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S4062-095-87 (s4062-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: S4062-095-87 (s4062-il)
Reynolds number: 500,000
Max Cl/Cd: 128.49 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s4062-il-500000.txt
Download as CSV file: xf-s4062-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S4062-095-87                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.3110   0.10813   0.10588  -0.0414   1.0000   0.0172
 -10.000  -0.3118   0.10442   0.10221  -0.0440   1.0000   0.0177
  -9.750  -0.3081   0.10065   0.09848  -0.0465   0.9938   0.0178
  -9.500  -0.2941   0.09559   0.09342  -0.0521   0.9865   0.0179
  -9.250  -0.2851   0.08995   0.08779  -0.0564   0.9803   0.0183
  -9.000  -0.2670   0.08675   0.08457  -0.0597   0.9747   0.0187
  -8.750  -0.2477   0.08361   0.08141  -0.0634   0.9680   0.0195
  -8.500  -0.2313   0.07960   0.07737  -0.0683   0.9591   0.0202
  -8.250  -0.2221   0.07579   0.07354  -0.0719   0.9464   0.0212
  -8.000  -0.2204   0.07228   0.06999  -0.0739   0.9326   0.0219
  -7.750  -0.2288   0.06764   0.06534  -0.0772   0.9165   0.0233
  -7.500  -0.2294   0.06348   0.06116  -0.0808   0.9052   0.0234
  -7.250  -0.2264   0.05712   0.05474  -0.0877   0.8955   0.0235
  -7.000  -0.2371   0.04567   0.04306  -0.0967   0.8860   0.0241
  -6.750  -0.2230   0.04409   0.04147  -0.0973   0.8797   0.0247
  -6.500  -0.2077   0.04174   0.03900  -0.0985   0.8743   0.0254
  -6.250  -0.1920   0.03794   0.03502  -0.1006   0.8688   0.0263
  -6.000  -0.1853   0.02371   0.01923  -0.1037   0.8617   0.0181
  -5.750  -0.1659   0.01931   0.01442  -0.1037   0.8577   0.0163
  -5.500  -0.1415   0.01632   0.01087  -0.1034   0.8531   0.0152
  -5.250  -0.1154   0.01479   0.00907  -0.1031   0.8485   0.0151
  -5.000  -0.0890   0.01375   0.00785  -0.1028   0.8446   0.0154
  -4.750  -0.0622   0.01295   0.00691  -0.1026   0.8408   0.0161
  -4.500  -0.0349   0.01226   0.00613  -0.1025   0.8362   0.0169
  -4.250  -0.0075   0.01174   0.00550  -0.1023   0.8319   0.0178
  -4.000   0.0192   0.01094   0.00461  -0.1021   0.8283   0.0195
  -3.750   0.0471   0.01063   0.00427  -0.1021   0.8240   0.0226
  -3.500   0.0749   0.01011   0.00371  -0.1021   0.8195   0.0280
  -3.250   0.1026   0.00956   0.00322  -0.1020   0.8156   0.0543
  -3.000   0.1304   0.00930   0.00302  -0.1020   0.8119   0.0824
  -2.750   0.1584   0.00907   0.00289  -0.1021   0.8072   0.1096
  -2.500   0.1863   0.00886   0.00275  -0.1022   0.8029   0.1421
  -2.250   0.2142   0.00866   0.00263  -0.1022   0.7993   0.1799
  -2.000   0.2422   0.00848   0.00255  -0.1023   0.7949   0.2187
  -1.750   0.2702   0.00828   0.00246  -0.1024   0.7902   0.2651
  -1.500   0.2980   0.00807   0.00238  -0.1025   0.7863   0.3199
  -1.250   0.3257   0.00786   0.00234  -0.1025   0.7823   0.3870
  -1.000   0.3533   0.00761   0.00233  -0.1026   0.7773   0.4667
  -0.750   0.3803   0.00733   0.00231  -0.1025   0.7728   0.5669
  -0.500   0.4062   0.00701   0.00232  -0.1020   0.7688   0.6862
  -0.250   0.4280   0.00660   0.00238  -0.1004   0.7634   0.8338
   0.000   0.4660   0.00631   0.00225  -0.1020   0.7584   1.0000
   0.250   0.4938   0.00635   0.00220  -0.1019   0.7526   1.0000
   0.500   0.5215   0.00636   0.00216  -0.1018   0.7453   1.0000
   0.750   0.5492   0.00640   0.00211  -0.1017   0.7388   1.0000
   1.000   0.5769   0.00642   0.00209  -0.1016   0.7311   1.0000
   1.250   0.6048   0.00647   0.00207  -0.1015   0.7250   1.0000
   1.500   0.6326   0.00651   0.00210  -0.1015   0.7177   1.0000
   1.750   0.6604   0.00657   0.00209  -0.1014   0.7114   1.0000
   2.000   0.6881   0.00661   0.00213  -0.1013   0.7036   1.0000
   2.250   0.7158   0.00668   0.00215  -0.1012   0.6968   1.0000
   2.500   0.7435   0.00673   0.00221  -0.1012   0.6884   1.0000
   2.750   0.7710   0.00680   0.00224  -0.1011   0.6806   1.0000
   3.000   0.7985   0.00686   0.00230  -0.1010   0.6712   1.0000
   3.250   0.8259   0.00694   0.00238  -0.1009   0.6617   1.0000
   3.500   0.8530   0.00703   0.00244  -0.1007   0.6514   1.0000
