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MH 102 16.99% (mh102-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: MH 102 16.99% (mh102-il)
Reynolds number: 100,000
Max Cl/Cd: 45.83 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-mh102-il-100000-n5.txt
Download as CSV file: xf-mh102-il-100000-n5.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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.4869   0.14336   0.13769  -0.0250   1.0000   0.0290
 -15.750  -0.5754   0.11703   0.11105  -0.0373   1.0000   0.0289
 -15.500  -0.5936   0.10917   0.10305  -0.0412   1.0000   0.0292
 -15.250  -0.6053   0.10297   0.09671  -0.0442   1.0000   0.0297
 -15.000  -0.6168   0.09699   0.09056  -0.0470   1.0000   0.0306
 -14.750  -0.6199   0.09288   0.08641  -0.0488   1.0000   0.0314
 -14.500  -0.6196   0.08954   0.08306  -0.0502   1.0000   0.0320
 -14.250  -0.6234   0.08549   0.07897  -0.0519   1.0000   0.0332
 -14.000  -0.6276   0.08150   0.07489  -0.0536   1.0000   0.0343
 -13.750  -0.6324   0.07764   0.07096  -0.0551   1.0000   0.0355
 -13.500  -0.6356   0.07422   0.06756  -0.0565   1.0000   0.0366
 -13.250  -0.6403   0.07063   0.06394  -0.0578   1.0000   0.0378
 -13.000  -0.6451   0.06706   0.06031  -0.0590   1.0000   0.0389
 -12.750  -0.6527   0.06319   0.05641  -0.0605   1.0000   0.0403
 -12.500  -0.6608   0.05935   0.05256  -0.0620   1.0000   0.0413
 -12.250  -0.6721   0.05511   0.04829  -0.0637   1.0000   0.0426
 -12.000  -0.6837   0.05089   0.04400  -0.0655   1.0000   0.0439
 -11.750  -0.6973   0.04655   0.03958  -0.0673   1.0000   0.0452
 -11.500  -0.7140   0.04223   0.03521  -0.0691   1.0000   0.0459
 -11.250  -0.7311   0.03872   0.03163  -0.0696   1.0000   0.0467
 -11.000  -0.7494   0.03621   0.02907  -0.0679   1.0000   0.0476
 -10.750  -0.7693   0.03453   0.02733  -0.0639   1.0000   0.0492
 -10.500  -0.7827   0.03311   0.02588  -0.0599   1.0000   0.0511
 -10.250  -0.7947   0.03177   0.02455  -0.0557   1.0000   0.0536
 -10.000  -0.7981   0.03051   0.02324  -0.0528   0.9981   0.0576
  -9.750  -0.7721   0.02845   0.02115  -0.0556   0.9849   0.0687
  -9.500  -0.7462   0.02669   0.01942  -0.0577   0.9717   0.0848
  -9.250  -0.7188   0.02533   0.01813  -0.0595   0.9587   0.1067
  -9.000  -0.6878   0.02444   0.01724  -0.0613   0.9469   0.1302
  -8.750  -0.6522   0.02386   0.01661  -0.0635   0.9372   0.1508
  -8.500  -0.6208   0.02347   0.01611  -0.0646   0.9242   0.1668
  -8.250  -0.5885   0.02315   0.01564  -0.0658   0.9118   0.1804
  -8.000  -0.5546   0.02284   0.01517  -0.0671   0.9005   0.1931
  -7.750  -0.5238   0.02257   0.01465  -0.0679   0.8874   0.2051
  -7.500  -0.4945   0.02240   0.01447  -0.0681   0.8736   0.2142
  -7.250  -0.4655   0.02208   0.01394  -0.0683   0.8604   0.2236
  -7.000  -0.4357   0.02184   0.01361  -0.0686   0.8481   0.2312
  -6.750  -0.4099   0.02149   0.01302  -0.0682   0.8335   0.2390
  -6.500  -0.3827   0.02121   0.01272  -0.0679   0.8201   0.2447
  -6.250  -0.3552   0.02090   0.01224  -0.0676   0.8080   0.2515
  -6.000  -0.3291   0.02057   0.01174  -0.0672   0.7947   0.2576
