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S1048 14% (Danny Howell) (s1048-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S1048 14% (Danny Howell) (s1048-il)
Reynolds number: 200,000
Max Cl/Cd: 54.63 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1048-il-200000-n5.txt
Download as CSV file: xf-s1048-il-200000-n5.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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.000  -0.8498   0.15247   0.14855   0.0214   1.0000   0.0101
 -17.750  -0.8709   0.14211   0.13803   0.0155   1.0000   0.0100
 -17.500  -0.8873   0.13344   0.12920   0.0106   1.0000   0.0099
 -17.250  -0.9014   0.12564   0.12126   0.0062   1.0000   0.0100
 -17.000  -0.9132   0.11866   0.11413   0.0023   1.0000   0.0100
 -16.750  -0.9237   0.11210   0.10743  -0.0013   1.0000   0.0101
 -16.500  -0.9333   0.10594   0.10113  -0.0046   1.0000   0.0103
 -16.250  -0.9415   0.10025   0.09530  -0.0076   1.0000   0.0104
 -16.000  -0.9494   0.09468   0.08958  -0.0105   1.0000   0.0106
 -15.750  -0.9560   0.08956   0.08431  -0.0130   1.0000   0.0108
 -15.500  -0.9621   0.08465   0.07924  -0.0155   1.0000   0.0110
 -15.250  -0.9673   0.07999   0.07443  -0.0177   1.0000   0.0112
 -15.000  -0.9720   0.07567   0.07000  -0.0195   1.0000   0.0114
 -14.750  -0.9769   0.07151   0.06576  -0.0212   1.0000   0.0116
 -14.500  -0.9823   0.06737   0.06152  -0.0229   1.0000   0.0118
 -14.250  -0.9869   0.06345   0.05751  -0.0245   1.0000   0.0121
 -14.000  -0.9907   0.05975   0.05372  -0.0258   1.0000   0.0123
 -13.750  -0.9942   0.05617   0.05004  -0.0271   1.0000   0.0127
 -13.500  -0.9969   0.05282   0.04659  -0.0280   1.0000   0.0129
 -13.250  -0.9994   0.04955   0.04321  -0.0289   1.0000   0.0134
 -13.000  -1.0008   0.04653   0.04008  -0.0296   1.0000   0.0136
 -12.750  -1.0020   0.04361   0.03705  -0.0301   1.0000   0.0139
 -12.500  -1.0033   0.04080   0.03410  -0.0304   1.0000   0.0146
 -12.250  -1.0027   0.03829   0.03148  -0.0304   1.0000   0.0149
 -12.000  -1.0040   0.03573   0.02881  -0.0303   1.0000   0.0154
 -11.750  -1.0067   0.03325   0.02624  -0.0298   1.0000   0.0161
 -11.500  -1.0056   0.03127   0.02418  -0.0290   1.0000   0.0167
 -11.250  -1.0025   0.02960   0.02241  -0.0279   1.0000   0.0178
 -11.000  -0.9981   0.02815   0.02086  -0.0264   1.0000   0.0193
 -10.750  -0.9944   0.02680   0.01940  -0.0245   1.0000   0.0207
 -10.500  -0.9917   0.02552   0.01808  -0.0220   1.0000   0.0224
 -10.250  -0.9859   0.02451   0.01699  -0.0195   1.0000   0.0246
 -10.000  -0.9774   0.02356   0.01596  -0.0171   1.0000   0.0271
  -9.750  -0.9676   0.02253   0.01491  -0.0150   1.0000   0.0308
  -9.500  -0.9548   0.02164   0.01398  -0.0132   1.0000   0.0364
  -9.250  -0.9412   0.02077   0.01311  -0.0115   1.0000   0.0444
  -9.000  -0.9276   0.01985   0.01224  -0.0098   1.0000   0.0560
  -8.750  -0.9133   0.01897   0.01144  -0.0081   1.0000   0.0711
  -8.500  -0.8976   0.01818   0.01070  -0.0065   1.0000   0.0889
  -8.250  -0.8812   0.01745   0.01005  -0.0050   1.0000   0.1076
  -8.000  -0.8641   0.01679   0.00946  -0.0035   1.0000   0.1270
  -7.750  -0.8462   0.01621   0.00893  -0.0021   1.0000   0.1466
  -7.500  -0.8287   0.01563   0.00844  -0.0006   1.0000   0.1680
