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MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID) (marske2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYBRID) (marske2-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97 at α=10.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-marske2-il-1000000-n5.txt
Download as CSV file: xf-marske2-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MARSKE PIONEER IA AIRFOIL (NACA 23112/43012A HYB
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -1.2377   0.05400   0.05095  -0.0466   1.0000   0.0084
 -17.250  -1.2565   0.04869   0.04548  -0.0488   1.0000   0.0085
 -17.000  -1.2706   0.04456   0.04118  -0.0495   1.0000   0.0086
 -16.750  -1.2822   0.04109   0.03756  -0.0492   1.0000   0.0086
 -16.500  -1.2891   0.03833   0.03466  -0.0482   1.0000   0.0086
 -16.250  -1.2903   0.03622   0.03244  -0.0469   1.0000   0.0087
 -16.000  -1.2890   0.03443   0.03055  -0.0453   1.0000   0.0088
 -15.750  -1.2879   0.03271   0.02871  -0.0434   1.0000   0.0089
 -15.500  -1.2852   0.03116   0.02705  -0.0413   1.0000   0.0090
 -15.250  -1.2801   0.02983   0.02562  -0.0392   1.0000   0.0091
 -15.000  -1.2743   0.02858   0.02426  -0.0369   1.0000   0.0092
 -14.750  -1.2662   0.02752   0.02311  -0.0346   1.0000   0.0093
 -14.500  -1.2575   0.02651   0.02201  -0.0322   1.0000   0.0094
 -14.250  -1.2480   0.02557   0.02098  -0.0298   1.0000   0.0095
 -14.000  -1.2377   0.02468   0.01999  -0.0274   1.0000   0.0097
 -13.750  -1.2267   0.02388   0.01910  -0.0249   1.0000   0.0098
 -13.500  -1.2152   0.02312   0.01827  -0.0223   1.0000   0.0099
 -13.250  -1.2032   0.02241   0.01747  -0.0197   1.0000   0.0099
 -13.000  -1.1891   0.02179   0.01678  -0.0174   1.0000   0.0101
 -12.750  -1.1749   0.02100   0.01593  -0.0152   1.0000   0.0103
 -12.500  -1.1587   0.02032   0.01518  -0.0132   1.0000   0.0105
 -12.250  -1.1415   0.01969   0.01451  -0.0114   1.0000   0.0107
 -12.000  -1.1234   0.01914   0.01391  -0.0096   1.0000   0.0109
 -11.750  -1.1047   0.01861   0.01334  -0.0079   1.0000   0.0112
 -11.500  -1.0856   0.01812   0.01282  -0.0063   1.0000   0.0115
 -11.250  -1.0662   0.01764   0.01228  -0.0047   1.0000   0.0118
 -11.000  -1.0468   0.01715   0.01175  -0.0030   1.0000   0.0121
 -10.750  -1.0270   0.01669   0.01124  -0.0014   1.0000   0.0123
 -10.500  -1.0069   0.01627   0.01076   0.0002   1.0000   0.0125
 -10.250  -0.9873   0.01579   0.01026   0.0019   1.0000   0.0129
 -10.000  -0.9670   0.01538   0.00984   0.0034   1.0000   0.0133
  -9.750  -0.9464   0.01501   0.00945   0.0050   1.0000   0.0137
  -9.500  -0.9258   0.01466   0.00908   0.0066   1.0000   0.0141
  -9.250  -0.9052   0.01431   0.00871   0.0082   1.0000   0.0145
  -9.000  -0.8848   0.01398   0.00834   0.0098   1.0000   0.0149
  -8.750  -0.8525   0.01357   0.00790   0.0089   0.9966   0.0153
  -8.500  -0.8219   0.01318   0.00752   0.0084   0.9875   0.0160
  -8.250  -0.7834   0.01282   0.00717   0.0062   0.9754   0.0167
  -8.000  -0.7182   0.01236   0.00666  -0.0017   0.9399   0.0179
  -7.750  -0.6823   0.01221   0.00622  -0.0032   0.8446   0.0185
  -7.500  -0.6632   0.01219   0.00596  -0.0011   0.7751   0.0191
  -7.250  -0.6405   0.01210   0.00576   0.0002   0.7430   0.0197
