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SIKORSKY SC1095 AIRFOIL (sc1095-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: SIKORSKY SC1095 AIRFOIL (sc1095-il)
Reynolds number: 500,000
Max Cl/Cd: 70.18 at α=8.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sc1095-il-500000-n5.txt
Download as CSV file: xf-sc1095-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.9868   0.09701   0.09401   0.0120   1.0000   0.0047
 -14.000  -1.0529   0.08036   0.07725   0.0022   1.0000   0.0046
 -13.750  -1.1568   0.05026   0.04668  -0.0211   1.0000   0.0044
 -13.500  -1.1787   0.04297   0.03913  -0.0268   1.0000   0.0044
 -13.250  -1.1900   0.03907   0.03504  -0.0277   1.0000   0.0044
 -13.000  -1.1961   0.03639   0.03217  -0.0265   1.0000   0.0044
 -12.750  -1.1937   0.03417   0.02978  -0.0253   1.0000   0.0045
 -12.500  -1.1858   0.03220   0.02761  -0.0243   1.0000   0.0045
 -12.250  -1.1745   0.03043   0.02568  -0.0234   1.0000   0.0045
 -12.000  -1.1606   0.02885   0.02393  -0.0226   1.0000   0.0046
 -11.750  -1.1444   0.02743   0.02236  -0.0219   1.0000   0.0046
 -11.500  -1.1266   0.02616   0.02094  -0.0212   1.0000   0.0047
 -11.250  -1.1080   0.02488   0.01952  -0.0206   1.0000   0.0048
 -11.000  -1.0894   0.02350   0.01799  -0.0199   1.0000   0.0050
 -10.750  -1.0691   0.02232   0.01666  -0.0194   1.0000   0.0051
 -10.500  -1.0475   0.02128   0.01549  -0.0189   1.0000   0.0053
 -10.250  -1.0249   0.02035   0.01444  -0.0185   1.0000   0.0055
 -10.000  -1.0016   0.01950   0.01347  -0.0181   1.0000   0.0056
  -9.750  -0.9777   0.01872   0.01258  -0.0177   1.0000   0.0058
  -9.500  -0.9534   0.01798   0.01174  -0.0174   1.0000   0.0060
  -9.250  -0.9286   0.01731   0.01095  -0.0171   1.0000   0.0062
  -9.000  -0.9035   0.01667   0.01023  -0.0168   1.0000   0.0065
  -8.750  -0.8783   0.01602   0.00950  -0.0166   1.0000   0.0071
  -8.500  -0.8531   0.01536   0.00879  -0.0163   1.0000   0.0084
  -8.250  -0.8279   0.01466   0.00810  -0.0160   1.0000   0.0125
  -8.000  -0.8022   0.01411   0.00756  -0.0158   1.0000   0.0190
  -7.750  -0.7759   0.01369   0.00714  -0.0157   1.0000   0.0234
  -7.500  -0.7494   0.01329   0.00672  -0.0155   1.0000   0.0266
  -7.250  -0.7228   0.01293   0.00634  -0.0154   1.0000   0.0293
  -7.000  -0.6961   0.01261   0.00598  -0.0152   1.0000   0.0314
  -6.750  -0.6697   0.01223   0.00560  -0.0150   1.0000   0.0344
  -6.500  -0.6433   0.01191   0.00527  -0.0148   1.0000   0.0378
  -6.250  -0.6173   0.01157   0.00496  -0.0145   1.0000   0.0428
  -6.000  -0.5917   0.01125   0.00469  -0.0142   1.0000   0.0502
  -5.750  -0.5666   0.01100   0.00447  -0.0137   1.0000   0.0588
  -5.500  -0.5371   0.01078   0.00429  -0.0141   0.9974   0.0677
  -5.250  -0.5037   0.01055   0.00408  -0.0154   0.9935   0.0739
  -5.000  -0.4712   0.01036   0.00388  -0.0164   0.9885   0.0788
  -4.750  -0.4377   0.01019   0.00368  -0.0176   0.9839   0.0828
  -4.500  -0.4054   0.00997   0.00349  -0.0185   0.9787   0.0875
  -4.250  -0.3732   0.00981   0.00331  -0.0194   0.9733   0.0915
  -4.000  -0.3429   0.00968   0.00315  -0.0198   0.9663   0.0946
  -3.750  -0.3145   0.00951   0.00299  -0.0197   0.9576   0.0992
  -3.500  -0.2885   0.00936   0.00285  -0.0191   0.9435   0.1048
  -3.250  -0.2639   0.00925   0.00270  -0.0181   0.9245   0.1098
  -3.000  -0.2391   0.00908   0.00254  -0.0171   0.9058   0.1170
  -2.750  -0.2126   0.00896   0.00240  -0.0166   0.8924   0.1229
  -2.500  -0.1858   0.00882   0.00225  -0.0162   0.8794   0.1311
  -2.250  -0.1588   0.00869   0.00213  -0.0158   0.8659   0.1418
  -2.000  -0.1317   0.00854   0.00201  -0.0155   0.8512   0.1582
  -1.750  -0.1044   0.00838   0.00190  -0.0152   0.8358   0.1835
  -1.500  -0.0771   0.00817   0.00179  -0.0150   0.8194   0.2222
  -1.250  -0.0498   0.00796   0.00170  -0.0149   0.8006   0.2688
  -1.000  -0.0227   0.00778   0.00160  -0.0146   0.7738   0.3205
  -0.750   0.0039   0.00762   0.00151  -0.0143   0.7334   0.3810
  -0.500   0.0307   0.00748   0.00143  -0.0141   0.6863   0.4510
  -0.250   0.0578   0.00733   0.00138  -0.0140   0.6422   0.5277
   0.000   0.0845   0.00721   0.00138  -0.0138   0.5913   0.6150
