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SD7032-099-88 (sd7032-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: SD7032-099-88 (sd7032-il)
Reynolds number: 50,000
Max Cl/Cd: 39.85 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7032-il-50000-n5.txt
Download as CSV file: xf-sd7032-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7032-099-88                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.250  -0.3334   0.10082   0.09428  -0.0349   1.0000   0.1094
  -8.000  -0.3313   0.09418   0.08761  -0.0366   1.0000   0.0603
  -7.750  -0.3385   0.09133   0.08488  -0.0362   1.0000   0.0572
  -7.500  -0.3650   0.08812   0.08185  -0.0383   1.0000   0.0519
  -7.250  -0.3655   0.08562   0.07943  -0.0364   1.0000   0.0509
  -7.000  -0.3704   0.08287   0.07676  -0.0357   1.0000   0.0500
  -6.750  -0.3760   0.07990   0.07388  -0.0358   1.0000   0.0491
  -6.500  -0.3808   0.07666   0.07070  -0.0364   1.0000   0.0481
  -6.250  -0.3841   0.07302   0.06709  -0.0376   1.0000   0.0473
  -6.000  -0.3851   0.06906   0.06312  -0.0392   1.0000   0.0465
  -5.750  -0.3829   0.06486   0.05885  -0.0411   1.0000   0.0460
  -5.500  -0.3772   0.06062   0.05450  -0.0431   1.0000   0.0461
  -5.250  -0.3676   0.05637   0.05005  -0.0452   1.0000   0.0465
  -5.000  -0.3541   0.05212   0.04550  -0.0474   1.0000   0.0473
  -4.750  -0.3224   0.04688   0.03975  -0.0528   0.9953   0.0478
  -4.500  -0.2850   0.04192   0.03414  -0.0579   0.9893   0.0480
  -4.250  -0.2456   0.03779   0.02931  -0.0621   0.9838   0.0487
  -4.000  -0.2074   0.03467   0.02532  -0.0650   0.9773   0.0521
  -3.750  -0.1701   0.03238   0.02277  -0.0678   0.9716   0.0562
  -3.500  -0.1351   0.03044   0.02042  -0.0694   0.9645   0.0593
  -3.250  -0.0964   0.02888   0.01841  -0.0714   0.9584   0.0664
  -3.000  -0.0636   0.02763   0.01706  -0.0724   0.9505   0.0730
  -2.750  -0.0259   0.02649   0.01573  -0.0741   0.9439   0.0826
  -2.500   0.0066   0.02563   0.01475  -0.0750   0.9350   0.0981
  -2.250   0.0473   0.02459   0.01374  -0.0775   0.9286   0.1333
  -2.000   0.0794   0.02330   0.01313  -0.0791   0.9192   0.2543
  -1.750   0.1107   0.02194   0.01312  -0.0798   0.9123   0.5485
  -1.500   0.1279   0.02137   0.01316  -0.0759   0.9018   0.7553
  -1.250   0.1691   0.02090   0.01266  -0.0771   0.8921   1.0000
  -1.000   0.2126   0.02098   0.01228  -0.0802   0.8842   1.0000
  -0.750   0.2440   0.02110   0.01207  -0.0810   0.8723   1.0000
  -0.500   0.2760   0.02122   0.01189  -0.0819   0.8607   1.0000
  -0.250   0.3099   0.02130   0.01170  -0.0829   0.8499   1.0000
   0.000   0.3472   0.02130   0.01147  -0.0844   0.8406   1.0000
   0.250   0.3767   0.02139   0.01138  -0.0846   0.8279   1.0000
   0.500   0.4066   0.02148   0.01129  -0.0848   0.8154   1.0000
   0.750   0.4369   0.02154   0.01121  -0.0850   0.8030   1.0000
   1.000   0.4678   0.02157   0.01112  -0.0852   0.7908   1.0000
   1.250   0.4994   0.02157   0.01100  -0.0855   0.7789   1.0000
   1.500   0.5320   0.02151   0.01083  -0.0858   0.7674   1.0000
   1.750   0.5607   0.02156   0.01081  -0.0855   0.7537   1.0000
   2.000   0.5892   0.02162   0.01080  -0.0852   0.7397   1.0000
   2.250   0.6178   0.02167   0.01079  -0.0849   0.7255   1.0000
   2.500   0.6462   0.02173   0.01080  -0.0845   0.7111   1.0000
   2.750   0.6745   0.02180   0.01082  -0.0841   0.6963   1.0000
