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MH 95 15.86% (mh95-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: MH 95 15.86% (mh95-il)
Reynolds number: 500,000
Max Cl/Cd: 62.6 at α=7.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-mh95-il-500000.txt
Download as CSV file: xf-mh95-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.5776   0.08675   0.08384  -0.0657   1.0000   0.0218
 -14.750  -0.5938   0.08100   0.07805  -0.0671   1.0000   0.0215
 -14.500  -0.6232   0.07327   0.07021  -0.0700   1.0000   0.0214
 -14.250  -0.6529   0.06607   0.06288  -0.0723   1.0000   0.0212
 -14.000  -0.6802   0.05980   0.05649  -0.0735   1.0000   0.0210
 -13.750  -0.7085   0.05397   0.05051  -0.0739   1.0000   0.0208
 -13.500  -0.7370   0.04874   0.04513  -0.0734   1.0000   0.0207
 -13.250  -0.7632   0.06236   0.05895  -0.0722   1.0000   0.0248
 -13.000  -0.7870   0.05860   0.05508  -0.0709   1.0000   0.0245
 -12.750  -0.9603   0.04210   0.03703  -0.0595   1.0000   0.0189
 -12.500  -0.9730   0.04066   0.03546  -0.0552   1.0000   0.0188
 -12.250  -0.9836   0.03905   0.03373  -0.0509   1.0000   0.0189
 -12.000  -0.9957   0.03785   0.03239  -0.0459   1.0000   0.0189
 -11.750  -1.0100   0.03692   0.03133  -0.0402   1.0000   0.0188
 -11.500  -0.9939   0.03496   0.02920  -0.0401   0.9978   0.0188
 -11.250  -0.9738   0.03314   0.02724  -0.0404   0.9957   0.0189
 -11.000  -0.9503   0.03152   0.02550  -0.0411   0.9939   0.0191
 -10.750  -0.9276   0.03002   0.02388  -0.0413   0.9919   0.0191
 -10.500  -0.9056   0.02883   0.02263  -0.0413   0.9890   0.0193
 -10.250  -0.8808   0.02775   0.02148  -0.0417   0.9866   0.0196
 -10.000  -0.8528   0.02661   0.02027  -0.0426   0.9847   0.0197
  -9.750  -0.8233   0.02570   0.01931  -0.0438   0.9832   0.0202
  -9.500  -0.7923   0.02487   0.01841  -0.0452   0.9820   0.0207
  -9.250  -0.7752   0.02401   0.01749  -0.0437   0.9770   0.0209
  -9.000  -0.7483   0.02319   0.01660  -0.0442   0.9742   0.0213
  -8.750  -0.7186   0.02236   0.01570  -0.0451   0.9722   0.0216
  -8.500  -0.6867   0.02164   0.01492  -0.0465   0.9707   0.0220
  -8.250  -0.6571   0.02044   0.01374  -0.0477   0.9694   0.0224
  -8.000  -0.6458   0.01978   0.01308  -0.0450   0.9624   0.0228
  -7.750  -0.6183   0.01908   0.01238  -0.0455   0.9596   0.0234
  -7.500  -0.5874   0.01841   0.01169  -0.0466   0.9576   0.0241
  -7.250  -0.5547   0.01776   0.01102  -0.0481   0.9561   0.0248
  -7.000  -0.5376   0.01730   0.01052  -0.0462   0.9501   0.0254
  -6.750  -0.5140   0.01657   0.00979  -0.0458   0.9459   0.0263
  -6.500  -0.4825   0.01598   0.00920  -0.0469   0.9437   0.0277
  -6.250  -0.4476   0.01547   0.00868  -0.0486   0.9422   0.0295
  -6.000  -0.4128   0.01482   0.00806  -0.0503   0.9410   0.0323
  -5.750  -0.3952   0.01444   0.00766  -0.0483   0.9346   0.0349
  -5.500  -0.3678   0.01387   0.00715  -0.0484   0.9307   0.0416
  -5.250  -0.3392   0.01284   0.00643  -0.0492   0.9283   0.0917
  -5.000  -0.3104   0.01175   0.00582  -0.0501   0.9262   0.1855
  -4.750  -0.2795   0.01092   0.00535  -0.0513   0.9245   0.2613
