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MH 104 15.28% (mh104-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 104 15.28% (mh104-il)
Reynolds number: 500,000
Max Cl/Cd: 92.63 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh104-il-500000-n5.txt
Download as CSV file: xf-mh104-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 104  15.28%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.7583   0.14080   0.13807   0.0143   1.0000   0.0048
 -17.000  -0.7823   0.12986   0.12696   0.0083   1.0000   0.0047
 -16.750  -0.8004   0.12081   0.11779   0.0032   1.0000   0.0047
 -16.500  -0.8177   0.11246   0.10931  -0.0015   1.0000   0.0046
 -16.250  -0.8318   0.10492   0.10166  -0.0059   1.0000   0.0046
 -16.000  -0.8453   0.09785   0.09447  -0.0100   1.0000   0.0046
 -15.750  -0.8661   0.08987   0.08635  -0.0145   1.0000   0.0046
 -15.500  -0.8785   0.08342   0.07977  -0.0183   1.0000   0.0046
 -15.250  -0.8927   0.07712   0.07335  -0.0218   1.0000   0.0046
 -15.000  -0.9017   0.07175   0.06787  -0.0250   1.0000   0.0046
 -14.750  -0.9161   0.06595   0.06195  -0.0281   1.0000   0.0046
 -14.500  -0.9272   0.06060   0.05645  -0.0311   1.0000   0.0046
 -14.250  -0.9335   0.05613   0.05186  -0.0335   1.0000   0.0046
 -14.000  -0.9385   0.05194   0.04755  -0.0358   1.0000   0.0047
 -13.750  -0.9457   0.04767   0.04315  -0.0379   1.0000   0.0047
 -13.500  -0.9538   0.04358   0.03892  -0.0395   1.0000   0.0046
 -13.250  -0.9559   0.04044   0.03567  -0.0406   1.0000   0.0047
 -13.000  -0.9593   0.03742   0.03254  -0.0413   1.0000   0.0048
 -12.750  -0.9648   0.03451   0.02950  -0.0412   1.0000   0.0048
 -12.500  -0.9651   0.03236   0.02723  -0.0406   1.0000   0.0048
 -12.250  -0.9666   0.03033   0.02511  -0.0394   1.0000   0.0049
 -12.000  -0.9658   0.02865   0.02333  -0.0377   1.0000   0.0050
 -11.750  -0.9619   0.02731   0.02190  -0.0357   1.0000   0.0050
 -11.500  -0.9565   0.02615   0.02067  -0.0336   1.0000   0.0051
 -11.250  -0.9509   0.02506   0.01951  -0.0312   1.0000   0.0051
 -11.000  -0.9447   0.02405   0.01843  -0.0285   1.0000   0.0052
 -10.750  -0.9369   0.02316   0.01746  -0.0258   1.0000   0.0053
 -10.500  -0.9077   0.02214   0.01625  -0.0273   0.8945   0.0054
 -10.250  -0.8978   0.02148   0.01535  -0.0244   0.8456   0.0054
 -10.000  -0.8845   0.02084   0.01453  -0.0222   0.8154   0.0055
  -9.750  -0.8695   0.02017   0.01369  -0.0203   0.7909   0.0058
  -9.500  -0.8528   0.01954   0.01291  -0.0186   0.7702   0.0058
  -9.250  -0.8348   0.01892   0.01215  -0.0171   0.7525   0.0060
  -9.000  -0.8156   0.01835   0.01144  -0.0157   0.7361   0.0062
  -8.750  -0.7958   0.01778   0.01073  -0.0145   0.7208   0.0064
  -8.500  -0.7748   0.01727   0.01010  -0.0133   0.7060   0.0066
  -8.250  -0.7545   0.01666   0.00939  -0.0122   0.6921   0.0069
  -8.000  -0.7325   0.01618   0.00881  -0.0112   0.6793   0.0073
  -7.750  -0.7096   0.01575   0.00830  -0.0104   0.6674   0.0078
  -7.500  -0.6863   0.01535   0.00779  -0.0096   0.6553   0.0084
  -7.000  -0.6390   0.01458   0.00685  -0.0081   0.6318   0.0102
