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MH 102 16.99% (mh102-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: MH 102 16.99% (mh102-il)
Reynolds number: 500,000
Max Cl/Cd: 94.17 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh102-il-500000.txt
Download as CSV file: xf-mh102-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 102  16.99%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.7232   0.14966   0.14643  -0.0191   1.0000   0.0116
 -19.500  -0.7426   0.14126   0.13787  -0.0238   1.0000   0.0117
 -19.250  -0.7549   0.13471   0.13120  -0.0274   1.0000   0.0116
 -19.000  -0.7642   0.12883   0.12522  -0.0306   1.0000   0.0117
 -18.750  -0.7727   0.12333   0.11961  -0.0335   1.0000   0.0117
 -18.500  -0.7780   0.11863   0.11483  -0.0358   1.0000   0.0117
 -18.250  -0.7846   0.11362   0.10972  -0.0384   1.0000   0.0118
 -18.000  -0.7914   0.10862   0.10460  -0.0410   1.0000   0.0119
 -17.750  -0.7940   0.10453   0.10044  -0.0430   1.0000   0.0119
 -17.500  -0.7986   0.10008   0.09589  -0.0452   1.0000   0.0120
 -17.250  -0.8007   0.09618   0.09192  -0.0470   1.0000   0.0121
 -17.000  -0.8009   0.09267   0.08836  -0.0486   1.0000   0.0121
 -16.750  -0.7999   0.08989   0.08556  -0.0493   1.0000   0.0123
 -16.500  -0.7996   0.08671   0.08236  -0.0506   1.0000   0.0124
 -16.250  -0.8002   0.08345   0.07908  -0.0518   1.0000   0.0125
 -16.000  -0.8016   0.08001   0.07561  -0.0533   1.0000   0.0127
 -15.750  -0.8034   0.07651   0.07207  -0.0548   1.0000   0.0127
 -15.500  -0.8067   0.07286   0.06839  -0.0563   1.0000   0.0128
 -15.250  -0.8102   0.06929   0.06476  -0.0578   1.0000   0.0128
 -15.000  -0.8177   0.06532   0.06075  -0.0596   1.0000   0.0131
 -14.750  -0.8256   0.06133   0.05670  -0.0613   1.0000   0.0133
 -14.500  -0.8323   0.05756   0.05287  -0.0629   1.0000   0.0132
 -14.250  -0.8418   0.05339   0.04863  -0.0647   1.0000   0.0135
 -14.000  -0.8506   0.04933   0.04450  -0.0665   1.0000   0.0136
 -13.750  -0.8622   0.04496   0.04005  -0.0684   1.0000   0.0137
 -13.500  -0.8705   0.04089   0.03589  -0.0703   1.0000   0.0138
 -13.250  -0.8781   0.03691   0.03181  -0.0722   1.0000   0.0140
 -13.000  -0.8843   0.03331   0.02811  -0.0739   1.0000   0.0140
 -12.750  -0.8902   0.03026   0.02495  -0.0748   1.0000   0.0143
 -12.500  -0.8956   0.02799   0.02257  -0.0743   1.0000   0.0144
 -12.250  -0.9057   0.02618   0.02067  -0.0720   1.0000   0.0147
 -12.000  -0.9255   0.02482   0.01926  -0.0668   1.0000   0.0148
 -11.750  -0.9380   0.02390   0.01830  -0.0614   1.0000   0.0150
 -11.500  -0.9445   0.02305   0.01743  -0.0568   1.0000   0.0154
 -11.250  -0.9136   0.02191   0.01623  -0.0590   0.9959   0.0162
 -11.000  -0.8787   0.02095   0.01519  -0.0616   0.9910   0.0172
 -10.750  -0.8481   0.01964   0.01384  -0.0637   0.9839   0.0190
 -10.500  -0.8157   0.01863   0.01276  -0.0656   0.9769   0.0208
 -10.250  -0.7835   0.01765   0.01174  -0.0674   0.9684   0.0237
 -10.000  -0.7533   0.01669   0.01075  -0.0686   0.9566   0.0274
  -9.750  -0.7212   0.01570   0.00976  -0.0702   0.9440   0.0339
  -9.500  -0.6884   0.01477   0.00884  -0.0718   0.9294   0.0441
  -9.250  -0.6601   0.01392   0.00802  -0.0724   0.9107   0.0593
  -9.000  -0.6369   0.01318   0.00733  -0.0719   0.8903   0.0802
  -8.750  -0.6154   0.01259   0.00679  -0.0710   0.8711   0.1037
  -8.500  -0.5925   0.01220   0.00643  -0.0702   0.8537   0.1238
  -8.250  -0.5685   0.01193   0.00615  -0.0694   0.8379   0.1402
  -8.000  -0.5435   0.01174   0.00593  -0.0688   0.8234   0.1532
