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US1000ROOT (us1000root-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: US1000ROOT (us1000root-il)
Reynolds number: 100,000
Max Cl/Cd: 38.65 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-us1000root-il-100000-n5.txt
Download as CSV file: xf-us1000root-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.7039   0.11227   0.10508  -0.0154   1.0000   0.0194
 -15.000  -0.7101   0.10749   0.10022  -0.0172   1.0000   0.0203
 -14.750  -0.7211   0.10198   0.09461  -0.0192   1.0000   0.0223
 -14.500  -0.7269   0.09740   0.08993  -0.0209   1.0000   0.0226
 -14.250  -0.7360   0.09237   0.08477  -0.0226   1.0000   0.0245
 -14.000  -0.7428   0.08780   0.08012  -0.0242   1.0000   0.0250
 -13.750  -0.7523   0.08291   0.07512  -0.0259   1.0000   0.0253
 -13.500  -0.7687   0.07717   0.06928  -0.0279   1.0000   0.0269
 -13.250  -0.7886   0.07110   0.06310  -0.0299   1.0000   0.0293
 -13.000  -0.8092   0.06515   0.05705  -0.0318   1.0000   0.0331
 -12.750  -0.8055   0.06251   0.05425  -0.0325   1.0000   0.0298
 -12.500  -0.8353   0.05575   0.04741  -0.0345   1.0000   0.0362
 -12.250  -0.8483   0.05133   0.04290  -0.0355   1.0000   0.0383
 -11.500  -0.9281   0.03647   0.02834  -0.0356   1.0000   0.1045
 -11.250  -0.9461   0.03340   0.02544  -0.0337   1.0000   0.1307
 -11.000  -0.9576   0.03121   0.02338  -0.0312   1.0000   0.1548
 -10.750  -0.9675   0.02952   0.02183  -0.0281   1.0000   0.1813
 -10.500  -0.9801   0.02829   0.02068  -0.0238   1.0000   0.2102
 -10.250  -0.9887   0.02764   0.02008  -0.0190   1.0000   0.2266
 -10.000  -0.9953   0.02717   0.01953  -0.0138   1.0000   0.2388
  -9.750  -0.9954   0.02684   0.01922  -0.0095   1.0000   0.2485
  -9.500  -0.9909   0.02643   0.01873  -0.0059   1.0000   0.2566
  -9.250  -0.9843   0.02605   0.01824  -0.0025   1.0000   0.2637
  -9.000  -0.9772   0.02569   0.01780   0.0007   1.0000   0.2702
  -8.750  -0.9708   0.02543   0.01751   0.0041   1.0000   0.2771
  -8.500  -0.9671   0.02510   0.01707   0.0080   1.0000   0.2833
  -8.250  -0.9616   0.02493   0.01692   0.0115   1.0000   0.2888
  -8.000  -0.9465   0.02457   0.01640   0.0131   0.9969   0.2954
  -7.750  -0.9111   0.02414   0.01592   0.0110   0.9875   0.3012
  -7.500  -0.8787   0.02368   0.01532   0.0095   0.9760   0.3077
  -7.250  -0.8458   0.02321   0.01474   0.0080   0.9646   0.3136
  -7.000  -0.8102   0.02279   0.01422   0.0061   0.9547   0.3197
  -6.750  -0.7747   0.02230   0.01357   0.0042   0.9453   0.3265
  -6.500  -0.7379   0.02189   0.01315   0.0022   0.9363   0.3321
  -6.250  -0.6970   0.02142   0.01252  -0.0007   0.9291   0.3392
  -6.000  -0.6585   0.02102   0.01208  -0.0030   0.9197   0.3449
  -5.750  -0.6159   0.02060   0.01157  -0.0062   0.9118   0.3520
  -5.500  -0.5762   0.02022   0.01112  -0.0087   0.9020   0.3582
  -5.250  -0.5388   0.01989   0.01073  -0.0108   0.8912   0.3651
  -5.000  -0.5018   0.01957   0.01032  -0.0128   0.8800   0.3721
  -4.750  -0.4656   0.01929   0.01000  -0.0145   0.8684   0.3788
  -4.500  -0.4325   0.01903   0.00966  -0.0156   0.8558   0.3860
  -4.250  -0.4036   0.01882   0.00943  -0.0159   0.8419   0.3930
  -4.000  -0.3769   0.01863   0.00917  -0.0157   0.8277   0.4009
  -3.750  -0.3508   0.01844   0.00898  -0.0153   0.8130   0.4081
  -3.500  -0.3257   0.01825   0.00874  -0.0147   0.7981   0.4160
  -3.250  -0.3010   0.01806   0.00853  -0.0139   0.7828   0.4238
  -3.000  -0.2773   0.01788   0.00833  -0.0130   0.7668   0.4321
  -2.750  -0.2544   0.01772   0.00814  -0.0119   0.7501   0.4413
  -2.500  -0.2309   0.01755   0.00797  -0.0109   0.7334   0.4501
  -2.250  -0.2075   0.01739   0.00777  -0.0099   0.7163   0.4598
  -2.000  -0.1838   0.01725   0.00761  -0.0089   0.6993   0.4695
  -1.750  -0.1600   0.01711   0.00745  -0.0079   0.6822   0.4796
  -1.500  -0.1365   0.01700   0.00730  -0.0069   0.6654   0.4908
  -1.250  -0.1140   0.01691   0.00716  -0.0057   0.6480   0.5027
  -1.000  -0.0912   0.01684   0.00709  -0.0046   0.6309   0.5143
