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S1048 14% (Danny Howell) (s1048-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S1048 14% (Danny Howell) (s1048-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.87 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1048-il-1000000.txt
Download as CSV file: xf-s1048-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1048 14% (Danny Howell)                        
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -1.1134   0.08175   0.07812  -0.0154   1.0000   0.0055
 -16.750  -1.1237   0.07651   0.07280  -0.0178   1.0000   0.0056
 -16.500  -1.1344   0.07133   0.06751  -0.0202   1.0000   0.0057
 -16.250  -1.1378   0.06728   0.06339  -0.0220   1.0000   0.0057
 -16.000  -1.1504   0.06216   0.05816  -0.0241   1.0000   0.0057
 -15.750  -1.1586   0.05775   0.05365  -0.0259   1.0000   0.0057
 -15.500  -1.1644   0.05381   0.04963  -0.0274   1.0000   0.0059
 -15.250  -1.1719   0.04978   0.04550  -0.0288   1.0000   0.0059
 -15.000  -1.1758   0.04630   0.04194  -0.0299   1.0000   0.0060
 -14.750  -1.1810   0.04278   0.03831  -0.0309   1.0000   0.0060
 -14.500  -1.1803   0.04000   0.03547  -0.0316   1.0000   0.0062
 -14.250  -1.1820   0.03709   0.03246  -0.0321   1.0000   0.0062
 -14.000  -1.1817   0.03449   0.02978  -0.0324   1.0000   0.0064
 -13.750  -1.1796   0.03220   0.02741  -0.0324   1.0000   0.0066
 -13.500  -1.1777   0.03002   0.02514  -0.0322   1.0000   0.0067
 -13.250  -1.1777   0.02784   0.02285  -0.0316   1.0000   0.0066
 -13.000  -1.1706   0.02638   0.02132  -0.0309   1.0000   0.0069
 -12.750  -1.1643   0.02498   0.01985  -0.0299   1.0000   0.0071
 -12.500  -1.1598   0.02359   0.01838  -0.0284   1.0000   0.0071
 -12.250  -1.1554   0.02236   0.01706  -0.0265   1.0000   0.0072
 -12.000  -1.1546   0.02107   0.01568  -0.0239   1.0000   0.0074
 -11.750  -1.1539   0.01993   0.01447  -0.0206   1.0000   0.0078
 -11.500  -1.1477   0.01915   0.01364  -0.0176   1.0000   0.0081
 -11.250  -1.1364   0.01850   0.01294  -0.0153   1.0000   0.0085
 -11.000  -1.1216   0.01787   0.01226  -0.0136   1.0000   0.0089
 -10.750  -1.1050   0.01730   0.01165  -0.0121   1.0000   0.0094
 -10.500  -1.0871   0.01679   0.01108  -0.0107   1.0000   0.0097
 -10.250  -1.0725   0.01600   0.01024  -0.0088   1.0000   0.0107
 -10.000  -1.0544   0.01545   0.00966  -0.0074   1.0000   0.0116
  -9.750  -1.0348   0.01500   0.00917  -0.0062   1.0000   0.0127
  -9.500  -1.0167   0.01443   0.00858  -0.0047   1.0000   0.0144
  -9.250  -0.9976   0.01394   0.00809  -0.0033   1.0000   0.0162
  -9.000  -0.9788   0.01345   0.00758  -0.0019   1.0000   0.0192
  -8.750  -0.9597   0.01298   0.00711  -0.0004   1.0000   0.0232
  -8.500  -0.9414   0.01245   0.00663   0.0011   1.0000   0.0304
  -8.250  -0.9237   0.01191   0.00617   0.0028   1.0000   0.0421
  -8.000  -0.9053   0.01143   0.00577   0.0044   1.0000   0.0550
  -7.750  -0.8833   0.01091   0.00535   0.0051   0.9993   0.0719
  -7.500  -0.8478   0.01035   0.00492   0.0030   0.9954   0.0949
  -7.250  -0.8139   0.00981   0.00452   0.0013   0.9899   0.1207