  -5.750  -0.3029   0.02031   0.01144  -0.0667   0.7819   0.2632
  -5.500  -0.2758   0.02003   0.01097  -0.0664   0.7707   0.2698
  -5.250  -0.2500   0.01975   0.01059  -0.0659   0.7580   0.2757
  -5.000  -0.2238   0.01952   0.01031  -0.0654   0.7464   0.2816
  -4.750  -0.1970   0.01928   0.00990  -0.0650   0.7357   0.2885
  -4.500  -0.1714   0.01905   0.00962  -0.0645   0.7236   0.2945
  -4.250  -0.1448   0.01886   0.00935  -0.0640   0.7135   0.3013
  -4.000  -0.1187   0.01868   0.00902  -0.0636   0.7022   0.3089
  -3.750  -0.0926   0.01848   0.00882  -0.0631   0.6921   0.3152
  -3.500  -0.0663   0.01833   0.00858  -0.0626   0.6817   0.3234
  -3.250  -0.0403   0.01817   0.00838  -0.0621   0.6715   0.3312
  -3.000  -0.0139   0.01803   0.00818  -0.0616   0.6621   0.3395
  -2.750   0.0122   0.01792   0.00801  -0.0612   0.6523   0.3484
  -2.500   0.0385   0.01780   0.00786  -0.0607   0.6434   0.3579
  -2.250   0.0645   0.01771   0.00774  -0.0602   0.6338   0.3682
  -2.000   0.0908   0.01761   0.00760  -0.0598   0.6252   0.3790
  -1.750   0.1167   0.01754   0.00753  -0.0593   0.6165   0.3901
  -1.500   0.1430   0.01748   0.00743  -0.0589   0.6082   0.4033
  -1.250   0.1690   0.01742   0.00738  -0.0584   0.6003   0.4166
  -1.000   0.1948   0.01736   0.00736  -0.0579   0.5917   0.4308
  -0.750   0.2213   0.01732   0.00729  -0.0574   0.5848   0.4468
  -0.500   0.2467   0.01730   0.00733  -0.0569   0.5765   0.4643
  -0.250   0.2729   0.01727   0.00731  -0.0564   0.5697   0.4836
   0.000   0.2984   0.01726   0.00737  -0.0558   0.5622   0.5050
   0.250   0.3239   0.01724   0.00742  -0.0552   0.5549   0.5290
   0.750   0.3751   0.01725   0.00760  -0.0541   0.5414   0.5866
   1.000   0.4005   0.01725   0.00768  -0.0533   0.5350   0.6209
   1.250   0.4256   0.01726   0.00779  -0.0525   0.5290   0.6586
   1.500   0.4494   0.01730   0.00799  -0.0515   0.5219   0.6999
   1.750   0.4745   0.01732   0.00811  -0.0505   0.5160   0.7452
   2.000   0.5001   0.01738   0.00829  -0.0496   0.5100   0.7920
   2.250   0.5283   0.01749   0.00851  -0.0492   0.5031   0.8408
   2.500   0.5645   0.01760   0.00862  -0.0504   0.4971   0.8870
   2.750   0.6052   0.01779   0.00884  -0.0528   0.4900   0.9277
   3.000   0.6486   0.01798   0.00901  -0.0559   0.4829   0.9614
   3.250   0.6944   0.01815   0.00907  -0.0595   0.4768   0.9878
   3.500   0.7235   0.01842   0.00936  -0.0602   0.4697   1.0000
   3.750   0.7436   0.01863   0.00951  -0.0589   0.4640   1.0000
   4.000   0.7656   0.01885   0.00961  -0.0579   0.4591   1.0000
   4.250   0.7844   0.01915   0.00996  -0.0564   0.4526   1.0000
   4.500   0.8058   0.01940   0.01017  -0.0553   0.4467   1.0000
   4.750   0.8295   0.01963   0.01029  -0.0546   0.4419   1.0000
   5.000   0.8487   0.01998   0.01072  -0.0532   0.4352   1.0000
   5.250   0.8705   0.02025   0.01097  -0.0522   0.4292   1.0000
   5.500   0.8948   0.02049   0.01112  -0.0515   0.4242   1.0000
   5.750   0.9138   0.02087   0.01160  -0.0502   0.4173   1.0000
   6.000   0.9357   0.02116   0.01188  -0.0493   0.4112   1.0000
