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MH 114 13.02% (mh114-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 114 13.02% (mh114-il)
Reynolds number: 1,000,000
Max Cl/Cd: 140.57 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh114-il-1000000-n5.txt
Download as CSV file: xf-mh114-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 114  13.02%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.1602   0.02747   0.02449  -0.1785   0.8287   0.0040
  -9.500  -0.1576   0.02267   0.01928  -0.1832   0.8196   0.0040
  -9.250  -0.1411   0.02055   0.01689  -0.1845   0.8124   0.0040
  -9.000  -0.1218   0.01862   0.01468  -0.1856   0.8066   0.0040
  -8.750  -0.0998   0.01710   0.01292  -0.1863   0.8004   0.0041
  -8.500  -0.0760   0.01601   0.01162  -0.1868   0.7947   0.0041
  -8.250  -0.0508   0.01505   0.01049  -0.1872   0.7896   0.0041
  -8.000  -0.0250   0.01422   0.00950  -0.1876   0.7839   0.0041
  -7.750   0.0011   0.01355   0.00867  -0.1878   0.7787   0.0042
  -7.500   0.0281   0.01292   0.00792  -0.1881   0.7737   0.0042
  -7.250   0.0553   0.01238   0.00726  -0.1883   0.7684   0.0042
  -7.000   0.0823   0.01169   0.00642  -0.1886   0.7630   0.0044
  -6.750   0.1101   0.01111   0.00573  -0.1890   0.7581   0.0045
  -6.500   0.1380   0.01072   0.00526  -0.1892   0.7529   0.0047
  -6.250   0.1658   0.01041   0.00487  -0.1893   0.7474   0.0049
  -6.000   0.1939   0.01013   0.00453  -0.1895   0.7426   0.0051
  -5.750   0.2222   0.00987   0.00421  -0.1897   0.7371   0.0054
  -5.500   0.2501   0.00965   0.00392  -0.1898   0.7316   0.0057
  -5.250   0.2785   0.00944   0.00365  -0.1899   0.7266   0.0060
  -5.000   0.3069   0.00923   0.00339  -0.1901   0.7210   0.0064
  -4.750   0.3349   0.00904   0.00315  -0.1902   0.7153   0.0070
  -4.500   0.3633   0.00888   0.00295  -0.1903   0.7101   0.0077
  -4.250   0.3917   0.00875   0.00277  -0.1905   0.7041   0.0084
  -4.000   0.4195   0.00862   0.00259  -0.1905   0.6981   0.0098
  -3.750   0.4481   0.00849   0.00245  -0.1906   0.6924   0.0114
  -3.500   0.4762   0.00839   0.00232  -0.1907   0.6860   0.0139
  -3.250   0.5042   0.00829   0.00220  -0.1908   0.6799   0.0187
  -3.000   0.5326   0.00818   0.00210  -0.1909   0.6733   0.0255
  -2.750   0.5602   0.00811   0.00202  -0.1909   0.6664   0.0351
  -2.500   0.5887   0.00800   0.00194  -0.1911   0.6600   0.0475
  -2.250   0.6165   0.00793   0.00188  -0.1911   0.6528   0.0624
  -2.000   0.6445   0.00786   0.00183  -0.1912   0.6460   0.0824
  -1.750   0.6725   0.00778   0.00180  -0.1913   0.6384   0.1079
  -1.500   0.7003   0.00772   0.00178  -0.1914   0.6312   0.1383
  -1.250   0.7281   0.00767   0.00177  -0.1915   0.6233   0.1663
  -1.000   0.7555   0.00766   0.00178  -0.1914   0.6154   0.1944
  -0.750   0.7832   0.00763   0.00180  -0.1915   0.6073   0.2267
  -0.500   0.8105   0.00761   0.00183  -0.1914   0.5987   0.2662
  -0.250   0.8378   0.00761   0.00187  -0.1914   0.5898   0.3013
   0.000   0.8649   0.00762   0.00192  -0.1913   0.5812   0.3358
   0.250   0.8916   0.00766   0.00198  -0.1912   0.5719   0.3694
   0.500   0.9187   0.00769   0.00205  -0.1911   0.5628   0.4031
   0.750   0.9450   0.00775   0.00213  -0.1909   0.5534   0.4375
   1.000   0.9718   0.00780   0.00221  -0.1907   0.5440   0.4702
   1.250   0.9980   0.00788   0.00231  -0.1905   0.5345   0.5034
   1.500   1.0239   0.00797   0.00242  -0.1902   0.5242   0.5350
   1.750   1.0501   0.00805   0.00253  -0.1899   0.5147   0.5656
   2.000   1.0755   0.00816   0.00265  -0.1895   0.5048   0.5955
   2.250   1.1010   0.00827   0.00278  -0.1892   0.4942   0.6263
   2.500   1.1264   0.00838   0.00292  -0.1888   0.4846   0.6577
   2.750   1.1509   0.00852   0.00307  -0.1882   0.4739   0.6894
   3.000   1.1759   0.00864   0.00322  -0.1877   0.4636   0.7235
   3.250   1.2001   0.00876   0.00339  -0.1871   0.4535   0.7605
   3.500   1.2230   0.00890   0.00358  -0.1862   0.4428   0.8052
   3.750   1.2449   0.00897   0.00375  -0.1850   0.4330   0.8632
   4.000   1.2609   0.00897   0.00386  -0.1825   0.4235   1.0000
