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NACA 0010-65 (naca001065-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NACA 0010-65 (naca001065-il)
Reynolds number: 500,000
Max Cl/Cd: 50.72 at α=10°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca001065-il-500000-n5.txt
Download as CSV file: xf-naca001065-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0010-65                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -1.0849   0.05823   0.05517  -0.0563   1.0000   0.0077
 -15.250  -1.1135   0.05116   0.04787  -0.0593   1.0000   0.0076
 -15.000  -1.1331   0.04647   0.04297  -0.0594   1.0000   0.0077
 -14.750  -1.1477   0.04290   0.03920  -0.0582   1.0000   0.0077
 -14.500  -1.1585   0.04001   0.03611  -0.0562   1.0000   0.0078
 -14.250  -1.1660   0.03762   0.03352  -0.0536   1.0000   0.0079
 -14.000  -1.1711   0.03558   0.03129  -0.0507   1.0000   0.0080
 -13.750  -1.1768   0.03370   0.02925  -0.0472   1.0000   0.0081
 -13.500  -1.1813   0.03208   0.02749  -0.0433   1.0000   0.0084
 -13.250  -1.1833   0.03078   0.02604  -0.0394   1.0000   0.0086
 -13.000  -1.1840   0.02969   0.02484  -0.0352   1.0000   0.0088
 -12.750  -1.1848   0.02877   0.02380  -0.0308   1.0000   0.0090
 -12.500  -1.1859   0.02798   0.02290  -0.0259   1.0000   0.0092
 -12.250  -1.1848   0.02718   0.02199  -0.0215   1.0000   0.0095
 -12.000  -1.1799   0.02634   0.02102  -0.0177   1.0000   0.0098
 -11.750  -1.1736   0.02552   0.02008  -0.0141   1.0000   0.0101
 -11.500  -1.1659   0.02474   0.01916  -0.0108   1.0000   0.0105
 -11.250  -1.1556   0.02397   0.01825  -0.0079   0.9999   0.0109
 -11.000  -1.1336   0.02300   0.01719  -0.0076   0.9987   0.0117
 -10.750  -1.1092   0.02237   0.01648  -0.0077   0.9975   0.0125
 -10.500  -1.0847   0.02177   0.01580  -0.0077   0.9963   0.0133
 -10.250  -1.0601   0.02110   0.01501  -0.0077   0.9953   0.0142
 -10.000  -1.0349   0.02042   0.01420  -0.0077   0.9944   0.0150
  -9.750  -1.0107   0.01994   0.01371  -0.0076   0.9929   0.0161
  -9.500  -0.9846   0.01966   0.01340  -0.0077   0.9913   0.0172
  -9.250  -0.9585   0.01931   0.01297  -0.0078   0.9899   0.0185
  -9.000  -0.9321   0.01892   0.01247  -0.0080   0.9886   0.0197
  -8.750  -0.9052   0.01845   0.01191  -0.0082   0.9874   0.0205
  -8.500  -0.8785   0.01789   0.01133  -0.0086   0.9864   0.0218
  -8.250  -0.8495   0.01762   0.01102  -0.0093   0.9855   0.0230
  -8.000  -0.8232   0.01728   0.01062  -0.0094   0.9841   0.0242
  -7.750  -0.7997   0.01691   0.01019  -0.0088   0.9819   0.0254
  -7.500  -0.7733   0.01658   0.00978  -0.0088   0.9801   0.0264
  -7.250  -0.7453   0.01630   0.00943  -0.0092   0.9787   0.0271
  -7.000  -0.7192   0.01562   0.00868  -0.0093   0.9774   0.0282
  -6.750  -0.6921   0.01505   0.00808  -0.0095   0.9763   0.0296
  -6.500  -0.6634   0.01463   0.00763  -0.0101   0.9755   0.0307