  -7.750  -0.5180   0.01161   0.00573  -0.0682   0.8093   0.1635
  -7.500  -0.4919   0.01151   0.00556  -0.0677   0.7952   0.1729
  -7.250  -0.4662   0.01137   0.00539  -0.0672   0.7819   0.1811
  -7.000  -0.4393   0.01135   0.00525  -0.0668   0.7697   0.1888
  -6.750  -0.4135   0.01120   0.00510  -0.0663   0.7572   0.1967
  -6.500  -0.3864   0.01117   0.00497  -0.0659   0.7451   0.2035
  -6.250  -0.3603   0.01106   0.00479  -0.0654   0.7332   0.2096
  -6.000  -0.3335   0.01099   0.00469  -0.0651   0.7212   0.2167
  -5.750  -0.3062   0.01097   0.00456  -0.0648   0.7102   0.2230
  -5.500  -0.2801   0.01082   0.00440  -0.0643   0.6992   0.2292
  -5.250  -0.2528   0.01075   0.00427  -0.0640   0.6882   0.2346
  -5.000  -0.2256   0.01074   0.00413  -0.0637   0.6774   0.2388
  -4.750  -0.1992   0.01054   0.00395  -0.0633   0.6663   0.2448
  -4.500  -0.1721   0.01047   0.00383  -0.0629   0.6562   0.2501
  -4.250  -0.1446   0.01044   0.00371  -0.0627   0.6458   0.2550
  -4.000  -0.1179   0.01030   0.00356  -0.0623   0.6362   0.2611
  -3.750  -0.0909   0.01024   0.00345  -0.0620   0.6260   0.2670
  -3.500  -0.0632   0.01022   0.00336  -0.0618   0.6161   0.2727
  -3.250  -0.0366   0.01011   0.00324  -0.0614   0.6063   0.2797
  -3.000  -0.0091   0.01005   0.00316  -0.0612   0.5971   0.2865
  -2.750   0.0181   0.01003   0.00307  -0.0609   0.5881   0.2933
  -2.500   0.0453   0.00995   0.00301  -0.0606   0.5793   0.3016
  -2.250   0.0728   0.00996   0.00295  -0.0604   0.5703   0.3095
  -2.000   0.0998   0.00987   0.00290  -0.0601   0.5617   0.3186
  -1.500   0.1543   0.00982   0.00282  -0.0596   0.5457   0.3387
  -1.250   0.1817   0.00979   0.00279  -0.0593   0.5375   0.3498
  -1.000   0.2087   0.00980   0.00278  -0.0591   0.5300   0.3619
  -0.750   0.2361   0.00974   0.00277  -0.0588   0.5225   0.3745
  -0.500   0.2631   0.00976   0.00276  -0.0586   0.5153   0.3884
  -0.250   0.2905   0.00974   0.00277  -0.0583   0.5085   0.4042
   0.000   0.3177   0.00972   0.00278  -0.0581   0.5015   0.4211
   0.250   0.3443   0.00975   0.00281  -0.0578   0.4951   0.4390
   0.500   0.3716   0.00969   0.00283  -0.0576   0.4889   0.4588
   0.750   0.3984   0.00967   0.00287  -0.0573   0.4826   0.4816
   1.000   0.4246   0.00968   0.00292  -0.0569   0.4767   0.5078
   1.500   0.4778   0.00959   0.00304  -0.0562   0.4654   0.5700
   1.750   0.5034   0.00961   0.00312  -0.0557   0.4598   0.6072
   2.000   0.5295   0.00953   0.00321  -0.0552   0.4548   0.6491
   2.250   0.5550   0.00948   0.00330  -0.0546   0.4494   0.6924
   2.500   0.5797   0.00948   0.00340  -0.0538   0.4444   0.7362
   2.750   0.6042   0.00946   0.00353  -0.0529   0.4394   0.7828
   3.000   0.6286   0.00941   0.00365  -0.0519   0.4345   0.8302
   3.250   0.6528   0.00942   0.00377  -0.0508   0.4296   0.8771
   3.500   0.6808   0.00955   0.00392  -0.0506   0.4242   0.9202
   3.750   0.7208   0.00961   0.00405  -0.0529   0.4190   0.9528
   4.000   0.7647   0.00975   0.00418  -0.0562   0.4130   0.9725
   4.250   0.8072   0.00999   0.00432  -0.0593   0.4069   0.9853
   4.500   0.8493   0.01007   0.00445  -0.0622   0.4014   0.9962
   4.750   0.8817   0.01020   0.00455  -0.0633   0.3957   1.0000
   5.000   0.9019   0.01039   0.00467  -0.0619   0.3906   1.0000
   5.250   0.9241   0.01049   0.00480  -0.0607   0.3858   1.0000
   5.500   0.9464   0.01061   0.00492  -0.0597   0.3803   1.0000
   5.750   0.9680   0.01078   0.00505  -0.0585   0.3750   1.0000
   6.000   0.9904   0.01094   0.00521  -0.0574   0.3696   1.0000
