9880
   9.750   1.1662   0.01357   0.00822   0.0359   0.1455   0.9895
  10.000   1.1965   0.01374   0.00843   0.0351   0.1448   0.9911
  10.250   1.2256   0.01392   0.00866   0.0346   0.1439   0.9930
  10.500   1.2563   0.01411   0.00889   0.0337   0.1428   0.9941
  10.750   1.2885   0.01427   0.00909   0.0324   0.1413   0.9950
  11.000   1.3203   0.01444   0.00929   0.0312   0.1399   0.9962
  11.250   1.3520   0.01461   0.00948   0.0300   0.1381   0.9974
  11.500   1.3826   0.01491   0.00978   0.0289   0.1359   0.9987
  11.750   1.4120   0.01536   0.01026   0.0279   0.1337   0.9998
  12.000   1.4328   0.01551   0.01047   0.0289   0.1330   1.0000
  12.250   1.4500   0.01565   0.01068   0.0306   0.1319   1.0000
  12.500   1.4670   0.01581   0.01088   0.0324   0.1303   1.0000
  12.750   1.4838   0.01598   0.01110   0.0341   0.1287   1.0000
  13.000   1.4997   0.01620   0.01134   0.0360   0.1270   1.0000
  13.250   1.5141   0.01648   0.01162   0.0381   0.1243   1.0000
  13.500   1.5283   0.01680   0.01197   0.0401   0.1220   1.0000
  13.750   1.5459   0.01697   0.01220   0.0416   0.1199   1.0000
  14.000   1.5616   0.01723   0.01250   0.0434   0.1174   1.0000
  14.250   1.5755   0.01758   0.01286   0.0454   0.1147   1.0000
  14.500   1.5858   0.01808   0.01337   0.0478   0.1120   1.0000
  14.750   1.5964   0.01840   0.01375   0.0504   0.1103   1.0000
  15.000   1.6053   0.01879   0.01419   0.0531   0.1079   1.0000
  15.250   1.6135   0.01932   0.01475   0.0556   0.1051   1.0000
  15.750   1.6299   0.02071   0.01623   0.0597   0.0997   1.0000
  16.000   1.6380   0.02156   0.01712   0.0612   0.0973   1.0000
  16.250   1.6425   0.02275   0.01835   0.0627   0.0943   1.0000
  16.500   1.6468   0.02412   0.01977   0.0637   0.0919   1.0000
  16.750   1.6529   0.02552   0.02126   0.0642   0.0899   1.0000
  17.000   1.6545   0.02746   0.02325   0.0643   0.0873   1.0000
  17.250   1.6526   0.02988   0.02574   0.0640   0.0852   1.0000
  17.500   1.6478   0.03273   0.02868   0.0635   0.0832   1.0000
  17.750   1.6472   0.03527   0.03132   0.0628   0.0816   1.0000
  18.000   1.6386   0.03880   0.03495   0.0615   0.0795   1.0000
  18.250   1.6236   0.04329   0.03955   0.0597   0.0782   1.0000
  18.500   1.5985   0.04930   0.04570   0.0568   0.0773   1.0000
  18.750   1.5627   0.05705   0.05362   0.0530   0.0770   1.0000
  19.000   1.5048   0.06816   0.06493   0.0475   0.0771   1.0000
  19.250   1.4462   0.07946   0.07642   0.0419   0.0776   1.0000
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