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NACA 0010-66 (naca001066-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: NACA 0010-66 (naca001066-il)
Reynolds number: 1,000,000
Max Cl/Cd: 53.61 at α=9.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-naca001066-il-1000000.txt
Download as CSV file: xf-naca001066-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0010-66                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -1.0137   0.09712   0.09509  -0.0381   1.0000   0.0096
 -16.500  -1.1347   0.06734   0.06502  -0.0552   1.0000   0.0090
 -16.250  -1.1877   0.05424   0.05164  -0.0633   1.0000   0.0089
 -16.000  -1.2176   0.04901   0.04623  -0.0626   1.0000   0.0088
 -15.750  -1.2398   0.04547   0.04254  -0.0599   1.0000   0.0089
 -15.500  -1.2587   0.04265   0.03957  -0.0562   1.0000   0.0089
 -15.250  -1.2740   0.04035   0.03713  -0.0520   1.0000   0.0090
 -15.000  -1.2860   0.03847   0.03511  -0.0476   1.0000   0.0091
 -14.750  -1.2850   0.03657   0.03305  -0.0455   0.9993   0.0092
 -14.500  -1.2799   0.03509   0.03143  -0.0435   0.9986   0.0093
 -14.250  -1.2722   0.03383   0.03003  -0.0415   0.9978   0.0094
 -14.000  -1.2865   0.03082   0.02672  -0.0367   0.9964   0.0097
 -13.750  -1.2818   0.02923   0.02499  -0.0340   0.9955   0.0100
 -13.500  -1.2694   0.02822   0.02388  -0.0324   0.9948   0.0103
 -13.250  -1.2542   0.02743   0.02301  -0.0310   0.9943   0.0106
 -13.000  -1.2468   0.02673   0.02222  -0.0277   0.9924   0.0109
 -12.750  -1.2357   0.02605   0.02145  -0.0251   0.9909   0.0112
 -12.500  -1.2228   0.02535   0.02065  -0.0228   0.9894   0.0115
 -12.250  -1.2081   0.02465   0.01984  -0.0209   0.9882   0.0118
 -12.000  -1.1895   0.02400   0.01907  -0.0197   0.9872   0.0121
 -11.750  -1.1679   0.02343   0.01839  -0.0191   0.9864   0.0124
 -11.500  -1.1532   0.02195   0.01675  -0.0174   0.9856   0.0131
 -11.250  -1.1296   0.02147   0.01623  -0.0172   0.9851   0.0137
 -11.000  -1.1043   0.02114   0.01587  -0.0172   0.9847   0.0142
 -10.750  -1.0784   0.02086   0.01553  -0.0174   0.9843   0.0149
 -10.500  -1.0735   0.02055   0.01517  -0.0127   0.9810   0.0153
 -10.250  -1.0546   0.02027   0.01481  -0.0111   0.9793   0.0157
 -10.000  -1.0361   0.01951   0.01395  -0.0096   0.9780   0.0164
  -9.750  -1.0143   0.01893   0.01334  -0.0088   0.9770   0.0172
  -9.500  -0.9888   0.01870   0.01310  -0.0088   0.9761   0.0180
  -9.250  -0.9632   0.01846   0.01281  -0.0087   0.9754   0.0187
  -9.000  -0.9374   0.01818   0.01248  -0.0086   0.9748   0.0196
  -8.750  -0.9102   0.01805   0.01231  -0.0088   0.9743   0.0202
  -8.500  -0.8868   0.01723   0.01141  -0.0083   0.9738   0.0214
  -8.250  -0.8604   0.01690   0.01106  -0.0085   0.9734   0.0224
  -8.000  -0.8331   0.01667   0.01083  -0.0087   0.9730   0.0233
  -7.750  -0.8056   0.01644   0.01056  -0.0090   0.9726   0.0243
  -7.500  -0.8046   0.01628   0.01036  -0.0031   0.9684   0.0248
  -7.250  -0.7835   0.01614   0.01019  -0.0018   0.9666   0.0256
  -7.000  -0.7597   0.01606   0.01008  -0.0011   0.9654   0.0260
  -6.750  -0.7396   0.01508   0.00901   0.0002   0.9645   0.0277