  -4.000  -0.2099   0.00919   0.00433  -0.0490   0.9092   0.4391
  -3.750  -0.1911   0.00875   0.00409  -0.0471   0.9020   0.4918
  -3.500  -0.1675   0.00823   0.00385  -0.0462   0.8961   0.5611
  -3.250  -0.1364   0.00785   0.00368  -0.0467   0.8922   0.6256
  -3.000  -0.1147   0.00773   0.00364  -0.0451   0.8840   0.6624
  -2.750  -0.0845   0.00762   0.00359  -0.0452   0.8777   0.6893
  -2.500  -0.0545   0.00755   0.00350  -0.0453   0.8706   0.7039
  -2.250  -0.0269   0.00749   0.00339  -0.0450   0.8614   0.7152
  -2.000   0.0029   0.00744   0.00334  -0.0450   0.8522   0.7236
  -1.750   0.0328   0.00740   0.00322  -0.0452   0.8420   0.7328
  -1.500   0.0597   0.00739   0.00320  -0.0447   0.8299   0.7398
  -1.250   0.0886   0.00740   0.00315  -0.0446   0.8179   0.7473
  -1.000   0.1178   0.00741   0.00309  -0.0447   0.8051   0.7542
  -0.750   0.1442   0.00745   0.00311  -0.0440   0.7908   0.7606
  -0.500   0.1706   0.00751   0.00309  -0.0435   0.7758   0.7678
  -0.250   0.1969   0.00756   0.00310  -0.0430   0.7605   0.7735
   0.000   0.2230   0.00764   0.00313  -0.0424   0.7443   0.7789
   0.250   0.2485   0.00773   0.00314  -0.0417   0.7274   0.7848
   0.500   0.2735   0.00781   0.00313  -0.0409   0.7096   0.7899
   0.750   0.2980   0.00791   0.00319  -0.0400   0.6915   0.7943
   1.000   0.3220   0.00803   0.00324  -0.0390   0.6724   0.7994
   1.250   0.3456   0.00816   0.00328  -0.0380   0.6531   0.8052
   1.500   0.3684   0.00827   0.00332  -0.0368   0.6328   0.8098
   1.750   0.3907   0.00842   0.00340  -0.0355   0.6118   0.8143
   2.000   0.4125   0.00858   0.00347  -0.0341   0.5893   0.8192
   2.250   0.4337   0.00874   0.00352  -0.0328   0.5630   0.8243
   2.500   0.4531   0.00891   0.00358  -0.0309   0.5353   0.8284
   2.750   0.4731   0.00910   0.00368  -0.0292   0.5082   0.8325
   3.250   0.5144   0.00949   0.00387  -0.0263   0.4605   0.8417
   3.500   0.5347   0.00967   0.00395  -0.0249   0.4366   0.8456
   3.750   0.5540   0.00988   0.00408  -0.0231   0.4139   0.8493
   4.000   0.5731   0.01009   0.00421  -0.0214   0.3928   0.8536
   4.250   0.5931   0.01029   0.00433  -0.0199   0.3729   0.8582
   4.500   0.6133   0.01048   0.00444  -0.0185   0.3537   0.8624
   4.750   0.6318   0.01068   0.00459  -0.0167   0.3356   0.8663
   5.000   0.6507   0.01091   0.00475  -0.0150   0.3179   0.8707
   5.250   0.6707   0.01114   0.00492  -0.0136   0.3017   0.8754
   5.500   0.6910   0.01139   0.00510  -0.0123   0.2868   0.8799
   5.750   0.7095   0.01162   0.00530  -0.0105   0.2730   0.8842
   6.000   0.7290   0.01184   0.00550  -0.0090   0.2598   0.8891
   6.250   0.7491   0.01210   0.00571  -0.0077   0.2468   0.8942
   6.500   0.7679   0.01235   0.00592  -0.0061   0.2346   0.8989
   6.750   0.7851   0.01262   0.00616  -0.0042   0.2224   0.9042
   7.000   0.8044   0.01286   0.00638  -0.0027   0.2109   0.9102
   7.250   0.8220   0.01313   0.00662  -0.0010   0.1993   0.9158
   7.500   0.8379   0.01343   0.00689   0.0011   0.1876   0.9221
   7.750   0.8547   0.01374   0.00716   0.0029   0.1756   0.9292
