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MH 94 16.03% (mh94-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: MH 94 16.03% (mh94-il)
Reynolds number: 1,000,000
Max Cl/Cd: 75.82 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh94-il-1000000-n5.txt
Download as CSV file: xf-mh94-il-1000000-n5.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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.9488   0.09857   0.09490  -0.0558   1.0000   0.0059
 -18.750  -0.9628   0.09293   0.08917  -0.0583   1.0000   0.0059
 -18.500  -0.9791   0.08706   0.08319  -0.0608   1.0000   0.0058
 -18.250  -0.9861   0.08272   0.07877  -0.0624   1.0000   0.0058
 -18.000  -0.9985   0.07773   0.07369  -0.0643   1.0000   0.0059
 -17.750  -1.0105   0.07295   0.06881  -0.0660   1.0000   0.0058
 -17.500  -1.0204   0.06858   0.06435  -0.0675   1.0000   0.0059
 -17.250  -1.0306   0.06433   0.06000  -0.0687   1.0000   0.0059
 -17.000  -1.0361   0.06083   0.05642  -0.0695   1.0000   0.0059
 -16.750  -1.0437   0.05720   0.05271  -0.0702   1.0000   0.0059
 -16.500  -1.0516   0.05371   0.04913  -0.0707   1.0000   0.0060
 -16.250  -1.0611   0.05019   0.04552  -0.0709   1.0000   0.0061
 -16.000  -1.0633   0.04762   0.04289  -0.0708   1.0000   0.0060
 -15.750  -1.0689   0.04483   0.04003  -0.0704   1.0000   0.0060
 -15.500  -1.0705   0.04260   0.03773  -0.0698   1.0000   0.0061
 -15.250  -1.0771   0.04002   0.03507  -0.0690   1.0000   0.0061
 -15.000  -1.0798   0.03793   0.03291  -0.0679   1.0000   0.0061
 -14.750  -1.0833   0.03585   0.03077  -0.0667   1.0000   0.0062
 -14.500  -1.0731   0.03387   0.02872  -0.0676   0.9994   0.0062
 -14.250  -1.0612   0.03205   0.02685  -0.0685   0.9985   0.0063
 -14.000  -1.0497   0.03030   0.02503  -0.0692   0.9975   0.0063
 -13.750  -1.0353   0.02883   0.02351  -0.0699   0.9964   0.0064
 -13.500  -1.0209   0.02729   0.02191  -0.0706   0.9952   0.0064
 -13.250  -1.0036   0.02607   0.02065  -0.0713   0.9941   0.0065
 -13.000  -0.9873   0.02477   0.01929  -0.0720   0.9930   0.0066
 -12.750  -0.9730   0.02366   0.01814  -0.0718   0.9911   0.0067
 -12.500  -0.9558   0.02266   0.01710  -0.0719   0.9893   0.0067
 -12.250  -0.9375   0.02165   0.01605  -0.0722   0.9876   0.0068
 -12.000  -0.9170   0.02076   0.01512  -0.0727   0.9862   0.0069
 -11.750  -0.8948   0.01991   0.01423  -0.0734   0.9849   0.0070
 -11.500  -0.8712   0.01914   0.01343  -0.0742   0.9838   0.0071
 -11.250  -0.8464   0.01838   0.01263  -0.0752   0.9829   0.0073
 -11.000  -0.8287   0.01776   0.01198  -0.0745   0.9802   0.0073
 -10.750  -0.8097   0.01716   0.01136  -0.0739   0.9772   0.0075
 -10.500  -0.7867   0.01654   0.01070  -0.0741   0.9752   0.0076
 -10.250  -0.7610   0.01597   0.01010  -0.0746   0.9736   0.0077
 -10.000  -0.7334   0.01539   0.00949  -0.0755   0.9725   0.0080
  -9.750  -0.7047   0.01486   0.00894  -0.0765   0.9713   0.0081
  -9.500  -0.6890   0.01444   0.00850  -0.0746   0.9669   0.0084
  -9.250  -0.6699   0.01402   0.00807  -0.0734   0.9629   0.0089
  -9.000  -0.6440   0.01361   0.00766  -0.0735   0.9604   0.0093
  -8.750  -0.6173   0.01322   0.00724  -0.0736   0.9584   0.0097
  -8.500  -0.5945   0.01290   0.00691  -0.0729   0.9552   0.0102
  -8.250  -0.5774   0.01258   0.00659  -0.0710   0.9498   0.0109
  -8.000  -0.5535   0.01224   0.00625  -0.0705   0.9462   0.0118
  -7.750  -0.5270   0.01191   0.00591  -0.0705   0.9434   0.0128
  -7.500  -0.5066   0.01163   0.00563  -0.0691   0.9384   0.0142
