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RUTAN WING AIRFOIL (amsoil2-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RUTAN WING AIRFOIL (amsoil2-il)
Reynolds number: 1,000,000
Max Cl/Cd: 77.39 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-amsoil2-il-1000000-n5.txt
Download as CSV file: xf-amsoil2-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RUTAN WING 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
  ------ -------- --------- --------- -------- -------- --------
 -18.500  -1.3657   0.07342   0.07026  -0.0296   1.0000   0.0155
 -18.250  -1.4175   0.06018   0.05673  -0.0385   1.0000   0.0155
 -18.000  -1.4400   0.05334   0.04971  -0.0425   1.0000   0.0155
 -17.750  -1.4529   0.04841   0.04463  -0.0448   1.0000   0.0156
 -17.500  -1.4604   0.04455   0.04064  -0.0462   1.0000   0.0157
 -17.250  -1.4641   0.04135   0.03733  -0.0470   1.0000   0.0158
 -17.000  -1.4650   0.03864   0.03451  -0.0473   1.0000   0.0159
 -16.750  -1.4635   0.03629   0.03206  -0.0473   1.0000   0.0161
 -16.500  -1.4600   0.03427   0.02993  -0.0470   1.0000   0.0162
 -16.250  -1.4550   0.03247   0.02804  -0.0465   1.0000   0.0164
 -16.000  -1.4485   0.03088   0.02636  -0.0457   1.0000   0.0165
 -15.750  -1.4408   0.02946   0.02484  -0.0448   1.0000   0.0167
 -15.500  -1.4320   0.02819   0.02349  -0.0438   1.0000   0.0169
 -15.250  -1.4222   0.02706   0.02227  -0.0425   1.0000   0.0170
 -15.000  -1.4116   0.02606   0.02118  -0.0411   1.0000   0.0172
 -14.750  -1.4002   0.02517   0.02021  -0.0395   1.0000   0.0173
 -14.500  -1.3880   0.02425   0.01921  -0.0380   1.0000   0.0176
 -14.250  -1.3721   0.02339   0.01830  -0.0369   1.0000   0.0178
 -14.000  -1.3542   0.02264   0.01750  -0.0360   1.0000   0.0181
 -13.750  -1.3349   0.02197   0.01678  -0.0353   1.0000   0.0185
 -13.500  -1.3146   0.02133   0.01611  -0.0347   1.0000   0.0188
 -13.250  -1.2936   0.02073   0.01546  -0.0341   1.0000   0.0192
 -13.000  -1.2720   0.02015   0.01482  -0.0335   1.0000   0.0195
 -12.750  -1.2500   0.01959   0.01420  -0.0330   1.0000   0.0198
 -12.500  -1.2273   0.01905   0.01360  -0.0326   1.0000   0.0201
 -12.250  -1.2042   0.01854   0.01304  -0.0322   1.0000   0.0203
 -12.000  -1.1815   0.01794   0.01240  -0.0318   1.0000   0.0208
 -11.750  -1.1578   0.01742   0.01186  -0.0314   1.0000   0.0212
 -11.500  -1.1297   0.01695   0.01136  -0.0320   0.9804   0.0216
 -11.250  -1.1032   0.01652   0.01089  -0.0321   0.9665   0.0221
 -11.000  -1.0792   0.01614   0.01045  -0.0316   0.9538   0.0225
 -10.500  -1.0318   0.01545   0.00963  -0.0304   0.9328   0.0234
 -10.250  -1.0077   0.01512   0.00923  -0.0298   0.9245   0.0239
 -10.000  -0.9832   0.01471   0.00879  -0.0294   0.9164   0.0245
  -9.750  -0.9585   0.01437   0.00841  -0.0290   0.9089   0.0250
  -9.500  -0.9328   0.01404   0.00805  -0.0287   0.9020   0.0255
  -9.250  -0.9071   0.01374   0.00770  -0.0284   0.8951   0.0261
  -9.000  -0.8810   0.01345   0.00736  -0.0282   0.8890   0.0267
  -8.750  -0.8546   0.01317   0.00703  -0.0280   0.8826   0.0272
  -8.500  -0.8284   0.01288   0.00670  -0.0278   0.8764   0.0278
  -8.250  -0.8019   0.01257   0.00636  -0.0277   0.8710   0.0286
  -8.000  -0.7750   0.01229   0.00607  -0.0276   0.8654   0.0294
  -7.750  -0.7480   0.01204   0.00579  -0.0275   0.8600   0.0301
  -7.500  -0.7209   0.01180   0.00551  -0.0274   0.8550   0.0308
  -7.250  -0.6934   0.01157   0.00525  -0.0274   0.8498   0.0314
