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US1000ROOT (us1000root-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: US1000ROOT (us1000root-il)
Reynolds number: 500,000
Max Cl/Cd: 43.15 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-us1000root-il-500000-n5.txt
Download as CSV file: xf-us1000root-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.8909   0.09029   0.08536  -0.0182   1.0000   0.0023
 -15.500  -0.8957   0.08611   0.08111  -0.0197   1.0000   0.0023
 -15.250  -0.9095   0.08073   0.07563  -0.0214   1.0000   0.0023
 -15.000  -0.9162   0.07640   0.07122  -0.0228   1.0000   0.0024
 -14.750  -0.9300   0.07115   0.06587  -0.0245   1.0000   0.0024
 -14.500  -0.9380   0.06682   0.06146  -0.0259   1.0000   0.0024
 -14.250  -0.9480   0.06229   0.05682  -0.0273   1.0000   0.0024
 -14.000  -0.9517   0.05864   0.05310  -0.0283   1.0000   0.0024
 -13.750  -0.9582   0.05471   0.04909  -0.0294   1.0000   0.0024
 -13.500  -0.9675   0.05053   0.04480  -0.0305   1.0000   0.0023
 -13.250  -0.9782   0.04629   0.04043  -0.0314   1.0000   0.0024
 -13.000  -0.9869   0.04243   0.03646  -0.0321   1.0000   0.0024
 -12.750  -0.9792   0.04054   0.03451  -0.0323   1.0000   0.0023
 -12.500  -0.9927   0.03650   0.03032  -0.0326   1.0000   0.0025
 -12.250  -0.9876   0.03454   0.02829  -0.0324   1.0000   0.0024
 -12.000  -0.9918   0.03184   0.02549  -0.0318   1.0000   0.0025
 -11.750  -0.9935   0.02957   0.02312  -0.0309   1.0000   0.0025
 -11.500  -0.9936   0.02762   0.02108  -0.0297   1.0000   0.0026
 -11.250  -0.9891   0.02615   0.01954  -0.0283   1.0000   0.0026
 -11.000  -0.9833   0.02489   0.01821  -0.0268   1.0000   0.0026
 -10.750  -0.9786   0.02365   0.01690  -0.0249   1.0000   0.0027
 -10.500  -0.9758   0.02242   0.01559  -0.0226   1.0000   0.0030
 -10.250  -0.9684   0.02156   0.01469  -0.0204   1.0000   0.0030
 -10.000  -0.9609   0.02082   0.01389  -0.0179   1.0000   0.0031
  -9.750  -0.9460   0.02011   0.01313  -0.0167   0.9992   0.0032
  -9.500  -0.9283   0.01918   0.01212  -0.0159   0.9510   0.0037
  -9.250  -0.8739   0.01825   0.01112  -0.0226   0.9330   0.0047
  -9.000  -0.8172   0.01706   0.00994  -0.0302   0.9187   0.0177
  -8.750  -0.7743   0.01477   0.00796  -0.0367   0.9023   0.0946
  -8.250  -0.7133   0.01290   0.00640  -0.0408   0.8725   0.1709
  -8.000  -0.6944   0.01237   0.00600  -0.0398   0.8595   0.2050
  -7.750  -0.6731   0.01210   0.00574  -0.0388   0.8487   0.2201
  -7.500  -0.6517   0.01190   0.00552  -0.0377   0.8385   0.2290
  -7.250  -0.6314   0.01172   0.00532  -0.0364   0.8282   0.2401
  -7.000  -0.6132   0.01155   0.00516  -0.0345   0.8178   0.2511
  -6.750  -0.5944   0.01140   0.00499  -0.0328   0.8076   0.2579
  -6.500  -0.5742   0.01129   0.00481  -0.0313   0.7960   0.2618
  -6.250  -0.5526   0.01118   0.00464  -0.0300   0.7846   0.2666
  -6.000  -0.5324   0.01104   0.00447  -0.0285   0.7725   0.2714
  -5.750  -0.5116   0.01092   0.00431  -0.0271   0.7586   0.2767
  -5.500  -0.4898   0.01084   0.00416  -0.0258   0.7440   0.2807
  -5.250  -0.4688   0.01074   0.00399  -0.0244   0.7278   0.2843
  -5.000  -0.4479   0.01065   0.00384  -0.0230   0.7115   0.2885
  -4.750  -0.4266   0.01059   0.00370  -0.0216   0.6926   0.2933
  -4.500  -0.4047   0.01053   0.00356  -0.0203   0.6744   0.2975
  -4.250  -0.3839   0.01047   0.00343  -0.0188   0.6550   0.3019
  -4.000  -0.3623   0.01043   0.00332  -0.0175   0.6367   0.3067
  -3.500  -0.3191   0.01035   0.00311  -0.0149   0.5982   0.3173
  -3.250  -0.2970   0.01033   0.00302  -0.0137   0.5807   0.3230
  -3.000  -0.2748   0.01031   0.00294  -0.0125   0.5639   0.3282
  -2.750  -0.2530   0.01029   0.00287  -0.0113   0.5471   0.3341
  -2.500  -0.2302   0.01029   0.00280  -0.0102   0.5315   0.3401
  -2.250  -0.2081   0.01026   0.00274  -0.0090   0.5166   0.3461
  -2.000  -0.1852   0.01025   0.00269  -0.0079   0.5032   0.3533
  -1.750  -0.1626   0.01023   0.00264  -0.0068   0.4901   0.3603
  -1.500  -0.1396   0.01022   0.00261  -0.0058   0.4772   0.3682
  -1.250  -0.1169   0.01020   0.00257  -0.0047   0.4655   0.3759
  -1.000  -0.0935   0.01021   0.00255  -0.0038   0.4554   0.3836
