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MH 117 9.8% (mh117-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 117 9.8% (mh117-il)
Reynolds number: 1,000,000
Max Cl/Cd: 100.94 at α=3.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh117-il-1000000-n5.txt
Download as CSV file: xf-mh117-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 117  9.8%                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.7009   0.07721   0.07516  -0.0362   1.0000   0.0017
 -12.250  -0.7448   0.06580   0.06371  -0.0432   1.0000   0.0017
 -12.000  -0.8044   0.05146   0.04930  -0.0526   1.0000   0.0016
 -11.750  -0.8551   0.03567   0.03320  -0.0674   1.0000   0.0016
 -11.500  -0.8643   0.03182   0.02912  -0.0678   1.0000   0.0016
 -11.250  -0.8644   0.02897   0.02605  -0.0671   1.0000   0.0016
 -11.000  -0.8582   0.02678   0.02366  -0.0660   1.0000   0.0016
 -10.750  -0.8496   0.02481   0.02149  -0.0647   1.0000   0.0016
 -10.500  -0.8298   0.02300   0.01946  -0.0652   0.9987   0.0017
 -10.250  -0.8029   0.02130   0.01755  -0.0668   0.9957   0.0017
 -10.000  -0.7757   0.01986   0.01593  -0.0681   0.9925   0.0017
  -9.750  -0.7484   0.01876   0.01468  -0.0689   0.9884   0.0018
  -9.500  -0.7190   0.01775   0.01354  -0.0701   0.9847   0.0018
  -9.250  -0.6886   0.01687   0.01254  -0.0714   0.9810   0.0019
  -9.000  -0.6611   0.01587   0.01140  -0.0720   0.9741   0.0019
  -8.750  -0.6322   0.01445   0.00976  -0.0732   0.9671   0.0022
  -8.500  -0.6018   0.01372   0.00893  -0.0741   0.9576   0.0023
  -8.250  -0.5714   0.01314   0.00826  -0.0750   0.9461   0.0024
  -8.000  -0.5425   0.01265   0.00767  -0.0754   0.9314   0.0026
  -7.750  -0.5161   0.01217   0.00706  -0.0752   0.9151   0.0027
  -7.500  -0.4905   0.01177   0.00655  -0.0748   0.8991   0.0028
  -7.250  -0.4650   0.01139   0.00605  -0.0744   0.8842   0.0030
  -7.000  -0.4392   0.01104   0.00557  -0.0740   0.8698   0.0031
  -6.500  -0.3870   0.01041   0.00473  -0.0733   0.8436   0.0034
  -6.250  -0.3605   0.01012   0.00436  -0.0730   0.8315   0.0035
  -6.000  -0.3340   0.00978   0.00392  -0.0728   0.8201   0.0041
  -5.750  -0.3073   0.00952   0.00360  -0.0725   0.8093   0.0048
  -5.500  -0.2804   0.00929   0.00328  -0.0723   0.7987   0.0063
  -5.250  -0.2534   0.00901   0.00297  -0.0721   0.7884   0.0094
  -5.000  -0.2265   0.00873   0.00268  -0.0719   0.7786   0.0158
  -4.750  -0.1995   0.00848   0.00243  -0.0718   0.7691   0.0264
  -4.500  -0.1723   0.00824   0.00222  -0.0717   0.7594   0.0384
  -4.250  -0.1450   0.00804   0.00203  -0.0716   0.7503   0.0514
  -4.000  -0.1177   0.00786   0.00187  -0.0714   0.7415   0.0662
  -3.750  -0.0901   0.00770   0.00173  -0.0714   0.7323   0.0803
  -3.500  -0.0624   0.00757   0.00161  -0.0713   0.7241   0.0924
  -3.250  -0.0347   0.00748   0.00148  -0.0712   0.7152   0.1018