   6.250   1.0135   0.01106   0.00535  -0.0565   0.3638   1.0000
   6.500   1.0355   0.01126   0.00550  -0.0554   0.3578   1.0000
   6.750   1.0585   0.01143   0.00568  -0.0545   0.3521   1.0000
   7.000   1.0816   0.01158   0.00584  -0.0536   0.3456   1.0000
   7.250   1.1028   0.01183   0.00604  -0.0525   0.3391   1.0000
   7.500   1.1264   0.01197   0.00623  -0.0517   0.3325   1.0000
   7.750   1.1479   0.01220   0.00643  -0.0506   0.3253   1.0000
   8.000   1.1696   0.01242   0.00666  -0.0496   0.3185   1.0000
   8.250   1.1909   0.01265   0.00689  -0.0485   0.3109   1.0000
   8.500   1.2109   0.01293   0.00715  -0.0472   0.3037   1.0000
   8.750   1.2314   0.01318   0.00741  -0.0459   0.2958   1.0000
   9.000   1.2493   0.01352   0.00772  -0.0444   0.2884   1.0000
   9.250   1.2677   0.01379   0.00801  -0.0428   0.2806   1.0000
   9.500   1.2810   0.01418   0.00836  -0.0404   0.2734   1.0000
   9.750   1.2978   0.01449   0.00870  -0.0386   0.2661   1.0000
  10.000   1.3096   0.01497   0.00913  -0.0361   0.2589   1.0000
  10.250   1.3261   0.01533   0.00953  -0.0344   0.2519   1.0000
  10.500   1.3381   0.01586   0.01004  -0.0322   0.2448   1.0000
  10.750   1.3524   0.01634   0.01054  -0.0303   0.2384   1.0000
  11.000   1.3648   0.01690   0.01111  -0.0284   0.2317   1.0000
  11.250   1.3755   0.01758   0.01179  -0.0263   0.2256   1.0000
  11.500   1.3886   0.01819   0.01243  -0.0246   0.2189   1.0000
  11.750   1.3961   0.01909   0.01331  -0.0225   0.2127   1.0000
  12.000   1.4093   0.01978   0.01406  -0.0210   0.2070   1.0000
  12.250   1.4179   0.02074   0.01503  -0.0193   0.2009   1.0000
  12.500   1.4256   0.02182   0.01612  -0.0177   0.1954   1.0000
  12.750   1.4362   0.02280   0.01714  -0.0164   0.1897   1.0000
  13.000   1.4410   0.02419   0.01853  -0.0149   0.1842   1.0000
  13.250   1.4497   0.02539   0.01978  -0.0137   0.1791   1.0000
  13.500   1.4566   0.02678   0.02121  -0.0127   0.1738   1.0000
  13.750   1.4578   0.02865   0.02307  -0.0114   0.1688   1.0000
  14.000   1.4665   0.03003   0.02453  -0.0107   0.1640   1.0000
  14.250   1.4703   0.03184   0.02638  -0.0099   0.1592   1.0000
  14.500   1.4683   0.03419   0.02872  -0.0090   0.1546   1.0000
  14.750   1.4756   0.03583   0.03045  -0.0086   0.1503   1.0000
  15.000   1.4765   0.03808   0.03274  -0.0081   0.1458   1.0000
  15.250   1.4719   0.04090   0.03557  -0.0076   0.1415   1.0000
  15.500   1.4771   0.04289   0.03765  -0.0074   0.1375   1.0000
  15.750   1.4766   0.04550   0.04030  -0.0073   0.1334   1.0000
  16.000   1.4707   0.04870   0.04351  -0.0073   0.1295   1.0000
  16.250   1.4726   0.05120   0.04609  -0.0074   0.1257   1.0000
  16.500   1.4712   0.05408   0.04904  -0.0076   0.1220   1.0000
  16.750   1.4649   0.05759   0.05256  -0.0080   0.1183   1.0000
  17.000   1.4630   0.06065   0.05568  -0.0084   0.1151   1.0000
  17.250   1.4623   0.06363   0.05874  -0.0088   0.1114   1.0000
  17.500   1.4565   0.06727   0.06241  -0.0095   0.1082   1.0000
  17.750   1.4491   0.07115   0.06632  -0.0103   0.1050   1.0000
  18.000   1.4496   0.07414   0.06940  -0.0110   0.1020   1.0000
  18.250   1.4454   0.07776   0.07307  -0.0119   0.0989   1.0000
  18.500   1.4362   0.08208   0.07740  -0.0130   0.0958   1.0000
  18.750   1.4342   0.08551   0.08092  -0.0140   0.0929   1.0000
  19.000   1.4310   0.08916   0.08464  -0.0151   0.0900   1.0000
  19.250   1.4236   0.09343   0.08894  -0.0165   0.0872   1.0000
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