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US1000ROOT (us1000root-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: US1000ROOT (us1000root-il)
Reynolds number: 1,000,000
Max Cl/Cd: 45.95 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-us1000root-il-1000000-n5.txt
Download as CSV file: xf-us1000root-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: US1000ROOT                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.9822   0.08879   0.08461  -0.0164   1.0000   0.0011
 -16.250  -0.9855   0.08487   0.08064  -0.0177   1.0000   0.0012
 -16.000  -1.0046   0.07877   0.07442  -0.0198   1.0000   0.0011
 -15.750  -1.0030   0.07567   0.07128  -0.0208   1.0000   0.0012
 -15.500  -1.0049   0.07208   0.06764  -0.0219   1.0000   0.0012
 -15.250  -1.0312   0.06531   0.06072  -0.0241   1.0000   0.0012
 -15.000  -1.0448   0.06033   0.05563  -0.0256   1.0000   0.0012
 -14.750  -1.0626   0.05492   0.05010  -0.0272   1.0000   0.0012
 -14.500  -1.0624   0.05188   0.04700  -0.0280   1.0000   0.0012
 -14.250  -1.0647   0.04859   0.04364  -0.0288   1.0000   0.0012
 -14.000  -1.0790   0.04399   0.03891  -0.0298   1.0000   0.0012
 -13.750  -1.0800   0.04104   0.03588  -0.0302   1.0000   0.0012
 -13.500  -1.0795   0.03836   0.03314  -0.0306   1.0000   0.0012
 -13.250  -1.0841   0.03527   0.02994  -0.0307   1.0000   0.0012
 -13.000  -1.0892   0.03232   0.02689  -0.0304   1.0000   0.0012
 -12.750  -1.0739   0.03139   0.02597  -0.0303   1.0000   0.0012
 -12.500  -1.0760   0.02900   0.02347  -0.0295   1.0000   0.0013
 -12.250  -1.0663   0.02772   0.02216  -0.0289   1.0000   0.0013
 -12.000  -1.0678   0.02567   0.02002  -0.0275   1.0000   0.0013
 -11.750  -1.0642   0.02415   0.01842  -0.0260   1.0000   0.0013
 -11.500  -1.0577   0.02294   0.01715  -0.0245   1.0000   0.0013
 -11.250  -1.0526   0.02174   0.01589  -0.0226   1.0000   0.0014
 -10.750  -1.0357   0.01965   0.01370  -0.0189   0.9570   0.0014
 -10.500  -0.9807   0.01827   0.01222  -0.0267   0.9371   0.0017
 -10.250  -0.9112   0.01729   0.01114  -0.0367   0.9175   0.0017
 -10.000  -0.8571   0.01666   0.01035  -0.0434   0.8893   0.0018
  -9.750  -0.8226   0.01615   0.00973  -0.0460   0.8731   0.0019
  -9.500  -0.7913   0.01560   0.00910  -0.0478   0.8611   0.0022
  -9.250  -0.7643   0.01519   0.00862  -0.0485   0.8503   0.0023
  -9.000  -0.7398   0.01477   0.00814  -0.0486   0.8410   0.0028
  -8.750  -0.7179   0.01437   0.00769  -0.0481   0.8317   0.0036
  -8.500  -0.7040   0.01363   0.00700  -0.0463   0.8217   0.0211
  -8.000  -0.6632   0.01299   0.00629  -0.0442   0.8017   0.0310
  -7.750  -0.6680   0.01169   0.00527  -0.0390   0.7921   0.0981
  -7.500  -0.6623   0.01093   0.00469  -0.0351   0.7806   0.1351
  -7.250  -0.6568   0.01027   0.00423  -0.0311   0.7684   0.1767
  -7.000  -0.6365   0.01017   0.00408  -0.0296   0.7547   0.1795