  -6.750  -0.6146   0.01423   0.00643  -0.0075   0.6213   0.0119
  -6.500  -0.5901   0.01390   0.00604  -0.0068   0.6113   0.0145
  -6.250  -0.5653   0.01357   0.00567  -0.0063   0.6014   0.0182
  -6.000  -0.5406   0.01323   0.00530  -0.0057   0.5918   0.0241
  -5.750  -0.5162   0.01287   0.00495  -0.0051   0.5818   0.0344
  -5.500  -0.4921   0.01244   0.00458  -0.0044   0.5723   0.0533
  -5.250  -0.4688   0.01194   0.00419  -0.0037   0.5635   0.0849
  -5.000  -0.4457   0.01139   0.00383  -0.0030   0.5550   0.1302
  -4.750  -0.4220   0.01094   0.00356  -0.0024   0.5472   0.1764
  -4.500  -0.3967   0.01064   0.00336  -0.0019   0.5391   0.2101
  -4.250  -0.3704   0.01047   0.00319  -0.0016   0.5313   0.2315
  -4.000  -0.3442   0.01027   0.00304  -0.0013   0.5231   0.2537
  -3.750  -0.3182   0.01008   0.00291  -0.0009   0.5156   0.2817
  -3.500  -0.2917   0.00992   0.00278  -0.0006   0.5081   0.3039
  -3.250  -0.2648   0.00982   0.00267  -0.0003   0.5015   0.3187
  -3.000  -0.2376   0.00972   0.00256  -0.0001   0.4949   0.3323
  -2.750  -0.2105   0.00965   0.00246   0.0001   0.4886   0.3457
  -2.500  -0.1832   0.00956   0.00238   0.0003   0.4825   0.3597
  -2.250  -0.1559   0.00949   0.00230   0.0005   0.4760   0.3737
  -2.000  -0.1287   0.00943   0.00223   0.0007   0.4702   0.3880
  -1.750  -0.1013   0.00936   0.00217   0.0009   0.4645   0.4032
  -1.500  -0.0741   0.00930   0.00212   0.0011   0.4592   0.4186
  -1.250  -0.0470   0.00925   0.00207   0.0013   0.4546   0.4351
  -1.000  -0.0197   0.00918   0.00204   0.0014   0.4499   0.4520
  -0.750   0.0074   0.00912   0.00200   0.0017   0.4449   0.4705
  -0.500   0.0343   0.00908   0.00198   0.0019   0.4402   0.4899
  -0.250   0.0615   0.00901   0.00197   0.0021   0.4358   0.5106
   0.000   0.0882   0.00894   0.00196   0.0024   0.4316   0.5339
   0.250   0.1149   0.00889   0.00196   0.0027   0.4276   0.5586
   0.500   0.1413   0.00883   0.00197   0.0030   0.4240   0.5857
   0.750   0.1677   0.00876   0.00199   0.0034   0.4200   0.6149
   1.000   0.1939   0.00869   0.00202   0.0038   0.4160   0.6444
   1.250   0.2199   0.00865   0.00205   0.0042   0.4124   0.6756
   1.500   0.2456   0.00860   0.00210   0.0048   0.4090   0.7082
   1.750   0.2716   0.00853   0.00216   0.0053   0.4055   0.7417
   2.000   0.2976   0.00848   0.00222   0.0058   0.4017   0.7748
   2.250   0.3239   0.00846   0.00230   0.0063   0.3981   0.8073
   2.500   0.3509   0.00847   0.00238   0.0066   0.3945   0.8393
   2.750   0.3805   0.00847   0.00249   0.0064   0.3912   0.8691
   3.000   0.4130   0.00852   0.00261   0.0055   0.3873   0.8946
   3.250   0.4491   0.00863   0.00274   0.0039   0.3834   0.9136
   3.500   0.4861   0.00878   0.00287   0.0020   0.3795   0.9279
   3.750   0.5213   0.00888   0.00300   0.0005   0.3759   0.9395
   4.000   0.5590   0.00900   0.00313  -0.0016   0.3719   0.9466
   4.250   0.5912   0.00913   0.00326  -0.0025   0.3679   0.9552
   4.500   0.6266   0.00929   0.00340  -0.0042   0.3641   0.9604
   4.750   0.6563   0.00940   0.00354  -0.0045   0.3603   0.9682
   5.000   0.6920   0.00952   0.00368  -0.0062   0.3557   0.9720