  -7.250  -0.4847   0.01135   0.00535  -0.0681   0.9330   0.0160
  -7.000  -0.4584   0.01104   0.00505  -0.0679   0.9290   0.0188
  -6.750  -0.4348   0.01077   0.00479  -0.0671   0.9237   0.0220
  -6.500  -0.4113   0.01049   0.00453  -0.0664   0.9172   0.0271
  -6.250  -0.3842   0.01020   0.00426  -0.0663   0.9120   0.0326
  -6.000  -0.3610   0.00993   0.00402  -0.0655   0.9044   0.0406
  -5.750  -0.3354   0.00963   0.00375  -0.0651   0.8970   0.0526
  -5.500  -0.3111   0.00933   0.00351  -0.0645   0.8886   0.0681
  -5.250  -0.2872   0.00894   0.00322  -0.0639   0.8792   0.0960
  -5.000  -0.2650   0.00851   0.00295  -0.0630   0.8685   0.1343
  -4.750  -0.2424   0.00808   0.00267  -0.0622   0.8575   0.1813
  -4.500  -0.2205   0.00763   0.00242  -0.0612   0.8449   0.2350
  -4.250  -0.1977   0.00725   0.00221  -0.0604   0.8318   0.2850
  -4.000  -0.1730   0.00704   0.00207  -0.0598   0.8182   0.3168
  -3.750  -0.1490   0.00681   0.00193  -0.0590   0.8031   0.3554
  -3.500  -0.1252   0.00661   0.00182  -0.0583   0.7868   0.3945
  -3.250  -0.1004   0.00651   0.00174  -0.0576   0.7691   0.4218
  -3.000  -0.0752   0.00648   0.00168  -0.0569   0.7504   0.4381
  -2.750  -0.0499   0.00647   0.00163  -0.0563   0.7306   0.4501
  -2.500  -0.0245   0.00650   0.00159  -0.0557   0.7096   0.4616
  -2.250   0.0006   0.00652   0.00156  -0.0550   0.6887   0.4727
  -2.000   0.0259   0.00656   0.00154  -0.0544   0.6679   0.4829
  -1.750   0.0513   0.00660   0.00152  -0.0538   0.6473   0.4935
  -1.500   0.0768   0.00665   0.00151  -0.0532   0.6272   0.5024
  -1.250   0.1023   0.00671   0.00151  -0.0526   0.6073   0.5125
  -1.000   0.1277   0.00677   0.00152  -0.0520   0.5861   0.5224
  -0.750   0.1531   0.00685   0.00153  -0.0515   0.5649   0.5327
  -0.500   0.1786   0.00692   0.00155  -0.0509   0.5428   0.5418
  -0.250   0.2042   0.00702   0.00157  -0.0504   0.5203   0.5505
   0.000   0.2294   0.00713   0.00161  -0.0498   0.4962   0.5581
   0.250   0.2542   0.00728   0.00166  -0.0491   0.4687   0.5664
   0.500   0.2779   0.00750   0.00172  -0.0483   0.4301   0.5735
   0.750   0.3014   0.00772   0.00180  -0.0474   0.3907   0.5814
   1.000   0.3258   0.00792   0.00188  -0.0467   0.3605   0.5893
   1.250   0.3512   0.00806   0.00195  -0.0462   0.3391   0.5964
   1.500   0.3767   0.00821   0.00203  -0.0457   0.3186   0.6043
   1.750   0.4022   0.00836   0.00212  -0.0452   0.3003   0.6114
   2.000   0.4274   0.00851   0.00221  -0.0447   0.2814   0.6189
   2.250   0.4527   0.00868   0.00231  -0.0441   0.2631   0.6266
   2.500   0.4778   0.00884   0.00242  -0.0436   0.2465   0.6335
   2.750   0.5031   0.00899   0.00253  -0.0431   0.2324   0.6414
   3.250   0.5529   0.00934   0.00277  -0.0419   0.2035   0.6563
   3.500   0.5779   0.00951   0.00290  -0.0414   0.1903   0.6637
   3.750   0.6027   0.00968   0.00303  -0.0408   0.1777   0.6705
   4.000   0.6273   0.00986   0.00318  -0.0401   0.1666   0.6779
   4.250   0.6516   0.01006   0.00333  -0.0395   0.1551   0.6847
   4.500   0.6756   0.01026   0.00349  -0.0387   0.1441   0.6913
   4.750   0.6996   0.01045   0.00366  -0.0380   0.1339   0.6987
   5.000   0.7235   0.01066   0.00383  -0.0373   0.1252   0.7052
   5.250   0.7469   0.01087   0.00402  -0.0365   0.1173   0.7120
   5.500   0.7706   0.01104   0.00419  -0.0357   0.1119   0.7195
   6.000   0.8157   0.01142   0.00455  -0.0337   0.1024   0.7326
   6.250   0.8379   0.01160   0.00474  -0.0326   0.0983   0.7403