  -6.250  -0.6338   0.01426   0.00723  -0.0108   0.9747   0.0319
  -6.000  -0.6129   0.01394   0.00687  -0.0095   0.9714   0.0328
  -5.750  -0.5880   0.01359   0.00647  -0.0091   0.9692   0.0336
  -5.500  -0.5605   0.01325   0.00609  -0.0093   0.9675   0.0345
  -5.250  -0.5317   0.01295   0.00575  -0.0098   0.9661   0.0353
  -5.000  -0.5022   0.01266   0.00543  -0.0104   0.9651   0.0362
  -4.750  -0.4728   0.01228   0.00502  -0.0110   0.9641   0.0380
  -4.500  -0.4426   0.01198   0.00472  -0.0118   0.9633   0.0399
  -4.250  -0.4145   0.01173   0.00447  -0.0120   0.9618   0.0420
  -4.000  -0.3948   0.01156   0.00429  -0.0103   0.9575   0.0442
  -3.750  -0.3679   0.01134   0.00408  -0.0103   0.9553   0.0486
  -3.500  -0.3399   0.01108   0.00389  -0.0105   0.9535   0.0595
  -3.250  -0.3113   0.01081   0.00370  -0.0109   0.9521   0.0760
  -3.000  -0.2821   0.01056   0.00352  -0.0114   0.9508   0.0933
  -2.750  -0.2532   0.01027   0.00336  -0.0119   0.9496   0.1208
  -2.500  -0.2330   0.01004   0.00326  -0.0104   0.9455   0.1529
  -2.250  -0.2100   0.00976   0.00314  -0.0095   0.9421   0.1941
  -2.000  -0.1850   0.00940   0.00300  -0.0092   0.9397   0.2497
  -1.750  -0.1623   0.00879   0.00281  -0.0084   0.9374   0.3592
  -1.500  -0.1582   0.00731   0.00247  -0.0038   0.9338   0.6453
  -1.250  -0.1487   0.00683   0.00253   0.0005   0.9279   0.7730
  -1.000  -0.1215   0.00672   0.00262   0.0009   0.9256   0.8250
  -0.750  -0.0910   0.00672   0.00270   0.0005   0.9238   0.8545
  -0.500  -0.0596   0.00678   0.00283   0.0000   0.9222   0.8798
  -0.250  -0.0255   0.00683   0.00291  -0.0011   0.9200   0.8965
   0.000   0.0000   0.00687   0.00296   0.0000   0.9094   0.9094
   0.250   0.0255   0.00684   0.00291   0.0011   0.8967   0.9200
   0.500   0.0596   0.00678   0.00283   0.0000   0.8798   0.9222
   0.750   0.0910   0.00672   0.00270  -0.0005   0.8548   0.9238
   1.000   0.1215   0.00672   0.00262  -0.0009   0.8248   0.9256
   1.250   0.1488   0.00683   0.00253  -0.0005   0.7732   0.9279
   1.500   0.1581   0.00732   0.00247   0.0038   0.6450   0.9338
   1.750   0.1623   0.00879   0.00281   0.0084   0.3595   0.9374
   2.000   0.1850   0.00940   0.00300   0.0092   0.2497   0.9397
   2.250   0.2099   0.00976   0.00314   0.0095   0.1936   0.9421
   2.500   0.2329   0.01004   0.00326   0.0104   0.1530   0.9455
   2.750   0.2532   0.01027   0.00335   0.0119   0.1209   0.9496
   3.000   0.2821   0.01056   0.00352   0.0114   0.0934   0.9508
   3.250   0.3113   0.01081   0.00370   0.0109   0.0761   0.9521
   3.500   0.3399   0.01108   0.00389   0.0105   0.0595   0.9535
   3.750   0.3678   0.01133   0.00408   0.0103   0.0486   0.9553
   4.000   0.3948   0.01156   0.00429   0.0103   0.0442   0.9575
   4.250   0.4123   0.01171   0.00445   0.0125   0.0420   0.9625
   4.500   0.4426   0.01198   0.00471   0.0118   0.0399   0.9633
   4.750   0.4728   0.01228   0.00502   0.0110   0.0380   0.9641
