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MH 200 12.97% (mh200-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: MH 200 12.97% (mh200-il)
Reynolds number: 500,000
Max Cl/Cd: 85.66 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh200-il-500000-n5.txt
Download as CSV file: xf-mh200-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 200  12.97%                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.4666   0.08743   0.08518  -0.0529   1.0000   0.0045
 -11.000  -0.5452   0.06063   0.05826  -0.0684   1.0000   0.0041
 -10.750  -0.5752   0.05263   0.05008  -0.0737   0.9991   0.0041
 -10.250  -0.6152   0.03758   0.03425  -0.0841   0.9642   0.0040
 -10.000  -0.6094   0.03277   0.02898  -0.0874   0.9448   0.0040
  -9.750  -0.5945   0.02932   0.02510  -0.0893   0.9278   0.0041
  -9.500  -0.5791   0.02723   0.02270  -0.0894   0.9107   0.0042
  -9.250  -0.5678   0.02508   0.02018  -0.0881   0.8954   0.0042
  -9.000  -0.5506   0.02416   0.01909  -0.0872   0.8839   0.0044
  -8.750  -0.5346   0.02290   0.01758  -0.0860   0.8735   0.0047
  -8.500  -0.5177   0.02153   0.01596  -0.0848   0.8649   0.0048
  -8.250  -0.4985   0.02049   0.01469  -0.0838   0.8571   0.0050
  -8.000  -0.4790   0.01935   0.01335  -0.0828   0.8500   0.0051
  -7.750  -0.4585   0.01835   0.01217  -0.0819   0.8434   0.0052
  -7.500  -0.4378   0.01735   0.01102  -0.0810   0.8377   0.0052
  -7.250  -0.4166   0.01649   0.01004  -0.0802   0.8322   0.0052
  -7.000  -0.3951   0.01570   0.00911  -0.0794   0.8275   0.0053
  -6.750  -0.3731   0.01500   0.00832  -0.0787   0.8227   0.0053
  -6.500  -0.3508   0.01436   0.00758  -0.0780   0.8180   0.0054
  -6.250  -0.3278   0.01379   0.00692  -0.0774   0.8137   0.0055
  -6.000  -0.3049   0.01316   0.00621  -0.0768   0.8096   0.0057
  -5.750  -0.2814   0.01260   0.00558  -0.0763   0.8057   0.0060
  -5.500  -0.2566   0.01219   0.00511  -0.0760   0.8022   0.0065
  -5.250  -0.2311   0.01185   0.00469  -0.0757   0.7990   0.0071
  -5.000  -0.2052   0.01154   0.00431  -0.0755   0.7956   0.0080
  -4.750  -0.1795   0.01119   0.00393  -0.0753   0.7920   0.0104
  -4.500  -0.1536   0.01086   0.00361  -0.0752   0.7888   0.0179
  -4.250  -0.1285   0.01042   0.00329  -0.0750   0.7858   0.0484
  -4.000  -0.1045   0.00979   0.00298  -0.0748   0.7829   0.1227
  -3.750  -0.0803   0.00918   0.00273  -0.0748   0.7796   0.2119
  -3.500  -0.0557   0.00859   0.00251  -0.0747   0.7763   0.3089
  -3.250  -0.0303   0.00810   0.00232  -0.0747   0.7730   0.3970
  -3.000  -0.0041   0.00771   0.00215  -0.0748   0.7701   0.4736
  -2.750   0.0227   0.00744   0.00205  -0.0748   0.7671   0.5320
  -2.500   0.0498   0.00724   0.00200  -0.0749   0.7637   0.5833
  -2.250   0.0774   0.00713   0.00199  -0.0749   0.7603   0.6230
  -2.000   0.1053   0.00710   0.00199  -0.0749   0.7573   0.6517
  -1.750   0.1337   0.00711   0.00198  -0.0750   0.7544   0.6714
  -1.500   0.1620   0.00711   0.00199  -0.0751   0.7509   0.6860
  -1.250   0.1904   0.00712   0.00199  -0.0753   0.7472   0.6984
  -1.000   0.2187   0.00715   0.00200  -0.0754   0.7434   0.7082
  -0.750   0.2471   0.00718   0.00200  -0.0755   0.7395   0.7167
  -0.500   0.2753   0.00720   0.00201  -0.0756   0.7345   0.7248
  -0.250   0.3035   0.00722   0.00203  -0.0757   0.7297   0.7323
   0.000   0.3318   0.00727   0.00204  -0.0758   0.7252   0.7407
   0.250   0.3597   0.00729   0.00208  -0.0758   0.7198   0.7466
   0.500   0.3878   0.00732   0.00209  -0.0759   0.7143   0.7519
   0.750   0.4161   0.00735   0.00210  -0.0761   0.7084   0.7569
   1.000   0.4437   0.00736   0.00213  -0.0760   0.7010   0.7605
   1.250   0.4714   0.00739   0.00216  -0.0760   0.6935   0.7644
   1.500   0.4991   0.00742   0.00218  -0.0761   0.6852   0.7686
   1.750   0.5269   0.00745   0.00221  -0.0761   0.6764   0.7728
   2.000   0.5539   0.00749   0.00226  -0.0760   0.6670   0.7765
   2.250   0.5811   0.00754   0.00231  -0.0759   0.6555   0.7807
   2.500   0.6082   0.00760   0.00235  -0.0758   0.6415   0.7846
   2.750   0.6346   0.00767   0.00240  -0.0755   0.6238   0.7877
   3.000   0.6596   0.00779   0.00246  -0.0750   0.5990   0.7905
   3.250   0.6835   0.00798   0.00255  -0.0743   0.5692   0.7935
