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RUTAN CANARD AIRFOIL (amsoil1-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RUTAN CANARD AIRFOIL (amsoil1-il)
Reynolds number: 1,000,000
Max Cl/Cd: 81.08 at α=7.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-amsoil1-il-1000000-n5.txt
Download as CSV file: xf-amsoil1-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.3219   0.05242   0.04935  -0.0541   1.0000   0.0154
 -17.000  -1.3528   0.04447   0.04117  -0.0595   1.0000   0.0154
 -16.750  -1.3643   0.04025   0.03679  -0.0613   1.0000   0.0155
 -16.500  -1.3694   0.03717   0.03359  -0.0619   1.0000   0.0156
 -16.250  -1.3707   0.03476   0.03106  -0.0617   1.0000   0.0157
 -16.000  -1.3690   0.03281   0.02900  -0.0610   1.0000   0.0159
 -15.750  -1.3651   0.03119   0.02728  -0.0598   1.0000   0.0160
 -15.500  -1.3597   0.02982   0.02582  -0.0582   1.0000   0.0162
 -15.250  -1.3509   0.02865   0.02455  -0.0566   1.0000   0.0164
 -15.000  -1.3375   0.02755   0.02335  -0.0556   1.0000   0.0165
 -14.750  -1.3222   0.02652   0.02223  -0.0547   1.0000   0.0168
 -14.500  -1.3055   0.02555   0.02116  -0.0539   1.0000   0.0170
 -14.250  -1.2874   0.02464   0.02016  -0.0532   1.0000   0.0172
 -14.000  -1.2682   0.02379   0.01923  -0.0526   1.0000   0.0174
 -13.750  -1.2481   0.02300   0.01834  -0.0521   1.0000   0.0175
 -13.500  -1.2279   0.02216   0.01742  -0.0515   1.0000   0.0177
 -13.250  -1.2062   0.02136   0.01656  -0.0512   0.9920   0.0180
 -13.000  -1.1806   0.02067   0.01581  -0.0516   0.9685   0.0183
 -12.750  -1.1588   0.02011   0.01517  -0.0509   0.9511   0.0186
 -12.500  -1.1375   0.01959   0.01457  -0.0500   0.9379   0.0189
 -12.250  -1.1156   0.01911   0.01400  -0.0493   0.9268   0.0192
 -12.000  -1.0924   0.01862   0.01344  -0.0487   0.9171   0.0195
 -11.750  -1.0691   0.01816   0.01288  -0.0482   0.9088   0.0199
 -11.500  -1.0449   0.01769   0.01233  -0.0478   0.9008   0.0202
 -11.000  -0.9958   0.01678   0.01124  -0.0470   0.8874   0.0207
 -10.750  -0.9714   0.01625   0.01066  -0.0467   0.8808   0.0211
 -10.500  -0.9462   0.01583   0.01018  -0.0464   0.8747   0.0215
 -10.250  -0.9203   0.01544   0.00974  -0.0462   0.8689   0.0219
 -10.000  -0.8943   0.01507   0.00933  -0.0461   0.8632   0.0222
  -9.500  -0.8415   0.01441   0.00855  -0.0458   0.8529   0.0232
  -9.250  -0.8148   0.01409   0.00817  -0.0457   0.8473   0.0236
  -9.000  -0.7881   0.01378   0.00779  -0.0455   0.8420   0.0239
  -8.750  -0.7614   0.01341   0.00737  -0.0454   0.8376   0.0243
  -8.500  -0.7345   0.01304   0.00698  -0.0454   0.8327   0.0248
  -8.250  -0.7074   0.01275   0.00666  -0.0453   0.8274   0.0253
  -8.000  -0.6801   0.01249   0.00636  -0.0453   0.8224   0.0259
  -7.750  -0.6524   0.01223   0.00607  -0.0453   0.8181   0.0265
  -7.500  -0.6247   0.01197   0.00577  -0.0453   0.8133   0.0270
  -7.250  -0.5970   0.01172   0.00548  -0.0453   0.8084   0.0275
  -7.000  -0.5692   0.01150   0.00520  -0.0453   0.8036   0.0278
  -6.750  -0.5415   0.01118   0.00488  -0.0453   0.7992   0.0286
  -6.500  -0.5135   0.01094   0.00462  -0.0454   0.7947   0.0293
  -6.250  -0.4854   0.01073   0.00439  -0.0454   0.7901   0.0301
  -6.000  -0.4573   0.01054   0.00416  -0.0455   0.7856   0.0308
