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SIKORSKY SC1095 AIRFOIL (sc1095-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SIKORSKY SC1095 AIRFOIL (sc1095-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.55 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc1095-il-1000000-n5.txt
Download as CSV file: xf-sc1095-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SIKORSKY SC1095 AIRFOIL                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -1.0032   0.10707   0.10466   0.0182   1.0000   0.0032
 -14.750  -1.0759   0.08938   0.08686   0.0079   1.0000   0.0031
 -14.500  -1.2586   0.04490   0.04171  -0.0250   1.0000   0.0030
 -14.250  -1.2759   0.03956   0.03616  -0.0279   1.0000   0.0030
 -14.000  -1.2852   0.03632   0.03276  -0.0277   1.0000   0.0030
 -13.750  -1.2898   0.03401   0.03031  -0.0259   1.0000   0.0030
 -13.500  -1.2852   0.03205   0.02819  -0.0246   1.0000   0.0030
 -13.250  -1.2759   0.03029   0.02630  -0.0236   1.0000   0.0030
 -13.000  -1.2636   0.02872   0.02459  -0.0226   1.0000   0.0030
 -12.750  -1.2489   0.02730   0.02304  -0.0218   1.0000   0.0031
 -12.500  -1.2325   0.02599   0.02161  -0.0210   1.0000   0.0031
 -12.250  -1.2145   0.02479   0.02029  -0.0203   1.0000   0.0031
 -12.000  -1.1953   0.02367   0.01906  -0.0197   1.0000   0.0031
 -11.750  -1.1751   0.02264   0.01792  -0.0191   1.0000   0.0031
 -11.500  -1.1540   0.02168   0.01685  -0.0186   1.0000   0.0032
 -11.250  -1.1321   0.02078   0.01586  -0.0182   1.0000   0.0032
 -11.000  -1.1098   0.01987   0.01485  -0.0177   1.0000   0.0032
 -10.750  -1.0876   0.01889   0.01376  -0.0172   1.0000   0.0033
 -10.500  -1.0644   0.01800   0.01276  -0.0168   1.0000   0.0033
 -10.250  -1.0405   0.01722   0.01189  -0.0165   1.0000   0.0034
 -10.000  -1.0161   0.01650   0.01108  -0.0162   1.0000   0.0035
  -9.750  -0.9912   0.01583   0.01034  -0.0159   1.0000   0.0036
  -9.500  -0.9658   0.01522   0.00966  -0.0157   1.0000   0.0037
  -9.250  -0.9401   0.01467   0.00905  -0.0155   1.0000   0.0038
  -9.000  -0.9141   0.01415   0.00847  -0.0154   1.0000   0.0040
  -8.750  -0.8877   0.01368   0.00794  -0.0152   1.0000   0.0041
  -8.500  -0.8612   0.01323   0.00745  -0.0151   1.0000   0.0042
  -8.250  -0.8344   0.01282   0.00699  -0.0150   1.0000   0.0044
  -8.000  -0.8075   0.01242   0.00655  -0.0149   1.0000   0.0045
  -7.750  -0.7804   0.01206   0.00615  -0.0148   1.0000   0.0047
  -7.500  -0.7534   0.01167   0.00573  -0.0147   1.0000   0.0054
  -7.250  -0.7266   0.01120   0.00526  -0.0146   1.0000   0.0076
  -7.000  -0.7005   0.01062   0.00477  -0.0145   1.0000   0.0185
  -6.500  -0.6392   0.01003   0.00420  -0.0158   0.9885   0.0260
  -6.250  -0.6081   0.00976   0.00394  -0.0165   0.9832   0.0290
  -6.000  -0.5783   0.00954   0.00371  -0.0169   0.9778   0.0320
  -5.750  -0.5496   0.00930   0.00348  -0.0171   0.9724   0.0355
