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NACA 0010 (naca0010-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 0010 (naca0010-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.13 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca0010-il-1000000-n5.txt
Download as CSV file: xf-naca0010-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NACA 0010                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -1.1723   0.11150   0.10900   0.0130   1.0000   0.0055
 -17.500  -1.2382   0.09501   0.09230   0.0043   1.0000   0.0053
 -17.250  -1.3086   0.07798   0.07503  -0.0052   1.0000   0.0052
 -17.000  -1.3517   0.06616   0.06299  -0.0123   1.0000   0.0052
 -16.750  -1.3792   0.05742   0.05407  -0.0178   1.0000   0.0051
 -16.500  -1.3970   0.05074   0.04721  -0.0219   1.0000   0.0051
 -16.250  -1.4084   0.04549   0.04181  -0.0249   1.0000   0.0052
 -16.000  -1.4153   0.04137   0.03754  -0.0268   1.0000   0.0052
 -15.750  -1.4191   0.03803   0.03406  -0.0278   1.0000   0.0053
 -15.500  -1.4204   0.03533   0.03123  -0.0280   1.0000   0.0053
 -15.250  -1.4204   0.03303   0.02881  -0.0275   1.0000   0.0054
 -15.000  -1.4216   0.03086   0.02651  -0.0263   1.0000   0.0055
 -14.750  -1.4194   0.02915   0.02468  -0.0246   1.0000   0.0057
 -14.500  -1.4148   0.02774   0.02318  -0.0227   1.0000   0.0058
 -14.250  -1.4082   0.02655   0.02190  -0.0206   1.0000   0.0060
 -14.000  -1.3990   0.02552   0.02079  -0.0186   1.0000   0.0062
 -13.750  -1.3856   0.02455   0.01973  -0.0171   1.0000   0.0064
 -13.500  -1.3705   0.02365   0.01875  -0.0158   1.0000   0.0066
 -13.250  -1.3540   0.02280   0.01781  -0.0147   1.0000   0.0068
 -13.000  -1.3364   0.02200   0.01693  -0.0136   1.0000   0.0070
 -12.750  -1.3177   0.02126   0.01609  -0.0126   1.0000   0.0072
 -12.500  -1.2983   0.02056   0.01531  -0.0117   1.0000   0.0074
 -12.250  -1.2794   0.01973   0.01441  -0.0107   1.0000   0.0078
 -12.000  -1.2593   0.01901   0.01363  -0.0099   1.0000   0.0082
 -11.750  -1.2383   0.01836   0.01293  -0.0091   1.0000   0.0087
 -11.500  -1.2167   0.01776   0.01228  -0.0084   1.0000   0.0091
 -11.250  -1.1944   0.01721   0.01166  -0.0077   1.0000   0.0096
 -11.000  -1.1717   0.01671   0.01109  -0.0071   1.0000   0.0100
 -10.750  -1.1494   0.01613   0.01048  -0.0064   1.0000   0.0109
 -10.500  -1.1264   0.01562   0.00995  -0.0059   1.0000   0.0118
 -10.250  -1.1029   0.01516   0.00945  -0.0053   1.0000   0.0127
 -10.000  -1.0791   0.01474   0.00898  -0.0048   1.0000   0.0135
  -9.750  -1.0553   0.01431   0.00855  -0.0042   1.0000   0.0149
  -9.500  -1.0310   0.01394   0.00817  -0.0037   1.0000   0.0163
  -9.250  -1.0065   0.01360   0.00780  -0.0033   1.0000   0.0174
  -9.000  -0.9822   0.01325   0.00744  -0.0027   1.0000   0.0187
  -8.750  -0.9576   0.01294   0.00714  -0.0023   1.0000   0.0202
  -8.500  -0.9329   0.01267   0.00685  -0.0018   1.0000   0.0215
  -8.250  -0.9082   0.01241   0.00655  -0.0012   1.0000   0.0224
  -8.000  -0.8835   0.01217   0.00629  -0.0007   1.0000   0.0231
  -7.750  -0.8596   0.01188   0.00596   0.0000   1.0000   0.0240
  -7.500  -0.8361   0.01154   0.00562   0.0008   1.0000   0.0253
  -7.250  -0.8124   0.01126   0.00533   0.0016   1.0000   0.0264
  -7.000  -0.7886   0.01101   0.00507   0.0024   1.0000   0.0275