  -7.000  -0.6165   0.01195   0.00553   0.0012   0.7252   0.0203
  -6.750  -0.5921   0.01180   0.00530   0.0021   0.7097   0.0211
  -6.250  -0.5432   0.01145   0.00482   0.0039   0.6779   0.0223
  -6.000  -0.5179   0.01128   0.00464   0.0047   0.6676   0.0231
  -5.750  -0.4926   0.01113   0.00445   0.0054   0.6561   0.0238
  -5.500  -0.4674   0.01098   0.00424   0.0062   0.6395   0.0245
  -5.250  -0.4421   0.01086   0.00404   0.0070   0.6196   0.0253
  -5.000  -0.4171   0.01074   0.00384   0.0078   0.5958   0.0259
  -4.750  -0.3930   0.01061   0.00361   0.0087   0.5614   0.0267
  -4.500  -0.3684   0.01056   0.00345   0.0096   0.5259   0.0275
  -4.250  -0.3434   0.01052   0.00330   0.0104   0.4936   0.0284
  -4.000  -0.3184   0.01049   0.00315   0.0111   0.4602   0.0292
  -3.750  -0.2935   0.01048   0.00301   0.0119   0.4228   0.0298
  -3.500  -0.2686   0.01044   0.00285   0.0127   0.3889   0.0307
  -3.250  -0.2437   0.01040   0.00271   0.0135   0.3588   0.0318
  -3.000  -0.2183   0.01038   0.00260   0.0141   0.3317   0.0327
  -2.750  -0.1927   0.01036   0.00249   0.0148   0.3100   0.0337
  -2.500  -0.1668   0.01034   0.00240   0.0154   0.2924   0.0348
  -2.250  -0.1408   0.01030   0.00230   0.0160   0.2789   0.0358
  -2.000  -0.1148   0.01023   0.00221   0.0166   0.2695   0.0373
  -1.750  -0.0885   0.01019   0.00214   0.0171   0.2615   0.0390
  -1.500  -0.0620   0.01014   0.00207   0.0176   0.2556   0.0409
  -1.250  -0.0355   0.01009   0.00201   0.0181   0.2501   0.0440
  -1.000  -0.0091   0.01006   0.00197   0.0186   0.2441   0.0480
  -0.750   0.0173   0.01000   0.00192   0.0191   0.2393   0.0544
  -0.500   0.0438   0.00995   0.00189   0.0195   0.2347   0.0643
  -0.250   0.0693   0.00985   0.00185   0.0202   0.2291   0.0940
   0.000   0.0859   0.00905   0.00172   0.0222   0.2245   0.3171
   0.250   0.0983   0.00808   0.00157   0.0252   0.2222   0.5594
   0.500   0.1122   0.00747   0.00152   0.0282   0.2194   0.7164
   0.750   0.1338   0.00732   0.00156   0.0298   0.2157   0.7806
   1.000   0.1577   0.00729   0.00163   0.0310   0.2116   0.8195
   1.250   0.1834   0.00731   0.00169   0.0317   0.2078   0.8412
   1.500   0.2100   0.00735   0.00175   0.0322   0.2053   0.8562
   1.750   0.2361   0.00739   0.00182   0.0329   0.2023   0.8748
   2.000   0.2623   0.00747   0.00189   0.0335   0.1985   0.8876
   2.250   0.2898   0.00756   0.00196   0.0337   0.1944   0.8945
   2.500   0.3169   0.00764   0.00203   0.0341   0.1914   0.9015
   2.750   0.3441   0.00771   0.00209   0.0344   0.1891   0.9071
   3.000   0.3722   0.00779   0.00217   0.0345   0.1865   0.9116
   3.250   0.3997   0.00789   0.00225   0.0347   0.1837   0.9161
   3.500   0.4264   0.00800   0.00232   0.0350   0.1808   0.9206
   3.750   0.4543   0.00811   0.00243   0.0351   0.1777   0.9241
   4.000   0.4827   0.00820   0.00252   0.0351   0.1764   0.9279
   4.250   0.5104   0.00830   0.00262   0.0352   0.1746   0.9324
   4.500   0.5373   0.00840   0.00272   0.0355   0.1723   0.9367
   4.750   0.5665   0.00852   0.00283   0.0352   0.1697   0.9398
   5.000   0.5951   0.00866   0.00295   0.0351   0.1674   0.9436
   5.250   0.6224   0.00880   0.00309   0.0352   0.1649   0.9481
   5.500   0.6514   0.00894   0.00323   0.0350   0.1626   0.9516
   5.750   0.6820   0.00907   0.00336   0.0344   0.1608   0.9543
