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US1000ROOT (us1000root-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: US1000ROOT (us1000root-il)
Reynolds number: 500,000
Max Cl/Cd: 49.84 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-us1000root-il-500000.txt
Download as CSV file: xf-us1000root-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.8743   0.08785   0.08300  -0.0210   1.0000   0.0054
 -15.250  -0.8768   0.08449   0.07958  -0.0216   1.0000   0.0054
 -15.000  -0.8798   0.08082   0.07586  -0.0225   1.0000   0.0055
 -14.750  -0.8877   0.07659   0.07156  -0.0236   1.0000   0.0055
 -14.500  -0.8886   0.07313   0.06803  -0.0247   1.0000   0.0055
 -14.250  -0.8954   0.06900   0.06383  -0.0258   1.0000   0.0056
 -14.000  -0.9027   0.06489   0.05965  -0.0270   1.0000   0.0055
 -13.750  -0.9083   0.06100   0.05568  -0.0280   1.0000   0.0054
 -13.500  -0.9152   0.05703   0.05161  -0.0291   1.0000   0.0055
 -13.250  -0.9263   0.05261   0.04708  -0.0302   1.0000   0.0055
 -13.000  -0.9373   0.04830   0.04266  -0.0311   1.0000   0.0056
 -12.750  -0.9351   0.04565   0.03995  -0.0317   1.0000   0.0055
 -12.500  -0.9495   0.04117   0.03533  -0.0324   1.0000   0.0056
 -12.250  -0.9530   0.03812   0.03218  -0.0327   1.0000   0.0055
 -12.000  -0.9570   0.03516   0.02912  -0.0326   1.0000   0.0056
 -11.750  -0.9631   0.03225   0.02610  -0.0321   1.0000   0.0057
 -11.500  -0.9619   0.03018   0.02394  -0.0313   1.0000   0.0057
 -11.250  -0.9635   0.02808   0.02174  -0.0301   1.0000   0.0058
 -10.750  -0.9629   0.02468   0.01817  -0.0266   1.0000   0.0059
 -10.500  -0.9690   0.02285   0.01621  -0.0236   1.0000   0.0063
 -10.250  -0.9644   0.02182   0.01512  -0.0212   1.0000   0.0064
 -10.000  -0.9596   0.02092   0.01415  -0.0184   1.0000   0.0066
  -9.750  -0.9539   0.02019   0.01337  -0.0155   1.0000   0.0068
  -9.500  -0.9507   0.01948   0.01260  -0.0118   1.0000   0.0077
  -9.250  -0.9463   0.01897   0.01203  -0.0081   1.0000   0.0081
  -9.000  -0.9480   0.01849   0.01152  -0.0032   0.9998   0.0095
  -8.750  -0.9213   0.01701   0.01013  -0.0047   0.9898   0.0341
  -8.500  -0.9288   0.01385   0.00779  -0.0009   0.9520   0.1603
  -8.250  -0.8914   0.01302   0.00717  -0.0037   0.9441   0.1991
  -8.000  -0.8469   0.01251   0.00675  -0.0078   0.9370   0.2257
  -7.750  -0.7960   0.01212   0.00639  -0.0130   0.9304   0.2423
  -7.500  -0.7416   0.01180   0.00610  -0.0191   0.9235   0.2603
  -7.250  -0.6853   0.01155   0.00579  -0.0255   0.9153   0.2705
  -7.000  -0.6367   0.01143   0.00560  -0.0302   0.9042   0.2820
  -6.750  -0.5995   0.01123   0.00540  -0.0326   0.8920   0.2912
  -6.500  -0.5670   0.01115   0.00520  -0.0337   0.8797   0.2958
  -6.250  -0.5404   0.01098   0.00501  -0.0336   0.8687   0.3011
  -6.000  -0.5170   0.01090   0.00488  -0.0327   0.8573   0.3066
  -5.750  -0.4948   0.01085   0.00474  -0.0315   0.8455   0.3115
  -5.500  -0.4742   0.01067   0.00457  -0.0301   0.8344   0.3165
  -5.250  -0.4522   0.01057   0.00443  -0.0288   0.8232   0.3214
  -5.000  -0.4293   0.01050   0.00428  -0.0277   0.8121   0.3262
  -4.750  -0.4100   0.01033   0.00413  -0.0259   0.7992   0.3317
  -4.500  -0.3886   0.01024   0.00400  -0.0245   0.7865   0.3376
  -4.250  -0.3674   0.01012   0.00384  -0.0231   0.7730   0.3431
  -4.000  -0.3464   0.01001   0.00371  -0.0216   0.7590   0.3492
  -3.750  -0.3243   0.00994   0.00358  -0.0203   0.7434   0.3556
  -3.500  -0.3038   0.00983   0.00345  -0.0187   0.7275   0.3626
  -3.000  -0.2608   0.00969   0.00322  -0.0159   0.6938   0.3773
  -2.750  -0.2387   0.00967   0.00313  -0.0146   0.6751   0.3850
  -2.500  -0.2178   0.00960   0.00304  -0.0131   0.6565   0.3930
  -2.250  -0.1961   0.00959   0.00296  -0.0118   0.6378   0.4012
  -2.000  -0.1748   0.00956   0.00289  -0.0103   0.6198   0.4101
  -1.750  -0.1533   0.00953   0.00283  -0.0090   0.6012   0.4190
  -1.250  -0.1103   0.00952   0.00274  -0.0062   0.5652   0.4387
  -1.000  -0.0885   0.00952   0.00270  -0.0049   0.5493   0.4484
  -0.500  -0.0446   0.00952   0.00266  -0.0024   0.5197   0.4695
  -0.250  -0.0227   0.00951   0.00265  -0.0011   0.5063   0.4808
   0.000  -0.0008   0.00951   0.00264   0.0002   0.4929   0.4930
