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MH 95 15.86% (mh95-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: MH 95 15.86% (mh95-il)
Reynolds number: 1,000,000
Max Cl/Cd: 78.01 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh95-il-1000000.txt
Download as CSV file: xf-mh95-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: MH 95  15.86%                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.7407   0.11647   0.11401  -0.0508   1.0000   0.0128
 -17.500  -0.7887   0.09917   0.09646  -0.0602   1.0000   0.0126
 -17.250  -0.8204   0.08979   0.08692  -0.0652   1.0000   0.0126
 -17.000  -0.8511   0.08117   0.07813  -0.0697   1.0000   0.0125
 -16.750  -0.8711   0.07467   0.07148  -0.0730   1.0000   0.0125
 -16.500  -0.8946   0.06824   0.06488  -0.0757   1.0000   0.0125
 -16.250  -0.9116   0.06314   0.05965  -0.0774   1.0000   0.0124
 -16.000  -0.9241   0.05902   0.05541  -0.0784   1.0000   0.0125
 -15.750  -0.9365   0.05530   0.05155  -0.0789   1.0000   0.0125
 -15.500  -0.9452   0.05235   0.04850  -0.0788   1.0000   0.0126
 -15.250  -0.9574   0.04916   0.04518  -0.0780   1.0000   0.0126
 -15.000  -0.9670   0.04655   0.04247  -0.0768   1.0000   0.0126
 -14.750  -0.9755   0.04424   0.04005  -0.0753   1.0000   0.0126
 -14.500  -0.9839   0.04216   0.03785  -0.0734   1.0000   0.0126
 -14.250  -0.9906   0.04040   0.03601  -0.0711   1.0000   0.0127
 -14.000  -0.9972   0.03860   0.03410  -0.0686   1.0000   0.0127
 -13.750  -1.0033   0.03725   0.03266  -0.0658   1.0000   0.0127
 -13.500  -1.0120   0.03520   0.03047  -0.0627   1.0000   0.0128
 -13.250  -1.0008   0.03342   0.02858  -0.0626   0.9992   0.0128
 -13.000  -0.9900   0.03118   0.02622  -0.0625   0.9981   0.0129
 -12.750  -0.9751   0.02943   0.02437  -0.0627   0.9968   0.0130
 -12.500  -0.9572   0.02805   0.02293  -0.0631   0.9955   0.0131
 -12.250  -0.9385   0.02673   0.02156  -0.0635   0.9943   0.0133
 -12.000  -0.9171   0.02564   0.02042  -0.0643   0.9934   0.0134
 -11.750  -0.9006   0.02456   0.01930  -0.0638   0.9912   0.0135
 -11.500  -0.8815   0.02363   0.01832  -0.0637   0.9890   0.0136
 -11.250  -0.8597   0.02275   0.01739  -0.0640   0.9871   0.0138
 -11.000  -0.8364   0.02187   0.01647  -0.0646   0.9856   0.0139
 -10.750  -0.8120   0.02098   0.01553  -0.0653   0.9842   0.0141
 -10.500  -0.7854   0.02021   0.01473  -0.0663   0.9832   0.0143
 -10.250  -0.7573   0.01949   0.01397  -0.0674   0.9823   0.0145
 -10.000  -0.7423   0.01878   0.01322  -0.0659   0.9782   0.0147
  -9.750  -0.7191   0.01815   0.01255  -0.0658   0.9754   0.0150
  -9.500  -0.6914   0.01761   0.01197  -0.0666   0.9736   0.0153
  -9.250  -0.6628   0.01702   0.01134  -0.0675   0.9723   0.0155
  -9.000  -0.6368   0.01607   0.01036  -0.0682   0.9709   0.0158
  -8.750  -0.6084   0.01528   0.00954  -0.0693   0.9700   0.0163
  -8.500  -0.5929   0.01485   0.00910  -0.0672   0.9653   0.0166
  -8.250  -0.5699   0.01434   0.00858  -0.0667   0.9620   0.0169
  -8.000  -0.5397   0.01385   0.00808  -0.0677   0.9604   0.0174
  -7.750  -0.5090   0.01336   0.00757  -0.0686   0.9589   0.0178
  -7.500  -0.4775   0.01291   0.00710  -0.0697   0.9575   0.0183
  -7.250  -0.4458   0.01246   0.00663  -0.0708   0.9561   0.0187
  -7.000  -0.4303   0.01205   0.00620  -0.0686   0.9508   0.0195
  -6.750  -0.4070   0.01170   0.00585  -0.0678   0.9466   0.0203