   3.750   0.8800   0.00713   0.00251  -0.1005   0.6395   1.0000
   4.000   0.9069   0.00723   0.00261  -0.1003   0.6261   1.0000
   4.250   0.9335   0.00735   0.00272  -0.1001   0.6112   1.0000
   4.500   0.9597   0.00750   0.00284  -0.0997   0.5939   1.0000
   4.750   0.9855   0.00767   0.00298  -0.0994   0.5723   1.0000
   5.000   1.0104   0.00791   0.00315  -0.0989   0.5464   1.0000
   5.250   1.0339   0.00825   0.00336  -0.0981   0.5104   1.0000
   5.500   1.0553   0.00875   0.00365  -0.0971   0.4617   1.0000
   5.750   1.0746   0.00944   0.00405  -0.0958   0.4048   1.0000
   6.000   1.0945   0.01009   0.00448  -0.0947   0.3580   1.0000
   6.250   1.1152   0.01067   0.00490  -0.0937   0.3219   1.0000
   6.500   1.1359   0.01123   0.00532  -0.0927   0.2906   1.0000
   6.750   1.1562   0.01181   0.00576  -0.0916   0.2588   1.0000
   7.000   1.1761   0.01240   0.00622  -0.0905   0.2300   1.0000
   7.250   1.1957   0.01299   0.00668  -0.0894   0.2034   1.0000
   7.500   1.2154   0.01354   0.00714  -0.0883   0.1798   1.0000
   7.750   1.2342   0.01414   0.00763  -0.0870   0.1560   1.0000
   8.250   1.2702   0.01536   0.00870  -0.0843   0.1170   1.0000
   8.500   1.2869   0.01601   0.00927  -0.0828   0.0997   1.0000
   8.750   1.3010   0.01670   0.00988  -0.0808   0.0841   1.0000
   9.000   1.3137   0.01741   0.01054  -0.0786   0.0703   1.0000
   9.250   1.3262   0.01816   0.01125  -0.0764   0.0574   1.0000
   9.500   1.3378   0.01900   0.01205  -0.0742   0.0455   1.0000
   9.750   1.3472   0.02004   0.01303  -0.0719   0.0335   1.0000
  10.000   1.3561   0.02116   0.01414  -0.0695   0.0258   1.0000
  10.250   1.3638   0.02241   0.01541  -0.0671   0.0220   1.0000
  10.500   1.3756   0.02338   0.01646  -0.0653   0.0201   1.0000
  10.750   1.3856   0.02451   0.01763  -0.0634   0.0185   1.0000
  11.000   1.3893   0.02616   0.01936  -0.0609   0.0171   1.0000
  11.250   1.3980   0.02745   0.02076  -0.0592   0.0164   1.0000
  11.500   1.4068   0.02877   0.02219  -0.0575   0.0157   1.0000
  11.750   1.4139   0.03027   0.02379  -0.0558   0.0151   1.0000
  12.000   1.4206   0.03184   0.02544  -0.0542   0.0144   1.0000
  12.250   1.4259   0.03358   0.02728  -0.0526   0.0140   1.0000
  12.500   1.4296   0.03552   0.02929  -0.0511   0.0134   1.0000
  12.750   1.4286   0.03799   0.03185  -0.0495   0.0129   1.0000
  13.000   1.4217   0.04120   0.03521  -0.0477   0.0125   1.0000
  13.250   1.4285   0.04305   0.03718  -0.0468   0.0122   1.0000
  13.500   1.4330   0.04519   0.03944  -0.0459   0.0119   1.0000
  13.750   1.4358   0.04759   0.04198  -0.0451   0.0115   1.0000
  14.000   1.4368   0.05028   0.04479  -0.0444   0.0113   1.0000
  14.250   1.4377   0.05306   0.04771  -0.0439   0.0110   1.0000
  14.500   1.4376   0.05606   0.05083  -0.0436   0.0107   1.0000
  14.750   1.4377   0.05912   0.05402  -0.0435   0.0104   1.0000
  15.000   1.4361   0.06251   0.05752  -0.0436   0.0102   1.0000
  15.250   1.4343   0.06600   0.06110  -0.0439   0.0099   1.0000
  15.500   1.4305   0.06992   0.06514  -0.0445   0.0097   1.0000
  15.750   1.4236   0.07442   0.06976  -0.0452   0.0094   1.0000
  16.000   1.4113   0.07994   0.07546  -0.0461   0.0092   1.0000
  16.250   1.3997   0.08560   0.08133  -0.0477   0.0090   1.0000
  16.500   1.3925   0.09079   0.08669  -0.0496   0.0089   1.0000
  16.750   1.3845   0.09630   0.09237  -0.0520   0.0088   1.0000
  17.000   1.3760   0.10209   0.09833  -0.0548   0.0087   1.0000
  17.250   1.3647   0.10858   0.10501  -0.0579   0.0086   1.0000
  17.500   1.3532   0.11538   0.11197  -0.0615   0.0086   1.0000
  17.750   1.3404   0.12263   0.11940  -0.0655   0.0085   1.0000
  18.000   1.3274   0.13015   0.12709  -0.0699   0.0085   1.0000
  18.250   1.3132   0.13817   0.13528  -0.0748   0.0085   1.0000
  18.500   1.2983   0.14668   0.14395  -0.0802   0.0084   1.0000
  18.750   1.2827   0.15558   0.15301  -0.0859   0.0085   1.0000
  19.000   1.2662   0.16510   0.16269  -0.0922   0.0085   1.0000
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