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SD7003-085-88 (sd7003-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: SD7003-085-88 (sd7003-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.15 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7003-il-1000000-n5.txt
Download as CSV file: xf-sd7003-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7003-085-88                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.8200   0.09509   0.09314  -0.0049   1.0000   0.0040
 -13.250  -0.9124   0.07343   0.07139  -0.0184   1.0000   0.0037
 -13.000  -1.0534   0.03891   0.03636  -0.0466   1.0000   0.0034
 -12.750  -1.0731   0.03525   0.03251  -0.0463   1.0000   0.0034
 -12.500  -1.0751   0.03229   0.02935  -0.0460   1.0000   0.0034
 -12.250  -1.0699   0.02981   0.02667  -0.0455   1.0000   0.0034
 -12.000  -1.0582   0.02796   0.02466  -0.0450   1.0000   0.0035
 -11.750  -1.0448   0.02615   0.02267  -0.0444   1.0000   0.0036
 -11.500  -1.0291   0.02457   0.02092  -0.0438   1.0000   0.0036
 -11.250  -1.0113   0.02319   0.01938  -0.0433   1.0000   0.0037
 -11.000  -0.9922   0.02194   0.01799  -0.0427   1.0000   0.0038
 -10.750  -0.9718   0.02085   0.01676  -0.0422   1.0000   0.0039
 -10.500  -0.9511   0.01975   0.01551  -0.0417   1.0000   0.0040
 -10.250  -0.9293   0.01882   0.01446  -0.0412   1.0000   0.0041
 -10.000  -0.9070   0.01798   0.01350  -0.0406   1.0000   0.0042
  -9.750  -0.8842   0.01718   0.01259  -0.0401   1.0000   0.0043
  -9.500  -0.8612   0.01643   0.01174  -0.0396   1.0000   0.0043
  -9.250  -0.8376   0.01578   0.01099  -0.0390   1.0000   0.0044
  -9.000  -0.8144   0.01505   0.01015  -0.0384   1.0000   0.0045
  -8.750  -0.7916   0.01419   0.00918  -0.0378   1.0000   0.0047
  -8.500  -0.7680   0.01354   0.00846  -0.0371   1.0000   0.0049
  -8.250  -0.7441   0.01298   0.00783  -0.0365   1.0000   0.0051
  -8.000  -0.7199   0.01249   0.00729  -0.0359   1.0000   0.0054
  -7.750  -0.6955   0.01204   0.00678  -0.0352   1.0000   0.0056
  -7.500  -0.6711   0.01163   0.00632  -0.0346   1.0000   0.0059
  -7.250  -0.6465   0.01124   0.00588  -0.0340   1.0000   0.0062
  -7.000  -0.6219   0.01088   0.00548  -0.0333   1.0000   0.0065
  -6.750  -0.5966   0.01049   0.00505  -0.0328   0.9998   0.0071
  -6.500  -0.5636   0.01009   0.00463  -0.0340   0.9976   0.0081
  -6.250  -0.5303   0.00976   0.00427  -0.0352   0.9951   0.0092
  -6.000  -0.4981   0.00942   0.00393  -0.0362   0.9919   0.0110
  -5.750  -0.4655   0.00913   0.00363  -0.0372   0.9879   0.0133
  -5.250  -0.4003   0.00858   0.00308  -0.0392   0.9764   0.0191
  -5.000  -0.3672   0.00834   0.00285  -0.0403   0.9677   0.0224
  -4.750  -0.3342   0.00808   0.00261  -0.0413   0.9535   0.0277
  -4.500  -0.3024   0.00788   0.00239  -0.0420   0.9302   0.0326
  -4.250  -0.2750   0.00777   0.00220  -0.0416   0.8986   0.0377
  -4.000  -0.2491   0.00767   0.00203  -0.0410   0.8658   0.0454
  -3.750  -0.2229   0.00762   0.00187  -0.0404   0.8338   0.0516
  -3.500  -0.1965   0.00756   0.00172  -0.0400   0.8035   0.0577
  -3.250  -0.1697   0.00752   0.00159  -0.0396   0.7746   0.0642
  -3.000  -0.1427   0.00748   0.00147  -0.0393   0.7473   0.0726
  -2.750  -0.1156   0.00741   0.00135  -0.0390   0.7212   0.0847
  -2.500  -0.0883   0.00734   0.00125  -0.0388   0.6957   0.1012
  -2.250  -0.0610   0.00726   0.00115  -0.0386   0.6707   0.1209
  -2.000  -0.0337   0.00720   0.00106  -0.0384   0.6457   0.1434
  -1.500   0.0212   0.00705   0.00093  -0.0382   0.5966   0.1991
  -1.250   0.0486   0.00697   0.00088  -0.0381   0.5718   0.2363
  -1.000   0.0761   0.00691   0.00083  -0.0379   0.5472   0.2706
  -0.750   0.1037   0.00687   0.00080  -0.0378   0.5235   0.3034
  -0.500   0.1312   0.00681   0.00079  -0.0378   0.5007   0.3443
  -0.250   0.1586   0.00669   0.00077  -0.0377   0.4795   0.4061
   0.000   0.1859   0.00659   0.00078  -0.0376   0.4573   0.4657
   0.250   0.2132   0.00649   0.00079  -0.0375   0.4364   0.5301
   0.500   0.2406   0.00641   0.00082  -0.0374   0.4157   0.5888
   0.750   0.2678   0.00638   0.00086  -0.0372   0.3948   0.6417
   1.000   0.2951   0.00637   0.00092  -0.0370   0.3753   0.6870
   1.250   0.3224   0.00640   0.00098  -0.0368   0.3549   0.7249
   1.500   0.3495   0.00645   0.00104  -0.0365   0.3352   0.7561