   0.250   0.0211   0.00951   0.00265   0.0015   0.4806   0.5063
   0.500   0.0431   0.00952   0.00266   0.0027   0.4696   0.5198
   0.750   0.0648   0.00953   0.00268   0.0040   0.4589   0.5340
   1.000   0.0870   0.00952   0.00270   0.0053   0.4484   0.5492
   1.250   0.1087   0.00952   0.00274   0.0066   0.4387   0.5651
   1.750   0.1518   0.00954   0.00284   0.0093   0.4192   0.6004
   2.000   0.1733   0.00956   0.00289   0.0107   0.4101   0.6190
   2.250   0.1945   0.00959   0.00296   0.0121   0.4014   0.6377
   2.500   0.2161   0.00960   0.00304   0.0135   0.3930   0.6563
   2.750   0.2369   0.00967   0.00314   0.0150   0.3851   0.6753
   3.000   0.2590   0.00969   0.00323   0.0163   0.3774   0.6939
   3.500   0.3017   0.00982   0.00346   0.0192   0.3625   0.7281
   3.750   0.3225   0.00994   0.00359   0.0207   0.3557   0.7435
   4.000   0.3445   0.01000   0.00372   0.0220   0.3491   0.7588
   4.250   0.3643   0.01009   0.00379   0.0237   0.3346   0.7730
   4.500   0.3849   0.01020   0.00392   0.0253   0.3281   0.7866
   4.750   0.4044   0.01030   0.00400   0.0271   0.3138   0.7994
   5.000   0.4238   0.01042   0.00410   0.0288   0.3008   0.8120
   5.250   0.4443   0.01053   0.00422   0.0304   0.2886   0.8234
   5.500   0.4648   0.01065   0.00436   0.0319   0.2799   0.8349
   5.750   0.4845   0.01080   0.00448   0.0335   0.2666   0.8463
   6.000   0.5061   0.01089   0.00460   0.0348   0.2586   0.8579
   6.500   0.5508   0.01127   0.00491   0.0366   0.2247   0.8824
   6.750   0.5801   0.01164   0.00519   0.0358   0.1930   0.8953
   7.000   0.6147   0.01250   0.00579   0.0332   0.1378   0.9084
   7.250   0.6488   0.01494   0.00765   0.0290   0.0079   0.9226
   7.500   0.7053   0.01550   0.00825   0.0224   0.0067   0.9307
   7.750   0.7570   0.01611   0.00894   0.0169   0.0063   0.9384
   8.000   0.8029   0.01678   0.00969   0.0125   0.0061   0.9464
   8.250   0.8431   0.01740   0.01038   0.0094   0.0061   0.9559
   8.500   0.8700   0.01811   0.01118   0.0088   0.0060   0.9816
   8.750   0.8988   0.01897   0.01211   0.0077   0.0060   0.9984
   9.000   0.9128   0.01961   0.01281   0.0093   0.0060   1.0000
   9.250   0.9149   0.02016   0.01340   0.0133   0.0060   1.0000
   9.500   0.9172   0.02091   0.01421   0.0169   0.0060   1.0000
   9.750   0.9196   0.02181   0.01519   0.0202   0.0060   1.0000
  10.000   0.9205   0.02296   0.01642   0.0231   0.0060   1.0000
  10.250   0.9214   0.02428   0.01782   0.0256   0.0060   1.0000
  10.500   0.9236   0.02569   0.01930   0.0276   0.0060   1.0000
  10.750   0.9250   0.02729   0.02098   0.0293   0.0060   1.0000
  11.000   0.9223   0.02939   0.02317   0.0308   0.0060   1.0000
  11.250   0.9198   0.03169   0.02557   0.0318   0.0060   1.0000
  11.500   0.9095   0.03494   0.02893   0.0325   0.0061   1.0000
  11.750   0.9065   0.03776   0.03184   0.0326   0.0061   1.0000
  12.000   0.9025   0.04084   0.03501   0.0324   0.0061   1.0000
  12.250   0.8970   0.04424   0.03849   0.0320   0.0061   1.0000
  12.500   0.8876   0.04815   0.04250   0.0313   0.0062   1.0000
  12.750   0.8825   0.05165   0.04608   0.0307   0.0062   1.0000
  13.000   0.8775   0.05518   0.04968   0.0300   0.0062   1.0000
  13.250   0.8789   0.05810   0.05266   0.0293   0.0063   1.0000
  13.500   0.8756   0.06154   0.05617   0.0286   0.0063   1.0000
  13.750   0.8732   0.06491   0.05960   0.0280   0.0063   1.0000
  14.000   0.8727   0.06806   0.06281   0.0272   0.0064   1.0000
  14.250   0.8739   0.07113   0.06593   0.0264   0.0064   1.0000
  14.500   0.8743   0.07415   0.06902   0.0259   0.0065   1.0000
  14.750   0.8772   0.07686   0.07181   0.0255   0.0067   1.0000
  15.000   0.8805   0.07936   0.07437   0.0254   0.0068   1.0000
  15.250   0.8911   0.08012   0.07518   0.0274   0.0074   1.0000
  15.500   0.8927   0.08344   0.07855   0.0259   0.0072   1.0000
  15.750   0.9092   0.08307   0.07822   0.0291   0.0079   1.0000
  16.000   0.9176   0.08478   0.07997   0.0298   0.0081   1.0000
  16.250   0.9456   0.08336   0.07848   0.0335   0.0089   1.0000
  16.500   0.7386   0.09565   0.09149   0.0316   0.0079   1.0000
  16.750   0.7389   0.09858   0.09448   0.0307   0.0078   1.0000
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