  -7.000  -0.6661   0.01131   0.00497  -0.0273   0.8443   0.0324
  -6.750  -0.6388   0.01107   0.00472  -0.0273   0.8392   0.0334
  -6.500  -0.6110   0.01085   0.00449  -0.0273   0.8349   0.0344
  -6.250  -0.5830   0.01065   0.00426  -0.0274   0.8303   0.0354
  -6.000  -0.5550   0.01046   0.00405  -0.0274   0.8256   0.0363
  -5.750  -0.5273   0.01024   0.00383  -0.0274   0.8211   0.0379
  -5.500  -0.4991   0.01005   0.00363  -0.0275   0.8169   0.0394
  -5.250  -0.4707   0.00988   0.00345  -0.0276   0.8121   0.0408
  -5.000  -0.4425   0.00970   0.00327  -0.0276   0.8068   0.0427
  -4.750  -0.4143   0.00954   0.00310  -0.0277   0.8018   0.0450
  -4.500  -0.3857   0.00938   0.00295  -0.0278   0.7973   0.0474
  -4.250  -0.3571   0.00921   0.00280  -0.0280   0.7925   0.0505
  -4.000  -0.3284   0.00908   0.00266  -0.0281   0.7879   0.0533
  -3.500  -0.2710   0.00880   0.00241  -0.0284   0.7792   0.0610
  -3.250  -0.2421   0.00866   0.00230  -0.0286   0.7748   0.0658
  -3.000  -0.2132   0.00854   0.00219  -0.0287   0.7704   0.0698
  -2.750  -0.1844   0.00843   0.00209  -0.0289   0.7662   0.0751
  -2.500  -0.1553   0.00831   0.00200  -0.0291   0.7622   0.0809
  -2.250  -0.1262   0.00819   0.00192  -0.0293   0.7575   0.0877
  -2.000  -0.0972   0.00807   0.00184  -0.0295   0.7529   0.0957
  -1.750  -0.0681   0.00797   0.00177  -0.0297   0.7487   0.1048
  -1.500  -0.0390   0.00785   0.00171  -0.0299   0.7449   0.1177
  -1.250  -0.0098   0.00772   0.00165  -0.0302   0.7394   0.1351
  -1.000   0.0189   0.00759   0.00158  -0.0303   0.7293   0.1613
  -0.750   0.0477   0.00739   0.00151  -0.0305   0.7175   0.2014
  -0.500   0.0762   0.00715   0.00143  -0.0308   0.7034   0.2619
  -0.250   0.1034   0.00640   0.00127  -0.0311   0.6835   0.4546
   0.000   0.1315   0.00605   0.00122  -0.0313   0.6657   0.5634
   0.250   0.1600   0.00589   0.00122  -0.0315   0.6471   0.6284
   0.500   0.1888   0.00588   0.00125  -0.0316   0.6279   0.6609
   0.750   0.2173   0.00595   0.00128  -0.0317   0.5970   0.6851
   1.000   0.2447   0.00624   0.00136  -0.0316   0.5259   0.7065
   1.250   0.2683   0.00725   0.00166  -0.0313   0.3343   0.7235
   1.500   0.2938   0.00788   0.00190  -0.0312   0.2177   0.7404
   1.750   0.3211   0.00816   0.00206  -0.0311   0.1733   0.7620
   2.000   0.3488   0.00838   0.00219  -0.0311   0.1440   0.7741
   2.250   0.3771   0.00856   0.00229  -0.0312   0.1263   0.7805
   2.500   0.4054   0.00873   0.00240  -0.0313   0.1118   0.7857
   2.750   0.4334   0.00889   0.00252  -0.0313   0.0994   0.7916
   3.000   0.4615   0.00906   0.00264  -0.0313   0.0899   0.7984
   3.250   0.4898   0.00921   0.00276  -0.0314   0.0828   0.8043
   3.500   0.5177   0.00937   0.00290  -0.0313   0.0763   0.8099
   3.750   0.5456   0.00953   0.00304  -0.0313   0.0710   0.8155
   4.000   0.5737   0.00970   0.00318  -0.0314   0.0672   0.8208
   4.250   0.6013   0.00986   0.00334  -0.0313   0.0634   0.8265
   4.500   0.6289   0.01003   0.00350  -0.0313   0.0599   0.8328
   4.750   0.6567   0.01020   0.00367  -0.0312   0.0568   0.8387
   5.000   0.6839   0.01040   0.00385  -0.0311   0.0537   0.8443
   5.250   0.7113   0.01056   0.00404  -0.0310   0.0515   0.8505
   5.500   0.7385   0.01077   0.00423  -0.0309   0.0487   0.8567
   5.750   0.7652   0.01096   0.00444  -0.0307   0.0465   0.8633
   6.000   0.7920   0.01116   0.00465  -0.0305   0.0446   0.8713
   6.250   0.8184   0.01137   0.00487  -0.0303   0.0425   0.8794