  -6.500  -0.3784   0.01135   0.00549  -0.0681   0.9437   0.0213
  -6.250  -0.3495   0.01098   0.00510  -0.0684   0.9411   0.0225
  -6.000  -0.3299   0.01070   0.00483  -0.0668   0.9358   0.0244
  -5.750  -0.3073   0.01040   0.00454  -0.0657   0.9305   0.0274
  -5.500  -0.2821   0.01000   0.00420  -0.0653   0.9263   0.0366
  -5.250  -0.2633   0.00949   0.00386  -0.0637   0.9205   0.0691
  -5.000  -0.2456   0.00900   0.00355  -0.0618   0.9136   0.1094
  -4.750  -0.2234   0.00842   0.00321  -0.0610   0.9081   0.1659
  -4.500  -0.2064   0.00802   0.00300  -0.0589   0.9002   0.2121
  -4.250  -0.1840   0.00761   0.00276  -0.0580   0.8934   0.2602
  -4.000  -0.1630   0.00725   0.00257  -0.0567   0.8856   0.3077
  -3.750  -0.1407   0.00689   0.00238  -0.0556   0.8771   0.3584
  -3.500  -0.1189   0.00656   0.00221  -0.0545   0.8681   0.4062
  -3.250  -0.0960   0.00622   0.00203  -0.0535   0.8584   0.4613
  -3.000  -0.0754   0.00587   0.00189  -0.0521   0.8471   0.5234
  -2.750  -0.0530   0.00559   0.00178  -0.0510   0.8357   0.5828
  -2.500  -0.0293   0.00543   0.00173  -0.0500   0.8229   0.6320
  -2.250  -0.0043   0.00539   0.00171  -0.0493   0.8089   0.6612
  -2.000   0.0216   0.00538   0.00169  -0.0487   0.7943   0.6766
  -1.750   0.0477   0.00540   0.00167  -0.0482   0.7796   0.6866
  -1.500   0.0739   0.00545   0.00165  -0.0477   0.7644   0.6960
  -1.250   0.0994   0.00550   0.00164  -0.0470   0.7481   0.7039
  -1.000   0.1249   0.00556   0.00164  -0.0464   0.7315   0.7116
  -0.750   0.1502   0.00563   0.00164  -0.0458   0.7144   0.7182
  -0.500   0.1752   0.00571   0.00166  -0.0450   0.6969   0.7250
  -0.250   0.2004   0.00580   0.00168  -0.0443   0.6793   0.7314
   0.000   0.2251   0.00588   0.00170  -0.0436   0.6610   0.7377
   0.250   0.2497   0.00598   0.00175  -0.0428   0.6419   0.7439
   0.500   0.2744   0.00610   0.00178  -0.0420   0.6230   0.7497
   0.750   0.2988   0.00620   0.00182  -0.0412   0.6024   0.7548
   1.000   0.3228   0.00632   0.00187  -0.0404   0.5813   0.7597
   1.250   0.3466   0.00647   0.00193  -0.0395   0.5589   0.7646
   1.500   0.3697   0.00665   0.00199  -0.0384   0.5321   0.7691
   1.750   0.3914   0.00684   0.00206  -0.0372   0.5004   0.7739
   2.000   0.4144   0.00703   0.00216  -0.0361   0.4727   0.7789
   2.250   0.4379   0.00722   0.00225  -0.0352   0.4496   0.7839
   2.500   0.4616   0.00741   0.00234  -0.0344   0.4270   0.7882
   2.750   0.4849   0.00757   0.00243  -0.0335   0.4042   0.7929
   3.000   0.5082   0.00776   0.00255  -0.0326   0.3823   0.7973
   3.250   0.5317   0.00795   0.00266  -0.0317   0.3626   0.8016
   3.500   0.5552   0.00816   0.00277  -0.0309   0.3436   0.8054
   3.750   0.5782   0.00834   0.00288  -0.0300   0.3246   0.8094
   4.250   0.6233   0.00871   0.00314  -0.0279   0.2912   0.8169
   4.500   0.6459   0.00888   0.00326  -0.0269   0.2773   0.8208
   4.750   0.6685   0.00907   0.00339  -0.0259   0.2641   0.8243
   5.000   0.6903   0.00925   0.00352  -0.0248   0.2510   0.8281
   5.250   0.7115   0.00945   0.00368  -0.0236   0.2378   0.8321
   5.500   0.7337   0.00964   0.00384  -0.0225   0.2266   0.8360
   5.750   0.7558   0.00984   0.00400  -0.0215   0.2158   0.8399
   6.000   0.7774   0.01009   0.00419  -0.0204   0.2043   0.8433
   6.250   0.7989   0.01028   0.00437  -0.0192   0.1939   0.8477