  -3.000  -0.0068   0.00736   0.00138  -0.0712   0.7068   0.1153
  -2.750   0.0209   0.00727   0.00129  -0.0711   0.6984   0.1288
  -2.500   0.0488   0.00717   0.00120  -0.0711   0.6895   0.1451
  -2.250   0.0766   0.00708   0.00112  -0.0710   0.6808   0.1626
  -2.000   0.1043   0.00702   0.00106  -0.0709   0.6714   0.1785
  -1.750   0.1322   0.00693   0.00100  -0.0709   0.6615   0.1975
  -1.500   0.1599   0.00685   0.00095  -0.0709   0.6517   0.2215
  -1.250   0.1877   0.00680   0.00091  -0.0708   0.6417   0.2415
  -1.000   0.2155   0.00672   0.00088  -0.0708   0.6316   0.2685
  -0.750   0.2433   0.00666   0.00086  -0.0707   0.6217   0.2934
  -0.500   0.2710   0.00660   0.00085  -0.0707   0.6117   0.3227
   0.000   0.3263   0.00647   0.00085  -0.0706   0.5903   0.3907
   0.250   0.3539   0.00641   0.00086  -0.0705   0.5792   0.4282
   0.500   0.3814   0.00636   0.00088  -0.0705   0.5674   0.4695
   0.750   0.4088   0.00631   0.00091  -0.0704   0.5550   0.5122
   1.000   0.4361   0.00626   0.00095  -0.0703   0.5420   0.5585
   1.250   0.4632   0.00622   0.00100  -0.0701   0.5276   0.6080
   1.500   0.4902   0.00618   0.00106  -0.0699   0.5125   0.6589
   1.750   0.5168   0.00615   0.00113  -0.0697   0.4961   0.7123
   2.000   0.5428   0.00614   0.00122  -0.0692   0.4770   0.7681
   2.250   0.5680   0.00614   0.00132  -0.0686   0.4570   0.8230
   2.500   0.5918   0.00617   0.00142  -0.0676   0.4341   0.8788
   2.750   0.6145   0.00624   0.00153  -0.0663   0.4079   0.9367
   3.000   0.6499   0.00645   0.00164  -0.0680   0.3763   0.9871
   3.250   0.6783   0.00672   0.00178  -0.0683   0.3462   1.0000
   3.500   0.7039   0.00700   0.00193  -0.0679   0.3165   1.0000
   3.750   0.7294   0.00729   0.00210  -0.0675   0.2892   1.0000
   4.000   0.7548   0.00759   0.00227  -0.0671   0.2605   1.0000
   4.250   0.7801   0.00791   0.00246  -0.0667   0.2328   1.0000
   4.500   0.8058   0.00818   0.00265  -0.0664   0.2119   1.0000
   4.750   0.8315   0.00846   0.00285  -0.0661   0.1935   1.0000
   5.000   0.8568   0.00876   0.00306  -0.0657   0.1726   1.0000
   5.250   0.8821   0.00907   0.00329  -0.0653   0.1539   1.0000
   5.500   0.9074   0.00936   0.00351  -0.0649   0.1391   1.0000
   5.750   0.9325   0.00968   0.00376  -0.0645   0.1228   1.0000
   6.000   0.9575   0.01000   0.00403  -0.0641   0.1079   1.0000
   6.250   0.9824   0.01032   0.00430  -0.0637   0.0953   1.0000
   6.500   1.0069   0.01068   0.00459  -0.0632   0.0820   1.0000
   6.750   1.0314   0.01103   0.00490  -0.0627   0.0712   1.0000
   7.000   1.0555   0.01140   0.00522  -0.0622   0.0611   1.0000
   7.250   1.0803   0.01170   0.00553  -0.0617   0.0553   1.0000
   7.500   1.1043   0.01207   0.00588  -0.0612   0.0486   1.0000
   7.750   1.1285   0.01240   0.00621  -0.0606   0.0437   1.0000
