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S1048 14% (Danny Howell) (s1048-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: S1048 14% (Danny Howell) (s1048-il)
Reynolds number: 100,000
Max Cl/Cd: 41.61 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1048-il-100000-n5.txt
Download as CSV file: xf-s1048-il-100000-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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8295   0.12513   0.11958   0.0030   1.0000   0.0201
 -16.000  -0.8463   0.11674   0.11104  -0.0018   1.0000   0.0201
 -15.750  -0.8621   0.10892   0.10304  -0.0064   1.0000   0.0201
 -15.500  -0.8734   0.10248   0.09647  -0.0099   1.0000   0.0203
 -15.250  -0.8800   0.09737   0.09131  -0.0125   1.0000   0.0209
 -15.000  -0.8883   0.09188   0.08570  -0.0153   1.0000   0.0211
 -14.750  -0.8953   0.08683   0.08053  -0.0178   1.0000   0.0214
 -14.500  -0.9022   0.08201   0.07562  -0.0203   1.0000   0.0220
 -14.250  -0.9083   0.07744   0.07091  -0.0224   1.0000   0.0225
 -14.000  -0.9138   0.07312   0.06646  -0.0243   1.0000   0.0231
 -13.750  -0.9187   0.06902   0.06221  -0.0259   1.0000   0.0239
 -13.500  -0.9211   0.06536   0.05840  -0.0270   1.0000   0.0246
 -13.250  -0.9231   0.06185   0.05470  -0.0279   1.0000   0.0255
 -13.000  -0.9224   0.05880   0.05149  -0.0284   1.0000   0.0262
 -12.750  -0.9227   0.05577   0.04838  -0.0288   1.0000   0.0270
 -12.500  -0.9263   0.05246   0.04503  -0.0294   1.0000   0.0281
 -12.250  -0.9278   0.04948   0.04197  -0.0299   1.0000   0.0291
 -12.000  -0.9290   0.04659   0.03899  -0.0303   1.0000   0.0308
 -11.750  -0.9287   0.04398   0.03624  -0.0305   1.0000   0.0330
 -11.500  -0.9272   0.04159   0.03368  -0.0302   1.0000   0.0349
 -11.250  -0.9318   0.03884   0.03090  -0.0299   1.0000   0.0369
 -11.000  -0.9328   0.03656   0.02855  -0.0292   1.0000   0.0396
 -10.750  -0.9316   0.03461   0.02648  -0.0281   1.0000   0.0429
 -10.500  -0.9333   0.03266   0.02449  -0.0265   1.0000   0.0467
 -10.250  -0.9333   0.03100   0.02278  -0.0244   1.0000   0.0518
 -10.000  -0.9333   0.02949   0.02125  -0.0218   1.0000   0.0575
  -9.750  -0.9298   0.02815   0.01986  -0.0192   1.0000   0.0664
  -9.500  -0.9242   0.02677   0.01853  -0.0170   1.0000   0.0783
  -9.250  -0.9162   0.02550   0.01731  -0.0149   1.0000   0.0931
  -9.000  -0.9063   0.02433   0.01621  -0.0130   1.0000   0.1114
  -8.750  -0.8937   0.02332   0.01522  -0.0113   1.0000   0.1327
  -8.500  -0.8806   0.02238   0.01435  -0.0096   1.0000   0.1561
  -8.250  -0.8663   0.02154   0.01360  -0.0080   1.0000   0.1811
  -8.000  -0.8507   0.02082   0.01294  -0.0064   1.0000   0.2062
  -7.750  -0.8338   0.02022   0.01234  -0.0049   1.0000   0.2300
  -7.500  -0.8165   0.01966   0.01182  -0.0034   1.0000   0.2499
  -7.250  -0.7983   0.01919   0.01131  -0.0020   1.0000   0.2693
  -7.000  -0.7797   0.01876   0.01085  -0.0005   1.0000   0.2881
  -6.750  -0.7614   0.01837   0.01046   0.0010   1.0000   0.3058
  -6.500  -0.7428   0.01801   0.01010   0.0025   1.0000   0.3223
