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MH 93 15.98% (mh93-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: MH 93 15.98% (mh93-il)
Reynolds number: 200,000
Max Cl/Cd: 52.52 at α=8.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh93-il-200000.txt
Download as CSV file: xf-mh93-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 93  15.98%                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.7668   0.05679   0.05257  -0.0253   1.0000   0.0333
 -11.500  -0.7764   0.05257   0.04826  -0.0250   1.0000   0.0328
 -11.250  -0.8652   0.05605   0.05122  -0.0207   1.0000   0.0329
 -11.000  -0.9252   0.05015   0.04449  -0.0133   1.0000   0.0291
 -10.750  -0.9164   0.04711   0.04136  -0.0121   1.0000   0.0287
 -10.500  -0.9137   0.04423   0.03827  -0.0099   1.0000   0.0283
 -10.250  -0.9090   0.04139   0.03517  -0.0078   1.0000   0.0279
 -10.000  -0.9004   0.03865   0.03215  -0.0059   1.0000   0.0276
  -9.750  -0.8876   0.03609   0.02930  -0.0043   1.0000   0.0273
  -9.500  -0.8709   0.03383   0.02678  -0.0031   1.0000   0.0272
  -9.250  -0.8513   0.03194   0.02468  -0.0022   1.0000   0.0276
  -9.000  -0.8314   0.03045   0.02298  -0.0014   1.0000   0.0285
  -8.750  -0.8098   0.02901   0.02129  -0.0007   1.0000   0.0292
  -8.500  -0.7804   0.02715   0.01944  -0.0014   1.0000   0.0301
  -8.250  -0.7519   0.02581   0.01812  -0.0020   1.0000   0.0308
  -8.000  -0.7231   0.02456   0.01689  -0.0028   0.9959   0.0316
  -7.750  -0.6801   0.02312   0.01537  -0.0058   0.9615   0.0333
  -7.500  -0.6487   0.02186   0.01410  -0.0068   0.9342   0.0347
  -7.250  -0.6333   0.02112   0.01335  -0.0045   0.9082   0.0366
  -7.000  -0.6203   0.02054   0.01266  -0.0015   0.8863   0.0387
  -6.750  -0.6098   0.01977   0.01189   0.0016   0.8674   0.0413
  -6.500  -0.5964   0.01914   0.01120   0.0043   0.8508   0.0458
  -6.250  -0.5829   0.01844   0.01047   0.0069   0.8355   0.0523
  -6.000  -0.5697   0.01763   0.00967   0.0096   0.8214   0.0623
  -5.750  -0.5590   0.01651   0.00875   0.0126   0.8083   0.0951
  -5.500  -0.5541   0.01485   0.00787   0.0160   0.7946   0.2200
  -5.250  -0.5431   0.01393   0.00743   0.0187   0.7820   0.3229
  -5.000  -0.5283   0.01336   0.00710   0.0212   0.7708   0.3927
  -4.750  -0.5108   0.01288   0.00686   0.0232   0.7577   0.4536
  -4.500  -0.4916   0.01253   0.00668   0.0251   0.7460   0.5072
  -4.250  -0.4713   0.01227   0.00650   0.0270   0.7352   0.5546
  -4.000  -0.4489   0.01203   0.00642   0.0284   0.7226   0.5981
  -3.750  -0.4259   0.01191   0.00636   0.0299   0.7116   0.6382
  -3.500  -0.4020   0.01186   0.00637   0.0314   0.7001   0.6751
  -3.250  -0.3766   0.01194   0.00649   0.0326   0.6883   0.7073
  -3.000  -0.3511   0.01205   0.00653   0.0338   0.6779   0.7323
  -2.750  -0.3238   0.01217   0.00664   0.0346   0.6655   0.7516
  -2.500  -0.2969   0.01233   0.00672   0.0355   0.6545   0.7689
  -2.250  -0.2705   0.01250   0.00677   0.0365   0.6436   0.7848
  -2.000  -0.2430   0.01270   0.00692   0.0372   0.6316   0.7989
  -1.750  -0.2133   0.01297   0.00709   0.0377   0.6210   0.8093
  -1.500  -0.1865   0.01312   0.00716   0.0385   0.6092   0.8214
  -1.250  -0.1564   0.01337   0.00733   0.0388   0.5979   0.8303
  -1.000  -0.1290   0.01355   0.00738   0.0394   0.5874   0.8401
  -0.750  -0.0978   0.01379   0.00757   0.0394   0.5751   0.8477
  -0.500  -0.0712   0.01394   0.00760   0.0401   0.5648   0.8573
  -0.250  -0.0373   0.01419   0.00776   0.0396   0.5530   0.8629
   0.000  -0.0137   0.01428   0.00778   0.0407   0.5420   0.8737
   0.250   0.0234   0.01456   0.00792   0.0396   0.5313   0.8777
   0.500   0.0575   0.01475   0.00807   0.0388   0.5188   0.8839
   0.750   0.0839   0.01486   0.00810   0.0393   0.5083   0.8926
   1.000   0.1248   0.01512   0.00822   0.0373   0.4971   0.8963
   1.250   0.1621   0.01531   0.00837   0.0357   0.4849   0.9021
   1.500   0.1898   0.01542   0.00839   0.0359   0.4751   0.9102
   1.750   0.2350   0.01558   0.00847   0.0327   0.4632   0.9130
   2.000   0.2758   0.01572   0.00855   0.0302   0.4515   0.9171
   2.250   0.2973   0.01582   0.00853   0.0314   0.4432   0.9261
   2.500   0.3414   0.01590   0.00860   0.0282   0.4314   0.9286
   2.750   0.3810   0.01603   0.00865   0.0258   0.4216   0.9322
