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DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il)
Reynolds number: 200,000
Max Cl/Cd: 71.65 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-du84132v-il-200000.txt
Download as CSV file: xf-du84132v-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: DELFT DU84-132V3 AIRFOIL (MEASURED)             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.250  -0.3730   0.09993   0.09667  -0.0451   1.0000   0.0762
 -10.000  -0.3758   0.09606   0.09285  -0.0433   1.0000   0.0769
  -9.750  -0.4864   0.08990   0.08647  -0.0547   1.0000   0.0762
  -9.500  -0.4601   0.08887   0.08550  -0.0487   1.0000   0.0772
  -9.250  -0.4521   0.08822   0.08487  -0.0448   1.0000   0.0779
  -9.000  -0.4543   0.08676   0.08345  -0.0422   1.0000   0.0786
  -8.750  -0.4626   0.08487   0.08161  -0.0402   1.0000   0.0793
  -8.500  -0.4774   0.08255   0.07936  -0.0387   1.0000   0.0801
  -8.250  -0.4745   0.07671   0.07351  -0.0463   0.9951   0.0823
  -8.000  -0.5264   0.06131   0.05737  -0.0693   0.9752   0.0892
  -7.750  -0.4976   0.05820   0.05444  -0.0704   0.9723   0.0907
  -7.500  -0.4684   0.05572   0.05196  -0.0729   0.9690   0.0928
  -7.250  -0.4518   0.05259   0.04867  -0.0753   0.9618   0.0973
  -7.000  -0.4186   0.02307   0.01731  -0.0814   0.9430   0.0577
  -6.750  -0.4247   0.03288   0.02668  -0.0811   0.9482   0.0535
  -6.250  -0.3617   0.02785   0.02063  -0.0833   0.9398   0.0472
  -6.000  -0.3245   0.02597   0.01853  -0.0855   0.9377   0.0469
  -5.750  -0.3012   0.02475   0.01715  -0.0848   0.9306   0.0467
  -5.500  -0.2672   0.02349   0.01574  -0.0861   0.9267   0.0469
  -5.250  -0.2295   0.02237   0.01449  -0.0879   0.9241   0.0472
  -5.000  -0.1893   0.02144   0.01345  -0.0902   0.9222   0.0479
  -4.750  -0.1681   0.02030   0.01240  -0.0892   0.9145   0.0495
  -4.500  -0.1335   0.01940   0.01157  -0.0906   0.9107   0.0516
  -4.250  -0.0943   0.01853   0.01071  -0.0929   0.9083   0.0541
  -4.000  -0.0529   0.01759   0.00977  -0.0956   0.9066   0.0570
  -3.750  -0.0291   0.01690   0.00913  -0.0951   0.8987   0.0616
  -3.500   0.0086   0.01600   0.00828  -0.0971   0.8944   0.0769
  -3.250   0.0465   0.01421   0.00740  -0.1001   0.8913   0.2559
  -3.000   0.0774   0.01323   0.00706  -0.1012   0.8850   0.4121
  -2.750   0.1071   0.01256   0.00682  -0.1015   0.8780   0.5191
  -2.500   0.1395   0.01234   0.00716  -0.1011   0.8739   0.6423
  -2.250   0.1646   0.01256   0.00738  -0.0998   0.8649   0.6883
  -2.000   0.1989   0.01277   0.00753  -0.1000   0.8592   0.7213
  -1.750   0.2262   0.01310   0.00780  -0.0989   0.8510   0.7420
  -1.500   0.2559   0.01330   0.00794  -0.0982   0.8436   0.7576
  -1.250   0.2809   0.01348   0.00807  -0.0968   0.8344   0.7712
  -1.000   0.3106   0.01354   0.00804  -0.0964   0.8264   0.7844
  -0.750   0.3324   0.01361   0.00807  -0.0945   0.8155   0.7957
  -0.500   0.3581   0.01355   0.00796  -0.0932   0.8067   0.8058
  -0.250   0.3830   0.01348   0.00783  -0.0921   0.7968   0.8162
   0.000   0.4056   0.01347   0.00778  -0.0906   0.7865   0.8280
   0.250   0.4272   0.01334   0.00762  -0.0884   0.7780   0.8408
   0.500   0.4466   0.01318   0.00744  -0.0859   0.7677   0.8537
   0.750   0.4676   0.01303   0.00723  -0.0838   0.7574   0.8654
   1.000   0.4921   0.01294   0.00707  -0.0828   0.7469   0.8752
   1.250   0.5142   0.01281   0.00690  -0.0812   0.7359   0.8822
   1.500   0.5402   0.01276   0.00678  -0.0808   0.7246   0.8879
   1.750   0.5639   0.01266   0.00666  -0.0798   0.7142   0.8926
   2.000   0.5888   0.01261   0.00657  -0.0791   0.7042   0.8975
   2.250   0.6157   0.01261   0.00652  -0.0790   0.6939   0.9015
   2.500   0.6409   0.01258   0.00645  -0.0785   0.6817   0.9056
   2.750   0.6634   0.01246   0.00630  -0.0772   0.6698   0.9107
   3.000   0.6861   0.01243   0.00624  -0.0760   0.6573   0.9171
   3.250   0.7081   0.01239   0.00618  -0.0748   0.6435   0.9225