   3.500   0.7067   0.00825   0.00269  -0.0735   0.5358   0.7967
   3.750   0.7289   0.00859   0.00288  -0.0726   0.4987   0.8000
   4.000   0.7508   0.00893   0.00309  -0.0716   0.4625   0.8027
   4.250   0.7719   0.00931   0.00334  -0.0705   0.4253   0.8055
   4.500   0.7933   0.00970   0.00359  -0.0695   0.3895   0.8086
   4.750   0.8144   0.01011   0.00387  -0.0685   0.3546   0.8119
   5.000   0.8361   0.01051   0.00415  -0.0676   0.3237   0.8153
   5.250   0.8568   0.01090   0.00444  -0.0665   0.2928   0.8180
   5.500   0.8773   0.01131   0.00475  -0.0654   0.2630   0.8211
   5.750   0.8980   0.01172   0.00507  -0.0643   0.2374   0.8246
   6.000   0.9189   0.01212   0.00539  -0.0633   0.2136   0.8283
   6.250   0.9390   0.01254   0.00573  -0.0622   0.1908   0.8315
   6.500   0.9590   0.01293   0.00607  -0.0610   0.1716   0.8349
   6.750   0.9786   0.01334   0.00645  -0.0598   0.1539   0.8390
   7.000   0.9977   0.01379   0.00683  -0.0585   0.1341   0.8433
   7.250   1.0155   0.01422   0.00721  -0.0570   0.1177   0.8471
   7.500   1.0320   0.01463   0.00761  -0.0552   0.1037   0.8518
   7.750   1.0487   0.01507   0.00803  -0.0534   0.0916   0.8572
   8.000   1.0645   0.01554   0.00849  -0.0516   0.0796   0.8625
   8.250   1.0798   0.01605   0.00900  -0.0497   0.0680   0.8685
   8.500   1.0952   0.01656   0.00952  -0.0479   0.0588   0.8750
   8.750   1.1095   0.01710   0.01008  -0.0459   0.0508   0.8829
   9.000   1.1240   0.01762   0.01064  -0.0439   0.0441   0.8922
   9.250   1.1373   0.01818   0.01124  -0.0419   0.0383   0.9041
   9.500   1.1488   0.01874   0.01185  -0.0395   0.0333   0.9213
  10.000   1.1804   0.01997   0.01322  -0.0368   0.0260   1.0000
  10.250   1.1945   0.02080   0.01406  -0.0354   0.0228   1.0000
  10.500   1.2103   0.02150   0.01482  -0.0343   0.0205   1.0000
  10.750   1.2238   0.02237   0.01570  -0.0330   0.0177   1.0000
  11.000   1.2375   0.02324   0.01661  -0.0317   0.0156   1.0000
  11.250   1.2511   0.02413   0.01753  -0.0305   0.0135   1.0000
  11.500   1.2629   0.02516   0.01858  -0.0292   0.0112   1.0000
  11.750   1.2758   0.02612   0.01961  -0.0280   0.0101   1.0000
  12.000   1.2867   0.02725   0.02076  -0.0268   0.0083   1.0000
  12.250   1.2978   0.02839   0.02198  -0.0256   0.0070   1.0000
  12.500   1.3083   0.02960   0.02326  -0.0244   0.0063   1.0000
  12.750   1.3173   0.03095   0.02466  -0.0232   0.0054   1.0000
  13.000   1.3263   0.03233   0.02613  -0.0221   0.0048   1.0000
  13.250   1.3342   0.03383   0.02772  -0.0210   0.0041   1.0000
  13.500   1.3400   0.03556   0.02952  -0.0199   0.0035   1.0000
  13.750   1.3461   0.03731   0.03136  -0.0189   0.0032   1.0000
  14.000   1.3512   0.03917   0.03334  -0.0180   0.0029   1.0000
  14.250   1.3551   0.04121   0.03548  -0.0172   0.0025   1.0000
  14.500   1.3567   0.04356   0.03792  -0.0165   0.0021   1.0000
  14.750   1.3602   0.04577   0.04027  -0.0159   0.0022   1.0000
  15.000   1.3584   0.04865   0.04327  -0.0155   0.0019   1.0000
  15.250   1.3590   0.05139   0.04614  -0.0153   0.0019   1.0000
  15.500   1.3582   0.05440   0.04929  -0.0153   0.0018   1.0000
  15.750   1.3549   0.05785   0.05289  -0.0156   0.0016   1.0000
  16.000   1.3521   0.06141   0.05658  -0.0162   0.0016   1.0000
  16.250   1.3470   0.06546   0.06077  -0.0171   0.0015   1.0000
  16.500   1.3411   0.06981   0.06526  -0.0184   0.0014   1.0000
  16.750   1.3335   0.07464   0.07025  -0.0201   0.0014   1.0000
  17.000   1.3232   0.08012   0.07587  -0.0222   0.0013   1.0000
  17.250   1.3131   0.08583   0.08175  -0.0247   0.0013   1.0000
  17.500   1.2992   0.09242   0.08850  -0.0279   0.0013   1.0000
  17.750   1.2843   0.09950   0.09574  -0.0315   0.0013   1.0000
  18.000   1.2687   0.10695   0.10335  -0.0354   0.0013   1.0000
  18.250   1.2509   0.11503   0.11160  -0.0399   0.0013   1.0000
  18.500   1.2324   0.12351   0.12024  -0.0447   0.0013   1.0000
  18.750   1.2135   0.13229   0.12917  -0.0497   0.0013   1.0000
  19.000   1.1924   0.14172   0.13875  -0.0553   0.0013   1.0000
  19.250   1.1750   0.15052   0.14769  -0.0606   0.0014   1.0000
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