  -6.500  -0.7151   0.01474   0.00866   0.0007   0.9637   0.0288
  -6.250  -0.6893   0.01449   0.00841   0.0008   0.9631   0.0299
  -6.000  -0.6629   0.01426   0.00815   0.0009   0.9625   0.0311
  -5.750  -0.6361   0.01402   0.00788   0.0009   0.9620   0.0320
  -5.500  -0.6087   0.01383   0.00767   0.0008   0.9615   0.0327
  -5.250  -0.5817   0.01352   0.00731   0.0007   0.9611   0.0338
  -5.000  -0.5548   0.01313   0.00690   0.0007   0.9606   0.0356
  -4.750  -0.5265   0.01289   0.00666   0.0004   0.9602   0.0373
  -4.500  -0.4978   0.01273   0.00649   0.0000   0.9598   0.0391
  -4.250  -0.5043   0.01273   0.00646   0.0078   0.9545   0.0398
  -4.000  -0.4828   0.01260   0.00631   0.0090   0.9530   0.0412
  -3.750  -0.4591   0.01243   0.00613   0.0098   0.9518   0.0437
  -3.500  -0.4337   0.01222   0.00597   0.0102   0.9509   0.0498
  -3.250  -0.4077   0.01197   0.00582   0.0105   0.9501   0.0682
  -3.000  -0.3823   0.01170   0.00571   0.0107   0.9494   0.1024
  -2.750  -0.3563   0.01150   0.00564   0.0109   0.9489   0.1303
  -2.500  -0.3301   0.01130   0.00557   0.0111   0.9483   0.1640
  -2.250  -0.3047   0.01102   0.00551   0.0113   0.9478   0.2154
  -2.000  -0.2799   0.01074   0.00547   0.0117   0.9473   0.2787
  -1.750  -0.2561   0.01041   0.00543   0.0123   0.9468   0.3546
  -1.500  -0.2609   0.01023   0.00546   0.0196   0.9411   0.4166
  -1.250  -0.2499   0.00943   0.00525   0.0231   0.9381   0.5696
  -1.000  -0.2438   0.00806   0.00518   0.0286   0.9359   0.8951
  -0.750  -0.1998   0.00792   0.00505   0.0253   0.9347   0.9176
  -0.500  -0.1417   0.00791   0.00506   0.0189   0.9341   0.9273
  -0.250  -0.0722   0.00737   0.00449   0.0099   0.9334   0.9328
   0.000   0.0000   0.00721   0.00433   0.0000   0.9332   0.9332
   0.250   0.0728   0.00736   0.00448  -0.0101   0.9328   0.9333
   0.500   0.1420   0.00791   0.00506  -0.0189   0.9273   0.9342
   0.750   0.1997   0.00792   0.00505  -0.0253   0.9176   0.9347
   1.000   0.2445   0.00805   0.00517  -0.0288   0.8939   0.9359
   1.250   0.2501   0.00943   0.00525  -0.0232   0.5706   0.9381
   1.500   0.2609   0.01022   0.00546  -0.0196   0.4176   0.9412
   1.750   0.2561   0.01041   0.00543  -0.0123   0.3546   0.9468
   2.000   0.2799   0.01074   0.00546  -0.0117   0.2781   0.9473
   2.250   0.3047   0.01102   0.00551  -0.0113   0.2150   0.9478
   2.500   0.3302   0.01129   0.00556  -0.0111   0.1644   0.9483
   2.750   0.3563   0.01150   0.00564  -0.0109   0.1302   0.9489
   3.000   0.3823   0.01170   0.00571  -0.0108   0.1024   0.9494
   3.250   0.4076   0.01197   0.00581  -0.0104   0.0680   0.9501
   3.500   0.4336   0.01222   0.00597  -0.0102   0.0497   0.9509
   3.750   0.4590   0.01243   0.00613  -0.0098   0.0437   0.9519
   4.000   0.4828   0.01260   0.00631  -0.0090   0.0411   0.9530
   4.250   0.5042   0.01273   0.00645  -0.0077   0.0398   0.9545
   4.500   0.4979   0.01272   0.00649   0.0000   0.0391   0.9598
   4.750   0.5266   0.01289   0.00666  -0.0004   0.0373   0.9602
   5.000   0.5549   0.01313   0.00689  -0.0008   0.0356   0.9606
