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MH 201 13.08% (mh201-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: MH 201 13.08% (mh201-il)
Reynolds number: 200,000
Max Cl/Cd: 73.46 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh201-il-200000.txt
Download as CSV file: xf-mh201-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 201  13.08%                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.250  -0.4161   0.09149   0.08823  -0.0447   1.0000   0.0543
  -9.000  -0.4314   0.08844   0.08526  -0.0439   1.0000   0.0554
  -8.750  -0.4521   0.08538   0.08229  -0.0430   1.0000   0.0560
  -8.500  -0.4769   0.08231   0.07930  -0.0421   1.0000   0.0561
  -8.250  -0.4024   0.06079   0.05790  -0.0607   0.9860   0.0628
  -8.000  -0.4236   0.05499   0.05200  -0.0652   0.9782   0.0631
  -7.750  -0.4236   0.04971   0.04659  -0.0697   0.9723   0.0647
  -7.500  -0.4289   0.04519   0.04188  -0.0718   0.9633   0.0673
  -7.250  -0.4862   0.05397   0.05024  -0.0700   0.9667   0.0656
  -7.000  -0.4741   0.04892   0.04460  -0.0741   0.9603   0.0734
  -6.750  -0.4541   0.04618   0.04191  -0.0746   0.9554   0.0759
  -6.500  -0.4371   0.03123   0.02450  -0.0725   0.9493   0.0266
  -6.250  -0.4045   0.02835   0.02141  -0.0740   0.9472   0.0257
  -6.000  -0.3692   0.02600   0.01878  -0.0757   0.9456   0.0249
  -5.750  -0.3501   0.02457   0.01716  -0.0742   0.9386   0.0248
  -5.500  -0.3174   0.02305   0.01545  -0.0750   0.9355   0.0253
  -5.250  -0.2819   0.02178   0.01406  -0.0765   0.9333   0.0259
  -5.000  -0.2461   0.02028   0.01258  -0.0783   0.9315   0.0279
  -4.750  -0.2273   0.01980   0.01209  -0.0770   0.9240   0.0319
  -4.500  -0.1938   0.01872   0.01105  -0.0786   0.9208   0.0380
  -4.250  -0.1566   0.01735   0.00976  -0.0809   0.9185   0.0613
  -4.000  -0.1194   0.01494   0.00873  -0.0848   0.9170   0.3165
  -3.750  -0.0992   0.01411   0.00865  -0.0842   0.9102   0.4851
  -3.500  -0.0688   0.01382   0.00887  -0.0843   0.9064   0.6143
  -3.250  -0.0335   0.01400   0.00911  -0.0849   0.9039   0.6784
  -3.000   0.0052   0.01421   0.00924  -0.0861   0.9021   0.7109
  -2.750   0.0228   0.01457   0.00955  -0.0836   0.8942   0.7289
  -2.500   0.0560   0.01473   0.00963  -0.0839   0.8908   0.7456
  -2.250   0.0922   0.01482   0.00965  -0.0848   0.8883   0.7597
  -2.000   0.1294   0.01483   0.00958  -0.0858   0.8864   0.7724
  -1.750   0.1462   0.01505   0.00975  -0.0834   0.8775   0.7843
  -1.500   0.1783   0.01504   0.00970  -0.0834   0.8740   0.7937
  -1.250   0.2148   0.01492   0.00951  -0.0844   0.8714   0.8030
  -1.000   0.2343   0.01505   0.00959  -0.0826   0.8629   0.8136
  -0.750   0.2634   0.01495   0.00947  -0.0819   0.8585   0.8210
  -0.500   0.3006   0.01478   0.00923  -0.0832   0.8554   0.8308
  -0.250   0.3142   0.01487   0.00933  -0.0799   0.8458   0.8389
   0.000   0.3499   0.01465   0.00905  -0.0811   0.8415   0.8465
   0.250   0.3703   0.01461   0.00901  -0.0792   0.8334   0.8529
   0.500   0.4045   0.01443   0.00877  -0.0803   0.8273   0.8599
   0.750   0.4287   0.01429   0.00862  -0.0791   0.8201   0.8649
   1.000   0.4565   0.01413   0.00844  -0.0788   0.8123   0.8710
   1.250   0.4851   0.01399   0.00827  -0.0788   0.8047   0.8767
   1.500   0.5104   0.01381   0.00808  -0.0778   0.7961   0.8820
   1.750   0.5371   0.01371   0.00797  -0.0775   0.7870   0.8881
   2.000   0.5662   0.01349   0.00772  -0.0774   0.7788   0.8928
   2.250   0.5876   0.01338   0.00763  -0.0759   0.7680   0.8984
   2.500   0.6175   0.01324   0.00746  -0.0762   0.7586   0.9035
   2.750   0.6429   0.01305   0.00727  -0.0754   0.7480   0.9078
   3.000   0.6653   0.01292   0.00715  -0.0742   0.7357   0.9130
   3.250   0.6915   0.01281   0.00704  -0.0738   0.7233   0.9179
   3.500   0.7156   0.01265   0.00687  -0.0729   0.7107   0.9223
   3.750   0.7397   0.01250   0.00674  -0.0720   0.6967   0.9273
   4.000   0.7642   0.01241   0.00665  -0.0713   0.6809   0.9324
   4.250   0.7854   0.01228   0.00652  -0.0698   0.6637   0.9375