   8.000   0.8694   0.01401   0.00743   0.0052   0.1647   0.9370
   8.250   0.8843   0.01434   0.00774   0.0073   0.1551   0.9459
   8.500   0.8985   0.01472   0.00808   0.0095   0.1455   0.9565
   8.750   0.9208   0.01508   0.00845   0.0100   0.1378   0.9661
   9.000   0.9475   0.01566   0.00899   0.0093   0.1300   0.9754
   9.250   0.9796   0.01612   0.00947   0.0077   0.1243   0.9839
   9.500   1.0073   0.01679   0.01010   0.0065   0.1186   1.0000
   9.750   1.0249   0.01720   0.01053   0.0076   0.1154   1.0000
  10.000   1.0437   0.01764   0.01098   0.0084   0.1123   1.0000
  10.250   1.0605   0.01819   0.01153   0.0095   0.1094   1.0000
  10.500   1.0740   0.01893   0.01224   0.0111   0.1064   1.0000
  10.750   1.0895   0.01955   0.01290   0.0123   0.1044   1.0000
  11.000   1.1071   0.02008   0.01347   0.0134   0.1025   1.0000
  11.250   1.1234   0.02066   0.01409   0.0145   0.1006   1.0000
  11.500   1.1384   0.02132   0.01477   0.0157   0.0987   1.0000
  11.750   1.1512   0.02210   0.01556   0.0172   0.0968   1.0000
  12.000   1.1609   0.02311   0.01657   0.0189   0.0947   1.0000
  12.250   1.1729   0.02402   0.01752   0.0203   0.0934   1.0000
  12.500   1.1880   0.02471   0.01829   0.0214   0.0923   1.0000
  12.750   1.2018   0.02551   0.01914   0.0225   0.0911   1.0000
  13.000   1.2151   0.02634   0.02003   0.0235   0.0894   1.0000
  13.250   1.2272   0.02726   0.02100   0.0247   0.0882   1.0000
  13.500   1.2383   0.02828   0.02205   0.0258   0.0870   1.0000
  13.750   1.2480   0.02943   0.02322   0.0269   0.0857   1.0000
  14.000   1.2559   0.03079   0.02459   0.0282   0.0843   1.0000
  14.250   1.2653   0.03207   0.02593   0.0292   0.0830   1.0000
  14.500   1.2766   0.03317   0.02712   0.0300   0.0822   1.0000
  14.750   1.2868   0.03438   0.02842   0.0307   0.0812   1.0000
  15.000   1.2965   0.03567   0.02978   0.0314   0.0801   1.0000
  15.250   1.3055   0.03704   0.03122   0.0320   0.0789   1.0000
  15.500   1.3138   0.03850   0.03274   0.0326   0.0779   1.0000
  15.750   1.3214   0.04007   0.03436   0.0331   0.0769   1.0000
  16.000   1.3279   0.04177   0.03609   0.0335   0.0758   1.0000
  16.250   1.3344   0.04354   0.03787   0.0340   0.0746   1.0000
  16.500   1.3407   0.04536   0.03976   0.0344   0.0736   1.0000
  16.750   1.3460   0.04731   0.04183   0.0344   0.0729   1.0000
  17.000   1.3508   0.04938   0.04401   0.0344   0.0721   1.0000
  17.250   1.3552   0.05154   0.04627   0.0343   0.0712   1.0000
  17.500   1.3591   0.05381   0.04863   0.0340   0.0703   1.0000
  17.750   1.3625   0.05618   0.05108   0.0336   0.0693   1.0000
  18.000   1.3657   0.05861   0.05358   0.0331   0.0685   1.0000
  18.250   1.3682   0.06119   0.05621   0.0324   0.0676   1.0000
  18.500   1.3708   0.06377   0.05882   0.0319   0.0667   1.0000
  18.750   1.3751   0.06601   0.06108   0.0317   0.0654   1.0000
  19.000   1.3735   0.06930   0.06450   0.0306   0.0648   1.0000
  19.250   1.3704   0.07288   0.06823   0.0291   0.0642   1.0000
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