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MH 95 15.86% (mh95-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 95 15.86% (mh95-il)
Reynolds number: 500,000
Max Cl/Cd: 60.83 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh95-il-500000-n5.txt
Download as CSV file: xf-mh95-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 95  15.86%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.7652   0.10892   0.10545  -0.0540   1.0000   0.0114
 -17.500  -0.7982   0.09860   0.09493  -0.0596   1.0000   0.0114
 -17.250  -0.8233   0.09033   0.08648  -0.0639   1.0000   0.0113
 -17.000  -0.8453   0.08300   0.07898  -0.0677   1.0000   0.0113
 -16.750  -0.8622   0.07686   0.07270  -0.0706   1.0000   0.0114
 -16.500  -0.8786   0.07115   0.06683  -0.0731   1.0000   0.0114
 -16.250  -0.8911   0.06630   0.06185  -0.0749   1.0000   0.0114
 -16.000  -0.9010   0.06211   0.05753  -0.0762   1.0000   0.0114
 -15.750  -0.9104   0.05825   0.05354  -0.0771   1.0000   0.0115
 -15.500  -0.9177   0.05490   0.05008  -0.0775   1.0000   0.0115
 -15.250  -0.9250   0.05178   0.04684  -0.0774   1.0000   0.0115
 -15.000  -0.9312   0.04901   0.04396  -0.0769   1.0000   0.0116
 -14.750  -0.9364   0.04654   0.04138  -0.0761   1.0000   0.0116
 -14.500  -0.9418   0.04421   0.03894  -0.0749   1.0000   0.0118
 -14.250  -0.9456   0.04219   0.03682  -0.0734   1.0000   0.0118
 -14.000  -0.9493   0.04029   0.03482  -0.0716   1.0000   0.0118
 -13.750  -0.9523   0.03859   0.03303  -0.0695   1.0000   0.0120
 -13.500  -0.9545   0.03707   0.03142  -0.0673   1.0000   0.0120
 -13.250  -0.9552   0.03554   0.02981  -0.0651   0.9999   0.0121
 -13.000  -0.9412   0.03394   0.02810  -0.0657   0.9987   0.0122
 -12.750  -0.9269   0.03238   0.02643  -0.0660   0.9971   0.0123
 -12.500  -0.9113   0.03105   0.02501  -0.0663   0.9955   0.0124
 -12.250  -0.8934   0.02988   0.02372  -0.0668   0.9939   0.0126
 -12.000  -0.8759   0.02878   0.02253  -0.0669   0.9922   0.0127
 -11.750  -0.8638   0.02731   0.02103  -0.0663   0.9898   0.0129
 -11.500  -0.8467   0.02621   0.01988  -0.0663   0.9875   0.0131
 -11.250  -0.8275   0.02520   0.01881  -0.0665   0.9855   0.0132
 -11.000  -0.8066   0.02424   0.01782  -0.0669   0.9838   0.0134
 -10.750  -0.7838   0.02335   0.01689  -0.0675   0.9825   0.0136
 -10.500  -0.7671   0.02254   0.01603  -0.0667   0.9794   0.0138
 -10.250  -0.7490   0.02179   0.01524  -0.0661   0.9760   0.0140
 -10.000  -0.7276   0.02101   0.01442  -0.0661   0.9735   0.0142
  -9.750  -0.7032   0.02028   0.01364  -0.0665   0.9716   0.0145
  -9.500  -0.6770   0.01959   0.01290  -0.0673   0.9701   0.0148
  -9.250  -0.6582   0.01896   0.01224  -0.0664   0.9666   0.0150
  -9.000  -0.6404   0.01840   0.01163  -0.0652   0.9620   0.0153
  -8.750  -0.6157   0.01782   0.01100  -0.0653   0.9594   0.0155
  -8.500  -0.5899   0.01712   0.01029  -0.0657   0.9575   0.0159
  -8.250  -0.5613   0.01650   0.00965  -0.0666   0.9560   0.0164
  -8.000  -0.5453   0.01610   0.00923  -0.0646   0.9508   0.0167
  -7.750  -0.5248   0.01566   0.00878  -0.0636   0.9464   0.0172
  -7.500  -0.4980   0.01520   0.00829  -0.0637   0.9437   0.0179
  -7.250  -0.4685   0.01477   0.00783  -0.0644   0.9417   0.0185
  -7.000  -0.4390   0.01427   0.00733  -0.0652   0.9398   0.0196
  -6.750  -0.4280   0.01402   0.00707  -0.0619   0.9319   0.0204
