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RUTAN CANARD AIRFOIL (amsoil1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RUTAN CANARD AIRFOIL (amsoil1-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.01 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-amsoil1-il-1000000.txt
Download as CSV file: xf-amsoil1-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -1.1743   0.04854   0.04568  -0.0566   1.0000   0.0198
 -15.250  -1.1924   0.04287   0.03981  -0.0601   1.0000   0.0199
 -15.000  -1.2018   0.03909   0.03586  -0.0614   1.0000   0.0200
 -14.750  -1.2058   0.03630   0.03292  -0.0615   1.0000   0.0201
 -14.500  -1.2068   0.03409   0.03056  -0.0608   1.0000   0.0203
 -14.250  -1.2045   0.03238   0.02871  -0.0595   1.0000   0.0204
 -14.000  -1.1986   0.03104   0.02724  -0.0578   1.0000   0.0205
 -13.750  -1.1915   0.02929   0.02532  -0.0565   1.0000   0.0207
 -13.500  -1.1858   0.02717   0.02304  -0.0551   1.0000   0.0211
 -13.250  -1.1692   0.02612   0.02193  -0.0544   1.0000   0.0214
 -13.000  -1.1497   0.02534   0.02111  -0.0538   1.0000   0.0216
 -12.750  -1.1289   0.02463   0.02035  -0.0534   1.0000   0.0219
 -12.500  -1.1076   0.02392   0.01959  -0.0530   1.0000   0.0222
 -12.250  -1.0858   0.02318   0.01878  -0.0527   1.0000   0.0226
 -12.000  -1.0636   0.02243   0.01793  -0.0524   1.0000   0.0230
 -11.750  -1.0407   0.02169   0.01711  -0.0522   1.0000   0.0233
 -11.500  -1.0128   0.02107   0.01639  -0.0529   0.9885   0.0237
 -11.250  -0.9841   0.02059   0.01581  -0.0535   0.9748   0.0240
 -11.000  -0.9657   0.01922   0.01430  -0.0526   0.9597   0.0246
 -10.750  -0.9446   0.01866   0.01368  -0.0517   0.9475   0.0250
 -10.500  -0.9220   0.01823   0.01319  -0.0509   0.9376   0.0254
 -10.250  -0.8989   0.01781   0.01271  -0.0501   0.9286   0.0258
 -10.000  -0.8744   0.01737   0.01219  -0.0497   0.9211   0.0262
  -9.750  -0.8501   0.01692   0.01165  -0.0492   0.9136   0.0267
  -9.500  -0.8250   0.01648   0.01112  -0.0489   0.9070   0.0272
  -9.250  -0.7992   0.01613   0.01068  -0.0486   0.9002   0.0276
  -9.000  -0.7749   0.01552   0.00996  -0.0481   0.8939   0.0281
  -8.750  -0.7499   0.01482   0.00923  -0.0479   0.8883   0.0288
  -8.500  -0.7237   0.01444   0.00882  -0.0477   0.8823   0.0293
  -8.250  -0.6975   0.01411   0.00844  -0.0474   0.8766   0.0299
  -8.000  -0.6705   0.01376   0.00804  -0.0474   0.8714   0.0305
  -7.750  -0.6434   0.01343   0.00766  -0.0473   0.8660   0.0311
  -7.500  -0.6163   0.01319   0.00734  -0.0471   0.8608   0.0317
  -7.250  -0.5897   0.01271   0.00680  -0.0470   0.8558   0.0324
  -7.000  -0.5631   0.01218   0.00627  -0.0469   0.8508   0.0332
  -6.750  -0.5357   0.01189   0.00595  -0.0468   0.8458   0.0339
  -6.500  -0.5083   0.01164   0.00565  -0.0467   0.8409   0.0347
  -6.250  -0.4803   0.01137   0.00536  -0.0468   0.8364   0.0356
  -6.000  -0.4520   0.01116   0.00512  -0.0468   0.8316   0.0364
  -5.750  -0.4248   0.01076   0.00468  -0.0468   0.8267   0.0374
  -5.500  -0.3972   0.01049   0.00438  -0.0467   0.8218   0.0385
  -5.250  -0.3687   0.01025   0.00415  -0.0468   0.8176   0.0396
  -5.000  -0.3403   0.01005   0.00393  -0.0469   0.8129   0.0408