  -6.250  -0.7240   0.01769   0.00975   0.0039   1.0000   0.3382
  -6.000  -0.7055   0.01739   0.00942   0.0054   1.0000   0.3533
  -5.750  -0.6874   0.01712   0.00913   0.0070   1.0000   0.3676
  -5.500  -0.6701   0.01688   0.00888   0.0087   1.0000   0.3815
  -5.250  -0.6377   0.01666   0.00862   0.0073   0.9917   0.3978
  -5.000  -0.5993   0.01644   0.00835   0.0049   0.9786   0.4146
  -4.750  -0.5610   0.01623   0.00807   0.0026   0.9655   0.4308
  -4.500  -0.5227   0.01602   0.00782   0.0004   0.9527   0.4462
  -4.250  -0.4853   0.01582   0.00759  -0.0016   0.9391   0.4613
  -4.000  -0.4489   0.01564   0.00735  -0.0033   0.9248   0.4757
  -3.750  -0.4140   0.01547   0.00715  -0.0046   0.9097   0.4897
  -3.500  -0.3810   0.01532   0.00697  -0.0054   0.8937   0.5032
  -3.250  -0.3498   0.01519   0.00679  -0.0059   0.8773   0.5164
  -3.000  -0.3201   0.01507   0.00663  -0.0060   0.8608   0.5293
  -2.750  -0.2918   0.01497   0.00649  -0.0059   0.8443   0.5422
  -2.500  -0.2643   0.01488   0.00635  -0.0055   0.8282   0.5551
  -2.250  -0.2374   0.01481   0.00622  -0.0051   0.8124   0.5681
  -2.000  -0.2108   0.01475   0.00612  -0.0045   0.7970   0.5809
  -1.750  -0.1841   0.01470   0.00605  -0.0040   0.7820   0.5933
  -1.500  -0.1576   0.01465   0.00598  -0.0035   0.7673   0.6058
  -1.250  -0.1312   0.01461   0.00593  -0.0029   0.7528   0.6186
  -1.000  -0.1048   0.01458   0.00587  -0.0023   0.7387   0.6315
  -0.750  -0.0786   0.01456   0.00583  -0.0018   0.7248   0.6447
  -0.500  -0.0524   0.01455   0.00579  -0.0012   0.7112   0.6580
  -0.250  -0.0262   0.01454   0.00577  -0.0006   0.6978   0.6716
   0.000   0.0000   0.01454   0.00576   0.0000   0.6847   0.6846
   0.250   0.0262   0.01454   0.00577   0.0006   0.6716   0.6978
   0.500   0.0524   0.01455   0.00579   0.0012   0.6580   0.7112
   0.750   0.0786   0.01456   0.00583   0.0018   0.6447   0.7248
   1.000   0.1048   0.01458   0.00587   0.0023   0.6315   0.7387
   1.250   0.1312   0.01461   0.00593   0.0029   0.6186   0.7529
   1.500   0.1576   0.01465   0.00598   0.0035   0.6058   0.7673
   1.750   0.1841   0.01470   0.00605   0.0040   0.5932   0.7820
   2.000   0.2108   0.01475   0.00612   0.0045   0.5809   0.7971
   2.250   0.2374   0.01481   0.00622   0.0051   0.5681   0.8125
   2.500   0.2643   0.01488   0.00635   0.0055   0.5551   0.8283
   2.750   0.2918   0.01497   0.00649   0.0059   0.5422   0.8443
   3.000   0.3201   0.01507   0.00663   0.0060   0.5293   0.8608
   3.250   0.3498   0.01519   0.00679   0.0059   0.5164   0.8773
   3.500   0.3810   0.01532   0.00697   0.0054   0.5032   0.8937
   3.750   0.4140   0.01547   0.00715   0.0046   0.4897   0.9097
   4.000   0.4488   0.01564   0.00735   0.0033   0.4756   0.9248
   4.250   0.4853   0.01582   0.00759   0.0016   0.4612   0.9392
   4.500   0.5227   0.01602   0.00782  -0.0004   0.4463   0.9526
   4.750   0.5610   0.01623   0.00807  -0.0026   0.4307   0.9655
   5.000   0.5993   0.01644   0.00835  -0.0049   0.4147   0.9786
