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Falcon (falcon-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Falcon (falcon-il)
Reynolds number: 1,000,000
Max Cl/Cd: 92.37 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-falcon-il-1000000-n5.txt
Download as CSV file: xf-falcon-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Falcon                                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -0.9737   0.12941   0.12703  -0.0029   1.0000   0.0091
 -18.250  -1.1019   0.10093   0.09822  -0.0185   1.0000   0.0088
 -18.000  -1.2000   0.07813   0.07503  -0.0312   1.0000   0.0085
 -17.750  -1.2423   0.06702   0.06369  -0.0378   1.0000   0.0085
 -17.500  -1.2687   0.05917   0.05566  -0.0423   1.0000   0.0084
 -17.250  -1.2878   0.05299   0.04932  -0.0456   1.0000   0.0085
 -17.000  -1.3012   0.04801   0.04420  -0.0477   1.0000   0.0085
 -16.750  -1.3105   0.04397   0.04003  -0.0489   1.0000   0.0086
 -16.500  -1.3160   0.04069   0.03663  -0.0494   1.0000   0.0087
 -16.250  -1.3192   0.03790   0.03374  -0.0493   1.0000   0.0088
 -16.000  -1.3198   0.03556   0.03130  -0.0488   1.0000   0.0089
 -15.750  -1.3181   0.03359   0.02924  -0.0478   1.0000   0.0090
 -15.500  -1.3152   0.03185   0.02742  -0.0466   1.0000   0.0091
 -15.250  -1.3108   0.03035   0.02582  -0.0451   1.0000   0.0092
 -15.000  -1.3051   0.02903   0.02443  -0.0434   1.0000   0.0094
 -14.750  -1.2990   0.02783   0.02315  -0.0415   1.0000   0.0095
 -14.500  -1.2920   0.02676   0.02200  -0.0394   1.0000   0.0096
 -14.250  -1.2841   0.02583   0.02100  -0.0371   1.0000   0.0098
 -14.000  -1.2764   0.02496   0.02005  -0.0345   1.0000   0.0099
 -13.750  -1.2682   0.02419   0.01921  -0.0317   1.0000   0.0101
 -13.500  -1.2603   0.02348   0.01843  -0.0287   1.0000   0.0102
 -13.250  -1.2503   0.02282   0.01770  -0.0259   1.0000   0.0104
 -13.000  -1.2363   0.02214   0.01695  -0.0238   1.0000   0.0105
 -12.750  -1.2208   0.02150   0.01625  -0.0220   1.0000   0.0107
 -12.500  -1.2045   0.02091   0.01559  -0.0203   1.0000   0.0108
 -12.250  -1.1897   0.02015   0.01478  -0.0183   1.0000   0.0111
 -12.000  -1.1728   0.01952   0.01410  -0.0166   1.0000   0.0114
 -11.750  -1.1545   0.01896   0.01351  -0.0151   1.0000   0.0117
 -11.500  -1.1353   0.01846   0.01297  -0.0137   1.0000   0.0120
 -11.250  -1.1157   0.01798   0.01245  -0.0124   1.0000   0.0123
 -11.000  -1.0957   0.01752   0.01196  -0.0111   1.0000   0.0126
 -10.750  -1.0754   0.01707   0.01147  -0.0098   1.0000   0.0130
 -10.500  -1.0550   0.01664   0.01099  -0.0085   1.0000   0.0133
 -10.250  -1.0344   0.01623   0.01054  -0.0072   1.0000   0.0135
 -10.000  -1.0056   0.01575   0.01001  -0.0077   0.9990   0.0138
  -9.750  -0.9877   0.01520   0.00944  -0.0059   0.9759   0.0143
  -9.500  -0.9539   0.01470   0.00892  -0.0074   0.9698   0.0149
  -9.250  -0.9183   0.01423   0.00843  -0.0094   0.9655   0.0154
  -9.000  -0.8807   0.01379   0.00795  -0.0118   0.9619   0.0160
  -8.750  -0.8408   0.01337   0.00750  -0.0147   0.9584   0.0167
  -8.250  -0.7561   0.01247   0.00655  -0.0217   0.9506   0.0185
  -8.000  -0.7146   0.01208   0.00613  -0.0250   0.9440   0.0195
  -7.750  -0.6790   0.01178   0.00578  -0.0269   0.9348   0.0204
  -7.500  -0.6474   0.01153   0.00548  -0.0278   0.9244   0.0211
  -7.250  -0.6205   0.01125   0.00517  -0.0277   0.9124   0.0226