  -4.750  -0.3118   0.00989   0.00373  -0.0470   0.8082   0.0417
  -4.500  -0.2839   0.00959   0.00342  -0.0470   0.8035   0.0438
  -4.250  -0.2551   0.00941   0.00325  -0.0471   0.7993   0.0455
  -4.000  -0.2263   0.00925   0.00308  -0.0473   0.7949   0.0472
  -3.750  -0.1978   0.00903   0.00285  -0.0474   0.7906   0.0498
  -3.500  -0.1691   0.00891   0.00272  -0.0475   0.7860   0.0525
  -3.250  -0.1401   0.00872   0.00256  -0.0477   0.7820   0.0563
  -3.000  -0.1111   0.00859   0.00245  -0.0478   0.7775   0.0604
  -2.750  -0.0822   0.00843   0.00231  -0.0480   0.7731   0.0658
  -2.500  -0.0534   0.00834   0.00220  -0.0481   0.7686   0.0712
  -2.250  -0.0242   0.00821   0.00212  -0.0483   0.7647   0.0777
  -2.000   0.0050   0.00807   0.00202  -0.0486   0.7601   0.0853
  -1.750   0.0341   0.00796   0.00194  -0.0487   0.7553   0.0929
  -1.500   0.0631   0.00790   0.00187  -0.0489   0.7503   0.1018
  -1.250   0.0924   0.00776   0.00181  -0.0492   0.7462   0.1154
  -1.000   0.1217   0.00761   0.00175  -0.0494   0.7418   0.1352
  -0.750   0.1508   0.00747   0.00170  -0.0497   0.7375   0.1623
  -0.500   0.1797   0.00728   0.00165  -0.0499   0.7328   0.2121
  -0.250   0.2071   0.00621   0.00153  -0.0506   0.7287   0.5034
   0.000   0.2348   0.00562   0.00154  -0.0507   0.7236   0.6903
   0.250   0.2630   0.00552   0.00155  -0.0506   0.7138   0.7450
   0.500   0.2916   0.00545   0.00155  -0.0506   0.7023   0.7739
   0.750   0.3203   0.00544   0.00157  -0.0505   0.6923   0.7959
   1.000   0.3490   0.00544   0.00158  -0.0505   0.6822   0.8122
   1.250   0.3777   0.00545   0.00161  -0.0505   0.6715   0.8280
   1.500   0.4063   0.00548   0.00163  -0.0505   0.6587   0.8414
   2.000   0.4624   0.00556   0.00171  -0.0502   0.6314   0.8692
   2.250   0.4905   0.00562   0.00175  -0.0500   0.6159   0.8808
   2.500   0.5176   0.00573   0.00181  -0.0497   0.5924   0.8950
   2.750   0.5437   0.00589   0.00188  -0.0492   0.5606   0.9089
   3.000   0.5692   0.00612   0.00199  -0.0486   0.5146   0.9187
   3.250   0.5931   0.00672   0.00220  -0.0481   0.4247   0.9277
   3.500   0.6131   0.00763   0.00258  -0.0469   0.2992   0.9382
   3.750   0.6340   0.00833   0.00291  -0.0458   0.2117   0.9499
   4.000   0.6570   0.00874   0.00313  -0.0449   0.1684   0.9633
   4.250   0.6838   0.00906   0.00331  -0.0448   0.1397   0.9775
   4.500   0.7155   0.00936   0.00351  -0.0458   0.1195   0.9910
   4.750   0.7462   0.00965   0.00370  -0.0466   0.1049   1.0000
   5.000   0.7737   0.00992   0.00390  -0.0468   0.0943   1.0000
   5.250   0.8011   0.01019   0.00411  -0.0468   0.0858   1.0000
   5.500   0.8280   0.01049   0.00435  -0.0468   0.0782   1.0000
   5.750   0.8552   0.01073   0.00456  -0.0469   0.0730   1.0000
   6.000   0.8818   0.01102   0.00481  -0.0468   0.0675   1.0000
   6.250   0.9082   0.01132   0.00506  -0.0467   0.0625   1.0000
   6.500   0.9346   0.01161   0.00533  -0.0465   0.0586   1.0000
   6.750   0.9605   0.01193   0.00562  -0.0463   0.0550   1.0000
   7.000   0.9862   0.01225   0.00593  -0.0461   0.0522   1.0000
   7.250   1.0120   0.01254   0.00621  -0.0458   0.0498   1.0000
