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BOEING 106 AIRFOIL (boe106-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: BOEING 106 AIRFOIL (boe106-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.22 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-boe106-il-1000000-n5.txt
Download as CSV file: xf-boe106-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: BOEING 106 AIRFOIL                              
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -1.1668   0.04490   0.04179  -0.0766   1.0000   0.0091
 -16.500  -1.1863   0.03850   0.03518  -0.0819   1.0000   0.0091
 -16.250  -1.1946   0.03475   0.03128  -0.0838   1.0000   0.0092
 -16.000  -1.1976   0.03215   0.02855  -0.0841   1.0000   0.0093
 -15.750  -1.1971   0.03021   0.02648  -0.0834   1.0000   0.0094
 -15.500  -1.1946   0.02861   0.02477  -0.0820   1.0000   0.0095
 -15.250  -1.1921   0.02717   0.02323  -0.0800   1.0000   0.0098
 -15.000  -1.1863   0.02597   0.02194  -0.0779   1.0000   0.0100
 -14.750  -1.1759   0.02489   0.02079  -0.0763   1.0000   0.0103
 -14.500  -1.1641   0.02394   0.01977  -0.0746   1.0000   0.0106
 -14.250  -1.1526   0.02311   0.01886  -0.0726   1.0000   0.0110
 -14.000  -1.1337   0.02225   0.01792  -0.0720   0.9978   0.0113
 -13.750  -1.1076   0.02137   0.01695  -0.0727   0.9942   0.0117
 -13.500  -1.0823   0.02059   0.01607  -0.0731   0.9892   0.0120
 -13.250  -1.0558   0.01975   0.01517  -0.0738   0.9846   0.0125
 -13.000  -1.0301   0.01905   0.01442  -0.0741   0.9787   0.0131
 -12.750  -1.0029   0.01842   0.01372  -0.0746   0.9730   0.0137
 -12.500  -0.9779   0.01784   0.01308  -0.0746   0.9654   0.0142
 -12.250  -0.9527   0.01730   0.01247  -0.0745   0.9582   0.0147
 -12.000  -0.9292   0.01680   0.01189  -0.0740   0.9493   0.0153
 -11.750  -0.9051   0.01637   0.01143  -0.0736   0.9411   0.0160
 -11.500  -0.8811   0.01600   0.01100  -0.0730   0.9322   0.0167
 -11.250  -0.8567   0.01563   0.01058  -0.0725   0.9242   0.0174
 -11.000  -0.8324   0.01527   0.01013  -0.0720   0.9154   0.0180
 -10.750  -0.8079   0.01490   0.00968  -0.0715   0.9073   0.0185
 -10.500  -0.7832   0.01454   0.00927  -0.0711   0.8988   0.0191
 -10.250  -0.7579   0.01425   0.00894  -0.0707   0.8910   0.0197
 -10.000  -0.7324   0.01398   0.00861  -0.0703   0.8823   0.0204
  -9.750  -0.7068   0.01373   0.00829  -0.0699   0.8727   0.0211
  -9.500  -0.6812   0.01348   0.00796  -0.0695   0.8618   0.0217
  -9.250  -0.6554   0.01324   0.00763  -0.0692   0.8509   0.0221
  -9.000  -0.6299   0.01290   0.00723  -0.0688   0.8423   0.0226
  -8.750  -0.6042   0.01260   0.00688  -0.0684   0.8340   0.0233
  -8.500  -0.5778   0.01237   0.00661  -0.0682   0.8265   0.0240
  -8.250  -0.5513   0.01216   0.00634  -0.0680   0.8187   0.0246
  -8.000  -0.5248   0.01193   0.00606  -0.0677   0.8115   0.0252
  -7.750  -0.4981   0.01172   0.00580  -0.0675   0.8039   0.0258
  -7.500  -0.4713   0.01152   0.00553  -0.0673   0.7969   0.0264
  -7.250  -0.4444   0.01132   0.00528  -0.0671   0.7895   0.0267
  -7.000  -0.4184   0.01101   0.00491  -0.0668   0.7826   0.0275
  -6.750  -0.3917   0.01074   0.00462  -0.0666   0.7753   0.0282
  -6.500  -0.3649   0.01055   0.00438  -0.0663   0.7681   0.0289
  -6.250  -0.3377   0.01036   0.00416  -0.0662   0.7616   0.0296
  -6.000  -0.3107   0.01018   0.00393  -0.0660   0.7542   0.0302