  -6.500  -0.4016   0.01366   0.00669  -0.0618   0.9282   0.0216
  -6.250  -0.3730   0.01324   0.00627  -0.0622   0.9253   0.0232
  -6.000  -0.3520   0.01295   0.00598  -0.0609   0.9199   0.0254
  -5.750  -0.3309   0.01263   0.00567  -0.0597   0.9137   0.0289
  -5.500  -0.3034   0.01225   0.00532  -0.0598   0.9096   0.0360
  -5.250  -0.2816   0.01188   0.00502  -0.0587   0.9036   0.0498
  -5.000  -0.2614   0.01148   0.00473  -0.0574   0.8963   0.0707
  -4.750  -0.2350   0.01097   0.00436  -0.0574   0.8914   0.1048
  -4.500  -0.2186   0.01054   0.00411  -0.0552   0.8822   0.1454
  -4.250  -0.1941   0.01005   0.00381  -0.0548   0.8754   0.1923
  -4.000  -0.1737   0.00970   0.00359  -0.0535   0.8661   0.2305
  -3.750  -0.1494   0.00924   0.00332  -0.0530   0.8577   0.2835
  -3.500  -0.1316   0.00874   0.00309  -0.0512   0.8466   0.3520
  -3.250  -0.1116   0.00822   0.00285  -0.0499   0.8359   0.4285
  -3.000  -0.0923   0.00770   0.00263  -0.0483   0.8239   0.5107
  -2.750  -0.0715   0.00737   0.00253  -0.0469   0.8107   0.5756
  -2.500  -0.0462   0.00726   0.00245  -0.0462   0.7971   0.6084
  -2.250  -0.0202   0.00721   0.00239  -0.0457   0.7822   0.6295
  -2.000   0.0058   0.00720   0.00234  -0.0451   0.7655   0.6464
  -1.750   0.0314   0.00723   0.00230  -0.0445   0.7479   0.6607
  -1.500   0.0566   0.00726   0.00228  -0.0438   0.7297   0.6729
  -1.250   0.0816   0.00732   0.00226  -0.0430   0.7109   0.6832
  -1.000   0.1062   0.00739   0.00226  -0.0422   0.6917   0.6937
  -0.750   0.1308   0.00747   0.00226  -0.0414   0.6738   0.7026
  -0.500   0.1552   0.00756   0.00228  -0.0405   0.6549   0.7119
  -0.250   0.1795   0.00765   0.00230  -0.0397   0.6368   0.7198
   0.000   0.2035   0.00775   0.00233  -0.0388   0.6176   0.7271
   0.250   0.2276   0.00787   0.00235  -0.0380   0.5985   0.7339
   0.500   0.2511   0.00798   0.00240  -0.0369   0.5782   0.7394
   0.750   0.2746   0.00811   0.00245  -0.0360   0.5583   0.7455
   1.250   0.3209   0.00840   0.00258  -0.0339   0.5169   0.7573
   1.500   0.3440   0.00856   0.00266  -0.0329   0.4958   0.7635
   1.750   0.3670   0.00873   0.00272  -0.0319   0.4734   0.7692
   2.000   0.3893   0.00890   0.00282  -0.0308   0.4512   0.7738
   2.250   0.4109   0.00911   0.00293  -0.0295   0.4258   0.7787
   2.500   0.4320   0.00936   0.00304  -0.0282   0.3964   0.7838
   3.000   0.4755   0.00982   0.00328  -0.0259   0.3467   0.7920
   3.250   0.4980   0.01001   0.00341  -0.0249   0.3294   0.7959
   3.500   0.5202   0.01021   0.00353  -0.0238   0.3124   0.8000
   3.750   0.5423   0.01040   0.00365  -0.0227   0.2964   0.8042
   4.000   0.5642   0.01060   0.00378  -0.0216   0.2818   0.8078
   4.250   0.5857   0.01079   0.00393  -0.0204   0.2689   0.8113
   4.500   0.6072   0.01098   0.00409  -0.0193   0.2564   0.8153
   4.750   0.6292   0.01118   0.00425  -0.0182   0.2445   0.8193
   5.000   0.6509   0.01141   0.00442  -0.0171   0.2322   0.8233
   5.250   0.6722   0.01165   0.00462  -0.0160   0.2206   0.8270
   5.500   0.6936   0.01186   0.00482  -0.0148   0.2103   0.8309
   5.750   0.7148   0.01210   0.00503  -0.0137   0.2008   0.8350
   6.000   0.7357   0.01237   0.00525  -0.0125   0.1901   0.8391
   6.250   0.7571   0.01262   0.00548  -0.0115   0.1793   0.8434