  -0.750  -0.0706   0.01019   0.00253  -0.0027   0.4455   0.3911
  -0.500  -0.0468   0.01020   0.00252  -0.0019   0.4360   0.3991
  -0.250  -0.0240   0.01019   0.00251  -0.0008   0.4270   0.4077
   0.000  -0.0008   0.01019   0.00251   0.0002   0.4166   0.4168
   0.250   0.0225   0.01019   0.00251   0.0012   0.4075   0.4270
   0.750   0.0691   0.01019   0.00253   0.0031   0.3913   0.4453
   1.000   0.0920   0.01021   0.00255   0.0041   0.3837   0.4553
   1.250   0.1154   0.01020   0.00258   0.0051   0.3759   0.4653
   1.500   0.1382   0.01023   0.00261   0.0061   0.3684   0.4764
   1.750   0.1613   0.01023   0.00265   0.0071   0.3605   0.4891
   2.000   0.1838   0.01026   0.00269   0.0083   0.3532   0.5022
   2.250   0.2065   0.01026   0.00274   0.0093   0.3465   0.5165
   2.500   0.2286   0.01029   0.00281   0.0106   0.3400   0.5313
   2.750   0.2512   0.01028   0.00287   0.0116   0.3342   0.5475
   3.000   0.2731   0.01031   0.00295   0.0129   0.3283   0.5642
   3.250   0.2952   0.01033   0.00303   0.0141   0.3230   0.5807
   3.500   0.3171   0.01035   0.00312   0.0154   0.3169   0.5998
   4.000   0.3605   0.01044   0.00333   0.0179   0.3049   0.6359
   4.250   0.3793   0.01056   0.00343   0.0197   0.2859   0.6546
   4.500   0.4001   0.01063   0.00356   0.0212   0.2808   0.6739
   4.750   0.4182   0.01082   0.00370   0.0231   0.2568   0.6918
   5.000   0.4361   0.01102   0.00386   0.0250   0.2370   0.7095
   5.250   0.4543   0.01122   0.00403   0.0269   0.2182   0.7267
   5.500   0.4724   0.01142   0.00423   0.0288   0.2016   0.7432
   5.750   0.4744   0.01232   0.00475   0.0333   0.1280   0.7580
   6.000   0.4899   0.01259   0.00501   0.0356   0.1148   0.7718
   6.250   0.4750   0.01403   0.00605   0.0431   0.0042   0.7852
   6.500   0.4929   0.01426   0.00633   0.0449   0.0038   0.7980
   6.750   0.5107   0.01451   0.00666   0.0467   0.0034   0.8103
   7.000   0.5300   0.01477   0.00698   0.0481   0.0033   0.8208
   7.250   0.5495   0.01506   0.00736   0.0495   0.0031   0.8324
   7.500   0.5700   0.01537   0.00774   0.0505   0.0030   0.8441
   7.750   0.5915   0.01572   0.00818   0.0512   0.0029   0.8556
   8.000   0.6179   0.01612   0.00868   0.0508   0.0029   0.8683
   8.250   0.6510   0.01649   0.00913   0.0489   0.0029   0.8813
   8.500   0.6926   0.01711   0.00991   0.0450   0.0028   0.8961
   8.750   0.7463   0.01787   0.01080   0.0384   0.0028   0.9094
   9.000   0.8029   0.01881   0.01186   0.0311   0.0028   0.9231
   9.250   0.8586   0.01990   0.01305   0.0238   0.0027   0.9380
   9.750   0.9102   0.02222   0.01553   0.0209   0.0027   1.0000
  10.000   0.9129   0.02332   0.01670   0.0235   0.0027   1.0000
  10.250   0.9162   0.02454   0.01798   0.0257   0.0027   1.0000
  10.500   0.9204   0.02583   0.01933   0.0274   0.0027   1.0000
  10.750   0.9231   0.02736   0.02093   0.0290   0.0027   1.0000
  11.000   0.9235   0.02921   0.02286   0.0304   0.0027   1.0000
  11.250   0.9241   0.03123   0.02495   0.0314   0.0027   1.0000
  11.500   0.9190   0.03395   0.02778   0.0320   0.0027   1.0000
  11.750   0.9194   0.03637   0.03027   0.0322   0.0027   1.0000
  12.000   0.9182   0.03910   0.03309   0.0321   0.0027   1.0000
  12.250   0.9151   0.04219   0.03627   0.0318   0.0027   1.0000
  12.500   0.9080   0.04587   0.04004   0.0312   0.0027   1.0000
  12.750   0.8972   0.05008   0.04437   0.0303   0.0027   1.0000
  13.000   0.8959   0.05328   0.04763   0.0295   0.0027   1.0000
  13.250   0.8885   0.05724   0.05168   0.0285   0.0027   1.0000
  13.500   0.8807   0.06134   0.05587   0.0274   0.0027   1.0000
  13.750   0.8741   0.06536   0.05997   0.0264   0.0027   1.0000
  14.000   0.8687   0.06926   0.06393   0.0253   0.0027   1.0000
  14.250   0.8672   0.07275   0.06748   0.0242   0.0027   1.0000
  14.500   0.8624   0.07667   0.07148   0.0231   0.0027   1.0000
  14.750   0.8588   0.08043   0.07529   0.0220   0.0027   1.0000
  15.000   0.8572   0.08401   0.07893   0.0210   0.0027   1.0000
  15.250   0.8555   0.08753   0.08250   0.0200   0.0027   1.0000
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