  -7.250  -0.8112   0.01509   0.00799   0.0010   1.0000   0.1925
  -7.000  -0.7933   0.01461   0.00760   0.0025   1.0000   0.2175
  -6.750  -0.7752   0.01419   0.00726   0.0040   1.0000   0.2391
  -6.500  -0.7499   0.01385   0.00693   0.0041   0.9966   0.2580
  -6.250  -0.7144   0.01348   0.00659   0.0021   0.9854   0.2786
  -6.000  -0.6793   0.01316   0.00626   0.0003   0.9727   0.2993
  -5.750  -0.6442   0.01287   0.00597  -0.0014   0.9587   0.3181
  -5.500  -0.6088   0.01260   0.00570  -0.0031   0.9437   0.3352
  -5.250  -0.5733   0.01237   0.00544  -0.0047   0.9279   0.3511
  -5.000  -0.5390   0.01215   0.00518  -0.0061   0.9108   0.3664
  -4.750  -0.5075   0.01197   0.00495  -0.0068   0.8918   0.3805
  -4.500  -0.4782   0.01182   0.00475  -0.0069   0.8724   0.3940
  -4.250  -0.4503   0.01169   0.00455  -0.0068   0.8537   0.4067
  -3.750  -0.3974   0.01148   0.00422  -0.0060   0.8184   0.4313
  -3.500  -0.3714   0.01139   0.00407  -0.0054   0.8018   0.4430
  -3.250  -0.3453   0.01130   0.00393  -0.0049   0.7859   0.4548
  -3.000  -0.3191   0.01123   0.00380  -0.0045   0.7708   0.4667
  -2.750  -0.2928   0.01117   0.00368  -0.0040   0.7561   0.4789
  -2.500  -0.2666   0.01111   0.00358  -0.0036   0.7419   0.4907
  -2.250  -0.2402   0.01105   0.00349  -0.0032   0.7282   0.5023
  -2.000  -0.2138   0.01100   0.00341  -0.0028   0.7148   0.5142
  -1.750  -0.1872   0.01096   0.00332  -0.0024   0.7015   0.5261
  -1.500  -0.1605   0.01092   0.00326  -0.0020   0.6883   0.5383
  -1.250  -0.1338   0.01089   0.00321  -0.0017   0.6752   0.5504
  -1.000  -0.1071   0.01086   0.00317  -0.0013   0.6624   0.5625
  -0.750  -0.0804   0.01083   0.00314  -0.0010   0.6498   0.5746
  -0.500  -0.0536   0.01082   0.00312  -0.0007   0.6372   0.5869
  -0.250  -0.0268   0.01082   0.00310  -0.0003   0.6248   0.5995
   0.000   0.0000   0.01082   0.00309   0.0000   0.6122   0.6122
   0.250   0.0268   0.01082   0.00310   0.0003   0.5995   0.6248
   0.500   0.0536   0.01082   0.00312   0.0007   0.5870   0.6372
   0.750   0.0804   0.01083   0.00315   0.0010   0.5746   0.6498
   1.000   0.1071   0.01086   0.00317   0.0013   0.5625   0.6624
   1.250   0.1338   0.01089   0.00321   0.0017   0.5504   0.6752
   1.500   0.1605   0.01092   0.00326   0.0020   0.5384   0.6883
   1.750   0.1872   0.01096   0.00332   0.0024   0.5261   0.7015
   2.000   0.2137   0.01100   0.00341   0.0028   0.5142   0.7148
   2.250   0.2402   0.01105   0.00349   0.0032   0.5024   0.7282
   2.500   0.2665   0.01111   0.00358   0.0036   0.4907   0.7420
   2.750   0.2928   0.01117   0.00368   0.0040   0.4788   0.7562
   3.000   0.3191   0.01123   0.00380   0.0045   0.4667   0.7708
   3.250   0.3453   0.01130   0.00393   0.0049   0.4547   0.7859
   3.500   0.3713   0.01139   0.00407   0.0054   0.4429   0.8018
   3.750   0.3974   0.01148   0.00421   0.0060   0.4312   0.8184
   4.250   0.4503   0.01169   0.00455   0.0068   0.4067   0.8537
   4.500   0.4782   0.01182   0.00475   0.0069   0.3939   0.8724
   4.750   0.5075   0.01197   0.00496   0.0068   0.3806   0.8918
   5.000   0.5390   0.01216   0.00518   0.0061   0.3662   0.9108
   5.250   0.5733   0.01237   0.00544   0.0047   0.3511   0.9279
   5.500   0.6088   0.01260   0.00570   0.0031   0.3351   0.9437
   5.750   0.6442   0.01287   0.00597   0.0014   0.3180   0.9587