   6.250   0.9591   0.02144   0.01210  -0.0485   0.4058   1.0000
   6.500   0.9778   0.02185   0.01261  -0.0472   0.3988   1.0000
   6.750   0.9998   0.02213   0.01288  -0.0462   0.3927   1.0000
   7.000   1.0208   0.02249   0.01325  -0.0452   0.3867   1.0000
   7.250   1.0395   0.02290   0.01374  -0.0439   0.3797   1.0000
   7.500   1.0615   0.02318   0.01398  -0.0429   0.3737   1.0000
   7.750   1.0789   0.02365   0.01455  -0.0415   0.3669   1.0000
   8.000   1.0974   0.02404   0.01498  -0.0401   0.3601   1.0000
   8.250   1.1177   0.02439   0.01529  -0.0390   0.3541   1.0000
   8.500   1.1318   0.02493   0.01597  -0.0372   0.3466   1.0000
   8.750   1.1504   0.02530   0.01632  -0.0358   0.3404   1.0000
   9.000   1.1638   0.02586   0.01697  -0.0339   0.3333   1.0000
   9.250   1.1776   0.02636   0.01753  -0.0320   0.3264   1.0000
   9.500   1.1922   0.02682   0.01798  -0.0302   0.3204   1.0000
   9.750   1.1989   0.02752   0.01879  -0.0275   0.3132   1.0000
  10.000   1.2120   0.02802   0.01927  -0.0256   0.3072   1.0000
  10.250   1.2185   0.02887   0.02022  -0.0231   0.3003   1.0000
  10.500   1.2269   0.02964   0.02104  -0.0210   0.2936   1.0000
  10.750   1.2365   0.03044   0.02185  -0.0192   0.2875   1.0000
  11.000   1.2408   0.03158   0.02309  -0.0172   0.2807   1.0000
  11.250   1.2514   0.03239   0.02388  -0.0157   0.2748   1.0000
  11.500   1.2532   0.03384   0.02545  -0.0139   0.2681   1.0000
  11.750   1.2586   0.03511   0.02677  -0.0124   0.2619   1.0000
  12.000   1.2658   0.03635   0.02802  -0.0112   0.2561   1.0000
  12.250   1.2652   0.03823   0.03002  -0.0099   0.2496   1.0000
  12.500   1.2727   0.03953   0.03132  -0.0089   0.2439   1.0000
  12.750   1.2726   0.04159   0.03347  -0.0079   0.2381   1.0000
  13.000   1.2723   0.04371   0.03568  -0.0071   0.2320   1.0000
  13.250   1.2818   0.04499   0.03690  -0.0064   0.2268   1.0000
  13.500   1.2739   0.04804   0.04014  -0.0060   0.2209   1.0000
  13.750   1.2746   0.05030   0.04246  -0.0057   0.2155   1.0000
  14.000   1.2798   0.05214   0.04431  -0.0053   0.2104   1.0000
  14.250   1.2701   0.05571   0.04805  -0.0054   0.2049   1.0000
  14.500   1.2717   0.05808   0.05045  -0.0054   0.1999   1.0000
  14.750   1.2741   0.06042   0.05282  -0.0053   0.1951   1.0000
  15.000   1.2620   0.06467   0.05724  -0.0061   0.1898   1.0000
  15.250   1.2638   0.06722   0.05983  -0.0064   0.1850   1.0000
  15.500   1.2652   0.06989   0.06254  -0.0067   0.1805   1.0000
  15.750   1.2487   0.07514   0.06797  -0.0082   0.1756   1.0000
  16.000   1.2496   0.07801   0.07088  -0.0088   0.1710   1.0000
  16.250   1.2538   0.08046   0.07334  -0.0092   0.1669   1.0000
  16.500   1.2283   0.08747   0.08058  -0.0117   0.1620   1.0000
  16.750   1.2275   0.09081   0.08397  -0.0127   0.1577   1.0000
  17.000   1.2411   0.09189   0.08501  -0.0127   0.1539   1.0000
  17.250   1.1965   0.10250   0.09591  -0.0173   0.1490   1.0000
  17.500   1.1913   0.10679   0.10027  -0.0189   0.1448   1.0000
  17.750   1.2212   0.10507   0.09847  -0.0176   0.1416   1.0000
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