   0.250   0.1112   0.00719   0.00141  -0.0135   0.5398   0.6846
   0.500   0.1381   0.00728   0.00146  -0.0133   0.4897   0.7317
   0.750   0.1647   0.00740   0.00153  -0.0129   0.4414   0.7738
   1.000   0.1901   0.00749   0.00163  -0.0122   0.3995   0.8251
   1.250   0.2143   0.00760   0.00174  -0.0112   0.3643   0.8686
   1.500   0.2378   0.00774   0.00184  -0.0099   0.3345   0.9032
   1.750   0.2609   0.00790   0.00193  -0.0085   0.3078   0.9323
   2.000   0.2858   0.00805   0.00201  -0.0076   0.2833   0.9547
   2.250   0.3137   0.00820   0.00207  -0.0074   0.2609   0.9701
   2.500   0.3467   0.00838   0.00215  -0.0085   0.2364   0.9785
   2.750   0.3803   0.00860   0.00224  -0.0098   0.2101   0.9858
   3.000   0.4137   0.00885   0.00236  -0.0111   0.1844   0.9930
   3.250   0.4475   0.00908   0.00249  -0.0125   0.1658   0.9992
   3.500   0.4744   0.00928   0.00262  -0.0123   0.1541   1.0000
   4.000   0.5279   0.00967   0.00293  -0.0120   0.1357   1.0000
   4.250   0.5550   0.00989   0.00310  -0.0119   0.1278   1.0000
   4.500   0.5824   0.01009   0.00328  -0.0118   0.1199   1.0000
   4.750   0.6098   0.01032   0.00347  -0.0118   0.1132   1.0000
   5.000   0.6373   0.01053   0.00367  -0.0117   0.1077   1.0000
   5.250   0.6646   0.01079   0.00390  -0.0117   0.1022   1.0000
   5.500   0.6922   0.01101   0.00413  -0.0117   0.0986   1.0000
   5.750   0.7196   0.01124   0.00437  -0.0116   0.0947   1.0000
   6.000   0.7468   0.01152   0.00464  -0.0116   0.0909   1.0000
   6.250   0.7740   0.01181   0.00493  -0.0115   0.0875   1.0000
   6.500   0.8013   0.01205   0.00521  -0.0114   0.0848   1.0000
   6.750   0.8284   0.01233   0.00550  -0.0114   0.0821   1.0000
   7.000   0.8553   0.01263   0.00583  -0.0113   0.0795   1.0000
   7.250   0.8817   0.01302   0.00621  -0.0111   0.0760   1.0000
   7.500   0.9087   0.01327   0.00651  -0.0110   0.0737   1.0000
   7.750   0.9355   0.01354   0.00681  -0.0110   0.0705   1.0000
   8.000   0.9619   0.01386   0.00715  -0.0108   0.0670   1.0000
   8.250   0.9880   0.01423   0.00752  -0.0107   0.0633   1.0000
   8.500   1.0146   0.01450   0.00785  -0.0106   0.0605   1.0000
   8.750   1.0407   0.01483   0.00820  -0.0104   0.0568   1.0000
   9.000   1.0664   0.01523   0.00860  -0.0102   0.0525   1.0000
   9.250   1.0921   0.01558   0.00899  -0.0100   0.0475   1.0000
   9.500   1.1171   0.01605   0.00944  -0.0098   0.0404   1.0000
   9.750   1.1401   0.01681   0.01010  -0.0094   0.0267   1.0000
  10.000   1.1602   0.01800   0.01121  -0.0087   0.0140   1.0000
  10.250   1.1821   0.01888   0.01215  -0.0081   0.0108   1.0000
  10.500   1.2046   0.01963   0.01297  -0.0076   0.0093   1.0000
  10.750   1.2261   0.02047   0.01390  -0.0069   0.0084   1.0000
  11.000   1.2473   0.02130   0.01483  -0.0063   0.0078   1.0000
  11.250   1.2683   0.02211   0.01575  -0.0056   0.0074   1.0000
  11.500   1.2884   0.02299   0.01673  -0.0049   0.0070   1.0000
  11.750   1.3073   0.02394   0.01781  -0.0041   0.0067   1.0000
  12.000   1.3249   0.02500   0.01899  -0.0031   0.0064   1.0000
  12.250   1.3404   0.02619   0.02030  -0.0020   0.0062   1.0000
  12.500   1.3531   0.02759   0.02183  -0.0007   0.0060   1.0000
  12.750   1.3640   0.02901   0.02339   0.0007   0.0058   1.0000
  13.000   1.3737   0.03035   0.02486   0.0023   0.0057   1.0000
  13.250   1.3780   0.03181   0.02645   0.0045   0.0056   1.0000
  13.500   1.3803   0.03354   0.02832   0.0062   0.0055   1.0000
  13.750   1.3805   0.03562   0.03057   0.0075   0.0054   1.0000
  14.000   1.3784   0.03817   0.03326   0.0081   0.0053   1.0000
  14.250   1.3734   0.04138   0.03664   0.0079   0.0052   1.0000
  14.500   1.3650   0.04554   0.04097   0.0063   0.0052   1.0000
  14.750   1.3519   0.05114   0.04677   0.0031   0.0051   1.0000
  15.000   1.3306   0.05924   0.05509  -0.0026   0.0051   1.0000
  15.250   1.2947   0.07105   0.06716  -0.0105   0.0052   1.0000
  15.500   1.2425   0.08550   0.08184  -0.0188   0.0054   1.0000
  15.750   1.1865   0.10011   0.09663  -0.0263   0.0056   1.0000
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