  -5.750  -0.2835   0.01000   0.00371  -0.0658   0.7473   0.0308
  -5.500  -0.2563   0.00983   0.00350  -0.0657   0.7399   0.0314
  -5.250  -0.2290   0.00969   0.00331  -0.0655   0.7332   0.0319
  -5.000  -0.2019   0.00951   0.00309  -0.0653   0.7256   0.0327
  -4.750  -0.1749   0.00934   0.00289  -0.0651   0.7181   0.0338
  -4.500  -0.1475   0.00919   0.00272  -0.0650   0.7103   0.0349
  -4.250  -0.1203   0.00907   0.00257  -0.0648   0.7022   0.0360
  -4.000  -0.0929   0.00896   0.00242  -0.0646   0.6928   0.0371
  -3.750  -0.0657   0.00888   0.00229  -0.0645   0.6810   0.0381
  -3.500  -0.0388   0.00879   0.00215  -0.0642   0.6672   0.0400
  -3.250  -0.0119   0.00871   0.00203  -0.0640   0.6540   0.0428
  -3.000   0.0155   0.00863   0.00193  -0.0638   0.6432   0.0455
  -2.750   0.0428   0.00855   0.00182  -0.0636   0.6328   0.0496
  -2.500   0.0699   0.00848   0.00173  -0.0635   0.6213   0.0546
  -2.250   0.0969   0.00840   0.00164  -0.0633   0.6097   0.0644
  -2.000   0.1236   0.00826   0.00157  -0.0631   0.5992   0.0891
  -1.750   0.1506   0.00820   0.00152  -0.0629   0.5884   0.1059
  -1.500   0.1776   0.00816   0.00148  -0.0627   0.5767   0.1190
  -1.250   0.2048   0.00811   0.00145  -0.0625   0.5656   0.1336
  -1.000   0.2318   0.00807   0.00142  -0.0624   0.5557   0.1511
  -0.750   0.2587   0.00799   0.00139  -0.0622   0.5463   0.1761
  -0.500   0.2850   0.00783   0.00136  -0.0620   0.5381   0.2279
  -0.250   0.3107   0.00764   0.00135  -0.0616   0.5291   0.2999
   0.000   0.3363   0.00741   0.00135  -0.0613   0.5207   0.3817
   0.250   0.3615   0.00722   0.00136  -0.0609   0.5118   0.4605
   0.500   0.3859   0.00691   0.00137  -0.0603   0.5042   0.5708
   0.750   0.4104   0.00673   0.00142  -0.0597   0.4966   0.6611
   1.000   0.4366   0.00666   0.00146  -0.0593   0.4897   0.7060
   1.250   0.4630   0.00664   0.00151  -0.0590   0.4819   0.7383
   1.500   0.4892   0.00660   0.00156  -0.0586   0.4750   0.7729
   1.750   0.5151   0.00659   0.00162  -0.0581   0.4667   0.8080
   2.000   0.5409   0.00657   0.00169  -0.0576   0.4587   0.8430
   2.250   0.5659   0.00657   0.00179  -0.0568   0.4488   0.8923
   2.500   0.5949   0.00665   0.00193  -0.0569   0.4354   0.9424
   2.750   0.6293   0.00683   0.00205  -0.0583   0.4197   0.9634
   3.000   0.6640   0.00700   0.00217  -0.0598   0.4063   0.9756
   3.250   0.6989   0.00718   0.00229  -0.0614   0.3937   0.9846
   3.500   0.7350   0.00736   0.00240  -0.0634   0.3808   0.9877
   3.750   0.7666   0.00755   0.00251  -0.0644   0.3669   0.9904
   4.000   0.7974   0.00772   0.00263  -0.0652   0.3556   0.9932
   4.250   0.8298   0.00787   0.00274  -0.0663   0.3456   0.9949
   4.500   0.8616   0.00808   0.00289  -0.0674   0.3312   0.9967
   4.750   0.8927   0.00831   0.00304  -0.0684   0.3157   0.9986
   5.000   0.9231   0.00853   0.00320  -0.0692   0.3027   1.0000
   5.250   0.9445   0.00874   0.00335  -0.0680   0.2910   1.0000
   5.500   0.9662   0.00894   0.00351  -0.0669   0.2785   1.0000
   5.750   0.9876   0.00916   0.00367  -0.0657   0.2653   1.0000
   6.000   1.0083   0.00942   0.00387  -0.0644   0.2495   1.0000
   6.250   1.0266   0.00982   0.00413  -0.0627   0.2221   1.0000
   6.500   1.0408   0.01045   0.00453  -0.0604   0.1807   1.0000
   6.750   1.0583   0.01092   0.00488  -0.0586   0.1592   1.0000
