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Falcon (falcon-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Falcon (falcon-il)
Reynolds number: 500,000
Max Cl/Cd: 78.59 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-falcon-il-500000-n5.txt
Download as CSV file: xf-falcon-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.8867   0.11589   0.11301  -0.0108   1.0000   0.0122
 -16.500  -0.9969   0.08893   0.08565  -0.0256   1.0000   0.0118
 -16.250  -1.0444   0.07557   0.07204  -0.0337   1.0000   0.0117
 -16.000  -1.0739   0.06644   0.06271  -0.0393   1.0000   0.0117
 -15.750  -1.0935   0.05953   0.05562  -0.0434   1.0000   0.0117
 -15.500  -1.1074   0.05400   0.04992  -0.0463   1.0000   0.0118
 -15.250  -1.1173   0.04945   0.04522  -0.0484   1.0000   0.0119
 -15.000  -1.1235   0.04575   0.04138  -0.0495   1.0000   0.0120
 -14.750  -1.1285   0.04250   0.03800  -0.0500   1.0000   0.0121
 -14.500  -1.1311   0.03978   0.03513  -0.0499   1.0000   0.0122
 -14.250  -1.1314   0.03748   0.03271  -0.0492   1.0000   0.0124
 -14.000  -1.1312   0.03541   0.03050  -0.0481   1.0000   0.0126
 -13.750  -1.1290   0.03364   0.02861  -0.0467   1.0000   0.0128
 -13.500  -1.1256   0.03208   0.02693  -0.0450   1.0000   0.0130
 -13.250  -1.1207   0.03073   0.02545  -0.0430   1.0000   0.0132
 -13.000  -1.1149   0.02952   0.02412  -0.0408   1.0000   0.0134
 -12.750  -1.1084   0.02844   0.02291  -0.0383   1.0000   0.0136
 -12.500  -1.1042   0.02731   0.02169  -0.0352   1.0000   0.0138
 -12.250  -1.1004   0.02629   0.02060  -0.0318   1.0000   0.0141
 -12.000  -1.0924   0.02542   0.01966  -0.0289   1.0000   0.0144
 -11.750  -1.0797   0.02461   0.01879  -0.0268   1.0000   0.0146
 -11.500  -1.0660   0.02385   0.01796  -0.0247   1.0000   0.0149
 -11.250  -1.0511   0.02315   0.01719  -0.0228   1.0000   0.0153
 -11.000  -1.0357   0.02244   0.01641  -0.0209   1.0000   0.0156
 -10.750  -1.0196   0.02176   0.01565  -0.0191   1.0000   0.0160
 -10.500  -1.0029   0.02110   0.01491  -0.0173   1.0000   0.0164
 -10.250  -0.9855   0.02048   0.01421  -0.0156   1.0000   0.0168
 -10.000  -0.9674   0.01992   0.01357  -0.0140   1.0000   0.0171
  -9.750  -0.9513   0.01918   0.01281  -0.0121   1.0000   0.0177
  -9.500  -0.9330   0.01865   0.01225  -0.0105   1.0000   0.0183
  -9.250  -0.9141   0.01817   0.01174  -0.0089   1.0000   0.0189
  -9.000  -0.8953   0.01771   0.01123  -0.0073   1.0000   0.0195
  -8.750  -0.8751   0.01724   0.01071  -0.0060   0.9997   0.0202
  -8.250  -0.8201   0.01607   0.00945  -0.0065   0.9769   0.0216
  -8.000  -0.7878   0.01550   0.00885  -0.0077   0.9707   0.0226
  -7.750  -0.7529   0.01502   0.00834  -0.0095   0.9660   0.0239
  -7.500  -0.7164   0.01456   0.00783  -0.0116   0.9614   0.0252
  -7.250  -0.6778   0.01403   0.00727  -0.0142   0.9573   0.0267
  -7.000  -0.6369   0.01353   0.00676  -0.0173   0.9531   0.0287
  -6.750  -0.5963   0.01313   0.00631  -0.0203   0.9464   0.0309
  -6.500  -0.5569   0.01268   0.00585  -0.0231   0.9384   0.0338