   5.000   0.5022   0.01266   0.00543   0.0104   0.0362   0.9651
   5.250   0.5317   0.01295   0.00575   0.0098   0.0353   0.9662
   5.500   0.5605   0.01325   0.00609   0.0093   0.0345   0.9675
   5.750   0.5879   0.01359   0.00647   0.0092   0.0337   0.9692
   6.000   0.6128   0.01394   0.00687   0.0096   0.0328   0.9715
   6.250   0.6338   0.01425   0.00722   0.0108   0.0319   0.9747
   6.500   0.6634   0.01463   0.00763   0.0101   0.0307   0.9755
   6.750   0.6922   0.01505   0.00808   0.0095   0.0296   0.9764
   7.000   0.7192   0.01561   0.00868   0.0092   0.0282   0.9774
   7.250   0.7453   0.01630   0.00943   0.0092   0.0271   0.9787
   7.500   0.7733   0.01658   0.00978   0.0088   0.0264   0.9802
   7.750   0.7997   0.01691   0.01018   0.0088   0.0254   0.9819
   8.000   0.8232   0.01728   0.01062   0.0094   0.0243   0.9842
   8.250   0.8496   0.01761   0.01101   0.0093   0.0230   0.9856
   8.500   0.8786   0.01789   0.01132   0.0085   0.0218   0.9864
   8.750   0.9053   0.01845   0.01191   0.0082   0.0205   0.9875
   9.000   0.9322   0.01891   0.01247   0.0079   0.0197   0.9886
   9.250   0.9586   0.01932   0.01297   0.0078   0.0185   0.9899
   9.500   0.9847   0.01966   0.01340   0.0077   0.0172   0.9913
   9.750   1.0109   0.01994   0.01370   0.0075   0.0161   0.9929
  10.000   1.0351   0.02041   0.01420   0.0077   0.0150   0.9944
  10.250   1.0604   0.02109   0.01501   0.0076   0.0142   0.9953
  10.500   1.0850   0.02176   0.01579   0.0076   0.0133   0.9964
  10.750   1.1095   0.02237   0.01648   0.0076   0.0125   0.9975
  11.000   1.1338   0.02300   0.01719   0.0076   0.0117   0.9987
  11.250   1.1559   0.02396   0.01825   0.0078   0.0109   0.9999
  11.500   1.1659   0.02473   0.01916   0.0108   0.0105   1.0000
  11.750   1.1736   0.02552   0.02008   0.0142   0.0102   1.0000
  12.000   1.1799   0.02633   0.02102   0.0177   0.0098   1.0000
  12.250   1.1849   0.02717   0.02198   0.0215   0.0095   1.0000
  12.500   1.1863   0.02797   0.02289   0.0259   0.0092   1.0000
  12.750   1.1850   0.02877   0.02380   0.0307   0.0090   1.0000
  13.000   1.1844   0.02969   0.02483   0.0352   0.0088   1.0000
  13.250   1.1837   0.03078   0.02604   0.0393   0.0086   1.0000
  13.500   1.1818   0.03208   0.02749   0.0432   0.0083   1.0000
  13.750   1.1773   0.03371   0.02926   0.0471   0.0081   1.0000
  14.000   1.1719   0.03559   0.03130   0.0506   0.0080   1.0000
  14.250   1.1670   0.03762   0.03353   0.0535   0.0079   1.0000
  14.500   1.1594   0.04003   0.03613   0.0560   0.0078   1.0000
  14.750   1.1488   0.04292   0.03922   0.0580   0.0077   1.0000
  15.000   1.1344   0.04650   0.04300   0.0592   0.0077   1.0000
  15.250   1.1145   0.05123   0.04794   0.0590   0.0076   1.0000
  15.500   1.0862   0.05830   0.05524   0.0560   0.0077   1.0000
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