   3.000   0.7027   0.02188   0.01088  -0.0837   0.6813   1.0000
   3.250   0.7307   0.02198   0.01094  -0.0832   0.6660   1.0000
   3.500   0.7581   0.02212   0.01104  -0.0827   0.6502   1.0000
   3.750   0.7838   0.02235   0.01129  -0.0820   0.6332   1.0000
   4.000   0.8097   0.02258   0.01151  -0.0814   0.6162   1.0000
   4.250   0.8357   0.02283   0.01175  -0.0807   0.5991   1.0000
   4.500   0.8617   0.02309   0.01204  -0.0800   0.5821   1.0000
   4.750   0.8876   0.02337   0.01230  -0.0794   0.5650   1.0000
   5.000   0.9136   0.02367   0.01258  -0.0787   0.5480   1.0000
   5.250   0.9370   0.02410   0.01305  -0.0778   0.5296   1.0000
   5.500   0.9607   0.02453   0.01354  -0.0770   0.5115   1.0000
   5.750   0.9847   0.02497   0.01400  -0.0761   0.4940   1.0000
   6.000   1.0087   0.02542   0.01448  -0.0753   0.4768   1.0000
   6.250   1.0325   0.02591   0.01497  -0.0745   0.4600   1.0000
   6.500   1.0544   0.02651   0.01569  -0.0736   0.4424   1.0000
   6.750   1.0762   0.02712   0.01638  -0.0726   0.4252   1.0000
   7.000   1.0978   0.02776   0.01709  -0.0716   0.4083   1.0000
   7.250   1.1191   0.02843   0.01783  -0.0706   0.3917   1.0000
   7.500   1.1400   0.02913   0.01863  -0.0695   0.3755   1.0000
   7.750   1.1604   0.02985   0.01943  -0.0684   0.3593   1.0000
   8.000   1.1803   0.03062   0.02026  -0.0673   0.3434   1.0000
   8.250   1.1981   0.03148   0.02122  -0.0660   0.3270   1.0000
   8.500   1.2150   0.03239   0.02225  -0.0646   0.3108   1.0000
   8.750   1.2308   0.03333   0.02336  -0.0631   0.2946   1.0000
   9.000   1.2455   0.03433   0.02446  -0.0615   0.2788   1.0000
   9.250   1.2590   0.03538   0.02563  -0.0598   0.2634   1.0000
   9.500   1.2708   0.03649   0.02685  -0.0579   0.2481   1.0000
   9.750   1.2811   0.03769   0.02815  -0.0560   0.2335   1.0000
  10.000   1.2890   0.03897   0.02954  -0.0539   0.2194   1.0000
  10.250   1.2947   0.04035   0.03106  -0.0516   0.2062   1.0000
  10.500   1.2988   0.04188   0.03269  -0.0493   0.1935   1.0000
  10.750   1.3020   0.04355   0.03445  -0.0472   0.1815   1.0000
  11.000   1.3049   0.04535   0.03629  -0.0453   0.1704   1.0000
  11.250   1.3059   0.04737   0.03842  -0.0435   0.1597   1.0000
  11.500   1.3058   0.04974   0.04097  -0.0420   0.1495   1.0000
  11.750   1.3065   0.05217   0.04351  -0.0407   0.1407   1.0000
  12.000   1.3062   0.05463   0.04600  -0.0396   0.1323   1.0000
  12.250   1.3025   0.05779   0.04941  -0.0388   0.1244   1.0000
  12.500   1.3024   0.06048   0.05209  -0.0382   0.1177   1.0000
  12.750   1.2969   0.06426   0.05618  -0.0380   0.1115   1.0000
  13.000   1.2975   0.06701   0.05893  -0.0376   0.1056   1.0000
  13.250   1.2868   0.07176   0.06402  -0.0383   0.1008   1.0000
  13.500   1.2804   0.07585   0.06827  -0.0389   0.0962   1.0000
  13.750   1.2788   0.07943   0.07189  -0.0392   0.0919   1.0000
  14.000   1.2634   0.08553   0.07834  -0.0412   0.0892   1.0000
  14.250   1.2482   0.09178   0.08484  -0.0436   0.0865   1.0000
  14.500   1.2387   0.09708   0.09027  -0.0456   0.0834   1.0000
  14.750   1.2360   0.10122   0.09443  -0.0469   0.0799   1.0000
  15.000   1.2105   0.11042   0.10391  -0.0518   0.0792   1.0000
  15.250   1.1798   0.12156   0.11527  -0.0582   0.0792   1.0000
  15.500   1.1413   0.13589   0.12967  -0.0668   0.0797   1.0000
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