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NACA 0010-66 (naca001066-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NACA 0010-66 (naca001066-il)
Reynolds number: 1,000,000
Max Cl/Cd: 59.66 at α=10.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-naca001066-il-1000000-n5.txt
Download as CSV file: xf-naca001066-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.8461   0.13558   0.13359  -0.0264   0.9986   0.0063
 -17.250  -1.2316   0.05315   0.05024  -0.0731   0.9983   0.0047
 -17.000  -1.2536   0.04725   0.04414  -0.0751   0.9975   0.0047
 -16.750  -1.2668   0.04330   0.04002  -0.0749   0.9968   0.0047
 -16.500  -1.2755   0.04024   0.03680  -0.0737   0.9962   0.0048
 -16.250  -1.2797   0.03775   0.03416  -0.0722   0.9956   0.0049
 -16.000  -1.2806   0.03564   0.03191  -0.0704   0.9951   0.0050
 -15.750  -1.2786   0.03380   0.02993  -0.0686   0.9947   0.0050
 -15.500  -1.2765   0.03220   0.02820  -0.0662   0.9939   0.0051
 -15.250  -1.2732   0.03080   0.02666  -0.0636   0.9927   0.0052
 -15.000  -1.2671   0.02950   0.02522  -0.0613   0.9915   0.0053
 -14.750  -1.2590   0.02831   0.02391  -0.0592   0.9904   0.0055
 -14.500  -1.2490   0.02722   0.02269  -0.0572   0.9895   0.0056
 -14.250  -1.2369   0.02622   0.02158  -0.0555   0.9887   0.0057
 -14.000  -1.2231   0.02530   0.02054  -0.0540   0.9879   0.0058
 -13.750  -1.2103   0.02418   0.01930  -0.0523   0.9873   0.0061
 -13.500  -1.1948   0.02322   0.01825  -0.0510   0.9867   0.0064
 -13.250  -1.1770   0.02237   0.01732  -0.0500   0.9862   0.0067
 -13.000  -1.1576   0.02159   0.01644  -0.0493   0.9858   0.0070
 -12.750  -1.1369   0.02087   0.01563  -0.0487   0.9854   0.0073
 -12.500  -1.1306   0.02039   0.01506  -0.0447   0.9822   0.0075
 -12.250  -1.1131   0.01981   0.01439  -0.0432   0.9809   0.0078
 -12.000  -1.0936   0.01925   0.01375  -0.0421   0.9799   0.0080
 -11.750  -1.0735   0.01859   0.01301  -0.0412   0.9790   0.0086
 -11.500  -1.0517   0.01799   0.01236  -0.0406   0.9784   0.0092
 -11.250  -1.0288   0.01746   0.01176  -0.0401   0.9778   0.0098
 -11.000  -1.0047   0.01696   0.01120  -0.0399   0.9773   0.0105
 -10.750  -0.9797   0.01648   0.01066  -0.0399   0.9769   0.0112
 -10.500  -0.9541   0.01600   0.01017  -0.0400   0.9765   0.0126
 -10.250  -0.9281   0.01560   0.00974  -0.0401   0.9762   0.0139
 -10.000  -0.9023   0.01522   0.00932  -0.0402   0.9758   0.0149
  -9.750  -0.8760   0.01487   0.00897  -0.0403   0.9755   0.0164
  -9.500  -0.8711   0.01478   0.00886  -0.0354   0.9713   0.0174
  -9.250  -0.8491   0.01455   0.00861  -0.0345   0.9700   0.0186
  -9.000  -0.8248   0.01432   0.00835  -0.0340   0.9691   0.0196
  -8.750  -0.7992   0.01411   0.00810  -0.0339   0.9683   0.0202
  -8.500  -0.7735   0.01372   0.00768  -0.0338   0.9677   0.0215
  -8.250  -0.7471   0.01343   0.00738  -0.0339   0.9671   0.0225
  -8.000  -0.7204   0.01319   0.00713  -0.0340   0.9665   0.0236
  -7.750  -0.6936   0.01295   0.00688  -0.0341   0.9660   0.0246
  -7.500  -0.6668   0.01272   0.00661  -0.0342   0.9656   0.0254
  -7.250  -0.6397   0.01249   0.00636  -0.0343   0.9651   0.0261
  -7.000  -0.6124   0.01229   0.00613  -0.0345   0.9647   0.0266