   1.750   0.3766   0.00651   0.00112  -0.0362   0.3170   0.7846
   2.000   0.4035   0.00657   0.00120  -0.0359   0.2979   0.8123
   2.250   0.4301   0.00665   0.00128  -0.0355   0.2804   0.8405
   2.500   0.4560   0.00673   0.00138  -0.0349   0.2623   0.8700
   2.750   0.4811   0.00679   0.00147  -0.0342   0.2475   0.9009
   3.000   0.5055   0.00685   0.00156  -0.0332   0.2329   0.9361
   3.250   0.5370   0.00696   0.00165  -0.0338   0.2157   0.9769
   3.500   0.5686   0.00713   0.00175  -0.0346   0.2016   1.0000
   3.750   0.5959   0.00732   0.00188  -0.0345   0.1862   1.0000
   4.000   0.6232   0.00752   0.00202  -0.0344   0.1730   1.0000
   4.250   0.6504   0.00773   0.00216  -0.0342   0.1589   1.0000
   4.500   0.6776   0.00794   0.00232  -0.0341   0.1463   1.0000
   4.750   0.7047   0.00817   0.00249  -0.0339   0.1335   1.0000
   5.000   0.7318   0.00838   0.00267  -0.0337   0.1233   1.0000
   5.250   0.7590   0.00858   0.00284  -0.0336   0.1148   1.0000
   5.500   0.7858   0.00884   0.00305  -0.0334   0.1034   1.0000
   5.750   0.8124   0.00912   0.00328  -0.0332   0.0911   1.0000
   6.000   0.8388   0.00943   0.00352  -0.0330   0.0785   1.0000
   6.250   0.8653   0.00973   0.00378  -0.0327   0.0688   1.0000
   6.500   0.8918   0.01001   0.00404  -0.0325   0.0614   1.0000
   6.750   0.9182   0.01030   0.00431  -0.0323   0.0549   1.0000
   7.000   0.9443   0.01064   0.00461  -0.0320   0.0475   1.0000
   7.250   0.9704   0.01095   0.00491  -0.0318   0.0416   1.0000
   7.500   0.9963   0.01131   0.00526  -0.0315   0.0356   1.0000
   7.750   1.0218   0.01170   0.00562  -0.0312   0.0298   1.0000
   8.000   1.0474   0.01207   0.00599  -0.0309   0.0254   1.0000
   8.250   1.0726   0.01250   0.00640  -0.0305   0.0208   1.0000
   8.500   1.0974   0.01296   0.00686  -0.0301   0.0171   1.0000
   8.750   1.1226   0.01336   0.00729  -0.0297   0.0152   1.0000
   9.000   1.1472   0.01383   0.00777  -0.0293   0.0135   1.0000
   9.250   1.1717   0.01430   0.00828  -0.0289   0.0122   1.0000
   9.500   1.1963   0.01473   0.00875  -0.0285   0.0116   1.0000
   9.750   1.2205   0.01520   0.00928  -0.0280   0.0110   1.0000
  10.000   1.2442   0.01572   0.00984  -0.0275   0.0104   1.0000
  10.250   1.2674   0.01630   0.01046  -0.0270   0.0098   1.0000
  10.500   1.2896   0.01697   0.01120  -0.0263   0.0092   1.0000
  10.750   1.3126   0.01751   0.01179  -0.0257   0.0089   1.0000
  11.000   1.3352   0.01806   0.01242  -0.0251   0.0086   1.0000
  11.250   1.3574   0.01864   0.01307  -0.0245   0.0083   1.0000
  11.500   1.3791   0.01924   0.01374  -0.0238   0.0079   1.0000
  11.750   1.4000   0.01990   0.01445  -0.0231   0.0075   1.0000
  12.000   1.4199   0.02063   0.01525  -0.0222   0.0072   1.0000
  12.250   1.4388   0.02143   0.01612  -0.0213   0.0069   1.0000
  12.500   1.4554   0.02241   0.01719  -0.0201   0.0066   1.0000
  12.750   1.4718   0.02333   0.01820  -0.0189   0.0064   1.0000
  13.000   1.4890   0.02410   0.01906  -0.0178   0.0062   1.0000
  13.250   1.5048   0.02492   0.01997  -0.0166   0.0060   1.0000
  13.500   1.5189   0.02579   0.02092  -0.0152   0.0058   1.0000
  13.750   1.5301   0.02671   0.02192  -0.0134   0.0056   1.0000
  14.000   1.5359   0.02771   0.02301  -0.0109   0.0054   1.0000
  14.250   1.5398   0.02887   0.02426  -0.0085   0.0053   1.0000
  14.500   1.5416   0.03028   0.02577  -0.0064   0.0051   1.0000
  14.750   1.5423   0.03196   0.02754  -0.0047   0.0050   1.0000
  15.000   1.5399   0.03412   0.02981  -0.0036   0.0049   1.0000
  15.250   1.5373   0.03663   0.03242  -0.0033   0.0047   1.0000
  15.500   1.5309   0.03992   0.03583  -0.0037   0.0046   1.0000
  15.750   1.5228   0.04387   0.03990  -0.0050   0.0045   1.0000
  16.000   1.5095   0.04898   0.04518  -0.0073   0.0045   1.0000
  16.250   1.4925   0.05522   0.05158  -0.0107   0.0044   1.0000
  16.500   1.4720   0.06245   0.05896  -0.0148   0.0044   1.0000
  16.750   1.4457   0.07104   0.06772  -0.0199   0.0044   1.0000
  17.000   1.4179   0.08020   0.07705  -0.0252   0.0045   1.0000
  17.250   1.3834   0.09087   0.08789  -0.0314   0.0046   1.0000
  17.500   1.3467   0.10236   0.09955  -0.0381   0.0047   1.0000
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