  -5.750  -0.4288   0.01034   0.00394  -0.0456   0.7813   0.0315
  -5.500  -0.4004   0.01015   0.00373  -0.0457   0.7766   0.0321
  -5.250  -0.3721   0.00993   0.00350  -0.0458   0.7720   0.0331
  -5.000  -0.3437   0.00976   0.00331  -0.0458   0.7676   0.0342
  -4.750  -0.3150   0.00959   0.00314  -0.0460   0.7636   0.0354
  -4.500  -0.2863   0.00944   0.00297  -0.0461   0.7591   0.0364
  -4.250  -0.2576   0.00926   0.00279  -0.0463   0.7546   0.0378
  -4.000  -0.2290   0.00912   0.00264  -0.0464   0.7504   0.0395
  -3.750  -0.2000   0.00898   0.00251  -0.0466   0.7469   0.0412
  -3.500  -0.1710   0.00883   0.00238  -0.0467   0.7429   0.0434
  -3.250  -0.1421   0.00871   0.00226  -0.0469   0.7385   0.0464
  -3.000  -0.1132   0.00859   0.00214  -0.0471   0.7341   0.0495
  -2.750  -0.0841   0.00848   0.00205  -0.0473   0.7302   0.0532
  -2.500  -0.0549   0.00836   0.00196  -0.0475   0.7261   0.0572
  -2.250  -0.0258   0.00826   0.00187  -0.0477   0.7218   0.0616
  -2.000   0.0033   0.00816   0.00179  -0.0479   0.7172   0.0670
  -1.750   0.0325   0.00808   0.00172  -0.0481   0.7126   0.0720
  -1.500   0.0618   0.00799   0.00166  -0.0483   0.7076   0.0777
  -1.250   0.0910   0.00790   0.00161  -0.0485   0.7026   0.0852
  -1.000   0.1201   0.00783   0.00155  -0.0487   0.6981   0.0932
  -0.500   0.1788   0.00766   0.00148  -0.0492   0.6898   0.1148
  -0.250   0.2080   0.00756   0.00145  -0.0495   0.6849   0.1337
   0.000   0.2371   0.00746   0.00143  -0.0497   0.6792   0.1627
   0.250   0.2660   0.00733   0.00139  -0.0499   0.6637   0.2035
   0.500   0.2945   0.00710   0.00135  -0.0502   0.6454   0.2890
   0.750   0.3214   0.00607   0.00129  -0.0508   0.6286   0.6216
   1.000   0.3498   0.00597   0.00133  -0.0509   0.6110   0.6842
   1.250   0.3783   0.00597   0.00138  -0.0509   0.5889   0.7253
   1.500   0.4062   0.00609   0.00144  -0.0509   0.5544   0.7511
   1.750   0.4337   0.00629   0.00154  -0.0508   0.5125   0.7752
   2.000   0.4599   0.00669   0.00171  -0.0506   0.4432   0.7965
   2.250   0.4852   0.00726   0.00196  -0.0503   0.3559   0.8123
   2.500   0.5089   0.00800   0.00229  -0.0499   0.2475   0.8302
   2.750   0.5340   0.00846   0.00253  -0.0495   0.1869   0.8484
   3.000   0.5606   0.00875   0.00271  -0.0493   0.1561   0.8594
   3.250   0.5876   0.00899   0.00286  -0.0492   0.1339   0.8665
   3.500   0.6149   0.00921   0.00301  -0.0491   0.1183   0.8736
   3.750   0.6418   0.00941   0.00317  -0.0489   0.1057   0.8807
   4.000   0.6687   0.00962   0.00333  -0.0488   0.0952   0.8885
   4.250   0.6955   0.00981   0.00350  -0.0486   0.0869   0.8961
   4.500   0.7219   0.01000   0.00366  -0.0483   0.0801   0.9049
   4.750   0.7483   0.01018   0.00383  -0.0480   0.0747   0.9135
   5.000   0.7740   0.01039   0.00402  -0.0476   0.0689   0.9233
   5.250   0.7995   0.01056   0.00420  -0.0471   0.0645   0.9337
   5.500   0.8244   0.01076   0.00439  -0.0465   0.0604   0.9465
   5.750   0.8499   0.01094   0.00457  -0.0460   0.0570   0.9626
   6.000   0.8782   0.01117   0.00478  -0.0462   0.0532   0.9819
   6.250   0.9073   0.01140   0.00499  -0.0467   0.0499   1.0000
   6.500   0.9336   0.01169   0.00524  -0.0465   0.0467   1.0000
   6.750   0.9601   0.01194   0.00548  -0.0464   0.0447   1.0000
   7.000   0.9861   0.01222   0.00575  -0.0462   0.0425   1.0000