  -6.750  -0.5848   0.01210   0.00592  -0.0347   0.9643   0.0269
  -6.500  -0.5743   0.01192   0.00571  -0.0309   0.9612   0.0278
  -6.250  -0.5563   0.01169   0.00545  -0.0289   0.9590   0.0290
  -6.000  -0.5325   0.01145   0.00518  -0.0282   0.9577   0.0300
  -5.750  -0.5071   0.01122   0.00495  -0.0278   0.9567   0.0309
  -5.500  -0.4812   0.01102   0.00474  -0.0276   0.9559   0.0319
  -5.250  -0.4549   0.01083   0.00454  -0.0275   0.9552   0.0329
  -5.000  -0.4282   0.01065   0.00435  -0.0274   0.9546   0.0337
  -4.750  -0.4012   0.01048   0.00417  -0.0274   0.9540   0.0344
  -4.500  -0.3740   0.01031   0.00399  -0.0275   0.9535   0.0351
  -4.250  -0.3465   0.01015   0.00382  -0.0276   0.9530   0.0366
  -4.000  -0.3189   0.00996   0.00367  -0.0278   0.9525   0.0402
  -3.750  -0.2911   0.00979   0.00353  -0.0279   0.9521   0.0446
  -3.500  -0.2633   0.00959   0.00339  -0.0282   0.9517   0.0566
  -3.250  -0.2608   0.00961   0.00346  -0.0223   0.9468   0.0686
  -3.000  -0.2402   0.00948   0.00340  -0.0208   0.9450   0.0844
  -2.750  -0.2167   0.00934   0.00332  -0.0200   0.9438   0.0997
  -2.500  -0.1922   0.00917   0.00324  -0.0194   0.9428   0.1195
  -2.250  -0.1671   0.00899   0.00317  -0.0190   0.9420   0.1436
  -2.000  -0.1407   0.00875   0.00306  -0.0189   0.9412   0.1769
  -1.750  -0.1100   0.00836   0.00287  -0.0198   0.9401   0.2283
  -1.500  -0.0762   0.00784   0.00262  -0.0214   0.9388   0.2991
  -1.000  -0.0465   0.00733   0.00243  -0.0155   0.9296   0.3939
  -0.750  -0.0128   0.00642   0.00195  -0.0170   0.9235   0.5186
  -0.500  -0.0300   0.00585   0.00181  -0.0065   0.9131   0.6398
  -0.250  -0.0421   0.00494   0.00176   0.0032   0.9050   0.8662
   0.000  -0.0002   0.00492   0.00179   0.0001   0.8941   0.8942
   0.250   0.0420   0.00494   0.00176  -0.0031   0.8661   0.9050
   0.500   0.0296   0.00587   0.00182   0.0066   0.6379   0.9132
   0.750   0.0126   0.00643   0.00195   0.0171   0.5157   0.9235
   1.000   0.0466   0.00733   0.00243   0.0155   0.3944   0.9296
   1.250   0.0624   0.00765   0.00256   0.0182   0.3393   0.9346
   1.500   0.0763   0.00784   0.00262   0.0214   0.2990   0.9388
   1.750   0.1101   0.00836   0.00287   0.0197   0.2298   0.9401
   2.000   0.1408   0.00875   0.00306   0.0188   0.1768   0.9412
   2.250   0.1671   0.00899   0.00317   0.0190   0.1434   0.9420
   2.500   0.1922   0.00917   0.00324   0.0194   0.1197   0.9428
   2.750   0.2167   0.00934   0.00332   0.0200   0.0999   0.9438
   3.000   0.2403   0.00948   0.00340   0.0208   0.0845   0.9450
   3.250   0.2608   0.00961   0.00346   0.0223   0.0687   0.9468
   3.500   0.2634   0.00959   0.00339   0.0281   0.0568   0.9517
   3.750   0.2912   0.00979   0.00353   0.0279   0.0446   0.9521
   4.000   0.3189   0.00996   0.00366   0.0277   0.0403   0.9525
   4.250   0.3466   0.01015   0.00382   0.0276   0.0364   0.9530
   4.500   0.3741   0.01031   0.00399   0.0275   0.0351   0.9535
   4.750   0.4013   0.01048   0.00417   0.0274   0.0344   0.9540
   5.000   0.4283   0.01065   0.00435   0.0274   0.0337   0.9546
   5.250   0.4550   0.01083   0.00454   0.0275   0.0329   0.9552
   5.500   0.4813   0.01102   0.00474   0.0276   0.0319   0.9559