   5.250   0.6377   0.01665   0.00862  -0.0073   0.3978   0.9917
   5.500   0.6701   0.01688   0.00888  -0.0087   0.3814   1.0000
   5.750   0.6874   0.01712   0.00913  -0.0070   0.3676   1.0000
   6.000   0.7055   0.01739   0.00942  -0.0054   0.3532   1.0000
   6.250   0.7241   0.01769   0.00976  -0.0039   0.3382   1.0000
   6.500   0.7428   0.01801   0.01010  -0.0025   0.3223   1.0000
   6.750   0.7614   0.01837   0.01046  -0.0010   0.3056   1.0000
   7.000   0.7798   0.01876   0.01085   0.0005   0.2881   1.0000
   7.250   0.7984   0.01919   0.01131   0.0020   0.2694   1.0000
   7.500   0.8166   0.01966   0.01182   0.0034   0.2499   1.0000
   7.750   0.8338   0.02022   0.01234   0.0049   0.2300   1.0000
   8.000   0.8507   0.02082   0.01294   0.0064   0.2062   1.0000
   8.250   0.8662   0.02154   0.01360   0.0080   0.1811   1.0000
   8.500   0.8805   0.02238   0.01435   0.0096   0.1560   1.0000
   8.750   0.8936   0.02332   0.01522   0.0113   0.1325   1.0000
   9.000   0.9063   0.02433   0.01621   0.0130   0.1112   1.0000
   9.250   0.9162   0.02550   0.01730   0.0149   0.0932   1.0000
   9.500   0.9242   0.02677   0.01853   0.0170   0.0784   1.0000
   9.750   0.9297   0.02815   0.01986   0.0193   0.0665   1.0000
  10.000   0.9332   0.02950   0.02125   0.0218   0.0574   1.0000
  10.250   0.9333   0.03100   0.02279   0.0244   0.0519   1.0000
  10.500   0.9334   0.03266   0.02450   0.0265   0.0468   1.0000
  10.750   0.9318   0.03462   0.02648   0.0281   0.0433   1.0000
  11.000   0.9331   0.03656   0.02855   0.0292   0.0396   1.0000
  11.250   0.9324   0.03881   0.03087   0.0299   0.0370   1.0000
  11.500   0.9275   0.04159   0.03367   0.0302   0.0348   1.0000
  11.750   0.9296   0.04394   0.03621   0.0303   0.0325   1.0000
  12.000   0.9299   0.04654   0.03893   0.0303   0.0309   1.0000
  12.250   0.9282   0.04947   0.04195   0.0298   0.0289   1.0000
  12.500   0.9267   0.05247   0.04503   0.0293   0.0280   1.0000
  12.750   0.9246   0.05561   0.04823   0.0287   0.0271   1.0000
  13.000   0.9231   0.05878   0.05148   0.0284   0.0261   1.0000
  13.250   0.9237   0.06186   0.05473   0.0278   0.0254   1.0000
  13.500   0.9224   0.06528   0.05831   0.0270   0.0246   1.0000
  13.750   0.9189   0.06910   0.06229   0.0257   0.0237   1.0000
  14.000   0.9147   0.07310   0.06643   0.0242   0.0230   1.0000
  14.250   0.9089   0.07745   0.07091   0.0222   0.0223   1.0000
  14.500   0.9033   0.08196   0.07556   0.0202   0.0219   1.0000
  14.750   0.8966   0.08675   0.08044   0.0177   0.0213   1.0000
  15.000   0.8893   0.09188   0.08572   0.0152   0.0212   1.0000
  15.250   0.8819   0.09714   0.09106   0.0125   0.0207   1.0000
  15.500   0.8738   0.10264   0.09665   0.0097   0.0204   1.0000
  15.750   0.8630   0.10896   0.10308   0.0062   0.0201   1.0000
  16.000   0.8472   0.11681   0.11111   0.0017   0.0201   1.0000
  16.250   0.8293   0.12549   0.11995  -0.0034   0.0201   1.0000
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