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MH 95 15.86% (mh95-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: MH 95 15.86% (mh95-il)
Reynolds number: 100,000
Max Cl/Cd: 37.44 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh95-il-100000-n5.txt
Download as CSV file: xf-mh95-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.5604   0.10287   0.09685  -0.0565   1.0000   0.0295
 -13.750  -0.5949   0.09231   0.08619  -0.0625   1.0000   0.0292
 -13.500  -0.6281   0.08370   0.07744  -0.0672   1.0000   0.0289
 -13.250  -0.6571   0.07704   0.07063  -0.0701   1.0000   0.0287
 -13.000  -0.6840   0.07158   0.06501  -0.0716   1.0000   0.0286
 -12.750  -0.7104   0.06691   0.06015  -0.0718   1.0000   0.0285
 -12.500  -0.7319   0.06321   0.05629  -0.0709   1.0000   0.0284
 -12.250  -0.7543   0.05983   0.05271  -0.0691   1.0000   0.0284
 -12.000  -0.7731   0.05705   0.04976  -0.0666   1.0000   0.0284
 -11.750  -0.7914   0.05456   0.04708  -0.0635   1.0000   0.0285
 -11.500  -0.8071   0.05241   0.04475  -0.0598   1.0000   0.0285
 -11.250  -0.8220   0.05050   0.04267  -0.0557   1.0000   0.0286
 -11.000  -0.8362   0.04879   0.04078  -0.0512   1.0000   0.0286
 -10.750  -0.8499   0.04731   0.03912  -0.0462   1.0000   0.0288
 -10.500  -0.8622   0.04590   0.03752  -0.0410   1.0000   0.0290
 -10.250  -0.8693   0.04434   0.03571  -0.0365   1.0000   0.0293
 -10.000  -0.8722   0.04277   0.03386  -0.0325   1.0000   0.0297
  -9.750  -0.8668   0.04157   0.03267  -0.0297   1.0000   0.0303
  -9.500  -0.8617   0.04045   0.03150  -0.0268   1.0000   0.0308
  -9.250  -0.8551   0.03925   0.03021  -0.0240   1.0000   0.0313
  -9.000  -0.8472   0.03804   0.02887  -0.0213   1.0000   0.0320
  -8.750  -0.8374   0.03680   0.02750  -0.0188   1.0000   0.0326
  -8.500  -0.8261   0.03561   0.02616  -0.0164   1.0000   0.0330
  -8.250  -0.8007   0.03425   0.02463  -0.0165   0.9975   0.0338
  -8.000  -0.7725   0.03303   0.02334  -0.0173   0.9943   0.0346
  -7.750  -0.7459   0.03195   0.02226  -0.0179   0.9907   0.0355
  -7.500  -0.7198   0.03094   0.02123  -0.0184   0.9866   0.0367
  -7.250  -0.6917   0.03004   0.02024  -0.0192   0.9828   0.0385
  -7.000  -0.6683   0.02916   0.01936  -0.0192   0.9779   0.0405
  -6.750  -0.6434   0.02835   0.01853  -0.0194   0.9730   0.0429
  -6.500  -0.6149   0.02753   0.01764  -0.0203   0.9691   0.0456
  -6.250  -0.5963   0.02673   0.01683  -0.0193   0.9624   0.0483
  -6.000  -0.5698   0.02594   0.01599  -0.0197   0.9575   0.0526
  -5.750  -0.5454   0.02519   0.01525  -0.0196   0.9522   0.0597
  -5.500  -0.5242   0.02439   0.01453  -0.0190   0.9455   0.0709
  -5.250  -0.4971   0.02341   0.01377  -0.0195   0.9410   0.1014
  -5.000  -0.4813   0.02240   0.01319  -0.0180   0.9335   0.1609
  -4.750  -0.4595   0.02139   0.01269  -0.0178   0.9275   0.2528
  -4.500  -0.4377   0.02043   0.01228  -0.0174   0.9220   0.3512