  -6.750  -0.7648   0.01078   0.00483   0.0031   1.0000   0.0284
  -6.500  -0.7396   0.01057   0.00459   0.0036   0.9997   0.0293
  -6.250  -0.7073   0.01035   0.00435   0.0026   0.9978   0.0299
  -6.000  -0.6748   0.01008   0.00406   0.0014   0.9957   0.0310
  -5.750  -0.6420   0.00978   0.00376   0.0002   0.9938   0.0330
  -5.500  -0.6105   0.00953   0.00352  -0.0006   0.9906   0.0347
  -5.250  -0.5783   0.00930   0.00329  -0.0016   0.9873   0.0364
  -5.000  -0.5457   0.00910   0.00308  -0.0027   0.9839   0.0381
  -4.750  -0.5156   0.00888   0.00288  -0.0032   0.9780   0.0422
  -4.500  -0.4841   0.00865   0.00268  -0.0041   0.9726   0.0487
  -4.250  -0.4551   0.00836   0.00248  -0.0044   0.9642   0.0649
  -4.000  -0.4262   0.00812   0.00230  -0.0046   0.9549   0.0802
  -3.750  -0.3981   0.00791   0.00214  -0.0046   0.9436   0.0951
  -3.500  -0.3712   0.00771   0.00198  -0.0043   0.9299   0.1121
  -3.250  -0.3449   0.00751   0.00183  -0.0039   0.9137   0.1325
  -3.000  -0.3186   0.00733   0.00169  -0.0035   0.8951   0.1554
  -2.750  -0.2927   0.00716   0.00156  -0.0030   0.8739   0.1819
  -2.500  -0.2666   0.00698   0.00143  -0.0026   0.8514   0.2137
  -2.250  -0.2405   0.00682   0.00132  -0.0022   0.8268   0.2481
  -2.000  -0.2141   0.00668   0.00122  -0.0019   0.8015   0.2808
  -1.750  -0.1876   0.00657   0.00114  -0.0016   0.7755   0.3148
  -1.500  -0.1613   0.00641   0.00106  -0.0012   0.7486   0.3621
  -1.250  -0.1347   0.00629   0.00100  -0.0010   0.7206   0.4026
  -1.000  -0.1079   0.00621   0.00096  -0.0008   0.6922   0.4407
  -0.750  -0.0813   0.00612   0.00092  -0.0005   0.6628   0.4840
  -0.500  -0.0543   0.00609   0.00090  -0.0003   0.6330   0.5157
  -0.250  -0.0271   0.00608   0.00088  -0.0002   0.6032   0.5441
   0.000   0.0000   0.00608   0.00088   0.0000   0.5725   0.5728
   0.250   0.0271   0.00608   0.00088   0.0002   0.5437   0.6029
   0.500   0.0543   0.00609   0.00090   0.0003   0.5153   0.6331
   0.750   0.0813   0.00612   0.00092   0.0005   0.4835   0.6628
   1.000   0.1080   0.00621   0.00096   0.0008   0.4405   0.6917
   1.250   0.1348   0.00629   0.00100   0.0010   0.4026   0.7203
   1.500   0.1614   0.00640   0.00106   0.0012   0.3645   0.7484
   1.750   0.1876   0.00657   0.00114   0.0016   0.3145   0.7757
   2.000   0.2141   0.00668   0.00122   0.0019   0.2808   0.8017
   2.250   0.2405   0.00682   0.00132   0.0022   0.2475   0.8270
   2.500   0.2666   0.00698   0.00143   0.0026   0.2135   0.8513
   2.750   0.2926   0.00716   0.00156   0.0030   0.1816   0.8739
   3.000   0.3187   0.00733   0.00169   0.0035   0.1554   0.8950
   3.250   0.3449   0.00751   0.00183   0.0039   0.1328   0.9136
   3.500   0.3712   0.00771   0.00198   0.0043   0.1121   0.9299
   3.750   0.3981   0.00791   0.00214   0.0046   0.0951   0.9437
   4.000   0.4262   0.00812   0.00230   0.0046   0.0802   0.9549
   4.250   0.4551   0.00836   0.00248   0.0044   0.0650   0.9642
   4.500   0.4841   0.00865   0.00268   0.0041   0.0487   0.9726
   4.750   0.5157   0.00888   0.00288   0.0032   0.0422   0.9780
   5.000   0.5458   0.00910   0.00308   0.0027   0.0380   0.9839
   5.250   0.5783   0.00930   0.00329   0.0016   0.0363   0.9872
   5.500   0.6105   0.00953   0.00352   0.0006   0.0347   0.9906