   6.000   0.6793   0.01316   0.00626  -0.0003   0.2995   0.9727
   6.250   0.7143   0.01348   0.00658  -0.0021   0.2784   0.9853
   6.500   0.7499   0.01385   0.00693  -0.0041   0.2581   0.9966
   6.750   0.7752   0.01419   0.00726  -0.0040   0.2392   1.0000
   7.000   0.7933   0.01461   0.00760  -0.0025   0.2174   1.0000
   7.250   0.8113   0.01509   0.00799  -0.0010   0.1926   1.0000
   7.500   0.8287   0.01563   0.00844   0.0006   0.1678   1.0000
   7.750   0.8462   0.01621   0.00893   0.0021   0.1465   1.0000
   8.000   0.8641   0.01679   0.00946   0.0035   0.1270   1.0000
   8.250   0.8812   0.01745   0.01005   0.0050   0.1077   1.0000
   8.500   0.8977   0.01817   0.01070   0.0065   0.0893   1.0000
   8.750   0.9133   0.01897   0.01144   0.0081   0.0711   1.0000
   9.000   0.9277   0.01985   0.01224   0.0098   0.0563   1.0000
   9.250   0.9413   0.02076   0.01310   0.0115   0.0447   1.0000
   9.500   0.9549   0.02164   0.01398   0.0132   0.0364   1.0000
   9.750   0.9676   0.02253   0.01491   0.0151   0.0309   1.0000
  10.000   0.9773   0.02357   0.01596   0.0172   0.0270   1.0000
  10.250   0.9858   0.02451   0.01699   0.0195   0.0247   1.0000
  10.500   0.9917   0.02552   0.01808   0.0220   0.0225   1.0000
  10.750   0.9948   0.02678   0.01937   0.0244   0.0206   1.0000
  11.000   0.9983   0.02815   0.02085   0.0264   0.0193   1.0000
  11.250   1.0030   0.02957   0.02238   0.0278   0.0178   1.0000
  11.500   1.0055   0.03128   0.02420   0.0290   0.0168   1.0000
  11.750   1.0065   0.03328   0.02627   0.0298   0.0160   1.0000
  12.000   1.0056   0.03562   0.02869   0.0302   0.0155   1.0000
  12.250   1.0030   0.03829   0.03147   0.0304   0.0149   1.0000
  12.500   1.0036   0.04080   0.03411   0.0303   0.0145   1.0000
  12.750   1.0032   0.04352   0.03695   0.0300   0.0141   1.0000
  13.000   1.0016   0.04649   0.04004   0.0295   0.0135   1.0000
  13.250   1.0001   0.04953   0.04319   0.0288   0.0133   1.0000
  13.500   0.9976   0.05279   0.04656   0.0280   0.0130   1.0000
  13.750   0.9947   0.05620   0.05007   0.0269   0.0126   1.0000
  14.000   0.9916   0.05972   0.05369   0.0258   0.0124   1.0000
  14.250   0.9874   0.06347   0.05752   0.0243   0.0120   1.0000
  14.500   0.9835   0.06731   0.06145   0.0228   0.0118   1.0000
  14.750   0.9783   0.07143   0.06568   0.0211   0.0116   1.0000
  15.000   0.9732   0.07564   0.06997   0.0193   0.0113   1.0000
  15.250   0.9685   0.07998   0.07443   0.0175   0.0112   1.0000
  15.500   0.9632   0.08469   0.07930   0.0152   0.0109   1.0000
  15.750   0.9577   0.08944   0.08419   0.0130   0.0108   1.0000
  16.000   0.9506   0.09470   0.08959   0.0103   0.0106   1.0000
  16.250   0.9422   0.10039   0.09545   0.0072   0.0102   1.0000
  16.500   0.9334   0.10623   0.10143   0.0042   0.0101   1.0000
  16.750   0.9242   0.11230   0.10763   0.0010   0.0100   1.0000
  17.000   0.9141   0.11874   0.11421  -0.0025   0.0100   1.0000
  17.250   0.9024   0.12570   0.12131  -0.0064   0.0100   1.0000
  17.500   0.8894   0.13323   0.12899  -0.0106   0.0100   1.0000
  17.750   0.8725   0.14207   0.13798  -0.0157   0.0100   1.0000
  18.000   0.8515   0.15239   0.14846  -0.0215   0.0101   1.0000
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