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RUTAN CANARD AIRFOIL (amsoil1-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RUTAN CANARD AIRFOIL (amsoil1-il)
Reynolds number: 500,000
Max Cl/Cd: 68.14 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-amsoil1-il-500000-n5.txt
Download as CSV file: xf-amsoil1-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RUTAN CANARD AIRFOIL                            
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -1.0672   0.05495   0.05161  -0.0521   1.0000   0.0200
 -14.500  -1.1026   0.04571   0.04206  -0.0593   1.0000   0.0200
 -14.250  -1.1188   0.04098   0.03709  -0.0612   1.0000   0.0201
 -14.000  -1.1276   0.03767   0.03355  -0.0613   1.0000   0.0203
 -13.750  -1.1316   0.03516   0.03083  -0.0602   1.0000   0.0205
 -13.500  -1.1310   0.03321   0.02868  -0.0586   1.0000   0.0207
 -13.250  -1.1217   0.03176   0.02714  -0.0575   1.0000   0.0209
 -13.000  -1.1078   0.03059   0.02590  -0.0568   1.0000   0.0212
 -12.750  -1.0916   0.02956   0.02480  -0.0561   1.0000   0.0214
 -12.500  -1.0741   0.02857   0.02373  -0.0555   1.0000   0.0217
 -12.250  -1.0560   0.02756   0.02261  -0.0550   1.0000   0.0220
 -12.000  -1.0373   0.02652   0.02147  -0.0545   1.0000   0.0223
 -11.750  -1.0176   0.02549   0.02031  -0.0540   0.9978   0.0227
 -11.500  -0.9924   0.02442   0.01907  -0.0547   0.9767   0.0231
 -11.250  -0.9682   0.02341   0.01789  -0.0549   0.9624   0.0235
 -11.000  -0.9459   0.02255   0.01685  -0.0545   0.9497   0.0239
 -10.750  -0.9251   0.02175   0.01594  -0.0538   0.9386   0.0243
 -10.500  -0.9035   0.02115   0.01528  -0.0530   0.9285   0.0247
 -10.250  -0.8806   0.02062   0.01468  -0.0524   0.9198   0.0251
 -10.000  -0.8577   0.02010   0.01407  -0.0518   0.9120   0.0256
  -9.750  -0.8340   0.01952   0.01339  -0.0513   0.9049   0.0260
  -9.500  -0.8103   0.01893   0.01269  -0.0508   0.8977   0.0265
  -9.250  -0.7861   0.01836   0.01200  -0.0503   0.8914   0.0271
  -9.000  -0.7611   0.01783   0.01134  -0.0500   0.8851   0.0276
  -8.750  -0.7365   0.01727   0.01069  -0.0496   0.8792   0.0281
  -8.500  -0.7113   0.01678   0.01017  -0.0493   0.8737   0.0287
  -8.250  -0.6853   0.01636   0.00970  -0.0492   0.8678   0.0292
  -8.000  -0.6594   0.01594   0.00921  -0.0489   0.8622   0.0298
  -7.750  -0.6335   0.01553   0.00872  -0.0487   0.8574   0.0305
  -7.500  -0.6068   0.01511   0.00824  -0.0486   0.8523   0.0311
  -7.250  -0.5800   0.01474   0.00778  -0.0484   0.8468   0.0318
  -7.000  -0.5539   0.01431   0.00731  -0.0482   0.8418   0.0326
  -6.750  -0.5270   0.01395   0.00693  -0.0481   0.8373   0.0334
  -6.500  -0.4996   0.01362   0.00657  -0.0481   0.8323   0.0342
  -6.250  -0.4724   0.01330   0.00621  -0.0480   0.8273   0.0350
  -6.000  -0.4453   0.01301   0.00585  -0.0479   0.8227   0.0359
  -5.750  -0.4176   0.01271   0.00551  -0.0478   0.8181   0.0368
  -5.500  -0.3901   0.01238   0.00519  -0.0479   0.8134   0.0380
  -5.250  -0.3623   0.01213   0.00492  -0.0478   0.8086   0.0393
  -5.000  -0.3346   0.01190   0.00464  -0.0478   0.8043   0.0405
  -4.750  -0.3064   0.01166   0.00438  -0.0478   0.7997   0.0417