   6.500   0.7771   0.01289   0.00573  -0.0101   0.1696   0.8473
   6.750   0.7965   0.01319   0.00599  -0.0087   0.1595   0.8518
   7.000   0.8170   0.01345   0.00625  -0.0075   0.1509   0.8564
   7.250   0.8367   0.01378   0.00654  -0.0063   0.1425   0.8610
   7.500   0.8559   0.01407   0.00683  -0.0048   0.1348   0.8653
   7.750   0.8743   0.01439   0.00714  -0.0033   0.1281   0.8705
   8.000   0.8931   0.01472   0.00747  -0.0019   0.1215   0.8760
   8.250   0.9115   0.01507   0.00781  -0.0005   0.1165   0.8810
   8.500   0.9296   0.01537   0.00814   0.0010   0.1119   0.8862
   8.750   0.9469   0.01574   0.00852   0.0026   0.1079   0.8925
   9.000   0.9640   0.01611   0.00890   0.0042   0.1045   0.8988
   9.250   0.9813   0.01642   0.00927   0.0058   0.1019   0.9059
   9.750   1.0132   0.01720   0.01011   0.0093   0.0964   0.9217
  10.000   1.0280   0.01764   0.01058   0.0111   0.0937   0.9317
  10.500   1.0678   0.01845   0.01153   0.0127   0.0900   0.9581
  10.750   1.0957   0.01900   0.01212   0.0115   0.0878   0.9741
  11.000   1.1160   0.01957   0.01270   0.0118   0.0859   1.0000
  11.250   1.1311   0.02020   0.01334   0.0131   0.0843   1.0000
  11.500   1.1461   0.02084   0.01401   0.0144   0.0829   1.0000
  11.750   1.1625   0.02141   0.01463   0.0154   0.0818   1.0000
  12.000   1.1778   0.02204   0.01531   0.0166   0.0804   1.0000
  12.250   1.1923   0.02273   0.01604   0.0178   0.0792   1.0000
  12.500   1.2060   0.02348   0.01682   0.0190   0.0779   1.0000
  12.750   1.2188   0.02429   0.01767   0.0202   0.0769   1.0000
  13.000   1.2301   0.02521   0.01862   0.0215   0.0755   1.0000
  13.250   1.2399   0.02626   0.01970   0.0229   0.0744   1.0000
  13.500   1.2509   0.02725   0.02075   0.0241   0.0735   1.0000
  13.750   1.2635   0.02817   0.02173   0.0250   0.0726   1.0000
  14.000   1.2749   0.02919   0.02283   0.0260   0.0718   1.0000
  14.250   1.2857   0.03028   0.02399   0.0269   0.0708   1.0000
  14.500   1.2958   0.03146   0.02523   0.0278   0.0699   1.0000
  14.750   1.3049   0.03275   0.02656   0.0286   0.0688   1.0000
  15.000   1.3131   0.03415   0.02801   0.0294   0.0678   1.0000
  15.250   1.3197   0.03573   0.02964   0.0301   0.0668   1.0000
  15.500   1.3245   0.03752   0.03148   0.0308   0.0659   1.0000
  15.750   1.3295   0.03934   0.03337   0.0313   0.0651   1.0000
  16.000   1.3382   0.04090   0.03503   0.0316   0.0642   1.0000
  16.250   1.3446   0.04272   0.03693   0.0318   0.0636   1.0000
  16.500   1.3509   0.04460   0.03889   0.0319   0.0627   1.0000
  16.750   1.3560   0.04665   0.04103   0.0319   0.0618   1.0000
  17.000   1.3599   0.04888   0.04334   0.0318   0.0609   1.0000
  17.250   1.3626   0.05130   0.04583   0.0316   0.0601   1.0000
  17.500   1.3642   0.05393   0.04852   0.0312   0.0594   1.0000
  17.750   1.3637   0.05685   0.05152   0.0306   0.0586   1.0000
  18.000   1.3612   0.06007   0.05480   0.0298   0.0580   1.0000
  18.250   1.3612   0.06309   0.05792   0.0290   0.0573   1.0000
  18.500   1.3620   0.06608   0.06102   0.0281   0.0567   1.0000
  18.750   1.3622   0.06923   0.06428   0.0270   0.0560   1.0000
  19.000   1.3608   0.07263   0.06779   0.0258   0.0551   1.0000
  19.250   1.3580   0.07627   0.07153   0.0244   0.0545   1.0000
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