  -6.250  -0.5216   0.01235   0.00548  -0.0249   0.9277   0.0369
  -6.000  -0.4919   0.01205   0.00516  -0.0254   0.9148   0.0403
  -5.750  -0.4641   0.01180   0.00488  -0.0254   0.9010   0.0447
  -5.500  -0.4377   0.01154   0.00461  -0.0251   0.8856   0.0503
  -5.250  -0.4119   0.01133   0.00437  -0.0246   0.8685   0.0566
  -5.000  -0.3865   0.01113   0.00414  -0.0241   0.8497   0.0640
  -4.750  -0.3617   0.01094   0.00391  -0.0234   0.8285   0.0721
  -4.500  -0.3371   0.01080   0.00371  -0.0226   0.8051   0.0804
  -4.250  -0.3128   0.01069   0.00352  -0.0217   0.7804   0.0893
  -4.000  -0.2888   0.01057   0.00334  -0.0208   0.7555   0.0988
  -3.750  -0.2647   0.01049   0.00318  -0.0199   0.7311   0.1076
  -3.500  -0.2404   0.01041   0.00303  -0.0191   0.7077   0.1176
  -3.250  -0.2165   0.01032   0.00288  -0.0182   0.6858   0.1288
  -3.000  -0.1923   0.01022   0.00274  -0.0174   0.6658   0.1421
  -2.750  -0.1681   0.01010   0.00261  -0.0166   0.6471   0.1592
  -2.500  -0.1442   0.00995   0.00247  -0.0157   0.6301   0.1831
  -2.250  -0.1243   0.00948   0.00226  -0.0142   0.6146   0.2644
  -2.000  -0.1058   0.00895   0.00212  -0.0125   0.6004   0.3859
  -1.500  -0.0605   0.00855   0.00196  -0.0102   0.5732   0.4870
  -1.250  -0.0374   0.00840   0.00191  -0.0092   0.5608   0.5293
  -1.000  -0.0145   0.00827   0.00187  -0.0080   0.5485   0.5713
  -0.750   0.0087   0.00816   0.00183  -0.0069   0.5366   0.6077
  -0.500   0.0318   0.00805   0.00182  -0.0058   0.5248   0.6486
  -0.250   0.0549   0.00796   0.00182  -0.0046   0.5133   0.6872
   0.000   0.0789   0.00792   0.00183  -0.0036   0.5021   0.7185
   0.250   0.1032   0.00790   0.00186  -0.0027   0.4907   0.7499
   0.500   0.1280   0.00789   0.00189  -0.0019   0.4793   0.7771
   0.750   0.1533   0.00790   0.00192  -0.0011   0.4679   0.8018
   1.250   0.2054   0.00795   0.00202  -0.0001   0.4446   0.8479
   1.500   0.2328   0.00801   0.00206   0.0001   0.4329   0.8620
   1.750   0.2611   0.00809   0.00211   0.0001   0.4205   0.8738
   2.000   0.2897   0.00818   0.00217   0.0000   0.4081   0.8854
   2.250   0.3188   0.00827   0.00223  -0.0003   0.3958   0.8972
   2.500   0.3502   0.00837   0.00230  -0.0010   0.3840   0.9084
   2.750   0.3834   0.00849   0.00239  -0.0023   0.3719   0.9187
   3.000   0.4174   0.00863   0.00248  -0.0037   0.3600   0.9295
   3.250   0.4569   0.00877   0.00259  -0.0064   0.3482   0.9387
   3.500   0.4974   0.00894   0.00273  -0.0093   0.3365   0.9458
   3.750   0.5385   0.00913   0.00286  -0.0124   0.3246   0.9507
   4.000   0.5752   0.00931   0.00301  -0.0145   0.3141   0.9561
   4.250   0.6136   0.00950   0.00317  -0.0170   0.3025   0.9590
   4.500   0.6500   0.00971   0.00334  -0.0190   0.2915   0.9623
   4.750   0.6844   0.00993   0.00352  -0.0205   0.2814   0.9665
   5.000   0.7192   0.01013   0.00371  -0.0222   0.2714   0.9702
   5.250   0.7535   0.01036   0.00391  -0.0237   0.2611   0.9742
   5.500   0.7856   0.01062   0.00413  -0.0248   0.2498   0.9794
