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US1000ROOT (us1000root-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: US1000ROOT (us1000root-il)
Reynolds number: 200,000
Max Cl/Cd: 44.25 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-us1000root-il-200000-n5.txt
Download as CSV file: xf-us1000root-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.8075   0.09482   0.08862  -0.0198   1.0000   0.0058
 -15.000  -0.8184   0.08957   0.08329  -0.0217   1.0000   0.0059
 -14.750  -0.8337   0.08374   0.07737  -0.0239   1.0000   0.0063
 -14.500  -0.8378   0.07967   0.07316  -0.0253   1.0000   0.0060
 -14.250  -0.8517   0.07429   0.06767  -0.0272   1.0000   0.0062
 -14.000  -0.8579   0.07009   0.06337  -0.0287   1.0000   0.0062
 -13.750  -0.8629   0.06612   0.05929  -0.0299   1.0000   0.0060
 -13.500  -0.8705   0.06190   0.05494  -0.0313   1.0000   0.0059
 -13.250  -0.8858   0.05681   0.04973  -0.0328   1.0000   0.0063
 -13.000  -0.8951   0.05267   0.04546  -0.0340   1.0000   0.0067
 -12.750  -0.8919   0.05013   0.04281  -0.0345   1.0000   0.0060
 -12.500  -0.9046   0.04586   0.03842  -0.0353   1.0000   0.0070
 -12.250  -0.9054   0.04308   0.03551  -0.0356   1.0000   0.0066
 -12.000  -0.9090   0.04015   0.03247  -0.0357   1.0000   0.0072
 -11.750  -0.9118   0.03747   0.02966  -0.0354   1.0000   0.0078
 -11.500  -0.9120   0.03521   0.02729  -0.0348   1.0000   0.0085
 -11.250  -0.9129   0.03306   0.02507  -0.0339   1.0000   0.0093
 -11.000  -0.9107   0.03130   0.02323  -0.0328   1.0000   0.0100
 -10.750  -0.9087   0.02967   0.02152  -0.0313   1.0000   0.0121
 -10.500  -0.9161   0.02758   0.01944  -0.0289   1.0000   0.0209
 -10.250  -0.9158   0.02617   0.01797  -0.0265   1.0000   0.0271
 -10.000  -0.9204   0.02468   0.01647  -0.0232   1.0000   0.0357
  -9.750  -0.9406   0.02273   0.01477  -0.0176   1.0000   0.0748
  -9.500  -0.9636   0.02102   0.01342  -0.0106   1.0000   0.1233
  -9.250  -0.9702   0.02023   0.01275  -0.0052   1.0000   0.1445
  -9.000  -0.9788   0.01953   0.01226   0.0007   1.0000   0.1718
  -8.750  -0.9561   0.01875   0.01165   0.0004   0.9908   0.2073
  -8.500  -0.9322   0.01824   0.01115   0.0005   0.9667   0.2257
  -8.250  -0.9007   0.01779   0.01072  -0.0009   0.9513   0.2429
  -8.000  -0.8626   0.01740   0.01026  -0.0034   0.9406   0.2553
  -7.750  -0.8213   0.01706   0.00982  -0.0066   0.9310   0.2677
  -7.500  -0.7777   0.01665   0.00937  -0.0103   0.9220   0.2758
  -7.250  -0.7295   0.01630   0.00888  -0.0148   0.9140   0.2833
  -7.000  -0.6855   0.01594   0.00848  -0.0186   0.9038   0.2899
  -6.750  -0.6419   0.01566   0.00806  -0.0222   0.8932   0.2967
  -6.500  -0.6017   0.01534   0.00771  -0.0251   0.8825   0.3021
  -6.250  -0.5649   0.01511   0.00738  -0.0271   0.8709   0.3078
  -6.000  -0.5350   0.01492   0.00711  -0.0277   0.8585   0.3127
  -5.750  -0.5087   0.01473   0.00690  -0.0276   0.8462   0.3175
  -5.500  -0.4833   0.01459   0.00668  -0.0272   0.8339   0.3229
  -5.250  -0.4592   0.01444   0.00646  -0.0265   0.8215   0.3275
  -5.000  -0.4366   0.01428   0.00627  -0.0254   0.8090   0.3325
  -4.750  -0.4138   0.01415   0.00608  -0.0244   0.7959   0.3383
  -4.500  -0.3920   0.01400   0.00590  -0.0232   0.7820   0.3437
  -4.250  -0.3702   0.01387   0.00572  -0.0219   0.7678   0.3496
  -4.000  -0.3479   0.01375   0.00553  -0.0207   0.7524   0.3556
  -3.750  -0.3266   0.01361   0.00537  -0.0193   0.7361   0.3612
  -3.500  -0.3045   0.01351   0.00519  -0.0181   0.7192   0.3680
  -3.250  -0.2828   0.01339   0.00504  -0.0168   0.7018   0.3747
  -3.000  -0.2609   0.01331   0.00489  -0.0155   0.6839   0.3825
  -2.750  -0.2392   0.01323   0.00476  -0.0142   0.6662   0.3896
  -2.500  -0.2172   0.01317   0.00462  -0.0129   0.6477   0.3976
  -2.250  -0.1957   0.01311   0.00451  -0.0116   0.6294   0.4048
  -2.000  -0.1737   0.01308   0.00440  -0.0103   0.6115   0.4134
  -1.750  -0.1524   0.01303   0.00432  -0.0089   0.5945   0.4219
  -1.500  -0.1306   0.01300   0.00425  -0.0076   0.5782   0.4311
  -1.250  -0.1091   0.01298   0.00418  -0.0063   0.5623   0.4407