  -4.500  -0.2785   0.01139   0.00412  -0.0479   0.7949   0.0434
  -4.250  -0.2503   0.01119   0.00391  -0.0479   0.7902   0.0454
  -3.750  -0.1937   0.01080   0.00351  -0.0480   0.7816   0.0500
  -3.500  -0.1652   0.01063   0.00333  -0.0482   0.7768   0.0529
  -3.250  -0.1368   0.01045   0.00316  -0.0482   0.7723   0.0561
  -3.000  -0.1084   0.01032   0.00301  -0.0483   0.7683   0.0602
  -2.750  -0.0796   0.01015   0.00288  -0.0485   0.7642   0.0648
  -2.500  -0.0507   0.01002   0.00276  -0.0486   0.7598   0.0695
  -2.250  -0.0221   0.00988   0.00265  -0.0487   0.7553   0.0753
  -2.000   0.0066   0.00976   0.00254  -0.0488   0.7511   0.0817
  -1.750   0.0355   0.00965   0.00245  -0.0490   0.7470   0.0891
  -1.500   0.0645   0.00952   0.00237  -0.0492   0.7425   0.0978
  -1.250   0.0934   0.00940   0.00230  -0.0494   0.7379   0.1085
  -1.000   0.1221   0.00929   0.00223  -0.0495   0.7334   0.1227
  -0.750   0.1511   0.00916   0.00218  -0.0498   0.7287   0.1430
  -0.500   0.1800   0.00898   0.00213  -0.0500   0.7236   0.1745
  -0.250   0.2086   0.00875   0.00208  -0.0502   0.7189   0.2290
   0.000   0.2342   0.00748   0.00195  -0.0507   0.7149   0.5768
   0.250   0.2617   0.00716   0.00203  -0.0505   0.7104   0.6868
   0.500   0.2898   0.00706   0.00209  -0.0504   0.7053   0.7348
   0.750   0.3176   0.00703   0.00210  -0.0501   0.6952   0.7669
   1.000   0.3452   0.00702   0.00210  -0.0498   0.6788   0.7902
   1.250   0.3728   0.00703   0.00212  -0.0495   0.6639   0.8120
   1.500   0.4003   0.00705   0.00216  -0.0492   0.6490   0.8312
   1.750   0.4276   0.00710   0.00220  -0.0488   0.6325   0.8476
   2.000   0.4539   0.00718   0.00224  -0.0483   0.6106   0.8659
   2.250   0.4795   0.00728   0.00230  -0.0475   0.5817   0.8837
   2.500   0.5057   0.00748   0.00236  -0.0471   0.5459   0.8945
   2.750   0.5308   0.00779   0.00247  -0.0465   0.4938   0.9022
   3.000   0.5533   0.00847   0.00273  -0.0457   0.3964   0.9110
   3.250   0.5727   0.00945   0.00315  -0.0446   0.2720   0.9206
   3.500   0.5948   0.01010   0.00347  -0.0437   0.2007   0.9309
   3.750   0.6189   0.01049   0.00371  -0.0431   0.1649   0.9424
   4.000   0.6443   0.01082   0.00392  -0.0427   0.1404   0.9542
   4.250   0.6722   0.01111   0.00412  -0.0428   0.1224   0.9662
   4.500   0.7023   0.01140   0.00434  -0.0435   0.1089   0.9794
   4.750   0.7336   0.01169   0.00456  -0.0445   0.0976   0.9991
   5.000   0.7598   0.01200   0.00480  -0.0444   0.0888   1.0000
   5.250   0.7863   0.01227   0.00504  -0.0443   0.0822   1.0000
   5.500   0.8124   0.01258   0.00530  -0.0441   0.0765   1.0000
   5.750   0.8383   0.01288   0.00557  -0.0439   0.0710   1.0000
   6.000   0.8640   0.01319   0.00586  -0.0437   0.0664   1.0000
   6.250   0.8895   0.01353   0.00615  -0.0435   0.0621   1.0000
   6.500   0.9148   0.01386   0.00647  -0.0432   0.0588   1.0000
   6.750   0.9398   0.01420   0.00680  -0.0428   0.0555   1.0000
   7.000   0.9643   0.01457   0.00715  -0.0424   0.0527   1.0000
   7.250   0.9889   0.01492   0.00750  -0.0420   0.0501   1.0000
   7.500   1.0128   0.01532   0.00788  -0.0416   0.0478   1.0000