   7.500   1.0362   0.01298   0.00661  -0.0454   0.0470   1.0000
   7.750   1.0619   0.01326   0.00690  -0.0451   0.0457   1.0000
   8.000   1.0869   0.01358   0.00723  -0.0448   0.0442   1.0000
   8.250   1.1110   0.01396   0.00760  -0.0443   0.0426   1.0000
   8.500   1.1334   0.01449   0.00813  -0.0436   0.0409   1.0000
   8.750   1.1579   0.01480   0.00846  -0.0432   0.0401   1.0000
   9.000   1.1816   0.01516   0.00884  -0.0426   0.0390   1.0000
   9.250   1.2047   0.01556   0.00924  -0.0420   0.0380   1.0000
   9.500   1.2264   0.01603   0.00972  -0.0412   0.0370   1.0000
   9.750   1.2449   0.01675   0.01045  -0.0400   0.0358   1.0000
  10.000   1.2675   0.01710   0.01083  -0.0393   0.0352   1.0000
  10.250   1.2887   0.01753   0.01129  -0.0384   0.0345   1.0000
  10.500   1.3087   0.01800   0.01179  -0.0374   0.0338   1.0000
  10.750   1.3267   0.01847   0.01229  -0.0360   0.0331   1.0000
  11.000   1.3430   0.01904   0.01288  -0.0344   0.0323   1.0000
  11.250   1.3556   0.01989   0.01374  -0.0324   0.0315   1.0000
  11.500   1.3701   0.02066   0.01456  -0.0308   0.0309   1.0000
  11.750   1.3877   0.02124   0.01520  -0.0297   0.0305   1.0000
  12.000   1.4042   0.02190   0.01591  -0.0284   0.0300   1.0000
  12.250   1.4203   0.02261   0.01667  -0.0273   0.0294   1.0000
  12.500   1.4359   0.02336   0.01746  -0.0261   0.0289   1.0000
  12.750   1.4509   0.02418   0.01831  -0.0249   0.0284   1.0000
  13.000   1.4646   0.02510   0.01926  -0.0237   0.0279   1.0000
  13.250   1.4738   0.02639   0.02058  -0.0221   0.0273   1.0000
  13.500   1.4834   0.02769   0.02195  -0.0207   0.0268   1.0000
  13.750   1.4981   0.02858   0.02291  -0.0197   0.0265   1.0000
  14.000   1.5116   0.02958   0.02397  -0.0188   0.0261   1.0000
  14.250   1.5239   0.03069   0.02515  -0.0178   0.0257   1.0000
  14.500   1.5355   0.03188   0.02640  -0.0168   0.0253   1.0000
  14.750   1.5465   0.03313   0.02771  -0.0158   0.0249   1.0000
  15.000   1.5568   0.03445   0.02908  -0.0149   0.0245   1.0000
  15.250   1.5655   0.03595   0.03062  -0.0140   0.0241   1.0000
  15.500   1.5713   0.03773   0.03246  -0.0130   0.0238   1.0000
  15.750   1.5710   0.04009   0.03489  -0.0119   0.0234   1.0000
  16.000   1.5728   0.04234   0.03723  -0.0109   0.0231   1.0000
  16.250   1.5803   0.04408   0.03907  -0.0104   0.0229   1.0000
  16.500   1.5859   0.04603   0.04111  -0.0098   0.0226   1.0000
  16.750   1.5902   0.04819   0.04336  -0.0094   0.0224   1.0000
  17.000   1.5939   0.05049   0.04575  -0.0091   0.0221   1.0000
  17.250   1.5969   0.05292   0.04828  -0.0089   0.0218   1.0000
  17.500   1.5989   0.05554   0.05097  -0.0089   0.0216   1.0000
  17.750   1.6008   0.05824   0.05376  -0.0091   0.0213   1.0000
  18.000   1.6010   0.06124   0.05683  -0.0094   0.0210   1.0000
  18.250   1.6002   0.06446   0.06014  -0.0099   0.0208   1.0000
  18.500   1.5966   0.06811   0.06387  -0.0106   0.0206   1.0000
  18.750   1.5896   0.07233   0.06818  -0.0116   0.0204   1.0000
  19.000   1.5793   0.07713   0.07308  -0.0130   0.0202   1.0000
  19.250   1.5644   0.08275   0.07881  -0.0148   0.0200   1.0000
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