   6.500   0.8593   0.01183   0.00495  -0.0314   0.0941   0.7468
   6.750   0.8816   0.01200   0.00516  -0.0304   0.0917   0.7541
   7.000   0.9037   0.01221   0.00538  -0.0294   0.0890   0.7615
   7.250   0.9253   0.01244   0.00562  -0.0282   0.0867   0.7687
   7.500   0.9462   0.01268   0.00587  -0.0270   0.0841   0.7766
   7.750   0.9681   0.01289   0.00611  -0.0260   0.0827   0.7840
   8.000   0.9895   0.01310   0.00636  -0.0249   0.0813   0.7921
   8.250   1.0107   0.01333   0.00662  -0.0237   0.0798   0.8003
   8.500   1.0309   0.01360   0.00691  -0.0225   0.0778   0.8081
   8.750   1.0508   0.01387   0.00721  -0.0211   0.0761   0.8174
   9.000   1.0707   0.01415   0.00752  -0.0198   0.0746   0.8261
   9.250   1.0909   0.01439   0.00781  -0.0186   0.0738   0.8362
   9.500   1.1105   0.01465   0.00813  -0.0173   0.0729   0.8460
   9.750   1.1297   0.01492   0.00845  -0.0159   0.0720   0.8572
  10.000   1.1482   0.01520   0.00879  -0.0144   0.0708   0.8694
  10.250   1.1657   0.01551   0.00915  -0.0128   0.0698   0.8826
  10.500   1.1820   0.01583   0.00953  -0.0109   0.0687   0.9001
  10.750   1.1968   0.01615   0.00993  -0.0089   0.0674   0.9244
  11.000   1.2218   0.01650   0.01038  -0.0089   0.0664   0.9686
  11.250   1.2431   0.01686   0.01078  -0.0083   0.0658   1.0000
  11.500   1.2616   0.01726   0.01120  -0.0072   0.0651   1.0000
  11.750   1.2792   0.01769   0.01167  -0.0059   0.0645   1.0000
  12.000   1.2964   0.01816   0.01216  -0.0046   0.0637   1.0000
  12.250   1.3131   0.01865   0.01267  -0.0033   0.0629   1.0000
  12.500   1.3288   0.01919   0.01324  -0.0019   0.0623   1.0000
  12.750   1.3445   0.01975   0.01382  -0.0006   0.0615   1.0000
  13.000   1.3587   0.02039   0.01448   0.0008   0.0605   1.0000
  13.250   1.3720   0.02110   0.01522   0.0023   0.0596   1.0000
  13.500   1.3862   0.02177   0.01593   0.0037   0.0591   1.0000
  13.750   1.4009   0.02243   0.01663   0.0049   0.0587   1.0000
  14.000   1.4147   0.02314   0.01740   0.0062   0.0582   1.0000
  14.250   1.4282   0.02390   0.01820   0.0074   0.0577   1.0000
  14.500   1.4408   0.02473   0.01908   0.0086   0.0571   1.0000
  14.750   1.4528   0.02562   0.02002   0.0098   0.0564   1.0000
  15.000   1.4642   0.02658   0.02102   0.0110   0.0558   1.0000
  15.250   1.4748   0.02761   0.02210   0.0121   0.0553   1.0000
  15.500   1.4844   0.02876   0.02328   0.0132   0.0547   1.0000
  15.750   1.4932   0.03001   0.02457   0.0142   0.0540   1.0000
  16.000   1.5005   0.03140   0.02601   0.0152   0.0533   1.0000
  16.250   1.5065   0.03295   0.02762   0.0162   0.0528   1.0000
  16.500   1.5161   0.03428   0.02901   0.0168   0.0524   1.0000
  16.750   1.5236   0.03582   0.03063   0.0174   0.0521   1.0000
  17.000   1.5313   0.03740   0.03228   0.0179   0.0516   1.0000
  17.250   1.5378   0.03913   0.03408   0.0183   0.0511   1.0000
  17.500   1.5437   0.04097   0.03599   0.0186   0.0506   1.0000
  17.750   1.5486   0.04298   0.03806   0.0188   0.0500   1.0000
  18.000   1.5523   0.04517   0.04032   0.0188   0.0494   1.0000
  18.250   1.5543   0.04760   0.04282   0.0187   0.0490   1.0000
  18.500   1.5554   0.05021   0.04549   0.0184   0.0485   1.0000
  18.750   1.5554   0.05304   0.04839   0.0180   0.0481   1.0000
  19.000   1.5524   0.05630   0.05173   0.0173   0.0475   1.0000
  19.250   1.5479   0.05984   0.05535   0.0163   0.0469   1.0000
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