  -6.750  -0.6214   0.00985   0.00384  -0.0273   0.7414   0.2024
  -6.500  -0.6024   0.00964   0.00365  -0.0256   0.7270   0.2181
  -6.000  -0.5610   0.00940   0.00336  -0.0228   0.6911   0.2380
  -5.750  -0.5404   0.00928   0.00322  -0.0213   0.6729   0.2478
  -5.500  -0.5180   0.00924   0.00310  -0.0202   0.6525   0.2517
  -5.250  -0.4957   0.00919   0.00298  -0.0190   0.6344   0.2557
  -5.000  -0.4738   0.00914   0.00287  -0.0178   0.6136   0.2606
  -4.750  -0.4510   0.00911   0.00278  -0.0168   0.5954   0.2659
  -4.500  -0.4284   0.00909   0.00269  -0.0157   0.5755   0.2693
  -4.250  -0.4057   0.00905   0.00259  -0.0146   0.5584   0.2734
  -4.000  -0.3826   0.00902   0.00252  -0.0136   0.5418   0.2775
  -3.750  -0.3589   0.00902   0.00245  -0.0127   0.5263   0.2817
  -3.500  -0.3361   0.00899   0.00237  -0.0117   0.5099   0.2858
  -3.250  -0.3127   0.00896   0.00231  -0.0107   0.4965   0.2904
  -3.000  -0.2888   0.00895   0.00225  -0.0098   0.4845   0.2948
  -2.750  -0.2654   0.00893   0.00219  -0.0089   0.4721   0.3002
  -2.500  -0.2420   0.00891   0.00215  -0.0080   0.4589   0.3057
  -2.250  -0.2176   0.00890   0.00210  -0.0072   0.4483   0.3107
  -2.000  -0.1938   0.00887   0.00206  -0.0063   0.4394   0.3163
  -1.750  -0.1698   0.00885   0.00203  -0.0055   0.4301   0.3221
  -1.500  -0.1454   0.00884   0.00200  -0.0047   0.4214   0.3275
  -1.250  -0.1216   0.00883   0.00197  -0.0039   0.4125   0.3340
  -1.000  -0.0972   0.00883   0.00195  -0.0031   0.4022   0.3403
  -0.750  -0.0735   0.00880   0.00193  -0.0022   0.3938   0.3485
  -0.500  -0.0492   0.00880   0.00192  -0.0014   0.3858   0.3560
  -0.250  -0.0250   0.00878   0.00191  -0.0006   0.3786   0.3637
   0.000  -0.0008   0.00880   0.00191   0.0002   0.3707   0.3706
   0.250   0.0235   0.00878   0.00191   0.0010   0.3638   0.3785
   0.500   0.0477   0.00881   0.00192   0.0018   0.3557   0.3855
   0.750   0.0719   0.00880   0.00193   0.0026   0.3486   0.3942
   1.250   0.1200   0.00882   0.00197   0.0042   0.3341   0.4128
   1.500   0.1438   0.00884   0.00200   0.0051   0.3276   0.4215
   1.750   0.1682   0.00885   0.00203   0.0058   0.3223   0.4299
   2.000   0.1923   0.00887   0.00206   0.0067   0.3164   0.4391
   2.250   0.2160   0.00890   0.00211   0.0076   0.3106   0.4484
   2.500   0.2403   0.00891   0.00215   0.0084   0.3058   0.4594
   2.750   0.2638   0.00893   0.00220   0.0093   0.2999   0.4708
   3.000   0.2872   0.00896   0.00226   0.0102   0.2946   0.4833
   3.250   0.3105   0.00899   0.00232   0.0112   0.2872   0.4961
   3.500   0.3276   0.00928   0.00244   0.0132   0.2476   0.5085
   3.750   0.3489   0.00936   0.00252   0.0146   0.2356   0.5265
   4.000   0.3712   0.00942   0.00261   0.0157   0.2271   0.5417
   4.250   0.3885   0.00970   0.00278   0.0177   0.1965   0.5562
   4.500   0.4023   0.01011   0.00303   0.0203   0.1549   0.5729