  -7.000  -0.7789   0.00932   0.00416  -0.0006   0.9831   0.1472
  -6.750  -0.7456   0.00889   0.00384  -0.0021   0.9714   0.1732
  -6.500  -0.7104   0.00847   0.00354  -0.0039   0.9564   0.2013
  -6.250  -0.6785   0.00816   0.00328  -0.0048   0.9328   0.2224
  -6.000  -0.6529   0.00795   0.00307  -0.0044   0.9047   0.2433
  -5.750  -0.6287   0.00777   0.00287  -0.0036   0.8786   0.2639
  -5.500  -0.6037   0.00761   0.00270  -0.0030   0.8555   0.2821
  -5.250  -0.5780   0.00750   0.00255  -0.0025   0.8349   0.2978
  -5.000  -0.5518   0.00739   0.00241  -0.0021   0.8162   0.3111
  -4.750  -0.5254   0.00728   0.00228  -0.0018   0.7986   0.3265
  -4.500  -0.4987   0.00719   0.00216  -0.0015   0.7822   0.3403
  -4.250  -0.4716   0.00711   0.00205  -0.0013   0.7667   0.3526
  -4.000  -0.4444   0.00704   0.00195  -0.0012   0.7523   0.3647
  -3.750  -0.4171   0.00697   0.00185  -0.0010   0.7384   0.3767
  -3.500  -0.3898   0.00690   0.00176  -0.0008   0.7251   0.3885
  -3.000  -0.3346   0.00678   0.00161  -0.0006   0.6991   0.4117
  -2.750  -0.3068   0.00674   0.00154  -0.0006   0.6866   0.4233
  -2.500  -0.2791   0.00668   0.00148  -0.0005   0.6745   0.4346
  -2.250  -0.2514   0.00663   0.00142  -0.0004   0.6623   0.4456
  -2.000  -0.2236   0.00660   0.00137  -0.0003   0.6501   0.4568
  -1.750  -0.1955   0.00657   0.00132  -0.0003   0.6375   0.4683
  -1.500  -0.1677   0.00653   0.00128  -0.0003   0.6252   0.4800
  -1.250  -0.1398   0.00650   0.00125  -0.0002   0.6128   0.4915
  -1.000  -0.1118   0.00648   0.00122  -0.0002   0.6004   0.5031
  -0.750  -0.0839   0.00648   0.00120  -0.0001   0.5881   0.5149
  -0.500  -0.0560   0.00646   0.00118  -0.0001   0.5755   0.5270
  -0.250  -0.0280   0.00644   0.00118   0.0000   0.5631   0.5392
   0.000   0.0000   0.00644   0.00117   0.0000   0.5512   0.5510
   0.250   0.0280   0.00644   0.00118   0.0000   0.5391   0.5633
   0.500   0.0560   0.00646   0.00118   0.0001   0.5272   0.5755
   0.750   0.0839   0.00647   0.00120   0.0001   0.5151   0.5880
   1.000   0.1118   0.00648   0.00122   0.0002   0.5032   0.6004
   1.250   0.1398   0.00650   0.00125   0.0002   0.4915   0.6128
   1.500   0.1677   0.00653   0.00128   0.0003   0.4800   0.6252
   1.750   0.1955   0.00657   0.00132   0.0003   0.4682   0.6375
   2.000   0.2236   0.00660   0.00137   0.0003   0.4568   0.6500
   2.250   0.2514   0.00663   0.00142   0.0004   0.4457   0.6623
   2.500   0.2791   0.00668   0.00148   0.0005   0.4347   0.6745
   2.750   0.3068   0.00673   0.00154   0.0006   0.4232   0.6866
   3.000   0.3346   0.00678   0.00161   0.0006   0.4117   0.6991
   3.500   0.3898   0.00690   0.00176   0.0008   0.3884   0.7250
   3.750   0.4171   0.00697   0.00185   0.0010   0.3768   0.7384
   4.000   0.4443   0.00704   0.00195   0.0012   0.3646   0.7524
   4.250   0.4716   0.00711   0.00205   0.0013   0.3524   0.7668
   4.500   0.4987   0.00719   0.00216   0.0015   0.3401   0.7822
   4.750   0.5254   0.00728   0.00228   0.0018   0.3264   0.7986
   5.000   0.5518   0.00739   0.00241   0.0021   0.3110   0.8161
   5.250   0.5780   0.00750   0.00255   0.0025   0.2978   0.8349