   5.750   0.6420   0.00978   0.00376  -0.0002   0.0330   0.9938
   6.000   0.6748   0.01008   0.00406  -0.0014   0.0310   0.9957
   6.250   0.7073   0.01035   0.00435  -0.0025   0.0299   0.9978
   6.500   0.7396   0.01057   0.00459  -0.0036   0.0293   0.9997
   6.750   0.7648   0.01078   0.00483  -0.0032   0.0284   1.0000
   7.000   0.7886   0.01101   0.00507  -0.0024   0.0275   1.0000
   7.250   0.8124   0.01126   0.00533  -0.0016   0.0264   1.0000
   7.500   0.8361   0.01154   0.00562  -0.0008   0.0253   1.0000
   7.750   0.8596   0.01188   0.00596   0.0000   0.0239   1.0000
   8.000   0.8835   0.01217   0.00629   0.0007   0.0231   1.0000
   8.250   0.9082   0.01241   0.00655   0.0012   0.0224   1.0000
   8.500   0.9329   0.01267   0.00685   0.0018   0.0215   1.0000
   8.750   0.9576   0.01294   0.00714   0.0023   0.0202   1.0000
   9.000   0.9822   0.01325   0.00744   0.0027   0.0187   1.0000
   9.250   1.0065   0.01360   0.00780   0.0033   0.0174   1.0000
   9.500   1.0310   0.01394   0.00817   0.0037   0.0163   1.0000
   9.750   1.0553   0.01431   0.00855   0.0042   0.0149   1.0000
  10.000   1.0791   0.01473   0.00898   0.0048   0.0135   1.0000
  10.250   1.1029   0.01516   0.00945   0.0053   0.0127   1.0000
  10.500   1.1264   0.01562   0.00994   0.0058   0.0118   1.0000
  10.750   1.1494   0.01613   0.01048   0.0064   0.0109   1.0000
  11.000   1.1718   0.01671   0.01109   0.0071   0.0100   1.0000
  11.250   1.1945   0.01721   0.01166   0.0077   0.0096   1.0000
  11.500   1.2167   0.01776   0.01228   0.0084   0.0091   1.0000
  11.750   1.2384   0.01836   0.01293   0.0091   0.0087   1.0000
  12.000   1.2593   0.01901   0.01363   0.0099   0.0082   1.0000
  12.250   1.2794   0.01973   0.01441   0.0107   0.0078   1.0000
  12.500   1.2983   0.02056   0.01531   0.0117   0.0074   1.0000
  12.750   1.3178   0.02126   0.01609   0.0126   0.0072   1.0000
  13.000   1.3365   0.02200   0.01692   0.0136   0.0070   1.0000
  13.250   1.3541   0.02280   0.01781   0.0146   0.0068   1.0000
  13.500   1.3707   0.02365   0.01875   0.0158   0.0066   1.0000
  13.750   1.3859   0.02455   0.01973   0.0171   0.0064   1.0000
  14.000   1.3993   0.02553   0.02079   0.0185   0.0062   1.0000
  14.250   1.4086   0.02656   0.02190   0.0205   0.0060   1.0000
  14.500   1.4154   0.02774   0.02318   0.0226   0.0058   1.0000
  14.750   1.4202   0.02914   0.02467   0.0245   0.0057   1.0000
  15.000   1.4223   0.03086   0.02652   0.0261   0.0055   1.0000
  15.250   1.4214   0.03301   0.02879   0.0273   0.0054   1.0000
  15.500   1.4215   0.03530   0.03121   0.0278   0.0053   1.0000
  15.750   1.4206   0.03797   0.03401   0.0276   0.0053   1.0000
  16.000   1.4169   0.04131   0.03748   0.0267   0.0052   1.0000
  16.250   1.4099   0.04546   0.04177   0.0247   0.0052   1.0000
  16.500   1.3988   0.05066   0.04713   0.0218   0.0051   1.0000
  16.750   1.3814   0.05730   0.05395   0.0176   0.0051   1.0000
  17.000   1.3536   0.06611   0.06295   0.0120   0.0051   1.0000
  17.250   1.3111   0.07786   0.07491   0.0049   0.0052   1.0000
  17.500   1.2406   0.09492   0.09221  -0.0046   0.0053   1.0000
  17.750   1.1733   0.11168   0.10918  -0.0134   0.0055   1.0000
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