   6.500   0.8199   0.01051   0.00457  -0.0180   0.1836   0.8520
   6.750   0.8402   0.01078   0.00479  -0.0167   0.1716   0.8563
   7.250   0.8807   0.01132   0.00525  -0.0141   0.1495   0.8648
   7.500   0.9000   0.01160   0.00551  -0.0126   0.1399   0.8695
   7.750   0.9186   0.01193   0.00579  -0.0111   0.1303   0.8745
   8.000   0.9387   0.01222   0.00605  -0.0099   0.1237   0.8790
   8.250   0.9568   0.01252   0.00635  -0.0083   0.1168   0.8841
   8.500   0.9759   0.01279   0.00663  -0.0068   0.1121   0.8895
   8.750   0.9937   0.01314   0.00696  -0.0052   0.1072   0.8952
   9.000   1.0121   0.01341   0.00726  -0.0037   0.1040   0.9011
   9.250   1.0306   0.01368   0.00757  -0.0022   0.1014   0.9075
   9.500   1.0480   0.01401   0.00790  -0.0006   0.0985   0.9140
   9.750   1.0628   0.01437   0.00829   0.0015   0.0955   0.9218
  10.000   1.0790   0.01470   0.00867   0.0033   0.0933   0.9305
  10.250   1.0953   0.01495   0.00899   0.0052   0.0920   0.9413
  10.500   1.1120   0.01524   0.00934   0.0068   0.0903   0.9555
  10.750   1.1378   0.01564   0.00977   0.0064   0.0882   0.9714
  11.000   1.1672   0.01619   0.01033   0.0050   0.0855   1.0000
  11.250   1.1817   0.01683   0.01097   0.0065   0.0834   1.0000
  11.500   1.2012   0.01721   0.01139   0.0074   0.0827   1.0000
  11.750   1.2193   0.01764   0.01186   0.0084   0.0818   1.0000
  12.000   1.2367   0.01811   0.01236   0.0095   0.0805   1.0000
  12.250   1.2529   0.01863   0.01291   0.0108   0.0795   1.0000
  12.500   1.2684   0.01920   0.01349   0.0120   0.0780   1.0000
  12.750   1.2824   0.01985   0.01416   0.0134   0.0769   1.0000
  13.000   1.2929   0.02070   0.01503   0.0152   0.0753   1.0000
  13.250   1.3009   0.02170   0.01607   0.0172   0.0738   1.0000
  13.500   1.3172   0.02227   0.01669   0.0181   0.0733   1.0000
  13.750   1.3328   0.02289   0.01735   0.0191   0.0725   1.0000
  14.000   1.3472   0.02359   0.01809   0.0202   0.0715   1.0000
  14.250   1.3598   0.02441   0.01896   0.0213   0.0706   1.0000
  14.500   1.3728   0.02524   0.01982   0.0224   0.0696   1.0000
  14.750   1.3836   0.02622   0.02083   0.0236   0.0686   1.0000
  15.000   1.3928   0.02734   0.02198   0.0248   0.0676   1.0000
  15.250   1.3984   0.02875   0.02343   0.0261   0.0665   1.0000
  15.500   1.4006   0.03045   0.02520   0.0275   0.0652   1.0000
  15.750   1.4122   0.03155   0.02636   0.0282   0.0649   1.0000
  16.000   1.4233   0.03269   0.02757   0.0289   0.0643   1.0000
  16.250   1.4338   0.03393   0.02887   0.0294   0.0635   1.0000
  16.500   1.4425   0.03535   0.03035   0.0300   0.0628   1.0000
  16.750   1.4509   0.03684   0.03189   0.0305   0.0620   1.0000
  17.000   1.4579   0.03849   0.03360   0.0309   0.0612   1.0000
  17.250   1.4635   0.04032   0.03547   0.0312   0.0604   1.0000
  17.500   1.4668   0.04243   0.03764   0.0314   0.0596   1.0000
  17.750   1.4654   0.04506   0.04032   0.0316   0.0586   1.0000
  18.000   1.4621   0.04796   0.04329   0.0316   0.0575   1.0000
  18.250   1.4694   0.04989   0.04530   0.0313   0.0571   1.0000
  18.500   1.4747   0.05205   0.04754   0.0310   0.0565   1.0000
  18.750   1.4800   0.05427   0.04984   0.0306   0.0556   1.0000
  19.000   1.4824   0.05687   0.05250   0.0300   0.0548   1.0000
  19.250   1.4817   0.05988   0.05560   0.0293   0.0543   1.0000
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