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MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: MH 94 16.03% (mh94-il)
Reynolds number: 500,000
Max Cl/Cd: 62.71 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh94-il-500000.txt
Download as CSV file: xf-mh94-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 94  16.03%                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.6598   0.12638   0.12337  -0.0433   1.0000   0.0150
 -17.000  -0.6965   0.11421   0.11106  -0.0497   1.0000   0.0146
 -16.750  -0.7325   0.10303   0.09971  -0.0559   1.0000   0.0143
 -16.500  -0.7676   0.09277   0.08924  -0.0616   1.0000   0.0143
 -16.250  -0.8001   0.08386   0.08011  -0.0662   1.0000   0.0142
 -16.000  -0.8215   0.07742   0.07350  -0.0691   1.0000   0.0140
 -15.750  -0.8478   0.07067   0.06651  -0.0717   1.0000   0.0138
 -15.500  -0.8611   0.06624   0.06196  -0.0731   1.0000   0.0139
 -15.250  -0.8832   0.06083   0.05630  -0.0742   1.0000   0.0136
 -15.000  -0.8958   0.05700   0.05230  -0.0745   1.0000   0.0136
 -14.750  -0.9030   0.05407   0.04926  -0.0744   1.0000   0.0137
 -14.500  -0.9111   0.05113   0.04617  -0.0739   1.0000   0.0137
 -14.250  -0.9166   0.04861   0.04355  -0.0731   1.0000   0.0138
 -14.000  -0.9224   0.04605   0.04084  -0.0720   1.0000   0.0137
 -13.750  -0.9250   0.04407   0.03877  -0.0708   1.0000   0.0139
 -13.500  -0.9278   0.04190   0.03646  -0.0691   1.0000   0.0138
 -13.250  -0.9290   0.04021   0.03469  -0.0675   1.0000   0.0140
 -13.000  -0.9293   0.03845   0.03282  -0.0655   1.0000   0.0139
 -12.750  -0.9292   0.03696   0.03125  -0.0635   1.0000   0.0141
 -12.500  -0.9287   0.03554   0.02974  -0.0613   1.0000   0.0142
 -12.250  -0.9276   0.03416   0.02828  -0.0589   1.0000   0.0142
 -12.000  -0.9269   0.03292   0.02696  -0.0564   1.0000   0.0143
 -11.750  -0.9263   0.03173   0.02571  -0.0537   1.0000   0.0144
 -11.500  -0.9260   0.03064   0.02455  -0.0508   1.0000   0.0145
 -11.250  -0.9268   0.02957   0.02342  -0.0476   1.0000   0.0146
 -11.000  -0.9283   0.02864   0.02242  -0.0443   1.0000   0.0147
 -10.750  -0.9313   0.02777   0.02149  -0.0405   1.0000   0.0148
 -10.500  -0.9267   0.02681   0.02045  -0.0381   0.9993   0.0149
 -10.250  -0.9037   0.02578   0.01936  -0.0390   0.9966   0.0151
 -10.000  -0.8818   0.02463   0.01814  -0.0398   0.9939   0.0154
  -9.750  -0.8651   0.02360   0.01709  -0.0395   0.9898   0.0156
  -9.500  -0.8441   0.02273   0.01621  -0.0396   0.9860   0.0160
  -9.250  -0.8164   0.02192   0.01538  -0.0409   0.9837   0.0165
  -9.000  -0.7920   0.02126   0.01468  -0.0412   0.9803   0.0172
  -8.750  -0.7697   0.02050   0.01387  -0.0410   0.9758   0.0177
  -8.500  -0.7417   0.01972   0.01305  -0.0419   0.9730   0.0183
  -8.250  -0.7113   0.01887   0.01221  -0.0434   0.9711   0.0193
  -8.000  -0.6928   0.01828   0.01159  -0.0421   0.9655   0.0202
  -7.750  -0.6655   0.01764   0.01091  -0.0425   0.9619   0.0215
  -7.500  -0.6346   0.01694   0.01021  -0.0438   0.9596   0.0235
  -7.250  -0.6013   0.01629   0.00957  -0.0454   0.9580   0.0267
  -7.000  -0.5825   0.01575   0.00903  -0.0439   0.9521   0.0307
  -6.750  -0.5556   0.01509   0.00842  -0.0441   0.9482   0.0398
  -6.500  -0.5248   0.01434   0.00782  -0.0452   0.9458   0.0619
  -6.250  -0.4932   0.01344   0.00720  -0.0467   0.9440   0.1069
