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RUTAN WING AIRFOIL (amsoil2-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RUTAN WING AIRFOIL (amsoil2-il)
Reynolds number: 500,000
Max Cl/Cd: 61.69 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-amsoil2-il-500000-n5.txt
Download as CSV file: xf-amsoil2-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -1.1416   0.08487   0.08141  -0.0222   1.0000   0.0201
 -16.500  -1.1979   0.06878   0.06501  -0.0333   1.0000   0.0200
 -16.250  -1.2265   0.05971   0.05571  -0.0396   1.0000   0.0200
 -16.000  -1.2439   0.05347   0.04926  -0.0434   1.0000   0.0201
 -15.750  -1.2550   0.04872   0.04432  -0.0457   1.0000   0.0202
 -15.500  -1.2616   0.04491   0.04033  -0.0471   1.0000   0.0204
 -15.250  -1.2657   0.04172   0.03703  -0.0478   1.0000   0.0206
 -15.000  -1.2660   0.03913   0.03434  -0.0480   1.0000   0.0207
 -14.750  -1.2634   0.03697   0.03208  -0.0478   1.0000   0.0209
 -14.500  -1.2588   0.03511   0.03013  -0.0474   1.0000   0.0211
 -14.250  -1.2526   0.03348   0.02840  -0.0467   1.0000   0.0214
 -14.000  -1.2454   0.03201   0.02683  -0.0458   1.0000   0.0216
 -13.750  -1.2371   0.03069   0.02541  -0.0446   1.0000   0.0219
 -13.500  -1.2282   0.02949   0.02411  -0.0432   1.0000   0.0221
 -13.250  -1.2182   0.02842   0.02293  -0.0415   1.0000   0.0224
 -13.000  -1.2048   0.02739   0.02179  -0.0403   1.0000   0.0228
 -12.750  -1.1892   0.02641   0.02068  -0.0393   1.0000   0.0232
 -12.500  -1.1720   0.02548   0.01962  -0.0384   1.0000   0.0235
 -12.250  -1.1542   0.02457   0.01861  -0.0376   1.0000   0.0238
 -12.000  -1.1357   0.02371   0.01772  -0.0368   1.0000   0.0242
 -11.750  -1.1152   0.02302   0.01698  -0.0362   1.0000   0.0247
 -11.500  -1.0938   0.02239   0.01630  -0.0357   1.0000   0.0251
 -11.250  -1.0718   0.02176   0.01561  -0.0353   1.0000   0.0257
 -11.000  -1.0496   0.02113   0.01491  -0.0348   1.0000   0.0262
 -10.750  -1.0270   0.02049   0.01419  -0.0344   1.0000   0.0268
 -10.500  -1.0040   0.01989   0.01349  -0.0340   1.0000   0.0273
 -10.250  -0.9810   0.01923   0.01278  -0.0336   0.9973   0.0278
  -9.750  -0.9235   0.01809   0.01158  -0.0351   0.9727   0.0290
  -9.500  -0.8962   0.01762   0.01106  -0.0354   0.9626   0.0297
  -9.250  -0.8704   0.01719   0.01055  -0.0353   0.9532   0.0306
  -9.000  -0.8458   0.01678   0.01006  -0.0348   0.9436   0.0313
  -8.750  -0.8220   0.01630   0.00953  -0.0342   0.9348   0.0319
  -8.500  -0.7985   0.01586   0.00906  -0.0336   0.9267   0.0326
  -8.250  -0.7737   0.01548   0.00865  -0.0331   0.9192   0.0334
  -8.000  -0.7490   0.01514   0.00825  -0.0326   0.9119   0.0343
  -7.500  -0.6978   0.01449   0.00747  -0.0319   0.8988   0.0362
  -7.250  -0.6729   0.01408   0.00705  -0.0315   0.8927   0.0372
  -7.000  -0.6466   0.01375   0.00670  -0.0313   0.8869   0.0383
  -6.750  -0.6202   0.01346   0.00638  -0.0311   0.8811   0.0395
  -6.500  -0.5938   0.01319   0.00606  -0.0308   0.8758   0.0408
  -6.250  -0.5671   0.01287   0.00572  -0.0306   0.8706   0.0422
  -6.000  -0.5402   0.01258   0.00544  -0.0305   0.8649   0.0436
  -5.750  -0.5132   0.01234   0.00516  -0.0304   0.8596   0.0453