  -5.500  -0.5224   0.00908   0.00328  -0.0169   0.9659   0.0407
  -5.250  -0.4960   0.00884   0.00310  -0.0165   0.9587   0.0499
  -5.000  -0.4692   0.00865   0.00293  -0.0162   0.9506   0.0585
  -4.750  -0.4428   0.00847   0.00280  -0.0157   0.9421   0.0674
  -4.500  -0.4165   0.00832   0.00266  -0.0152   0.9321   0.0733
  -4.250  -0.3904   0.00819   0.00253  -0.0147   0.9185   0.0784
  -4.000  -0.3648   0.00812   0.00238  -0.0139   0.8974   0.0810
  -3.750  -0.3384   0.00805   0.00223  -0.0133   0.8733   0.0839
  -3.500  -0.3108   0.00795   0.00210  -0.0131   0.8570   0.0882
  -3.250  -0.2828   0.00786   0.00198  -0.0130   0.8432   0.0919
  -3.000  -0.2545   0.00781   0.00187  -0.0129   0.8289   0.0948
  -2.750  -0.2262   0.00773   0.00177  -0.0129   0.8140   0.0994
  -2.500  -0.1979   0.00764   0.00166  -0.0128   0.7979   0.1064
  -2.250  -0.1695   0.00759   0.00157  -0.0128   0.7815   0.1121
  -2.000  -0.1410   0.00753   0.00149  -0.0128   0.7632   0.1194
  -1.750  -0.1126   0.00749   0.00140  -0.0128   0.7382   0.1278
  -1.500  -0.0844   0.00751   0.00132  -0.0128   0.6982   0.1402
  -1.250  -0.0564   0.00757   0.00126  -0.0128   0.6415   0.1591
  -1.000  -0.0282   0.00762   0.00120  -0.0129   0.5859   0.1850
  -0.750   0.0000   0.00762   0.00117  -0.0131   0.5358   0.2230
  -0.500   0.0283   0.00763   0.00115  -0.0133   0.4866   0.2647
  -0.250   0.0566   0.00763   0.00113  -0.0135   0.4447   0.3073
   0.000   0.0849   0.00761   0.00113  -0.0137   0.4038   0.3566
   0.250   0.1132   0.00757   0.00114  -0.0139   0.3687   0.4112
   0.750   0.1698   0.00738   0.00118  -0.0144   0.3100   0.5508
   1.000   0.1980   0.00730   0.00122  -0.0145   0.2867   0.6189
   1.250   0.2263   0.00728   0.00127  -0.0146   0.2642   0.6692
   1.500   0.2540   0.00718   0.00135  -0.0146   0.2454   0.7423
   1.750   0.2813   0.00715   0.00144  -0.0144   0.2248   0.8003
   2.000   0.3083   0.00723   0.00154  -0.0141   0.2019   0.8402
   2.250   0.3343   0.00731   0.00166  -0.0135   0.1798   0.8774
   2.500   0.3593   0.00742   0.00178  -0.0126   0.1630   0.9082
   2.750   0.3845   0.00752   0.00188  -0.0118   0.1524   0.9297
   3.000   0.4100   0.00765   0.00199  -0.0111   0.1427   0.9451
   3.250   0.4361   0.00777   0.00208  -0.0106   0.1349   0.9575
   3.500   0.4628   0.00789   0.00217  -0.0102   0.1274   0.9671
   3.750   0.4910   0.00801   0.00227  -0.0102   0.1194   0.9749
   4.000   0.5210   0.00815   0.00237  -0.0106   0.1120   0.9819
   4.250   0.5528   0.00831   0.00249  -0.0115   0.1055   0.9891
   4.500   0.5848   0.00847   0.00263  -0.0124   0.1001   0.9972
   4.750   0.6139   0.00863   0.00277  -0.0126   0.0959   1.0000
   5.000   0.6419   0.00882   0.00293  -0.0127   0.0912   1.0000
   5.250   0.6701   0.00900   0.00310  -0.0128   0.0874   1.0000
   5.500   0.6983   0.00916   0.00326  -0.0128   0.0849   1.0000
   5.750   0.7263   0.00936   0.00345  -0.0129   0.0813   1.0000