   7.250   1.0118   0.01252   0.00603  -0.0460   0.0407   1.0000
   7.500   1.0376   0.01280   0.00631  -0.0458   0.0392   1.0000
   7.750   1.0629   0.01311   0.00661  -0.0455   0.0376   1.0000
   8.000   1.0877   0.01345   0.00693  -0.0451   0.0362   1.0000
   8.250   1.1126   0.01377   0.00726  -0.0448   0.0353   1.0000
   8.500   1.1373   0.01409   0.00759  -0.0444   0.0344   1.0000
   8.750   1.1615   0.01443   0.00793  -0.0439   0.0334   1.0000
   9.000   1.1852   0.01480   0.00830  -0.0434   0.0324   1.0000
   9.250   1.2081   0.01521   0.00871  -0.0428   0.0314   1.0000
   9.500   1.2312   0.01559   0.00911  -0.0422   0.0308   1.0000
   9.750   1.2541   0.01596   0.00950  -0.0415   0.0302   1.0000
  10.000   1.2765   0.01635   0.00991  -0.0408   0.0295   1.0000
  10.250   1.2983   0.01676   0.01034  -0.0401   0.0288   1.0000
  10.500   1.3192   0.01721   0.01080  -0.0392   0.0281   1.0000
  10.750   1.3388   0.01770   0.01130  -0.0381   0.0274   1.0000
  11.000   1.3561   0.01822   0.01184  -0.0366   0.0269   1.0000
  11.250   1.3740   0.01868   0.01235  -0.0352   0.0264   1.0000
  11.500   1.3916   0.01919   0.01289  -0.0339   0.0259   1.0000
  11.750   1.4089   0.01974   0.01348  -0.0326   0.0254   1.0000
  12.000   1.4258   0.02034   0.01411  -0.0313   0.0249   1.0000
  12.250   1.4423   0.02099   0.01479  -0.0301   0.0244   1.0000
  12.500   1.4582   0.02169   0.01551  -0.0289   0.0240   1.0000
  12.750   1.4732   0.02247   0.01633  -0.0276   0.0235   1.0000
  13.000   1.4876   0.02331   0.01721  -0.0263   0.0231   1.0000
  13.250   1.5031   0.02408   0.01803  -0.0252   0.0228   1.0000
  13.500   1.5181   0.02490   0.01891  -0.0241   0.0224   1.0000
  13.750   1.5324   0.02577   0.01983  -0.0230   0.0220   1.0000
  14.000   1.5464   0.02669   0.02080  -0.0220   0.0216   1.0000
  14.250   1.5596   0.02768   0.02184  -0.0209   0.0212   1.0000
  14.500   1.5722   0.02873   0.02293  -0.0198   0.0208   1.0000
  14.750   1.5837   0.02989   0.02413  -0.0188   0.0205   1.0000
  15.000   1.5942   0.03116   0.02545  -0.0177   0.0201   1.0000
  15.250   1.6032   0.03255   0.02690  -0.0166   0.0198   1.0000
  15.500   1.6136   0.03386   0.02828  -0.0156   0.0196   1.0000
  15.750   1.6230   0.03526   0.02976  -0.0147   0.0193   1.0000
  16.000   1.6317   0.03675   0.03132  -0.0139   0.0191   1.0000
  16.250   1.6396   0.03833   0.03297  -0.0130   0.0188   1.0000
  16.500   1.6465   0.04003   0.03475  -0.0122   0.0185   1.0000
  16.750   1.6527   0.04184   0.03663  -0.0115   0.0183   1.0000
  17.000   1.6580   0.04376   0.03862  -0.0109   0.0180   1.0000
  17.250   1.6622   0.04581   0.04075  -0.0103   0.0178   1.0000
  17.500   1.6654   0.04807   0.04307  -0.0099   0.0176   1.0000
  17.750   1.6675   0.05051   0.04559  -0.0096   0.0173   1.0000
  18.000   1.6679   0.05323   0.04839  -0.0094   0.0171   1.0000
  18.250   1.6658   0.05631   0.05155  -0.0094   0.0168   1.0000
  18.500   1.6658   0.05924   0.05458  -0.0096   0.0167   1.0000
  18.750   1.6646   0.06240   0.05784  -0.0099   0.0165   1.0000
  19.000   1.6621   0.06581   0.06136  -0.0105   0.0164   1.0000
  19.250   1.6576   0.06956   0.06522  -0.0112   0.0162   1.0000
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