  -5.500  -0.4860   0.01211   0.00489  -0.0302   0.8550   0.0471
  -5.250  -0.4585   0.01184   0.00464  -0.0303   0.8501   0.0494
  -5.000  -0.4309   0.01162   0.00441  -0.0302   0.8451   0.0519
  -4.750  -0.4034   0.01141   0.00418  -0.0301   0.8404   0.0544
  -4.500  -0.3756   0.01120   0.00397  -0.0301   0.8358   0.0576
  -4.250  -0.3475   0.01101   0.00378  -0.0302   0.8306   0.0611
  -4.000  -0.3196   0.01080   0.00360  -0.0302   0.8255   0.0653
  -3.750  -0.2917   0.01065   0.00342  -0.0302   0.8207   0.0694
  -3.500  -0.2634   0.01046   0.00327  -0.0303   0.8159   0.0745
  -3.250  -0.2350   0.01030   0.00312  -0.0304   0.8110   0.0799
  -3.000  -0.2066   0.01014   0.00298  -0.0304   0.8064   0.0866
  -2.750  -0.1784   0.00999   0.00285  -0.0305   0.8021   0.0936
  -2.500  -0.1497   0.00984   0.00273  -0.0306   0.7975   0.1019
  -2.250  -0.1210   0.00968   0.00263  -0.0308   0.7928   0.1130
  -2.000  -0.0925   0.00952   0.00252  -0.0309   0.7885   0.1275
  -1.750  -0.0641   0.00934   0.00242  -0.0310   0.7844   0.1483
  -1.500  -0.0355   0.00911   0.00234  -0.0312   0.7799   0.1806
  -1.250  -0.0072   0.00879   0.00224  -0.0315   0.7750   0.2346
  -1.000   0.0198   0.00810   0.00206  -0.0317   0.7705   0.3776
  -0.750   0.0460   0.00734   0.00196  -0.0318   0.7663   0.5634
  -0.500   0.0739   0.00709   0.00198  -0.0318   0.7581   0.6387
  -0.250   0.1018   0.00700   0.00197  -0.0315   0.7471   0.6779
   0.000   0.1303   0.00695   0.00197  -0.0314   0.7345   0.7025
   0.250   0.1584   0.00694   0.00196  -0.0313   0.7179   0.7237
   0.500   0.1867   0.00694   0.00198  -0.0311   0.7017   0.7424
   0.750   0.2150   0.00696   0.00200  -0.0310   0.6866   0.7587
   1.000   0.2430   0.00699   0.00204  -0.0308   0.6685   0.7764
   1.250   0.2706   0.00706   0.00209  -0.0304   0.6459   0.7946
   1.500   0.2982   0.00722   0.00211  -0.0302   0.6081   0.8043
   1.750   0.3240   0.00757   0.00217  -0.0298   0.5302   0.8098
   2.000   0.3448   0.00878   0.00252  -0.0290   0.3273   0.8165
   2.250   0.3688   0.00958   0.00283  -0.0287   0.2115   0.8230
   2.500   0.3950   0.00993   0.00302  -0.0285   0.1688   0.8292
   2.750   0.4220   0.01022   0.00319  -0.0284   0.1425   0.8356
   3.000   0.4493   0.01045   0.00334  -0.0283   0.1248   0.8412
   3.250   0.4761   0.01066   0.00350  -0.0281   0.1111   0.8471
   3.500   0.5032   0.01088   0.00368  -0.0279   0.0996   0.8538
   3.750   0.5302   0.01109   0.00385  -0.0278   0.0908   0.8601
   4.000   0.5568   0.01129   0.00404  -0.0275   0.0842   0.8665
   4.250   0.5835   0.01152   0.00424  -0.0273   0.0780   0.8734
   4.500   0.6099   0.01172   0.00444  -0.0270   0.0732   0.8799
   4.750   0.6358   0.01196   0.00466  -0.0266   0.0690   0.8877
   5.000   0.6619   0.01216   0.00489  -0.0262   0.0656   0.8957
   5.250   0.6870   0.01240   0.00512  -0.0257   0.0621   0.9048
   5.500   0.7120   0.01263   0.00537  -0.0251   0.0592   0.9141
   5.750   0.7368   0.01286   0.00562  -0.0245   0.0565   0.9246
   6.000   0.7608   0.01312   0.00588  -0.0237   0.0540   0.9359
   6.250   0.7856   0.01336   0.00615  -0.0231   0.0519   0.9485