   4.500   0.8078   0.01219   0.00645  -0.0686   0.6446   0.9432
   4.750   0.8313   0.01214   0.00634  -0.0677   0.6239   0.9485
   5.000   0.8526   0.01213   0.00631  -0.0664   0.6003   0.9551
   5.250   0.8757   0.01221   0.00632  -0.0655   0.5748   0.9614
   5.500   0.8998   0.01237   0.00638  -0.0649   0.5469   0.9684
   5.750   0.9259   0.01263   0.00655  -0.0649   0.5163   0.9760
   6.000   0.9535   0.01298   0.00680  -0.0654   0.4836   0.9850
   6.250   0.9776   0.01336   0.00708  -0.0652   0.4514   1.0000
   6.500   0.9969   0.01384   0.00743  -0.0643   0.4213   1.0000
   6.750   1.0171   0.01438   0.00784  -0.0636   0.3912   1.0000
   7.000   1.0375   0.01495   0.00832  -0.0629   0.3620   1.0000
   7.250   1.0573   0.01555   0.00882  -0.0622   0.3341   1.0000
   7.500   1.0768   0.01619   0.00937  -0.0615   0.3080   1.0000
   7.750   1.0950   0.01692   0.00997  -0.0605   0.2841   1.0000
   8.000   1.1144   0.01761   0.01063  -0.0598   0.2608   1.0000
   8.250   1.1318   0.01840   0.01132  -0.0588   0.2402   1.0000
   8.500   1.1494   0.01919   0.01205  -0.0578   0.2209   1.0000
   8.750   1.1664   0.01999   0.01281  -0.0568   0.2030   1.0000
   9.000   1.1824   0.02085   0.01364  -0.0556   0.1871   1.0000
   9.250   1.1977   0.02175   0.01451  -0.0543   0.1728   1.0000
   9.500   1.2121   0.02271   0.01543  -0.0530   0.1601   1.0000
   9.750   1.2254   0.02374   0.01641  -0.0515   0.1488   1.0000
  10.000   1.2390   0.02474   0.01742  -0.0501   0.1383   1.0000
  10.250   1.2532   0.02572   0.01847  -0.0488   0.1286   1.0000
  10.500   1.2650   0.02693   0.01964  -0.0473   0.1203   1.0000
  10.750   1.2773   0.02801   0.02077  -0.0460   0.1124   1.0000
  11.000   1.2892   0.02927   0.02207  -0.0446   0.1052   1.0000
  11.250   1.2999   0.03052   0.02334  -0.0432   0.0987   1.0000
  11.500   1.3109   0.03190   0.02481  -0.0419   0.0925   1.0000
  11.750   1.3206   0.03323   0.02620  -0.0406   0.0868   1.0000
  12.000   1.3301   0.03485   0.02785  -0.0393   0.0815   1.0000
  12.250   1.3389   0.03628   0.02940  -0.0381   0.0764   1.0000
  12.500   1.3469   0.03817   0.03122  -0.0369   0.0716   1.0000
  12.750   1.3543   0.03976   0.03304  -0.0357   0.0676   1.0000
  13.000   1.3604   0.04152   0.03486  -0.0347   0.0637   1.0000
  13.250   1.3672   0.04367   0.03703  -0.0337   0.0599   1.0000
  13.500   1.3719   0.04566   0.03924  -0.0327   0.0567   1.0000
  13.750   1.3757   0.04775   0.04141  -0.0320   0.0536   1.0000
  14.000   1.3819   0.05020   0.04382  -0.0312   0.0504   1.0000
  14.250   1.3826   0.05272   0.04661  -0.0305   0.0482   1.0000
  14.500   1.3839   0.05529   0.04933  -0.0301   0.0458   1.0000
  14.750   1.3853   0.05792   0.05199  -0.0299   0.0436   1.0000
  15.000   1.3874   0.06098   0.05512  -0.0295   0.0413   1.0000
  15.250   1.3839   0.06438   0.05878  -0.0296   0.0397   1.0000
  15.500   1.3808   0.06786   0.06246  -0.0300   0.0380   1.0000
  15.750   1.3791   0.07122   0.06591  -0.0306   0.0364   1.0000
  16.000   1.3792   0.07455   0.06923  -0.0310   0.0346   1.0000
  16.250   1.3715   0.07916   0.07407  -0.0320   0.0335   1.0000
  16.500   1.3623   0.08408   0.07924  -0.0337   0.0324   1.0000
  16.750   1.3530   0.08918   0.08456  -0.0356   0.0314   1.0000
  17.000   1.3454   0.09415   0.08969  -0.0378   0.0303   1.0000
  17.250   1.3412   0.09861   0.09421  -0.0399   0.0291   1.0000
  17.500   1.3393   0.10265   0.09823  -0.0413   0.0278   1.0000
  17.750   1.3240   0.10946   0.10528  -0.0449   0.0273   1.0000
  18.000   1.3077   0.11674   0.11282  -0.0491   0.0269   1.0000
  18.250   1.2906   0.12446   0.12078  -0.0538   0.0265   1.0000
  18.500   1.2723   0.13274   0.12929  -0.0590   0.0263   1.0000
  18.750   1.2514   0.14195   0.13872  -0.0651   0.0262   1.0000
  19.000   1.2266   0.15246   0.14945  -0.0723   0.0264   1.0000
  19.250   1.1971   0.16469   0.16187  -0.0807   0.0270   1.0000
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