  -4.250  -0.4230   0.01969   0.01203  -0.0152   0.9136   0.4402
  -4.000  -0.3961   0.01921   0.01212  -0.0146   0.9090   0.5413
  -3.750  -0.3768   0.01922   0.01239  -0.0122   0.9009   0.6095
  -3.500  -0.3481   0.01939   0.01265  -0.0114   0.8949   0.6583
  -3.250  -0.3120   0.01957   0.01278  -0.0122   0.8912   0.6885
  -3.000  -0.2939   0.01967   0.01283  -0.0099   0.8810   0.7069
  -2.750  -0.2591   0.01972   0.01278  -0.0106   0.8763   0.7234
  -2.500  -0.2361   0.01977   0.01276  -0.0093   0.8677   0.7377
  -2.250  -0.2061   0.01972   0.01260  -0.0093   0.8611   0.7520
  -2.000  -0.1663   0.01980   0.01261  -0.0106   0.8576   0.7621
  -1.750  -0.1485   0.01983   0.01259  -0.0083   0.8463   0.7736
  -1.500  -0.1116   0.01976   0.01244  -0.0093   0.8417   0.7840
  -1.250  -0.0894   0.01978   0.01242  -0.0077   0.8315   0.7932
  -1.000  -0.0539   0.01965   0.01222  -0.0085   0.8256   0.8019
  -0.750  -0.0285   0.01957   0.01209  -0.0076   0.8159   0.8103
  -0.500   0.0078   0.01946   0.01192  -0.0084   0.8086   0.8172
  -0.250   0.0316   0.01928   0.01169  -0.0074   0.7979   0.8265
   0.000   0.0726   0.01917   0.01153  -0.0091   0.7902   0.8316
   0.250   0.0974   0.01904   0.01136  -0.0081   0.7778   0.8396
   0.500   0.1354   0.01880   0.01106  -0.0096   0.7681   0.8455
   0.750   0.1704   0.01869   0.01091  -0.0104   0.7551   0.8501
   1.000   0.1991   0.01855   0.01073  -0.0102   0.7407   0.8564
   1.250   0.2275   0.01836   0.01047  -0.0101   0.7262   0.8628
   1.500   0.2649   0.01826   0.01032  -0.0115   0.7106   0.8662
   1.750   0.2992   0.01817   0.01017  -0.0124   0.6940   0.8706
   2.000   0.3263   0.01805   0.00998  -0.0121   0.6765   0.8767
   2.250   0.3553   0.01799   0.00985  -0.0121   0.6579   0.8814
   2.500   0.3866   0.01799   0.00978  -0.0126   0.6373   0.8850
   2.750   0.4140   0.01800   0.00971  -0.0123   0.6168   0.8899
   3.000   0.4332   0.01796   0.00959  -0.0106   0.5963   0.8967
   3.250   0.4639   0.01805   0.00958  -0.0111   0.5739   0.8999
   3.500   0.4890   0.01815   0.00960  -0.0105   0.5505   0.9046
   3.750   0.5068   0.01821   0.00957  -0.0086   0.5283   0.9114
   4.000   0.5315   0.01835   0.00962  -0.0080   0.5042   0.9157
   4.250   0.5558   0.01854   0.00970  -0.0074   0.4796   0.9204
   4.500   0.5720   0.01868   0.00974  -0.0054   0.4563   0.9276
   4.750   0.5966   0.01894   0.00988  -0.0050   0.4312   0.9320
   5.000   0.6190   0.01920   0.01004  -0.0042   0.4076   0.9373
   5.250   0.6372   0.01943   0.01019  -0.0027   0.3862   0.9443
   5.500   0.6639   0.01979   0.01044  -0.0030   0.3638   0.9488
   5.750   0.6854   0.02011   0.01069  -0.0022   0.3445   0.9551
   6.000   0.7105   0.02048   0.01099  -0.0023   0.3256   0.9602
   6.250   0.7369   0.02089   0.01132  -0.0026   0.3076   0.9656
   6.500   0.7620   0.02130   0.01170  -0.0028   0.2907   0.9715