   6.000   0.7117   0.00920   0.00351   0.0340   0.1589   0.9575
   6.250   0.7391   0.00934   0.00364   0.0340   0.1567   0.9616
   6.500   0.7702   0.00951   0.00381   0.0332   0.1544   0.9638
   6.750   0.8017   0.00970   0.00399   0.0323   0.1520   0.9658
   7.000   0.8322   0.00990   0.00419   0.0316   0.1497   0.9682
   7.250   0.8615   0.01006   0.00437   0.0312   0.1486   0.9711
   7.500   0.8900   0.01021   0.00454   0.0310   0.1476   0.9740
   7.750   0.9223   0.01039   0.00474   0.0299   0.1460   0.9750
   8.000   0.9540   0.01057   0.00494   0.0289   0.1441   0.9763
   8.250   0.9849   0.01077   0.00514   0.0280   0.1415   0.9779
   8.500   1.0146   0.01100   0.00536   0.0274   0.1386   0.9799
   8.750   1.0426   0.01124   0.00561   0.0271   0.1361   0.9824
   9.000   1.0710   0.01142   0.00582   0.0268   0.1348   0.9846
   9.250   1.1020   0.01162   0.00605   0.0259   0.1329   0.9856
   9.500   1.1326   0.01184   0.00629   0.0250   0.1305   0.9870
   9.750   1.1625   0.01209   0.00654   0.0242   0.1279   0.9886
  10.000   1.1915   0.01237   0.00683   0.0236   0.1249   0.9905
  10.250   1.2199   0.01261   0.00710   0.0232   0.1221   0.9924
  10.500   1.2479   0.01287   0.00738   0.0228   0.1190   0.9942
  10.750   1.2775   0.01317   0.00768   0.0219   0.1154   0.9957
  11.000   1.3067   0.01350   0.00802   0.0211   0.1118   0.9972
  11.250   1.3359   0.01379   0.00835   0.0204   0.1088   0.9986
  11.500   1.3644   0.01415   0.00872   0.0197   0.1048   0.9997
  11.750   1.3846   0.01453   0.00910   0.0207   0.1013   1.0000
  12.000   1.4015   0.01482   0.00943   0.0224   0.0990   1.0000
  12.250   1.4175   0.01518   0.00981   0.0242   0.0957   1.0000
  12.500   1.4324   0.01561   0.01024   0.0262   0.0922   1.0000
  12.750   1.4477   0.01602   0.01067   0.0280   0.0885   1.0000
  13.000   1.4613   0.01652   0.01117   0.0301   0.0842   1.0000
  13.250   1.4740   0.01707   0.01173   0.0322   0.0799   1.0000
  13.500   1.4853   0.01768   0.01234   0.0345   0.0744   1.0000
  13.750   1.4936   0.01826   0.01294   0.0373   0.0714   1.0000
  14.000   1.4996   0.01889   0.01358   0.0404   0.0664   1.0000
  14.250   1.5037   0.01972   0.01441   0.0433   0.0612   1.0000
  14.500   1.5066   0.02075   0.01545   0.0460   0.0555   1.0000
  14.750   1.5064   0.02209   0.01680   0.0485   0.0489   1.0000
  15.000   1.5103   0.02336   0.01810   0.0501   0.0457   1.0000
  15.250   1.5104   0.02506   0.01984   0.0514   0.0424   1.0000
  15.500   1.5114   0.02693   0.02177   0.0521   0.0397   1.0000
  15.750   1.5132   0.02895   0.02387   0.0522   0.0384   1.0000
  16.000   1.5110   0.03153   0.02653   0.0520   0.0368   1.0000
  16.250   1.5071   0.03443   0.02952   0.0514   0.0351   1.0000
  16.500   1.5025   0.03761   0.03279   0.0505   0.0342   1.0000
  16.750   1.4937   0.04144   0.03674   0.0491   0.0334   1.0000
  17.000   1.4794   0.04623   0.04165   0.0470   0.0329   1.0000
  17.250   1.4566   0.05238   0.04795   0.0442   0.0323   1.0000
  17.500   1.4286   0.05948   0.05521   0.0408   0.0324   1.0000
  17.750   1.3869   0.06874   0.06466   0.0364   0.0325   1.0000
  18.000   1.3397   0.07894   0.07507   0.0317   0.0328   1.0000
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