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S1016 (s1016-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: S1016 (s1016-il)
Reynolds number: 50,000
Max Cl/Cd: 22.37 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1016-il-50000-n5.txt
Download as CSV file: xf-s1016-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1016                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.5794   0.11835   0.11021  -0.0509   1.0000   0.1124
 -14.750  -0.6725   0.09535   0.08720  -0.0632   1.0000   0.1153
 -14.500  -0.7679   0.07831   0.06989  -0.0712   1.0000   0.1145
 -14.250  -0.8124   0.07100   0.06232  -0.0727   1.0000   0.1152
 -14.000  -0.8448   0.06591   0.05696  -0.0723   1.0000   0.1165
 -13.750  -0.8738   0.06191   0.05265  -0.0706   1.0000   0.1180
 -13.500  -0.8777   0.05995   0.05065  -0.0688   1.0000   0.1205
 -13.250  -0.8776   0.05870   0.04941  -0.0667   1.0000   0.1233
 -13.000  -0.8898   0.05711   0.04772  -0.0634   1.0000   0.1257
 -12.750  -0.9061   0.05549   0.04594  -0.0594   1.0000   0.1281
 -12.500  -0.9246   0.05386   0.04409  -0.0549   1.0000   0.1305
 -12.250  -0.9445   0.05225   0.04219  -0.0501   1.0000   0.1328
 -12.000  -0.9366   0.05144   0.04148  -0.0478   1.0000   0.1363
 -11.750  -0.9393   0.05044   0.04041  -0.0444   1.0000   0.1398
 -11.500  -0.9458   0.04925   0.03906  -0.0405   1.0000   0.1436
 -11.250  -0.9549   0.04794   0.03746  -0.0363   1.0000   0.1474
 -11.000  -0.9454   0.04711   0.03672  -0.0341   1.0000   0.1519
 -10.750  -0.9434   0.04618   0.03572  -0.0310   1.0000   0.1567
 -10.500  -0.9447   0.04510   0.03441  -0.0274   1.0000   0.1620
 -10.250  -0.9357   0.04426   0.03360  -0.0251   1.0000   0.1675
 -10.000  -0.9299   0.04342   0.03268  -0.0223   1.0000   0.1735
  -9.750  -0.9241   0.04250   0.03160  -0.0195   1.0000   0.1803
  -9.500  -0.9135   0.04178   0.03093  -0.0173   1.0000   0.1872
  -9.250  -0.9075   0.04095   0.02990  -0.0145   1.0000   0.1953
  -9.000  -0.8936   0.04027   0.02932  -0.0127   1.0000   0.2033
  -8.750  -0.8839   0.03954   0.02847  -0.0103   1.0000   0.2128
  -8.500  -0.8645   0.03885   0.02781  -0.0095   0.9987   0.2238
  -8.250  -0.8435   0.03816   0.02714  -0.0090   0.9968   0.2363
  -8.000  -0.8249   0.03750   0.02646  -0.0082   0.9950   0.2500
  -7.750  -0.8071   0.03689   0.02584  -0.0072   0.9934   0.2647
  -7.500  -0.7907   0.03627   0.02525  -0.0060   0.9915   0.2811
  -7.250  -0.7748   0.03565   0.02471  -0.0047   0.9893   0.2988
  -7.000  -0.7601   0.03504   0.02420  -0.0032   0.9871   0.3183
  -6.750  -0.7472   0.03447   0.02375  -0.0014   0.9850   0.3401
  -6.500  -0.7331   0.03393   0.02332   0.0003   0.9828   0.3659
  -6.250  -0.7181   0.03345   0.02303   0.0020   0.9805   0.3956
  -6.000  -0.7060   0.03301   0.02280   0.0044   0.9780   0.4285
  -5.750  -0.6880   0.03280   0.02285   0.0061   0.9758   0.4687
  -5.500  -0.6536   0.03324   0.02359   0.0060   0.9741   0.5171
  -5.250  -0.6093   0.03442   0.02495   0.0049   0.9726   0.5626
  -5.000  -0.5685   0.03581   0.02635   0.0043   0.9709   0.5973
  -4.750  -0.5318   0.03712   0.02758   0.0041   0.9690   0.6243
  -4.500  -0.5097   0.03793   0.02829   0.0057   0.9662   0.6488
  -4.250  -0.4851   0.03887   0.02913   0.0070   0.9632   0.6687
  -4.000  -0.4614   0.03968   0.02982   0.0082   0.9600   0.6889
  -3.750  -0.4476   0.04014   0.03018   0.0104   0.9564   0.7116
  -3.500  -0.4204   0.04095   0.03088   0.0107   0.9534   0.7290
  -3.250  -0.4038   0.04148   0.03131   0.0128   0.9493   0.7456
  -3.000  -0.3818   0.04206   0.03180   0.0139   0.9454   0.7618
  -2.750  -0.3549   0.04263   0.03227   0.0140   0.9418   0.7772
  -2.500  -0.3313   0.04310   0.03265   0.0146   0.9381   0.7924
  -2.250  -0.2900   0.04366   0.03313   0.0124   0.9345   0.8024
  -2.000  -0.2591   0.04400   0.03339   0.0116   0.9303   0.8144
  -1.750  -0.2309   0.04427   0.03359   0.0110   0.9261   0.8273
  -1.500  -0.1862   0.04457   0.03383   0.0076   0.9226   0.8359
  -1.250  -0.1639   0.04464   0.03386   0.0081   0.9165   0.8466
  -1.000  -0.1304   0.04479   0.03397   0.0064   0.9117   0.8565
  -0.750  -0.0876   0.04491   0.03404   0.0030   0.9076   0.8640