   5.500   0.6036   0.00761   0.00270   0.0030   0.2823   0.8556
   5.750   0.6287   0.00776   0.00287   0.0036   0.2646   0.8787
   6.000   0.6529   0.00795   0.00307   0.0044   0.2433   0.9047
   6.250   0.6785   0.00816   0.00328   0.0048   0.2223   0.9326
   6.500   0.7104   0.00847   0.00354   0.0039   0.2005   0.9564
   7.000   0.7788   0.00933   0.00416   0.0006   0.1466   0.9831
   7.250   0.8137   0.00982   0.00452  -0.0013   0.1203   0.9899
   7.500   0.8477   0.01036   0.00492  -0.0030   0.0947   0.9954
   7.750   0.8832   0.01091   0.00535  -0.0051   0.0719   0.9992
   8.000   0.9054   0.01143   0.00577  -0.0044   0.0551   1.0000
   8.250   0.9237   0.01191   0.00617  -0.0028   0.0421   1.0000
   8.500   0.9415   0.01245   0.00663  -0.0011   0.0306   1.0000
   8.750   0.9596   0.01299   0.00712   0.0004   0.0230   1.0000
   9.000   0.9787   0.01345   0.00758   0.0019   0.0192   1.0000
   9.250   0.9976   0.01394   0.00809   0.0034   0.0163   1.0000
   9.500   1.0167   0.01443   0.00858   0.0047   0.0144   1.0000
   9.750   1.0348   0.01499   0.00917   0.0062   0.0127   1.0000
  10.000   1.0545   0.01544   0.00965   0.0074   0.0117   1.0000
  10.250   1.0722   0.01602   0.01025   0.0089   0.0106   1.0000
  10.500   1.0871   0.01678   0.01107   0.0107   0.0097   1.0000
  10.750   1.1052   0.01728   0.01163   0.0120   0.0092   1.0000
  11.000   1.1218   0.01785   0.01224   0.0136   0.0088   1.0000
  11.250   1.1366   0.01849   0.01292   0.0153   0.0084   1.0000
  11.500   1.1487   0.01911   0.01359   0.0175   0.0081   1.0000
  11.750   1.1540   0.01993   0.01446   0.0206   0.0078   1.0000
  12.000   1.1558   0.02101   0.01562   0.0237   0.0075   1.0000
  12.250   1.1544   0.02241   0.01712   0.0266   0.0073   1.0000
  12.500   1.1615   0.02350   0.01827   0.0283   0.0071   1.0000
  12.750   1.1659   0.02488   0.01975   0.0298   0.0071   1.0000
  13.000   1.1721   0.02628   0.02122   0.0308   0.0069   1.0000
  13.250   1.1754   0.02805   0.02308   0.0316   0.0068   1.0000
  13.500   1.1835   0.02954   0.02463   0.0321   0.0065   1.0000
  13.750   1.1805   0.03215   0.02736   0.0323   0.0066   1.0000
  14.000   1.1825   0.03445   0.02973   0.0323   0.0064   1.0000
  14.250   1.1826   0.03707   0.03244   0.0320   0.0063   1.0000
  14.500   1.1793   0.04017   0.03564   0.0315   0.0062   1.0000
  14.750   1.1775   0.04323   0.03879   0.0307   0.0062   1.0000
  15.000   1.1779   0.04613   0.04176   0.0299   0.0060   1.0000
  15.250   1.1721   0.04984   0.04556   0.0287   0.0059   1.0000
  15.500   1.1677   0.05349   0.04930   0.0274   0.0058   1.0000
  15.750   1.1580   0.05790   0.05382   0.0258   0.0058   1.0000
  16.000   1.1514   0.06212   0.05812   0.0240   0.0057   1.0000
  16.250   1.1416   0.06689   0.06298   0.0220   0.0056   1.0000
  16.500   1.1336   0.07158   0.06775   0.0199   0.0055   1.0000
  16.750   1.1226   0.07677   0.07307   0.0175   0.0056   1.0000
  17.000   1.1083   0.08263   0.07901   0.0148   0.0055   1.0000
  17.250   1.0932   0.08877   0.08526   0.0119   0.0053   1.0000
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