  -6.000  -0.4724   0.01257   0.00667  -0.0459   0.9392   0.1689
  -5.750  -0.4502   0.01181   0.00620  -0.0453   0.9338   0.2310
  -5.500  -0.4187   0.01108   0.00577  -0.0465   0.9314   0.2949
  -5.250  -0.3835   0.01051   0.00542  -0.0483   0.9298   0.3486
  -5.000  -0.3462   0.01004   0.00513  -0.0504   0.9287   0.3930
  -4.750  -0.3089   0.00966   0.00487  -0.0524   0.9276   0.4311
  -4.500  -0.2921   0.00944   0.00472  -0.0499   0.9188   0.4549
  -4.250  -0.2568   0.00917   0.00448  -0.0513   0.9162   0.4772
  -4.000  -0.2206   0.00890   0.00427  -0.0528   0.9140   0.5013
  -3.750  -0.1833   0.00865   0.00407  -0.0546   0.9119   0.5231
  -3.500  -0.1617   0.00853   0.00394  -0.0530   0.9032   0.5366
  -3.250  -0.1272   0.00831   0.00374  -0.0541   0.8990   0.5486
  -3.000  -0.0901   0.00810   0.00352  -0.0557   0.8954   0.5593
  -2.750  -0.0660   0.00800   0.00341  -0.0547   0.8855   0.5695
  -2.500  -0.0309   0.00782   0.00323  -0.0559   0.8795   0.5790
  -2.250  -0.0042   0.00774   0.00313  -0.0554   0.8688   0.5887
  -2.000   0.0299   0.00761   0.00298  -0.0564   0.8604   0.5978
  -1.750   0.0567   0.00756   0.00291  -0.0559   0.8477   0.6074
  -1.500   0.0855   0.00749   0.00284  -0.0559   0.8351   0.6162
  -1.250   0.1152   0.00747   0.00276  -0.0560   0.8222   0.6254
  -1.000   0.1439   0.00744   0.00269  -0.0559   0.8078   0.6334
  -0.750   0.1708   0.00744   0.00267  -0.0554   0.7922   0.6416
  -0.500   0.1979   0.00747   0.00263  -0.0551   0.7756   0.6496
  -0.250   0.2244   0.00749   0.00263  -0.0546   0.7582   0.6571
   0.000   0.2508   0.00755   0.00261  -0.0540   0.7397   0.6652
   0.250   0.2764   0.00760   0.00262  -0.0534   0.7205   0.6724
   0.500   0.3017   0.00769   0.00264  -0.0526   0.7002   0.6799
   1.000   0.3500   0.00790   0.00270  -0.0507   0.6525   0.6946
   1.250   0.3725   0.00807   0.00274  -0.0495   0.6232   0.7024
   1.500   0.3954   0.00820   0.00279  -0.0483   0.5948   0.7095
   1.750   0.4178   0.00837   0.00287  -0.0471   0.5683   0.7168
   2.000   0.4408   0.00855   0.00294  -0.0460   0.5415   0.7246
   2.250   0.4629   0.00872   0.00303  -0.0447   0.5138   0.7315
   2.500   0.4853   0.00892   0.00315  -0.0436   0.4880   0.7391
   2.750   0.5079   0.00913   0.00325  -0.0425   0.4603   0.7465
   3.000   0.5293   0.00935   0.00339  -0.0411   0.4327   0.7535
   3.250   0.5516   0.00959   0.00352  -0.0400   0.4053   0.7612
   3.500   0.5732   0.00984   0.00367  -0.0388   0.3795   0.7683
   3.750   0.5953   0.01006   0.00384  -0.0376   0.3554   0.7755
   4.000   0.6176   0.01033   0.00399  -0.0366   0.3315   0.7834
   4.250   0.6387   0.01059   0.00418  -0.0353   0.3086   0.7903
   4.500   0.6604   0.01085   0.00438  -0.0341   0.2877   0.7980
   4.750   0.6823   0.01111   0.00456  -0.0330   0.2682   0.8057
   5.000   0.7031   0.01136   0.00477  -0.0316   0.2501   0.8131
   5.250   0.7240   0.01164   0.00497  -0.0303   0.2329   0.8215
   5.500   0.7435   0.01189   0.00519  -0.0287   0.2160   0.8291
   5.750   0.7631   0.01217   0.00542  -0.0272   0.1998   0.8377
   6.000   0.7820   0.01247   0.00567  -0.0256   0.1840   0.8460
   6.250   0.8006   0.01279   0.00594  -0.0239   0.1694   0.8551
   6.500   0.8185   0.01313   0.00623  -0.0221   0.1563   0.8644
   6.750   0.8367   0.01345   0.00654  -0.0203   0.1457   0.8745