  -1.000  -0.0876   0.01296   0.00413  -0.0050   0.5471   0.4502
  -0.500  -0.0441   0.01294   0.00406  -0.0024   0.5187   0.4702
  -0.250  -0.0224   0.01293   0.00404  -0.0011   0.5056   0.4811
   0.000  -0.0008   0.01293   0.00404   0.0002   0.4932   0.4931
   0.250   0.0209   0.01293   0.00405   0.0015   0.4815   0.5056
   0.500   0.0426   0.01295   0.00406   0.0028   0.4704   0.5185
   1.000   0.0861   0.01296   0.00413   0.0053   0.4502   0.5467
   1.250   0.1075   0.01298   0.00418   0.0067   0.4407   0.5623
   1.500   0.1290   0.01300   0.00425   0.0080   0.4310   0.5782
   1.750   0.1507   0.01303   0.00432   0.0093   0.4219   0.5945
   2.000   0.1719   0.01308   0.00441   0.0107   0.4135   0.6117
   2.250   0.1940   0.01311   0.00452   0.0119   0.4049   0.6295
   2.500   0.2155   0.01317   0.00463   0.0133   0.3976   0.6478
   2.750   0.2375   0.01323   0.00476   0.0145   0.3897   0.6658
   3.000   0.2591   0.01331   0.00490   0.0159   0.3827   0.6838
   3.250   0.2810   0.01339   0.00505   0.0172   0.3748   0.7017
   3.500   0.3026   0.01351   0.00521   0.0185   0.3682   0.7193
   3.750   0.3247   0.01361   0.00538   0.0198   0.3614   0.7365
   4.000   0.3461   0.01375   0.00554   0.0211   0.3556   0.7523
   4.250   0.3683   0.01386   0.00573   0.0223   0.3497   0.7678
   4.500   0.3899   0.01400   0.00591   0.0236   0.3437   0.7821
   4.750   0.4119   0.01415   0.00610   0.0248   0.3385   0.7959
   5.000   0.4347   0.01427   0.00629   0.0259   0.3324   0.8088
   5.250   0.4572   0.01443   0.00648   0.0269   0.3275   0.8217
   5.500   0.4798   0.01454   0.00666   0.0279   0.3183   0.8342
   5.750   0.5023   0.01468   0.00681   0.0289   0.3070   0.8468
   6.000   0.5276   0.01484   0.00699   0.0292   0.2984   0.8593
   6.250   0.5561   0.01501   0.00720   0.0288   0.2860   0.8720
   6.500   0.5907   0.01523   0.00748   0.0271   0.2757   0.8844
   6.750   0.6305   0.01556   0.00780   0.0241   0.2563   0.8959
   7.000   0.6725   0.01599   0.00818   0.0205   0.2307   0.9066
   7.250   0.7164   0.01651   0.00865   0.0166   0.2080   0.9168
   7.500   0.7607   0.01719   0.00925   0.0124   0.1754   0.9261
   7.750   0.7806   0.01966   0.01101   0.0109   0.0649   0.9401
   8.000   0.7989   0.02164   0.01275   0.0104   0.0076   0.9611
   8.250   0.8232   0.02228   0.01345   0.0103   0.0075   0.9924
   8.500   0.8384   0.02307   0.01426   0.0115   0.0063   1.0000
   8.750   0.8400   0.02362   0.01484   0.0155   0.0060   1.0000
   9.000   0.8438   0.02426   0.01554   0.0188   0.0058   1.0000
   9.250   0.8493   0.02496   0.01630   0.0216   0.0058   1.0000
   9.500   0.8543   0.02582   0.01723   0.0242   0.0058   1.0000
   9.750   0.8590   0.02683   0.01831   0.0266   0.0056   1.0000
  10.000   0.8631   0.02800   0.01957   0.0286   0.0055   1.0000
  10.250   0.8670   0.02930   0.02100   0.0304   0.0053   1.0000
  10.500   0.8719   0.03066   0.02245   0.0319   0.0054   1.0000
  10.750   0.8758   0.03221   0.02408   0.0331   0.0053   1.0000
  11.000   0.8773   0.03409   0.02606   0.0341   0.0053   1.0000
  11.250   0.8783   0.03615   0.02824   0.0349   0.0052   1.0000
  11.500   0.8749   0.03880   0.03102   0.0353   0.0050   1.0000
  11.750   0.8745   0.04134   0.03367   0.0354   0.0051   1.0000
  12.000   0.8728   0.04415   0.03659   0.0352   0.0051   1.0000
  12.250   0.8696   0.04729   0.03985   0.0347   0.0051   1.0000
  12.500   0.8626   0.05100   0.04369   0.0339   0.0051   1.0000
  12.750   0.8520   0.05530   0.04813   0.0327   0.0049   1.0000
  13.000   0.8474   0.05895   0.05188   0.0317   0.0049   1.0000
  13.250   0.8392   0.06320   0.05625   0.0304   0.0050   1.0000
  13.500   0.8289   0.06785   0.06102   0.0289   0.0049   1.0000
  13.750   0.8188   0.07256   0.06584   0.0273   0.0049   1.0000
  14.000   0.8111   0.07703   0.07040   0.0258   0.0049   1.0000
  14.250   0.8066   0.08113   0.07459   0.0244   0.0050   1.0000
  14.500   0.7979   0.08587   0.07942   0.0227   0.0049   1.0000
  14.750   0.7915   0.09035   0.08399   0.0211   0.0049   1.0000
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