   7.750   1.0364   0.01573   0.00829  -0.0410   0.0461   1.0000
   8.000   1.0600   0.01612   0.00870  -0.0405   0.0445   1.0000
   8.250   1.0829   0.01654   0.00913  -0.0399   0.0428   1.0000
   8.500   1.1048   0.01703   0.00961  -0.0391   0.0413   1.0000
   8.750   1.1269   0.01748   0.01008  -0.0384   0.0402   1.0000
   9.000   1.1486   0.01794   0.01058  -0.0376   0.0391   1.0000
   9.250   1.1696   0.01843   0.01109  -0.0367   0.0380   1.0000
   9.500   1.1896   0.01896   0.01163  -0.0357   0.0370   1.0000
   9.750   1.2077   0.01957   0.01224  -0.0344   0.0360   1.0000
  10.000   1.2248   0.02012   0.01284  -0.0329   0.0353   1.0000
  10.250   1.2420   0.02069   0.01346  -0.0315   0.0345   1.0000
  10.500   1.2589   0.02132   0.01413  -0.0302   0.0338   1.0000
  10.750   1.2755   0.02198   0.01484  -0.0289   0.0331   1.0000
  11.000   1.2917   0.02270   0.01558  -0.0276   0.0323   1.0000
  11.250   1.3067   0.02351   0.01642  -0.0263   0.0316   1.0000
  11.500   1.3207   0.02442   0.01736  -0.0249   0.0310   1.0000
  11.750   1.3364   0.02522   0.01824  -0.0238   0.0305   1.0000
  12.000   1.3512   0.02609   0.01918  -0.0226   0.0299   1.0000
  12.250   1.3656   0.02701   0.02017  -0.0215   0.0293   1.0000
  12.500   1.3797   0.02797   0.02118  -0.0204   0.0288   1.0000
  12.750   1.3933   0.02897   0.02224  -0.0193   0.0282   1.0000
  13.000   1.4058   0.03006   0.02338  -0.0183   0.0277   1.0000
  13.250   1.4165   0.03133   0.02468  -0.0171   0.0272   1.0000
  13.500   1.4266   0.03267   0.02608  -0.0160   0.0268   1.0000
  13.750   1.4379   0.03393   0.02745  -0.0150   0.0264   1.0000
  14.000   1.4483   0.03528   0.02890  -0.0140   0.0260   1.0000
  14.250   1.4579   0.03672   0.03042  -0.0131   0.0256   1.0000
  14.500   1.4668   0.03825   0.03204  -0.0122   0.0252   1.0000
  14.750   1.4749   0.03987   0.03374  -0.0114   0.0248   1.0000
  15.000   1.4825   0.04156   0.03551  -0.0106   0.0244   1.0000
  15.250   1.4892   0.04336   0.03739  -0.0100   0.0241   1.0000
  15.500   1.4944   0.04535   0.03945  -0.0093   0.0238   1.0000
  15.750   1.4974   0.04759   0.04176  -0.0088   0.0234   1.0000
  16.000   1.4985   0.05009   0.04433  -0.0083   0.0231   1.0000
  16.250   1.5019   0.05244   0.04682  -0.0081   0.0229   1.0000
  16.500   1.5041   0.05499   0.04950  -0.0079   0.0226   1.0000
  16.750   1.5049   0.05778   0.05241  -0.0079   0.0223   1.0000
  17.000   1.5046   0.06082   0.05557  -0.0081   0.0220   1.0000
  17.250   1.5033   0.06408   0.05896  -0.0085   0.0218   1.0000
  17.500   1.5006   0.06761   0.06261  -0.0092   0.0215   1.0000
  17.750   1.4968   0.07140   0.06652  -0.0101   0.0213   1.0000
  18.000   1.4916   0.07553   0.07077  -0.0112   0.0211   1.0000
  18.250   1.4848   0.08003   0.07540  -0.0127   0.0209   1.0000
  18.500   1.4762   0.08494   0.08043  -0.0145   0.0207   1.0000
  18.750   1.4655   0.09032   0.08594  -0.0167   0.0206   1.0000
  19.000   1.4529   0.09621   0.09196  -0.0193   0.0205   1.0000
  19.250   1.4379   0.10270   0.09859  -0.0224   0.0203   1.0000
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