   3.000   0.4102   0.01611   0.00870   0.0254   0.4121   0.9389
   3.250   0.4437   0.01622   0.00874   0.0242   0.4032   0.9435
   3.500   0.4832   0.01629   0.00876   0.0217   0.3935   0.9470
   3.750   0.5162   0.01642   0.00887   0.0205   0.3848   0.9522
   4.000   0.5457   0.01651   0.00891   0.0199   0.3768   0.9577
   4.250   0.5847   0.01663   0.00901   0.0174   0.3683   0.9610
   4.500   0.6189   0.01672   0.00909   0.0159   0.3600   0.9657
   4.750   0.6486   0.01690   0.00922   0.0152   0.3527   0.9709
   5.000   0.6872   0.01696   0.00930   0.0127   0.3444   0.9742
   5.250   0.7214   0.01717   0.00943   0.0111   0.3377   0.9786
   5.500   0.7532   0.01727   0.00961   0.0099   0.3298   0.9832
   5.750   0.7905   0.01741   0.00965   0.0076   0.3229   0.9864
   6.000   0.8249   0.01756   0.00990   0.0058   0.3156   0.9905
   6.250   0.8589   0.01770   0.01002   0.0041   0.3089   0.9942
   6.500   0.8942   0.01790   0.01023   0.0021   0.3022   0.9975
   6.750   0.9255   0.01807   0.01046   0.0008   0.2955   1.0000
   7.000   0.9458   0.01834   0.01067   0.0017   0.2905   1.0000
   7.250   0.9654   0.01865   0.01106   0.0027   0.2851   1.0000
   7.500   0.9846   0.01890   0.01137   0.0038   0.2795   1.0000
   7.750   1.0040   0.01917   0.01161   0.0048   0.2747   1.0000
   8.000   1.0225   0.01957   0.01204   0.0060   0.2698   1.0000
   8.250   1.0399   0.01985   0.01243   0.0073   0.2644   1.0000
   8.500   1.0577   0.02014   0.01270   0.0087   0.2596   1.0000
   8.750   1.0749   0.02059   0.01313   0.0101   0.2549   1.0000
   9.000   1.0894   0.02092   0.01361   0.0118   0.2497   1.0000
   9.250   1.1049   0.02122   0.01393   0.0135   0.2451   1.0000
   9.500   1.1222   0.02172   0.01431   0.0149   0.2407   1.0000
   9.750   1.1323   0.02210   0.01490   0.0174   0.2363   1.0000
  10.000   1.1438   0.02246   0.01533   0.0197   0.2317   1.0000
  10.250   1.1566   0.02281   0.01566   0.0218   0.2277   1.0000
  10.500   1.1683   0.02334   0.01620   0.0240   0.2237   1.0000
  10.750   1.1737   0.02376   0.01677   0.0272   0.2195   1.0000
  11.000   1.1819   0.02413   0.01718   0.0300   0.2153   1.0000
  11.250   1.1946   0.02456   0.01755   0.0321   0.2114   1.0000
  11.500   1.2015   0.02516   0.01824   0.0348   0.2074   1.0000
  11.750   1.2067   0.02567   0.01887   0.0377   0.2031   1.0000
  12.000   1.2173   0.02613   0.01934   0.0397   0.1989   1.0000
  12.250   1.2332   0.02680   0.01994   0.0409   0.1946   1.0000
  12.500   1.2300   0.02754   0.02087   0.0445   0.1910   1.0000
  12.750   1.2336   0.02828   0.02168   0.0468   0.1868   1.0000
  13.000   1.2445   0.02895   0.02231   0.0481   0.1828   1.0000
  13.250   1.2500   0.03006   0.02349   0.0496   0.1786   1.0000
  13.500   1.2500   0.03133   0.02490   0.0511   0.1746   1.0000
  13.750   1.2565   0.03238   0.02598   0.0521   0.1704   1.0000
  14.000   1.2685   0.03343   0.02698   0.0527   0.1661   1.0000
  14.250   1.2627   0.03539   0.02915   0.0536   0.1624   1.0000
  14.500   1.2647   0.03700   0.03084   0.0541   0.1583   1.0000
  14.750   1.2780   0.03799   0.03172   0.0545   0.1541   1.0000
  15.000   1.2708   0.04052   0.03443   0.0547   0.1506   1.0000
  15.250   1.2664   0.04296   0.03702   0.0545   0.1469   1.0000
  15.500   1.2704   0.04473   0.03880   0.0544   0.1432   1.0000
  15.750   1.2767   0.04647   0.04052   0.0545   0.1394   1.0000
  16.000   1.2639   0.05005   0.04431   0.0536   0.1364   1.0000
  16.250   1.2593   0.05293   0.04728   0.0528   0.1329   1.0000
  16.500   1.2668   0.05456   0.04886   0.0525   0.1294   1.0000
  16.750   1.2621   0.05773   0.05212   0.0516   0.1264   1.0000
  17.000   1.2454   0.06244   0.05704   0.0496   0.1235   1.0000
  17.250   1.2403   0.06591   0.06058   0.0482   0.1204   1.0000
  17.500   1.2540   0.06692   0.06150   0.0481   0.1169   1.0000
  17.750   1.2388   0.07190   0.06665   0.0459   0.1144   1.0000
  18.000   1.2155   0.07828   0.07324   0.0427   0.1121   1.0000
  18.250   1.2037   0.08316   0.07823   0.0402   0.1094   1.0000
  18.500   1.2184   0.08410   0.07909   0.0400   0.1063   1.0000
  18.750   1.2105   0.08847   0.08354   0.0380   0.1038   1.0000
  19.000   1.1660   0.09892   0.09428   0.0322   0.1020   1.0000
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