  -0.500  -0.0714   0.04491   0.03403   0.0044   0.8998   0.8739
  -0.250  -0.0285   0.04494   0.03405   0.0009   0.8947   0.8802
   0.000   0.0000   0.04495   0.03406   0.0000   0.8876   0.8877
   0.250   0.0286   0.04494   0.03405  -0.0009   0.8801   0.8947
   0.500   0.0715   0.04491   0.03403  -0.0044   0.8740   0.8998
   0.750   0.0874   0.04491   0.03404  -0.0030   0.8640   0.9076
   1.000   0.1302   0.04478   0.03396  -0.0064   0.8565   0.9117
   1.250   0.1639   0.04464   0.03386  -0.0081   0.8466   0.9166
   1.500   0.1861   0.04456   0.03382  -0.0076   0.8359   0.9226
   1.750   0.2307   0.04426   0.03358  -0.0110   0.8273   0.9261
   2.000   0.2592   0.04398   0.03338  -0.0116   0.8144   0.9303
   2.250   0.2902   0.04365   0.03311  -0.0124   0.8025   0.9345
   2.500   0.3312   0.04309   0.03264  -0.0145   0.7924   0.9381
   2.750   0.3550   0.04262   0.03226  -0.0140   0.7773   0.9418
   3.000   0.3817   0.04205   0.03179  -0.0139   0.7618   0.9454
   3.250   0.4036   0.04148   0.03131  -0.0128   0.7457   0.9494
   3.500   0.4203   0.04094   0.03086  -0.0107   0.7290   0.9535
   3.750   0.4479   0.04012   0.03016  -0.0104   0.7116   0.9564
   4.000   0.4615   0.03966   0.02980  -0.0082   0.6889   0.9601
   4.250   0.4852   0.03886   0.02912  -0.0070   0.6688   0.9632
   4.500   0.5098   0.03791   0.02827  -0.0057   0.6488   0.9663
   4.750   0.5322   0.03710   0.02756  -0.0042   0.6247   0.9691
   5.000   0.5687   0.03579   0.02633  -0.0044   0.5974   0.9710
   5.250   0.6095   0.03441   0.02493  -0.0049   0.5627   0.9727
   5.500   0.6538   0.03321   0.02357  -0.0060   0.5169   0.9741
   5.750   0.6881   0.03278   0.02283  -0.0062   0.4686   0.9758
   6.000   0.7062   0.03299   0.02279  -0.0044   0.4286   0.9780
   6.250   0.7184   0.03343   0.02301  -0.0020   0.3957   0.9805
   6.500   0.7335   0.03391   0.02330  -0.0004   0.3659   0.9828
   6.750   0.7474   0.03445   0.02373   0.0013   0.3401   0.9851
   7.000   0.7605   0.03503   0.02418   0.0031   0.3182   0.9871
   7.250   0.7751   0.03563   0.02469   0.0047   0.2986   0.9894
   7.500   0.7911   0.03625   0.02524   0.0060   0.2811   0.9916
   7.750   0.8075   0.03687   0.02582   0.0072   0.2647   0.9935
   8.000   0.8252   0.03749   0.02644   0.0082   0.2498   0.9951
   8.250   0.8437   0.03814   0.02712   0.0090   0.2361   0.9969
   8.500   0.8648   0.03883   0.02780   0.0094   0.2237   0.9987
   8.750   0.8841   0.03952   0.02845   0.0102   0.2128   1.0000
   9.000   0.8934   0.04025   0.02930   0.0127   0.2032   1.0000
   9.250   0.9076   0.04094   0.02988   0.0145   0.1952   1.0000
   9.500   0.9141   0.04176   0.03091   0.0172   0.1872   1.0000
   9.750   0.9243   0.04248   0.03158   0.0195   0.1802   1.0000
  10.000   0.9301   0.04340   0.03266   0.0223   0.1735   1.0000
  10.250   0.9358   0.04424   0.03357   0.0251   0.1675   1.0000
  10.500   0.9442   0.04507   0.03438   0.0275   0.1619   1.0000
  10.750   0.9436   0.04615   0.03569   0.0310   0.1567   1.0000
  11.000   0.9455   0.04707   0.03668   0.0341   0.1518   1.0000
  11.250   0.9547   0.04792   0.03744   0.0363   0.1474   1.0000
  11.500   0.9453   0.04921   0.03902   0.0406   0.1435   1.0000
  11.750   0.9391   0.05040   0.04037   0.0444   0.1397   1.0000
  12.000   0.9369   0.05140   0.04143   0.0477   0.1363   1.0000
  12.250   0.9446   0.05222   0.04216   0.0501   0.1328   1.0000
  12.500   0.9247   0.05382   0.04405   0.0549   0.1305   1.0000
  12.750   0.9062   0.05544   0.04589   0.0594   0.1280   1.0000
  13.000   0.8899   0.05705   0.04766   0.0634   0.1256   1.0000
  13.250   0.8782   0.05864   0.04934   0.0667   0.1233   1.0000
  13.500   0.8786   0.05990   0.05060   0.0688   0.1205   1.0000
  13.750   0.8743   0.06192   0.05266   0.0705   0.1180   1.0000
  14.000   0.8456   0.06592   0.05697   0.0721   0.1165   1.0000
  14.250   0.8134   0.07102   0.06233   0.0725   0.1152   1.0000
  14.500   0.7689   0.07835   0.06993   0.0710   0.1144   1.0000
  14.750   0.6711   0.09588   0.08773   0.0627   0.1152   1.0000
  15.000   0.5812   0.11833   0.11019   0.0507   0.1122   1.0000
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