  -7.000  -0.5948   0.01101   0.00491  -0.0273   0.8999   0.0240
  -6.750  -0.5692   0.01082   0.00466  -0.0268   0.8861   0.0253
  -6.500  -0.5443   0.01062   0.00441  -0.0261   0.8696   0.0268
  -6.250  -0.5200   0.01043   0.00417  -0.0253   0.8505   0.0290
  -6.000  -0.4957   0.01028   0.00395  -0.0245   0.8293   0.0311
  -5.750  -0.4719   0.01012   0.00372  -0.0236   0.8057   0.0342
  -5.500  -0.4482   0.01001   0.00352  -0.0227   0.7804   0.0373
  -5.250  -0.4244   0.00989   0.00332  -0.0217   0.7543   0.0412
  -5.000  -0.4005   0.00979   0.00315  -0.0208   0.7287   0.0455
  -4.750  -0.3766   0.00968   0.00298  -0.0199   0.7036   0.0519
  -4.500  -0.3524   0.00958   0.00283  -0.0191   0.6812   0.0590
  -4.250  -0.3277   0.00949   0.00269  -0.0184   0.6599   0.0661
  -4.000  -0.3029   0.00939   0.00256  -0.0177   0.6409   0.0742
  -3.750  -0.2778   0.00931   0.00244  -0.0171   0.6234   0.0820
  -3.500  -0.2523   0.00924   0.00234  -0.0165   0.6077   0.0899
  -3.250  -0.2270   0.00914   0.00223  -0.0159   0.5928   0.1001
  -3.000  -0.2013   0.00908   0.00214  -0.0154   0.5790   0.1082
  -2.750  -0.1756   0.00901   0.00205  -0.0149   0.5658   0.1178
  -2.500  -0.1500   0.00893   0.00197  -0.0144   0.5531   0.1294
  -2.250  -0.1243   0.00883   0.00188  -0.0139   0.5413   0.1443
  -2.000  -0.0987   0.00874   0.00181  -0.0134   0.5297   0.1616
  -1.750  -0.0741   0.00858   0.00172  -0.0127   0.5181   0.1922
  -1.500  -0.0557   0.00797   0.00154  -0.0109   0.5074   0.3232
  -1.250  -0.0323   0.00774   0.00147  -0.0100   0.4967   0.3812
  -1.000  -0.0083   0.00759   0.00142  -0.0091   0.4858   0.4264
  -0.750   0.0165   0.00747   0.00138  -0.0084   0.4751   0.4618
  -0.500   0.0411   0.00736   0.00136  -0.0077   0.4645   0.5001
  -0.250   0.0656   0.00727   0.00134  -0.0069   0.4534   0.5364
   0.000   0.0903   0.00720   0.00133  -0.0062   0.4422   0.5704
   0.250   0.1145   0.00710   0.00132  -0.0054   0.4316   0.6073
   0.500   0.1387   0.00704   0.00133  -0.0045   0.4211   0.6432
   0.750   0.1628   0.00699   0.00134  -0.0036   0.4094   0.6778
   1.000   0.1869   0.00695   0.00137  -0.0027   0.3979   0.7136
   1.250   0.2110   0.00693   0.00141  -0.0018   0.3867   0.7456
   1.500   0.2352   0.00693   0.00146  -0.0009   0.3755   0.7749
   1.750   0.2599   0.00694   0.00151  -0.0001   0.3648   0.8015
   2.000   0.2857   0.00698   0.00156   0.0004   0.3541   0.8183
   2.250   0.3120   0.00706   0.00162   0.0008   0.3434   0.8297
   2.500   0.3385   0.00711   0.00167   0.0012   0.3340   0.8418
   2.750   0.3652   0.00718   0.00174   0.0015   0.3251   0.8535
   3.000   0.3918   0.00727   0.00181   0.0018   0.3146   0.8655
   3.250   0.4190   0.00733   0.00189   0.0019   0.3062   0.8782
   3.500   0.4467   0.00743   0.00198   0.0020   0.2972   0.8909
   3.750   0.4759   0.00751   0.00207   0.0017   0.2876   0.9041
   4.000   0.5072   0.00762   0.00217   0.0009   0.2779   0.9184
   4.250   0.5429   0.00774   0.00229  -0.0010   0.2682   0.9321
   4.500   0.5814   0.00788   0.00241  -0.0035   0.2594   0.9427
   4.750   0.6250   0.00806   0.00256  -0.0073   0.2486   0.9476
   5.250   0.7060   0.00846   0.00288  -0.0134   0.2256   0.9564
   5.500   0.7458   0.00868   0.00306  -0.0163   0.2160   0.9592
   5.750   0.7844   0.00893   0.00327  -0.0189   0.2057   0.9623