   6.500   0.8123   0.01362   0.00643  -0.0229   0.0495   0.9634
   7.000   0.8694   0.01427   0.00708  -0.0237   0.0457   1.0000
   7.250   0.8953   0.01460   0.00741  -0.0235   0.0440   1.0000
   7.500   0.9206   0.01497   0.00776  -0.0233   0.0424   1.0000
   7.750   0.9453   0.01539   0.00817  -0.0229   0.0410   1.0000
   8.000   0.9703   0.01575   0.00856  -0.0226   0.0397   1.0000
   8.250   0.9951   0.01613   0.00896  -0.0222   0.0383   1.0000
   8.500   1.0192   0.01655   0.00937  -0.0218   0.0371   1.0000
   8.750   1.0424   0.01706   0.00987  -0.0213   0.0361   1.0000
   9.000   1.0661   0.01748   0.01034  -0.0208   0.0352   1.0000
   9.250   1.0894   0.01793   0.01083  -0.0202   0.0342   1.0000
   9.500   1.1124   0.01839   0.01131  -0.0196   0.0332   1.0000
   9.750   1.1348   0.01888   0.01181  -0.0190   0.0323   1.0000
  10.000   1.1557   0.01948   0.01241  -0.0181   0.0314   1.0000
  10.250   1.1774   0.01999   0.01299  -0.0174   0.0307   1.0000
  10.500   1.1983   0.02054   0.01359  -0.0165   0.0300   1.0000
  10.750   1.2186   0.02111   0.01421  -0.0156   0.0293   1.0000
  11.000   1.2381   0.02169   0.01483  -0.0146   0.0286   1.0000
  11.250   1.2556   0.02231   0.01548  -0.0133   0.0281   1.0000
  11.500   1.2709   0.02304   0.01623  -0.0117   0.0275   1.0000
  11.750   1.2869   0.02375   0.01702  -0.0102   0.0270   1.0000
  12.000   1.3031   0.02447   0.01782  -0.0089   0.0264   1.0000
  12.250   1.3188   0.02523   0.01865  -0.0076   0.0258   1.0000
  12.500   1.3340   0.02604   0.01952  -0.0063   0.0253   1.0000
  12.750   1.3485   0.02690   0.02045  -0.0051   0.0248   1.0000
  13.000   1.3621   0.02783   0.02144  -0.0038   0.0244   1.0000
  13.250   1.3745   0.02888   0.02254  -0.0025   0.0240   1.0000
  13.500   1.3846   0.03013   0.02383  -0.0012   0.0236   1.0000
  13.750   1.3959   0.03132   0.02513   0.0000   0.0233   1.0000
  14.000   1.4065   0.03258   0.02651   0.0012   0.0230   1.0000
  14.250   1.4160   0.03396   0.02799   0.0023   0.0226   1.0000
  14.500   1.4247   0.03544   0.02957   0.0034   0.0223   1.0000
  14.750   1.4323   0.03702   0.03125   0.0044   0.0220   1.0000
  15.000   1.4391   0.03872   0.03305   0.0052   0.0217   1.0000
  15.250   1.4449   0.04055   0.03498   0.0060   0.0214   1.0000
  15.500   1.4497   0.04251   0.03703   0.0067   0.0212   1.0000
  15.750   1.4533   0.04465   0.03927   0.0072   0.0209   1.0000
  16.000   1.4551   0.04705   0.04176   0.0075   0.0207   1.0000
  16.250   1.4544   0.04977   0.04457   0.0077   0.0205   1.0000
  16.500   1.4511   0.05290   0.04780   0.0076   0.0203   1.0000
  16.750   1.4467   0.05631   0.05134   0.0072   0.0201   1.0000
  17.000   1.4416   0.05998   0.05516   0.0066   0.0200   1.0000
  17.250   1.4341   0.06420   0.05955   0.0054   0.0198   1.0000
  17.500   1.4242   0.06902   0.06453   0.0037   0.0197   1.0000
  17.750   1.4110   0.07461   0.07029   0.0014   0.0196   1.0000
  18.000   1.3939   0.08120   0.07705  -0.0018   0.0195   1.0000
  18.250   1.3717   0.08914   0.08519  -0.0061   0.0194   1.0000
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