   5.750   0.5072   0.01122   0.00495   0.0278   0.0309   0.9567
   6.000   0.5325   0.01145   0.00518   0.0282   0.0300   0.9577
   6.250   0.5564   0.01168   0.00544   0.0289   0.0290   0.9590
   6.500   0.5744   0.01192   0.00571   0.0309   0.0278   0.9612
   6.750   0.5850   0.01210   0.00592   0.0347   0.0269   0.9643
   7.000   0.6126   0.01229   0.00612   0.0344   0.0266   0.9647
   7.250   0.6400   0.01250   0.00637   0.0342   0.0261   0.9651
   7.500   0.6671   0.01272   0.00661   0.0341   0.0254   0.9656
   7.750   0.6939   0.01296   0.00688   0.0340   0.0246   0.9660
   8.000   0.7206   0.01319   0.00714   0.0339   0.0236   0.9665
   8.250   0.7474   0.01343   0.00738   0.0338   0.0225   0.9671
   8.500   0.7738   0.01372   0.00768   0.0338   0.0215   0.9677
   8.750   0.7995   0.01411   0.00810   0.0338   0.0202   0.9683
   9.000   0.8251   0.01433   0.00835   0.0340   0.0196   0.9691
   9.250   0.8493   0.01455   0.00861   0.0344   0.0186   0.9700
   9.500   0.8712   0.01478   0.00886   0.0354   0.0174   0.9714
   9.750   0.8765   0.01487   0.00896   0.0402   0.0164   0.9755
  10.000   0.9027   0.01522   0.00932   0.0401   0.0149   0.9758
  10.250   0.9286   0.01560   0.00974   0.0400   0.0139   0.9762
  10.500   0.9546   0.01600   0.01017   0.0399   0.0126   0.9765
  10.750   0.9802   0.01648   0.01066   0.0398   0.0112   0.9769
  11.000   1.0052   0.01696   0.01120   0.0398   0.0105   0.9773
  11.250   1.0293   0.01746   0.01176   0.0400   0.0098   0.9778
  11.500   1.0523   0.01800   0.01237   0.0404   0.0092   0.9784
  11.750   1.0740   0.01860   0.01302   0.0411   0.0086   0.9791
  12.000   1.0942   0.01926   0.01375   0.0420   0.0080   0.9799
  12.250   1.1137   0.01981   0.01439   0.0431   0.0078   0.9809
  12.500   1.1311   0.02039   0.01506   0.0446   0.0075   0.9823
  12.750   1.1377   0.02088   0.01563   0.0486   0.0073   0.9855
  13.000   1.1584   0.02161   0.01645   0.0491   0.0070   0.9858
  13.250   1.1779   0.02238   0.01733   0.0498   0.0067   0.9863
  13.500   1.1957   0.02323   0.01826   0.0508   0.0064   0.9867
  13.750   1.2114   0.02418   0.01931   0.0521   0.0061   0.9873
  14.000   1.2242   0.02530   0.02055   0.0537   0.0058   0.9880
  14.250   1.2381   0.02623   0.02159   0.0553   0.0057   0.9887
  14.500   1.2502   0.02722   0.02270   0.0570   0.0056   0.9896
  14.750   1.2603   0.02831   0.02391   0.0589   0.0055   0.9905
  15.000   1.2682   0.02950   0.02522   0.0611   0.0053   0.9916
  15.250   1.2745   0.03079   0.02665   0.0634   0.0052   0.9928
  15.500   1.2776   0.03220   0.02819   0.0660   0.0051   0.9941
  15.750   1.2804   0.03380   0.02993   0.0682   0.0050   0.9947
  16.000   1.2824   0.03564   0.03191   0.0701   0.0049   0.9952
  16.250   1.2815   0.03776   0.03417   0.0718   0.0049   0.9957
  16.500   1.2772   0.04026   0.03682   0.0734   0.0048   0.9963
  16.750   1.2688   0.04330   0.04002   0.0745   0.0047   0.9969
  17.000   1.2556   0.04725   0.04415   0.0747   0.0047   0.9976
  17.250   1.2337   0.05315   0.05025   0.0727   0.0047   0.9984
  17.500   0.8466   0.13616   0.13417   0.0256   0.0063   0.9987
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