   5.750   0.8157   0.01087   0.00435  -0.0255   0.2391   0.9869
   6.000   0.8443   0.01114   0.00461  -0.0259   0.2301   0.9952
   6.250   0.8769   0.01140   0.00483  -0.0272   0.2201   0.9979
   6.500   0.9101   0.01165   0.00507  -0.0286   0.2105   0.9997
   6.750   0.9335   0.01188   0.00528  -0.0279   0.2024   1.0000
   7.000   0.9541   0.01214   0.00551  -0.0266   0.1928   1.0000
   7.250   0.9749   0.01243   0.00576  -0.0254   0.1813   1.0000
   7.500   0.9957   0.01275   0.00603  -0.0242   0.1698   1.0000
   7.750   1.0165   0.01308   0.00632  -0.0230   0.1599   1.0000
   8.000   1.0375   0.01342   0.00663  -0.0219   0.1506   1.0000
   8.250   1.0590   0.01373   0.00694  -0.0208   0.1433   1.0000
   8.500   1.0801   0.01408   0.00728  -0.0197   0.1363   1.0000
   8.750   1.1014   0.01442   0.00761  -0.0186   0.1293   1.0000
   9.000   1.1214   0.01485   0.00801  -0.0174   0.1199   1.0000
   9.250   1.1416   0.01526   0.00840  -0.0162   0.1103   1.0000
   9.500   1.1612   0.01571   0.00883  -0.0149   0.1002   1.0000
   9.750   1.1783   0.01633   0.00936  -0.0133   0.0848   1.0000
  10.000   1.1875   0.01746   0.01026  -0.0106   0.0511   1.0000
  10.250   1.1925   0.01882   0.01146  -0.0073   0.0261   1.0000
  10.500   1.2058   0.01957   0.01222  -0.0051   0.0214   1.0000
  10.750   1.2200   0.02024   0.01292  -0.0031   0.0191   1.0000
  11.000   1.2326   0.02095   0.01367  -0.0009   0.0174   1.0000
  11.250   1.2408   0.02166   0.01444   0.0021   0.0162   1.0000
  11.500   1.2498   0.02233   0.01518   0.0049   0.0154   1.0000
  11.750   1.2582   0.02311   0.01602   0.0076   0.0146   1.0000
  12.000   1.2653   0.02405   0.01701   0.0101   0.0138   1.0000
  12.250   1.2711   0.02516   0.01820   0.0124   0.0133   1.0000
  12.500   1.2773   0.02637   0.01948   0.0144   0.0129   1.0000
  12.750   1.2841   0.02762   0.02082   0.0161   0.0125   1.0000
  13.000   1.2899   0.02906   0.02235   0.0175   0.0122   1.0000
  13.250   1.2944   0.03072   0.02411   0.0187   0.0118   1.0000
  13.500   1.2979   0.03262   0.02610   0.0196   0.0116   1.0000
  13.750   1.3004   0.03476   0.02834   0.0202   0.0113   1.0000
  14.000   1.3011   0.03726   0.03093   0.0204   0.0110   1.0000
  14.250   1.2999   0.04012   0.03390   0.0203   0.0109   1.0000
  14.500   1.2970   0.04334   0.03723   0.0199   0.0107   1.0000
  14.750   1.2912   0.04706   0.04105   0.0191   0.0105   1.0000
  15.000   1.2829   0.05121   0.04532   0.0181   0.0104   1.0000
  15.250   1.2714   0.05591   0.05014   0.0167   0.0102   1.0000
  15.500   1.2609   0.06053   0.05489   0.0154   0.0102   1.0000
  15.750   1.2498   0.06536   0.05984   0.0138   0.0101   1.0000
  16.000   1.2387   0.07029   0.06490   0.0122   0.0100   1.0000
  16.250   1.2269   0.07545   0.07017   0.0104   0.0099   1.0000
  16.500   1.2135   0.08097   0.07581   0.0084   0.0099   1.0000
  16.750   1.2006   0.08649   0.08145   0.0063   0.0098   1.0000
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