   6.500   0.8445   0.01159   0.00510  -0.0299   0.0408   0.8885
   6.750   0.8707   0.01180   0.00534  -0.0296   0.0394   0.8964
   7.000   0.8963   0.01203   0.00559  -0.0292   0.0378   0.9052
   7.250   0.9214   0.01229   0.00585  -0.0287   0.0363   0.9140
   7.500   0.9464   0.01252   0.00611  -0.0282   0.0353   0.9247
   7.750   0.9703   0.01273   0.00638  -0.0274   0.0343   0.9381
   8.000   0.9938   0.01297   0.00665  -0.0266   0.0333   0.9560
   8.250   1.0203   0.01325   0.00693  -0.0264   0.0322   0.9814
   8.500   1.0472   0.01357   0.00726  -0.0265   0.0312   1.0000
   8.750   1.0729   0.01387   0.00758  -0.0262   0.0304   1.0000
   9.000   1.0982   0.01419   0.00791  -0.0259   0.0295   1.0000
   9.250   1.1231   0.01454   0.00826  -0.0256   0.0287   1.0000
   9.500   1.1476   0.01492   0.00864  -0.0252   0.0279   1.0000
   9.750   1.1716   0.01532   0.00905  -0.0247   0.0272   1.0000
  10.000   1.1959   0.01568   0.00944  -0.0243   0.0267   1.0000
  10.250   1.2198   0.01605   0.00983  -0.0238   0.0260   1.0000
  10.500   1.2432   0.01645   0.01024  -0.0233   0.0253   1.0000
  10.750   1.2661   0.01687   0.01067  -0.0227   0.0245   1.0000
  11.000   1.2883   0.01734   0.01115  -0.0220   0.0238   1.0000
  11.250   1.3102   0.01780   0.01165  -0.0212   0.0234   1.0000
  11.500   1.3320   0.01825   0.01213  -0.0205   0.0229   1.0000
  11.750   1.3531   0.01872   0.01264  -0.0196   0.0224   1.0000
  12.000   1.3734   0.01921   0.01316  -0.0187   0.0219   1.0000
  12.250   1.3927   0.01973   0.01371  -0.0176   0.0215   1.0000
  12.500   1.4097   0.02027   0.01428  -0.0161   0.0210   1.0000
  12.750   1.4258   0.02088   0.01492  -0.0145   0.0206   1.0000
  13.000   1.4411   0.02158   0.01566  -0.0130   0.0202   1.0000
  13.250   1.4572   0.02222   0.01635  -0.0116   0.0199   1.0000
  13.500   1.4728   0.02291   0.01710  -0.0103   0.0196   1.0000
  13.750   1.4880   0.02365   0.01790  -0.0090   0.0193   1.0000
  14.000   1.5027   0.02443   0.01874  -0.0077   0.0190   1.0000
  14.250   1.5168   0.02527   0.01963  -0.0064   0.0186   1.0000
  14.500   1.5303   0.02618   0.02058  -0.0052   0.0183   1.0000
  14.750   1.5430   0.02716   0.02161  -0.0039   0.0180   1.0000
  15.000   1.5546   0.02824   0.02275  -0.0027   0.0177   1.0000
  15.250   1.5648   0.02946   0.02402  -0.0014   0.0174   1.0000
  15.500   1.5736   0.03080   0.02543  -0.0002   0.0172   1.0000
  15.750   1.5836   0.03207   0.02679   0.0009   0.0170   1.0000
  16.000   1.5926   0.03346   0.02825   0.0019   0.0169   1.0000
  16.250   1.6005   0.03496   0.02984   0.0029   0.0167   1.0000
  16.500   1.6075   0.03658   0.03154   0.0038   0.0165   1.0000
  16.750   1.6133   0.03835   0.03340   0.0047   0.0164   1.0000
  17.000   1.6179   0.04025   0.03539   0.0054   0.0162   1.0000
  17.250   1.6214   0.04233   0.03757   0.0060   0.0160   1.0000
  17.500   1.6237   0.04460   0.03993   0.0065   0.0159   1.0000
  17.750   1.6243   0.04709   0.04251   0.0068   0.0157   1.0000
  18.000   1.6234   0.04983   0.04534   0.0070   0.0156   1.0000
  18.250   1.6210   0.05288   0.04849   0.0068   0.0155   1.0000
  18.500   1.6166   0.05631   0.05203   0.0064   0.0154   1.0000
  18.750   1.6100   0.06017   0.05600   0.0056   0.0153   1.0000
  19.000   1.6009   0.06459   0.06055   0.0043   0.0152   1.0000
  19.250   1.5885   0.06972   0.06581   0.0025   0.0151   1.0000
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