   6.000   0.8216   0.00915   0.00347  -0.0211   0.1965   0.9664
   6.250   0.8571   0.00940   0.00369  -0.0230   0.1871   0.9703
   6.500   0.8904   0.00969   0.00393  -0.0244   0.1749   0.9738
   6.750   0.9214   0.01002   0.00418  -0.0254   0.1606   0.9777
   7.250   0.9735   0.01064   0.00473  -0.0250   0.1427   0.9973
   7.500   1.0048   0.01094   0.00498  -0.0261   0.1342   0.9988
   7.750   1.0364   0.01122   0.00524  -0.0272   0.1255   0.9998
   8.000   1.0607   0.01150   0.00549  -0.0267   0.1184   1.0000
   8.250   1.0819   0.01182   0.00576  -0.0256   0.1095   1.0000
   8.500   1.1034   0.01215   0.00605  -0.0245   0.1003   1.0000
   8.750   1.1245   0.01251   0.00638  -0.0234   0.0911   1.0000
   9.000   1.1439   0.01302   0.00679  -0.0221   0.0761   1.0000
   9.250   1.1513   0.01442   0.00788  -0.0189   0.0305   1.0000
   9.500   1.1685   0.01508   0.00849  -0.0172   0.0208   1.0000
   9.750   1.1880   0.01556   0.00898  -0.0159   0.0174   1.0000
  10.000   1.2078   0.01602   0.00944  -0.0147   0.0154   1.0000
  10.250   1.2271   0.01649   0.00993  -0.0134   0.0138   1.0000
  10.500   1.2461   0.01696   0.01042  -0.0121   0.0127   1.0000
  10.750   1.2652   0.01741   0.01091  -0.0108   0.0120   1.0000
  11.000   1.2832   0.01791   0.01144  -0.0093   0.0114   1.0000
  11.250   1.3002   0.01847   0.01202  -0.0078   0.0107   1.0000
  11.500   1.3160   0.01908   0.01266  -0.0061   0.0102   1.0000
  11.750   1.3316   0.01962   0.01325  -0.0043   0.0099   1.0000
  12.000   1.3427   0.02018   0.01385  -0.0017   0.0096   1.0000
  12.250   1.3524   0.02078   0.01450   0.0010   0.0093   1.0000
  12.500   1.3624   0.02144   0.01521   0.0035   0.0090   1.0000
  12.750   1.3717   0.02222   0.01604   0.0059   0.0088   1.0000
  13.000   1.3803   0.02311   0.01698   0.0080   0.0085   1.0000
  13.250   1.3878   0.02416   0.01808   0.0100   0.0082   1.0000
  13.500   1.3940   0.02538   0.01937   0.0119   0.0079   1.0000
  13.750   1.4004   0.02670   0.02075   0.0135   0.0078   1.0000
  14.000   1.4075   0.02806   0.02219   0.0147   0.0076   1.0000
  14.250   1.4134   0.02963   0.02383   0.0158   0.0075   1.0000
  14.500   1.4183   0.03139   0.02568   0.0166   0.0074   1.0000
  14.750   1.4218   0.03343   0.02779   0.0172   0.0073   1.0000
  15.000   1.4245   0.03569   0.03014   0.0175   0.0072   1.0000
  15.250   1.4254   0.03827   0.03282   0.0175   0.0071   1.0000
  15.500   1.4249   0.04114   0.03578   0.0172   0.0070   1.0000
  15.750   1.4223   0.04439   0.03913   0.0167   0.0069   1.0000
  16.000   1.4182   0.04790   0.04273   0.0159   0.0068   1.0000
  16.250   1.4122   0.05175   0.04669   0.0150   0.0067   1.0000
  16.500   1.4035   0.05601   0.05106   0.0138   0.0067   1.0000
  16.750   1.3933   0.06055   0.05570   0.0125   0.0066   1.0000
  17.000   1.3803   0.06562   0.06089   0.0109   0.0066   1.0000
  17.250   1.3655   0.07104   0.06642   0.0091   0.0066   1.0000
  17.500   1.3504   0.07664   0.07214   0.0071   0.0065   1.0000
  17.750   1.3335   0.08264   0.07826   0.0049   0.0065   1.0000
  18.000   1.3154   0.08892   0.08465   0.0025   0.0065   1.0000
  18.250   1.2967   0.09542   0.09127   0.0000   0.0064   1.0000
  18.500   1.2787   0.10191   0.09787  -0.0026   0.0064   1.0000
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