   8.000   1.1517   0.01283   0.00660  -0.0600   0.0364   1.0000
   8.250   1.1740   0.01331   0.00703  -0.0592   0.0282   1.0000
   8.500   1.1963   0.01379   0.00746  -0.0585   0.0220   1.0000
   8.750   1.2183   0.01427   0.00794  -0.0577   0.0170   1.0000
   9.000   1.2397   0.01478   0.00843  -0.0568   0.0129   1.0000
   9.250   1.2609   0.01530   0.00895  -0.0559   0.0101   1.0000
   9.500   1.2820   0.01580   0.00946  -0.0549   0.0079   1.0000
   9.750   1.3019   0.01638   0.01005  -0.0539   0.0057   1.0000
  10.000   1.3210   0.01699   0.01068  -0.0527   0.0039   1.0000
  10.250   1.3403   0.01756   0.01128  -0.0515   0.0031   1.0000
  10.500   1.3584   0.01818   0.01196  -0.0502   0.0025   1.0000
  10.750   1.3761   0.01878   0.01261  -0.0488   0.0020   1.0000
  11.000   1.3926   0.01942   0.01331  -0.0472   0.0017   1.0000
  11.250   1.4059   0.02008   0.01403  -0.0451   0.0015   1.0000
  11.500   1.4175   0.02079   0.01480  -0.0428   0.0013   1.0000
  11.750   1.4281   0.02157   0.01564  -0.0404   0.0012   1.0000
  12.000   1.4393   0.02232   0.01646  -0.0383   0.0011   1.0000
  12.250   1.4491   0.02319   0.01742  -0.0361   0.0010   1.0000
  12.500   1.4590   0.02408   0.01838  -0.0341   0.0009   1.0000
  12.750   1.4679   0.02508   0.01947  -0.0322   0.0009   1.0000
  13.000   1.4757   0.02621   0.02068  -0.0304   0.0009   1.0000
  13.250   1.4820   0.02752   0.02208  -0.0285   0.0008   1.0000
  13.500   1.4883   0.02889   0.02354  -0.0269   0.0008   1.0000
  13.750   1.4937   0.03040   0.02514  -0.0255   0.0007   1.0000
  14.000   1.4970   0.03218   0.02701  -0.0241   0.0006   1.0000
  14.250   1.5012   0.03397   0.02889  -0.0230   0.0007   1.0000
  14.500   1.5021   0.03617   0.03120  -0.0221   0.0006   1.0000
  14.750   1.5021   0.03857   0.03371  -0.0213   0.0006   1.0000
  15.000   1.5033   0.04095   0.03620  -0.0209   0.0006   1.0000
  15.250   1.4955   0.04449   0.03989  -0.0206   0.0005   1.0000
  15.500   1.4945   0.04739   0.04290  -0.0207   0.0005   1.0000
  15.750   1.4883   0.05109   0.04672  -0.0212   0.0005   1.0000
  16.000   1.4755   0.05583   0.05163  -0.0222   0.0004   1.0000
  16.250   1.4670   0.06031   0.05624  -0.0235   0.0004   1.0000
  16.500   1.4566   0.06532   0.06139  -0.0253   0.0004   1.0000
  16.750   1.4458   0.07067   0.06688  -0.0274   0.0004   1.0000
  17.000   1.4315   0.07692   0.07328  -0.0303   0.0004   1.0000
  17.250   1.4181   0.08330   0.07979  -0.0334   0.0004   1.0000
  17.500   1.3979   0.09131   0.08797  -0.0376   0.0004   1.0000
  17.750   1.3764   0.10000   0.09682  -0.0423   0.0004   1.0000
  18.000   1.3514   0.10973   0.10671  -0.0477   0.0004   1.0000
  18.250   1.3225   0.12070   0.11784  -0.0540   0.0004   1.0000
  18.500   1.3040   0.12953   0.12680  -0.0591   0.0005   1.0000
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