   4.250   1.2830   0.00921   0.00404  -0.1815   0.4127   1.0000
   4.500   1.3053   0.00942   0.00421  -0.1805   0.4023   1.0000
   4.750   1.3266   0.00967   0.00441  -0.1794   0.3923   1.0000
   5.000   1.3477   0.00993   0.00461  -0.1782   0.3819   1.0000
   5.250   1.3689   0.01017   0.00483  -0.1770   0.3720   1.0000
   5.500   1.3893   0.01046   0.00507  -0.1758   0.3621   1.0000
   5.750   1.4098   0.01074   0.00531  -0.1745   0.3518   1.0000
   6.000   1.4300   0.01103   0.00556  -0.1733   0.3425   1.0000
   6.250   1.4493   0.01137   0.00585  -0.1718   0.3326   1.0000
   6.500   1.4694   0.01166   0.00613  -0.1706   0.3229   1.0000
   6.750   1.4882   0.01202   0.00645  -0.1691   0.3134   1.0000
   7.000   1.5066   0.01239   0.00678  -0.1676   0.3036   1.0000
   7.250   1.5252   0.01276   0.00712  -0.1662   0.2936   1.0000
   7.500   1.5425   0.01319   0.00751  -0.1645   0.2841   1.0000
   7.750   1.5596   0.01363   0.00793  -0.1629   0.2738   1.0000
   8.000   1.5771   0.01406   0.00834  -0.1613   0.2650   1.0000
   8.250   1.5928   0.01459   0.00883  -0.1595   0.2552   1.0000
   8.500   1.6086   0.01512   0.00933  -0.1578   0.2447   1.0000
   8.750   1.6241   0.01567   0.00987  -0.1560   0.2353   1.0000
   9.000   1.6381   0.01631   0.01047  -0.1541   0.2251   1.0000
   9.250   1.6523   0.01696   0.01110  -0.1523   0.2150   1.0000
   9.500   1.6666   0.01762   0.01175  -0.1505   0.2061   1.0000
   9.750   1.6790   0.01841   0.01250  -0.1485   0.1963   1.0000
  10.000   1.6898   0.01931   0.01336  -0.1464   0.1844   1.0000
  10.250   1.7030   0.02010   0.01414  -0.1446   0.1757   1.0000
  10.500   1.7137   0.02105   0.01507  -0.1426   0.1661   1.0000
  10.750   1.7241   0.02207   0.01606  -0.1407   0.1571   1.0000
  11.000   1.7355   0.02304   0.01703  -0.1389   0.1488   1.0000
  11.250   1.7443   0.02422   0.01819  -0.1369   0.1395   1.0000
  11.500   1.7527   0.02546   0.01940  -0.1349   0.1306   1.0000
  11.750   1.7630   0.02659   0.02055  -0.1332   0.1236   1.0000
  12.000   1.7702   0.02800   0.02194  -0.1313   0.1157   1.0000
  12.250   1.7783   0.02938   0.02332  -0.1296   0.1081   1.0000
  12.500   1.7849   0.03092   0.02486  -0.1279   0.1000   1.0000
  12.750   1.7897   0.03265   0.02657  -0.1260   0.0922   1.0000
  13.000   1.7966   0.03427   0.02821  -0.1245   0.0858   1.0000
  13.250   1.8024   0.03604   0.02998  -0.1230   0.0800   1.0000
  13.500   1.8077   0.03790   0.03185  -0.1215   0.0740   1.0000
  13.750   1.8126   0.03984   0.03382  -0.1201   0.0690   1.0000
  14.000   1.8153   0.04205   0.03603  -0.1187   0.0629   1.0000
  14.250   1.8183   0.04431   0.03830  -0.1175   0.0569   1.0000
  14.500   1.8195   0.04683   0.04083  -0.1162   0.0513   1.0000
  14.750   1.8199   0.04949   0.04351  -0.1151   0.0458   1.0000
  15.000   1.8202   0.05225   0.04628  -0.1141   0.0407   1.0000
  15.250   1.8198   0.05517   0.04924  -0.1133   0.0367   1.0000
  15.500   1.8190   0.05822   0.05232  -0.1125   0.0323   1.0000
  15.750   1.8184   0.06132   0.05545  -0.1120   0.0288   1.0000
  16.000   1.8161   0.06472   0.05889  -0.1115   0.0256   1.0000
  16.250   1.8149   0.06806   0.06228  -0.1112   0.0227   1.0000
  16.500   1.8122   0.07168   0.06597  -0.1110   0.0203   1.0000
  16.750   1.8098   0.07535   0.06969  -0.1110   0.0182   1.0000
  17.000   1.8070   0.07913   0.07354  -0.1111   0.0165   1.0000
  17.250   1.8041   0.08298   0.07746  -0.1113   0.0148   1.0000
  17.500   1.8003   0.08705   0.08160  -0.1117   0.0135   1.0000
  17.750   1.7970   0.09109   0.08572  -0.1122   0.0122   1.0000
  18.000   1.7919   0.09548   0.09018  -0.1129   0.0111   1.0000
  18.250   1.7878   0.09975   0.09455  -0.1137   0.0101   1.0000
  18.500   1.7823   0.10429   0.09917  -0.1147   0.0092   1.0000
  18.750   1.7767   0.10890   0.10386  -0.1158   0.0084   1.0000
  19.000   1.7716   0.11347   0.10852  -0.1171   0.0077   1.0000
  19.250   1.7662   0.11810   0.11324  -0.1185   0.0071   1.0000
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