   5.250   0.5818   0.01352   0.00731  -0.0008   0.0338   0.9611
   5.500   0.6088   0.01383   0.00767  -0.0008   0.0327   0.9615
   5.750   0.6362   0.01401   0.00788  -0.0009   0.0320   0.9620
   6.000   0.6629   0.01426   0.00815  -0.0009   0.0311   0.9625
   6.250   0.6893   0.01449   0.00841  -0.0008   0.0299   0.9631
   6.500   0.7151   0.01473   0.00866  -0.0007   0.0288   0.9638
   6.750   0.7396   0.01507   0.00900  -0.0002   0.0277   0.9646
   7.000   0.7597   0.01605   0.01006   0.0011   0.0260   0.9654
   7.250   0.7836   0.01611   0.01015   0.0018   0.0255   0.9666
   7.500   0.8044   0.01626   0.01034   0.0031   0.0248   0.9684
   7.750   0.8056   0.01642   0.01055   0.0090   0.0243   0.9726
   8.000   0.8331   0.01666   0.01082   0.0087   0.0233   0.9730
   8.250   0.8604   0.01688   0.01105   0.0085   0.0224   0.9734
   8.500   0.8867   0.01723   0.01141   0.0083   0.0214   0.9739
   8.750   0.9103   0.01803   0.01229   0.0088   0.0202   0.9743
   9.000   0.9373   0.01818   0.01249   0.0086   0.0196   0.9748
   9.250   0.9632   0.01845   0.01281   0.0087   0.0187   0.9754
   9.500   0.9887   0.01870   0.01309   0.0088   0.0180   0.9761
   9.750   1.0143   0.01892   0.01333   0.0088   0.0172   0.9770
  10.000   1.0361   0.01950   0.01394   0.0096   0.0164   0.9780
  10.250   1.0546   0.02026   0.01480   0.0111   0.0157   0.9794
  10.500   1.0736   0.02052   0.01513   0.0126   0.0153   0.9810
  10.750   1.0787   0.02085   0.01552   0.0173   0.0148   0.9843
  11.000   1.1046   0.02113   0.01586   0.0172   0.0142   0.9847
  11.250   1.1300   0.02146   0.01622   0.0171   0.0136   0.9851
  11.500   1.1535   0.02195   0.01675   0.0173   0.0131   0.9856
  11.750   1.1684   0.02343   0.01839   0.0190   0.0123   0.9864
  12.000   1.1901   0.02400   0.01907   0.0196   0.0121   0.9872
  12.250   1.2086   0.02466   0.01985   0.0208   0.0118   0.9882
  12.500   1.2234   0.02535   0.02065   0.0227   0.0115   0.9895
  12.750   1.2365   0.02602   0.02142   0.0249   0.0112   0.9909
  13.000   1.2471   0.02675   0.02225   0.0276   0.0109   0.9925
  13.250   1.2548   0.02744   0.02303   0.0309   0.0106   0.9943
  13.500   1.2703   0.02821   0.02388   0.0322   0.0103   0.9948
  13.750   1.2829   0.02922   0.02498   0.0338   0.0100   0.9955
  14.000   1.2872   0.03085   0.02676   0.0365   0.0097   0.9965
  14.250   1.2731   0.03384   0.03004   0.0413   0.0094   0.9978
  14.500   1.2809   0.03509   0.03143   0.0432   0.0093   0.9986
  14.750   1.2858   0.03659   0.03308   0.0453   0.0092   0.9994
  15.000   1.2867   0.03843   0.03507   0.0475   0.0091   1.0000
  15.250   1.2746   0.04032   0.03710   0.0520   0.0090   1.0000
  15.500   1.2589   0.04265   0.03957   0.0562   0.0089   1.0000
  15.750   1.2408   0.04539   0.04246   0.0598   0.0089   1.0000
  16.000   1.2172   0.04905   0.04628   0.0626   0.0088   1.0000
  16.250   1.1882   0.05419   0.05159   0.0633   0.0089   1.0000
  16.500   1.1295   0.06881   0.06651   0.0539   0.0090   1.0000
  16.750   1.0135   0.09727   0.09525   0.0379   0.0096   1.0000
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