   4.750   0.3922   0.01159   0.00397   0.0273   0.0027   0.5843
   5.250   0.4336   0.01178   0.00430   0.0301   0.0023   0.6236
   5.500   0.4538   0.01188   0.00448   0.0316   0.0023   0.6452
   5.750   0.4737   0.01201   0.00470   0.0331   0.0021   0.6646
   6.000   0.4922   0.01212   0.00489   0.0349   0.0021   0.6836
   6.250   0.5100   0.01226   0.00511   0.0369   0.0021   0.7017
   6.500   0.5280   0.01244   0.00537   0.0388   0.0020   0.7216
   6.750   0.5465   0.01266   0.00567   0.0405   0.0019   0.7383
   7.000   0.5657   0.01289   0.00598   0.0420   0.0019   0.7534
   7.250   0.5847   0.01317   0.00632   0.0436   0.0019   0.7668
   7.500   0.6038   0.01346   0.00669   0.0450   0.0019   0.7801
   7.750   0.6234   0.01380   0.00709   0.0463   0.0019   0.7921
   8.000   0.6436   0.01416   0.00751   0.0473   0.0018   0.8027
   8.250   0.6653   0.01448   0.00786   0.0481   0.0019   0.8126
   8.500   0.6850   0.01501   0.00849   0.0489   0.0018   0.8232
   8.750   0.7060   0.01557   0.00912   0.0494   0.0018   0.8322
   9.000   0.7276   0.01614   0.00976   0.0496   0.0018   0.8422
   9.250   0.7544   0.01671   0.01040   0.0486   0.0018   0.8513
   9.500   0.7812   0.01732   0.01109   0.0475   0.0018   0.8624
   9.750   0.8032   0.01818   0.01206   0.0469   0.0018   0.8756
  10.000   0.8274   0.01918   0.01322   0.0454   0.0018   0.8961
  10.250   0.8851   0.02051   0.01476   0.0366   0.0018   0.9285
  10.500   0.9492   0.02225   0.01660   0.0262   0.0018   0.9476
  11.000   0.9661   0.02568   0.02017   0.0272   0.0018   1.0000
  11.250   0.9680   0.02743   0.02199   0.0285   0.0018   1.0000
  11.500   0.9653   0.02972   0.02437   0.0295   0.0018   1.0000
  11.750   0.9688   0.03168   0.02638   0.0301   0.0018   1.0000
  12.000   0.9674   0.03423   0.02901   0.0303   0.0018   1.0000
  12.250   0.9673   0.03684   0.03169   0.0303   0.0018   1.0000
  12.500   0.9639   0.03993   0.03486   0.0301   0.0018   1.0000
  12.750   0.9571   0.04353   0.03855   0.0295   0.0019   1.0000
  13.000   0.9544   0.04676   0.04185   0.0289   0.0018   1.0000
  13.250   0.9527   0.04994   0.04512   0.0282   0.0019   1.0000
  13.500   0.9461   0.05377   0.04903   0.0273   0.0019   1.0000
  13.750   0.9396   0.05763   0.05297   0.0264   0.0019   1.0000
  14.000   0.9333   0.06152   0.05692   0.0254   0.0019   1.0000
  14.250   0.9340   0.06469   0.06015   0.0245   0.0019   1.0000
  14.500   0.9271   0.06873   0.06425   0.0234   0.0019   1.0000
  14.750   0.9253   0.07226   0.06785   0.0224   0.0019   1.0000
  15.000   0.9206   0.07613   0.07178   0.0213   0.0019   1.0000
  15.250   0.9177   0.07980   0.07551   0.0203   0.0019   1.0000
  15.500   0.9175   0.08327   0.07902   0.0191   0.0019   1.0000
  15.750   0.9158   0.08679   0.08261   0.0181   0.0019   1.0000
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