  -0.750  -0.0685   0.01678   0.00702  -0.0034   0.6139   0.5265
  -0.500  -0.0459   0.01674   0.00697  -0.0022   0.5980   0.5395
  -0.250  -0.0233   0.01671   0.00694  -0.0010   0.5825   0.5533
   0.000  -0.0008   0.01670   0.00693   0.0002   0.5675   0.5674
   0.250   0.0217   0.01671   0.00694   0.0014   0.5532   0.5824
   0.500   0.0442   0.01674   0.00697   0.0026   0.5395   0.5980
   0.750   0.0669   0.01678   0.00702   0.0037   0.5267   0.6139
   1.000   0.0896   0.01683   0.00709   0.0049   0.5145   0.6307
   1.250   0.1124   0.01691   0.00717   0.0061   0.5029   0.6479
   1.500   0.1350   0.01700   0.00730   0.0072   0.4911   0.6652
   1.750   0.1585   0.01711   0.00746   0.0083   0.4798   0.6823
   2.000   0.1823   0.01724   0.00761   0.0092   0.4698   0.6992
   2.250   0.2059   0.01739   0.00778   0.0102   0.4599   0.7163
   2.500   0.2294   0.01754   0.00798   0.0113   0.4501   0.7333
   2.750   0.2528   0.01771   0.00815   0.0123   0.4414   0.7503
   3.000   0.2758   0.01788   0.00834   0.0133   0.4321   0.7668
   3.250   0.2994   0.01805   0.00854   0.0143   0.4238   0.7828
   3.500   0.3242   0.01824   0.00875   0.0150   0.4160   0.7981
   3.750   0.3493   0.01843   0.00898   0.0156   0.4082   0.8129
   4.000   0.3755   0.01862   0.00919   0.0160   0.4008   0.8277
   4.250   0.4024   0.01882   0.00946   0.0162   0.3929   0.8420
   4.500   0.4313   0.01902   0.00968   0.0159   0.3860   0.8559
   4.750   0.4646   0.01928   0.01002   0.0148   0.3789   0.8685
   5.000   0.5009   0.01956   0.01034   0.0130   0.3720   0.8801
   5.250   0.5382   0.01988   0.01076   0.0110   0.3649   0.8914
   5.500   0.5760   0.02021   0.01115   0.0088   0.3581   0.9022
   5.750   0.6156   0.02060   0.01161   0.0063   0.3519   0.9120
   6.000   0.6584   0.02101   0.01213   0.0031   0.3449   0.9197
   6.250   0.6969   0.02141   0.01257   0.0008   0.3391   0.9291
   6.500   0.7364   0.02178   0.01307  -0.0018   0.3295   0.9366
   6.750   0.7702   0.02208   0.01345  -0.0034   0.3180   0.9464
   7.000   0.8008   0.02232   0.01372  -0.0044   0.3032   0.9579
   7.250   0.8326   0.02264   0.01413  -0.0057   0.2910   0.9699
   7.500   0.8646   0.02304   0.01459  -0.0071   0.2832   0.9825
   7.750   0.8969   0.02343   0.01507  -0.0088   0.2697   0.9948
   8.000   0.9183   0.02376   0.01552  -0.0085   0.2604   1.0000
   8.250   0.9205   0.02400   0.01578  -0.0044   0.2554   1.0000
   8.500   0.9192   0.02426   0.01605   0.0002   0.2420   1.0000
   8.750   0.9147   0.02468   0.01637   0.0052   0.2182   1.0000
   9.000   0.9052   0.02538   0.01684   0.0107   0.1830   1.0000
   9.250   0.8963   0.02624   0.01749   0.0160   0.1549   1.0000
   9.500   0.8843   0.02751   0.01853   0.0211   0.1257   1.0000
   9.750   0.8611   0.02976   0.02042   0.0264   0.0773   1.0000
  10.000   0.8320   0.03293   0.02327   0.0307   0.0335   1.0000
  10.250   0.8177   0.03562   0.02595   0.0331   0.0240   1.0000
  10.500   0.8157   0.03768   0.02813   0.0344   0.0221   1.0000
  10.750   0.8123   0.04004   0.03060   0.0352   0.0206   1.0000
  11.000   0.8020   0.04331   0.03402   0.0357   0.0183   1.0000
  11.250   0.7938   0.04667   0.03749   0.0356   0.0168   1.0000
  11.500   0.7820   0.05071   0.04167   0.0350   0.0140   1.0000
  11.750   0.7747   0.05446   0.04556   0.0341   0.0139   1.0000
  12.000   0.7671   0.05843   0.04968   0.0331   0.0144   1.0000
  12.250   0.7583   0.06267   0.05405   0.0319   0.0140   1.0000
  12.500   0.7475   0.06729   0.05881   0.0305   0.0137   1.0000
  12.750   0.7310   0.07281   0.06442   0.0286   0.0123   1.0000
  13.000   0.7265   0.07680   0.06853   0.0274   0.0125   1.0000
  13.250   0.7173   0.08156   0.07343   0.0258   0.0125   1.0000
  13.500   0.7064   0.08669   0.07864   0.0240   0.0120   1.0000
  13.750   0.6990   0.09141   0.08349   0.0224   0.0117   1.0000
  14.000   0.6932   0.09594   0.08812   0.0208   0.0117   1.0000
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