   6.750   0.7908   0.02176   0.01211  -0.0038   0.2740   0.9761
   7.000   0.8156   0.02221   0.01253  -0.0040   0.2587   0.9823
   7.250   0.8441   0.02271   0.01302  -0.0051   0.2435   0.9874
   7.500   0.8698   0.02323   0.01352  -0.0056   0.2295   0.9944
   7.750   0.8852   0.02370   0.01395  -0.0043   0.2188   1.0000
   8.000   0.8804   0.02388   0.01415   0.0010   0.2115   1.0000
   8.250   0.8767   0.02418   0.01438   0.0060   0.2051   1.0000
   8.500   0.8830   0.02455   0.01478   0.0091   0.1963   1.0000
   8.750   0.8907   0.02513   0.01526   0.0118   0.1890   1.0000
   9.000   0.9039   0.02568   0.01587   0.0136   0.1806   1.0000
   9.250   0.9149   0.02640   0.01651   0.0155   0.1741   1.0000
   9.500   0.9297   0.02706   0.01723   0.0169   0.1671   1.0000
   9.750   0.9422   0.02783   0.01797   0.0185   0.1611   1.0000
  10.000   0.9559   0.02863   0.01878   0.0199   0.1558   1.0000
  10.250   0.9701   0.02944   0.01963   0.0212   0.1505   1.0000
  10.500   0.9827   0.03033   0.02050   0.0225   0.1462   1.0000
  10.750   0.9969   0.03125   0.02143   0.0237   0.1425   1.0000
  11.000   1.0112   0.03217   0.02244   0.0248   0.1383   1.0000
  11.250   1.0245   0.03313   0.02345   0.0259   0.1348   1.0000
  11.500   1.0371   0.03415   0.02444   0.0270   0.1318   1.0000
  11.750   1.0511   0.03523   0.02557   0.0279   0.1289   1.0000
  12.000   1.0644   0.03633   0.02680   0.0289   0.1259   1.0000
  12.250   1.0773   0.03748   0.02803   0.0298   0.1233   1.0000
  12.500   1.0893   0.03864   0.02923   0.0307   0.1209   1.0000
  12.750   1.1024   0.03982   0.03042   0.0315   0.1188   1.0000
  13.000   1.1150   0.04113   0.03178   0.0323   0.1166   1.0000
  13.250   1.1233   0.04263   0.03347   0.0332   0.1144   1.0000
  13.500   1.1322   0.04418   0.03516   0.0341   0.1124   1.0000
  13.750   1.1407   0.04576   0.03686   0.0348   0.1105   1.0000
  14.000   1.1496   0.04733   0.03852   0.0355   0.1088   1.0000
  14.250   1.1597   0.04883   0.04006   0.0360   0.1071   1.0000
  14.500   1.1733   0.05024   0.04145   0.0363   0.1056   1.0000
  14.750   1.1735   0.05255   0.04397   0.0370   0.1041   1.0000
  15.000   1.1700   0.05521   0.04687   0.0375   0.1027   1.0000
  15.250   1.1662   0.05806   0.04995   0.0377   0.1014   1.0000
  15.500   1.1609   0.06111   0.05319   0.0377   0.1001   1.0000
  15.750   1.1553   0.06433   0.05658   0.0374   0.0988   1.0000
  16.000   1.1500   0.06763   0.06004   0.0369   0.0976   1.0000
  16.250   1.1473   0.07074   0.06326   0.0363   0.0964   1.0000
  16.500   1.1511   0.07321   0.06578   0.0358   0.0952   1.0000
  16.750   1.1636   0.07488   0.06742   0.0356   0.0939   1.0000
  17.000   1.1311   0.08193   0.07478   0.0329   0.0933   1.0000
  17.250   1.0781   0.09272   0.08595   0.0275   0.0927   1.0000
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