   7.000   1.0786   0.01126   0.00516  -0.0574   0.1474   1.0000
   7.250   1.1000   0.01155   0.00543  -0.0563   0.1385   1.0000
   7.500   1.1210   0.01188   0.00572  -0.0552   0.1296   1.0000
   7.750   1.1426   0.01219   0.00600  -0.0543   0.1216   1.0000
   8.000   1.1639   0.01252   0.00630  -0.0533   0.1135   1.0000
   8.250   1.1844   0.01290   0.00663  -0.0522   0.1047   1.0000
   8.500   1.2057   0.01322   0.00696  -0.0513   0.0980   1.0000
   8.750   1.2252   0.01365   0.00733  -0.0501   0.0890   1.0000
   9.000   1.2436   0.01411   0.00774  -0.0488   0.0795   1.0000
   9.250   1.2621   0.01450   0.00812  -0.0474   0.0734   1.0000
   9.500   1.2791   0.01497   0.00855  -0.0458   0.0676   1.0000
   9.750   1.2974   0.01536   0.00896  -0.0445   0.0641   1.0000
  10.000   1.3144   0.01585   0.00944  -0.0431   0.0603   1.0000
  10.250   1.3314   0.01635   0.00994  -0.0417   0.0566   1.0000
  10.500   1.3485   0.01685   0.01045  -0.0404   0.0536   1.0000
  10.750   1.3644   0.01743   0.01104  -0.0390   0.0508   1.0000
  11.000   1.3803   0.01803   0.01166  -0.0376   0.0482   1.0000
  11.250   1.3971   0.01858   0.01224  -0.0365   0.0467   1.0000
  11.500   1.4123   0.01926   0.01294  -0.0352   0.0439   1.0000
  11.750   1.4253   0.02008   0.01376  -0.0337   0.0408   1.0000
  12.000   1.4402   0.02082   0.01453  -0.0326   0.0385   1.0000
  12.250   1.4524   0.02174   0.01546  -0.0312   0.0351   1.0000
  12.500   1.4647   0.02270   0.01644  -0.0300   0.0322   1.0000
  12.750   1.4744   0.02387   0.01760  -0.0286   0.0279   1.0000
  13.000   1.4812   0.02529   0.01901  -0.0271   0.0222   1.0000
  13.250   1.4854   0.02698   0.02070  -0.0256   0.0170   1.0000
  13.500   1.4911   0.02861   0.02235  -0.0243   0.0144   1.0000
  13.750   1.4965   0.03031   0.02410  -0.0232   0.0127   1.0000
  14.000   1.5036   0.03193   0.02577  -0.0222   0.0118   1.0000
  14.250   1.5091   0.03372   0.02761  -0.0213   0.0109   1.0000
  14.500   1.5132   0.03568   0.02963  -0.0205   0.0102   1.0000
  14.750   1.5187   0.03758   0.03160  -0.0198   0.0098   1.0000
  15.000   1.5236   0.03956   0.03366  -0.0192   0.0094   1.0000
  15.250   1.5274   0.04172   0.03588  -0.0187   0.0090   1.0000
  15.500   1.5301   0.04405   0.03829  -0.0183   0.0087   1.0000
  15.750   1.5317   0.04657   0.04087  -0.0180   0.0084   1.0000
  16.000   1.5321   0.04928   0.04366  -0.0178   0.0081   1.0000
  16.250   1.5313   0.05221   0.04666  -0.0177   0.0078   1.0000
  16.500   1.5313   0.05511   0.04964  -0.0178   0.0076   1.0000
  16.750   1.5315   0.05806   0.05267  -0.0180   0.0075   1.0000
  17.000   1.5305   0.06118   0.05589  -0.0182   0.0073   1.0000
  17.250   1.5286   0.06447   0.05927  -0.0186   0.0071   1.0000
  17.500   1.5258   0.06794   0.06282  -0.0191   0.0070   1.0000
  17.750   1.5221   0.07159   0.06655  -0.0197   0.0068   1.0000
  18.000   1.5173   0.07539   0.07044  -0.0204   0.0066   1.0000
  18.250   1.5115   0.07938   0.07453  -0.0213   0.0065   1.0000
  18.500   1.5049   0.08357   0.07880  -0.0222   0.0063   1.0000
  18.750   1.4972   0.08796   0.08328  -0.0234   0.0062   1.0000
  19.000   1.4885   0.09255   0.08796  -0.0246   0.0061   1.0000
  19.250   1.4788   0.09733   0.09284  -0.0260   0.0060   1.0000
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