   6.000   0.7542   0.00959   0.00365  -0.0129   0.0774   1.0000
   6.250   0.7821   0.00978   0.00385  -0.0130   0.0749   1.0000
   6.500   0.8101   0.00997   0.00405  -0.0130   0.0723   1.0000
   6.750   0.8377   0.01020   0.00426  -0.0131   0.0688   1.0000
   7.000   0.8653   0.01046   0.00451  -0.0131   0.0657   1.0000
   7.250   0.8928   0.01069   0.00476  -0.0131   0.0635   1.0000
   7.500   0.9205   0.01089   0.00498  -0.0131   0.0618   1.0000
   7.750   0.9477   0.01115   0.00523  -0.0131   0.0575   1.0000
   8.000   0.9746   0.01146   0.00551  -0.0130   0.0529   1.0000
   8.250   1.0018   0.01171   0.00578  -0.0130   0.0500   1.0000
   8.500   1.0281   0.01208   0.00610  -0.0129   0.0440   1.0000
   8.750   1.0544   0.01245   0.00645  -0.0128   0.0376   1.0000
   9.000   1.0789   0.01310   0.00701  -0.0125   0.0246   1.0000
   9.250   1.1017   0.01405   0.00788  -0.0120   0.0115   1.0000
   9.500   1.1263   0.01465   0.00848  -0.0117   0.0083   1.0000
   9.750   1.1513   0.01516   0.00903  -0.0114   0.0070   1.0000
  10.000   1.1759   0.01570   0.00961  -0.0111   0.0062   1.0000
  10.250   1.2003   0.01623   0.01019  -0.0108   0.0057   1.0000
  10.500   1.2247   0.01675   0.01077  -0.0104   0.0054   1.0000
  10.750   1.2485   0.01731   0.01138  -0.0100   0.0052   1.0000
  11.000   1.2719   0.01792   0.01205  -0.0096   0.0049   1.0000
  11.250   1.2947   0.01856   0.01276  -0.0091   0.0047   1.0000
  11.500   1.3168   0.01928   0.01355  -0.0085   0.0045   1.0000
  11.750   1.3378   0.02009   0.01444  -0.0078   0.0043   1.0000
  12.000   1.3579   0.02097   0.01541  -0.0071   0.0041   1.0000
  12.250   1.3787   0.02169   0.01621  -0.0064   0.0040   1.0000
  12.500   1.3986   0.02248   0.01707  -0.0056   0.0039   1.0000
  12.750   1.4173   0.02334   0.01801  -0.0048   0.0038   1.0000
  13.000   1.4348   0.02426   0.01904  -0.0038   0.0037   1.0000
  13.250   1.4509   0.02526   0.02013  -0.0027   0.0037   1.0000
  13.500   1.4654   0.02632   0.02129  -0.0014   0.0036   1.0000
  13.750   1.4777   0.02747   0.02255   0.0000   0.0035   1.0000
  14.000   1.4856   0.02869   0.02387   0.0020   0.0034   1.0000
  14.250   1.4898   0.03007   0.02536   0.0042   0.0034   1.0000
  14.500   1.4923   0.03171   0.02711   0.0060   0.0034   1.0000
  14.750   1.4930   0.03367   0.02918   0.0074   0.0033   1.0000
  15.000   1.4916   0.03605   0.03169   0.0081   0.0033   1.0000
  15.250   1.4875   0.03902   0.03480   0.0082   0.0032   1.0000
  15.500   1.4799   0.04284   0.03877   0.0072   0.0032   1.0000
  15.750   1.4677   0.04789   0.04399   0.0047   0.0032   1.0000
  16.000   1.4479   0.05503   0.05133   0.0002   0.0032   1.0000
  16.250   1.4112   0.06640   0.06294  -0.0076   0.0032   1.0000
  16.500   1.3387   0.08464   0.08149  -0.0182   0.0033   1.0000
  16.750   1.2427   0.10641   0.10355  -0.0293   0.0035   1.0000
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