   7.000   0.8540   0.01376   0.00685  -0.0184   0.1373   0.8848
   7.250   0.8702   0.01414   0.00720  -0.0163   0.1300   0.8968
   7.500   0.8868   0.01439   0.00751  -0.0142   0.1249   0.9098
   7.750   0.9012   0.01468   0.00782  -0.0117   0.1201   0.9257
   8.000   0.9148   0.01506   0.00822  -0.0092   0.1158   0.9477
   8.250   0.9456   0.01538   0.00861  -0.0102   0.1124   0.9719
   8.500   0.9742   0.01582   0.00903  -0.0110   0.1088   1.0000
   8.750   0.9920   0.01639   0.00956  -0.0099   0.1056   1.0000
   9.000   1.0113   0.01687   0.01005  -0.0088   0.1034   1.0000
   9.250   1.0316   0.01726   0.01047  -0.0079   0.1013   1.0000
   9.500   1.0509   0.01769   0.01092  -0.0069   0.0992   1.0000
   9.750   1.0684   0.01821   0.01144  -0.0056   0.0974   1.0000
  10.000   1.0834   0.01886   0.01208  -0.0040   0.0954   1.0000
  10.250   1.0961   0.01970   0.01290  -0.0022   0.0935   1.0000
  10.500   1.1145   0.02016   0.01343  -0.0011   0.0925   1.0000
  10.750   1.1318   0.02070   0.01402   0.0001   0.0912   1.0000
  11.000   1.1483   0.02129   0.01465   0.0014   0.0899   1.0000
  11.250   1.1642   0.02191   0.01530   0.0026   0.0885   1.0000
  11.500   1.1793   0.02258   0.01599   0.0039   0.0872   1.0000
  11.750   1.1930   0.02337   0.01679   0.0053   0.0861   1.0000
  12.000   1.2045   0.02437   0.01779   0.0069   0.0847   1.0000
  12.250   1.2167   0.02543   0.01888   0.0083   0.0835   1.0000
  12.500   1.2316   0.02617   0.01969   0.0094   0.0829   1.0000
  12.750   1.2458   0.02698   0.02057   0.0106   0.0821   1.0000
  13.000   1.2592   0.02785   0.02150   0.0117   0.0812   1.0000
  13.250   1.2722   0.02875   0.02246   0.0128   0.0802   1.0000
  13.500   1.2845   0.02973   0.02350   0.0138   0.0792   1.0000
  13.750   1.2965   0.03074   0.02455   0.0148   0.0783   1.0000
  14.000   1.3078   0.03184   0.02568   0.0158   0.0775   1.0000
  14.250   1.3186   0.03303   0.02690   0.0168   0.0767   1.0000
  14.500   1.3297   0.03432   0.02821   0.0176   0.0757   1.0000
  14.750   1.3417   0.03577   0.02970   0.0184   0.0746   1.0000
  15.000   1.3510   0.03706   0.03108   0.0193   0.0742   1.0000
  15.250   1.3591   0.03843   0.03255   0.0200   0.0735   1.0000
  15.500   1.3673   0.03992   0.03414   0.0206   0.0729   1.0000
  15.750   1.3750   0.04148   0.03580   0.0212   0.0722   1.0000
  16.000   1.3821   0.04315   0.03755   0.0216   0.0715   1.0000
  16.250   1.3888   0.04488   0.03936   0.0220   0.0708   1.0000
  16.500   1.3951   0.04667   0.04122   0.0222   0.0701   1.0000
  16.750   1.4013   0.04853   0.04314   0.0224   0.0693   1.0000
  17.000   1.4078   0.05042   0.04508   0.0224   0.0687   1.0000
  17.250   1.4148   0.05232   0.04702   0.0224   0.0681   1.0000
  17.500   1.4219   0.05429   0.04901   0.0225   0.0673   1.0000
  17.750   1.4256   0.05672   0.05154   0.0225   0.0665   1.0000
  18.000   1.4245   0.05957   0.05452   0.0219   0.0661   1.0000
  18.250   1.4231   0.06258   0.05767   0.0212   0.0656   1.0000
  18.500   1.4217   0.06569   0.06091   0.0203   0.0651   1.0000
  18.750   1.4182   0.06916   0.06451   0.0191   0.0644   1.0000
  19.000   1.4152   0.07270   0.06817   0.0178   0.0639   1.0000
  19.250   1.4115   0.07641   0.07199   0.0162   0.0632   1.0000
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