   5.250   0.7260   0.00968   0.00382  -0.0076   0.3510   0.9767
   5.500   0.7568   0.00982   0.00398  -0.0083   0.3466   0.9821
   5.750   0.7946   0.00993   0.00412  -0.0105   0.3408   0.9851
   6.000   0.8317   0.01009   0.00427  -0.0126   0.3352   0.9891
   6.250   0.8671   0.01022   0.00444  -0.0143   0.3292   0.9929
   6.500   0.9027   0.01035   0.00458  -0.0162   0.3224   0.9955
   6.750   0.9374   0.01049   0.00474  -0.0178   0.3158   0.9979
   7.000   0.9717   0.01064   0.00491  -0.0194   0.3075   0.9999
   7.250   0.9950   0.01081   0.00509  -0.0187   0.3002   1.0000
   7.500   1.0170   0.01102   0.00529  -0.0178   0.2913   1.0000
   7.750   1.0393   0.01122   0.00552  -0.0169   0.2821   1.0000
   8.000   1.0608   0.01148   0.00576  -0.0159   0.2717   1.0000
   8.250   1.0816   0.01178   0.00604  -0.0148   0.2605   1.0000
   8.500   1.1017   0.01213   0.00636  -0.0137   0.2480   1.0000
   8.750   1.1213   0.01250   0.00671  -0.0125   0.2350   1.0000
   9.000   1.1401   0.01292   0.00710  -0.0111   0.2221   1.0000
   9.250   1.1583   0.01336   0.00752  -0.0097   0.2093   1.0000
   9.500   1.1755   0.01385   0.00797  -0.0082   0.1963   1.0000
   9.750   1.1917   0.01437   0.00846  -0.0066   0.1832   1.0000
  10.000   1.2065   0.01495   0.00900  -0.0048   0.1695   1.0000
  10.250   1.2201   0.01556   0.00958  -0.0028   0.1566   1.0000
  10.500   1.2322   0.01620   0.01018  -0.0006   0.1444   1.0000
  10.750   1.2418   0.01692   0.01086   0.0018   0.1320   1.0000
  11.000   1.2492   0.01769   0.01160   0.0045   0.1215   1.0000
  11.250   1.2510   0.01841   0.01232   0.0082   0.1122   1.0000
  11.500   1.2525   0.01926   0.01318   0.0115   0.1053   1.0000
  11.750   1.2543   0.02035   0.01428   0.0140   0.0981   1.0000
  12.000   1.2574   0.02163   0.01558   0.0159   0.0910   1.0000
  12.250   1.2591   0.02323   0.01720   0.0172   0.0847   1.0000
  12.500   1.2630   0.02488   0.01889   0.0181   0.0786   1.0000
  13.000   1.2647   0.02914   0.02320   0.0191   0.0664   1.0000
  13.250   1.2631   0.03167   0.02575   0.0193   0.0614   1.0000
  13.500   1.2628   0.03417   0.02830   0.0194   0.0562   1.0000
  14.000   1.2570   0.03983   0.03405   0.0191   0.0479   1.0000
  14.250   1.2504   0.04312   0.03737   0.0189   0.0434   1.0000
  14.500   1.2464   0.04619   0.04049   0.0185   0.0399   1.0000
  14.750   1.2415   0.04938   0.04374   0.0181   0.0371   1.0000
  15.000   1.2343   0.05293   0.04733   0.0176   0.0340   1.0000
  15.250   1.2298   0.05630   0.05075   0.0169   0.0310   1.0000
  15.500   1.2229   0.06002   0.05450   0.0161   0.0283   1.0000
  15.750   1.2198   0.06336   0.05791   0.0154   0.0267   1.0000
  16.000   1.2138   0.06709   0.06169   0.0145   0.0241   1.0000
  16.250   1.2075   0.07093   0.06557   0.0135   0.0221   1.0000
  16.500   1.2043   0.07445   0.06916   0.0125   0.0208   1.0000
  16.750   1.2006   0.07808   0.07286   0.0115   0.0198   1.0000
  17.000   1.1930   0.08225   0.07706   0.0103   0.0179   1.0000
  17.250   1.1893   0.08597   0.08087   0.0092   0.0168   1.0000
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