   3.500   0.7303   0.01233   0.00611  -0.0736   0.6297   0.9277
   3.750   0.7542   0.01234   0.00607  -0.0728   0.6156   0.9325
   4.000   0.7778   0.01238   0.00608  -0.0720   0.5998   0.9364
   4.250   0.8008   0.01240   0.00605  -0.0710   0.5822   0.9401
   4.500   0.8249   0.01249   0.00605  -0.0704   0.5640   0.9436
   4.750   0.8479   0.01262   0.00613  -0.0696   0.5444   0.9471
   5.000   0.8714   0.01276   0.00625  -0.0689   0.5256   0.9502
   5.250   0.8958   0.01293   0.00639  -0.0685   0.5074   0.9539
   5.500   0.9207   0.01314   0.00657  -0.0682   0.4886   0.9580
   5.750   0.9455   0.01335   0.00679  -0.0679   0.4674   0.9623
   6.000   0.9712   0.01359   0.00699  -0.0679   0.4449   0.9675
   6.250   0.9981   0.01393   0.00726  -0.0682   0.4243   0.9750
   6.500   1.0224   0.01430   0.00754  -0.0681   0.4038   1.0000
   6.750   1.0429   0.01477   0.00789  -0.0672   0.3876   1.0000
   7.000   1.0648   0.01524   0.00830  -0.0666   0.3726   1.0000
   7.250   1.0875   0.01566   0.00874  -0.0662   0.3596   1.0000
   7.500   1.1095   0.01608   0.00916  -0.0656   0.3475   1.0000
   7.750   1.1301   0.01652   0.00959  -0.0647   0.3352   1.0000
   8.000   1.1505   0.01692   0.01002  -0.0638   0.3225   1.0000
   8.250   1.1699   0.01738   0.01050  -0.0628   0.3099   1.0000
   8.500   1.1878   0.01789   0.01101  -0.0616   0.2964   1.0000
   8.750   1.2047   0.01843   0.01155  -0.0602   0.2815   1.0000
   9.000   1.2195   0.01903   0.01214  -0.0586   0.2641   1.0000
   9.250   1.2325   0.01974   0.01282  -0.0567   0.2461   1.0000
   9.500   1.2455   0.02046   0.01354  -0.0550   0.2225   1.0000
   9.750   1.2541   0.02142   0.01436  -0.0527   0.1951   1.0000
  10.000   1.2617   0.02255   0.01537  -0.0505   0.1700   1.0000
  10.250   1.2671   0.02387   0.01655  -0.0483   0.1533   1.0000
  10.500   1.2732   0.02524   0.01786  -0.0462   0.1431   1.0000
  10.750   1.2795   0.02665   0.01925  -0.0442   0.1355   1.0000
  11.000   1.2891   0.02790   0.02055  -0.0426   0.1280   1.0000
  11.250   1.2979   0.02924   0.02192  -0.0411   0.1217   1.0000
  11.500   1.3089   0.03043   0.02319  -0.0399   0.1146   1.0000
  11.750   1.3171   0.03185   0.02464  -0.0386   0.1086   1.0000
  12.000   1.3246   0.03335   0.02617  -0.0373   0.1027   1.0000
  12.250   1.3284   0.03522   0.02802  -0.0358   0.0973   1.0000
  12.500   1.3346   0.03697   0.02986  -0.0346   0.0919   1.0000
  12.750   1.3356   0.03926   0.03208  -0.0333   0.0867   1.0000
  13.000   1.3419   0.04113   0.03410  -0.0323   0.0822   1.0000
  13.250   1.3464   0.04317   0.03622  -0.0314   0.0777   1.0000
  13.500   1.3498   0.04558   0.03853  -0.0304   0.0731   1.0000
  13.750   1.3542   0.04768   0.04087  -0.0298   0.0696   1.0000
  14.000   1.3584   0.04991   0.04318  -0.0293   0.0660   1.0000
  14.250   1.3617   0.05232   0.04557  -0.0288   0.0630   1.0000
  14.500   1.3662   0.05474   0.04811  -0.0284   0.0601   1.0000
  14.750   1.3697   0.05721   0.05073  -0.0282   0.0574   1.0000
  15.000   1.3729   0.05975   0.05335  -0.0282   0.0552   1.0000
  15.250   1.3759   0.06238   0.05598  -0.0283   0.0533   1.0000
  15.500   1.3792   0.06513   0.05884  -0.0283   0.0514   1.0000
  15.750   1.3801   0.06817   0.06205  -0.0286   0.0496   1.0000
  16.000   1.3807   0.07129   0.06526  -0.0293   0.0478   1.0000
  16.250   1.3805   0.07453   0.06854  -0.0302   0.0462   1.0000
  16.500   1.3822   0.07761   0.07162  -0.0307   0.0444   1.0000
  16.750   1.3795   0.08146   0.07567  -0.0318   0.0430   1.0000
  17.000   1.3779   0.08521   0.07956  -0.0329   0.0417   1.0000
  17.250   1.3778   0.08874   0.08317  -0.0340   0.0404   1.0000
  17.500   1.3803   0.09183   0.08624  -0.0348   0.0390   1.0000
  17.750   1.3807   0.09538   0.08989  -0.0355   0.0377   1.0000
  18.000   1.3730   0.10035   0.09509  -0.0377   0.0368   1.0000
  18.250   1.3667   0.10519   0.10012  -0.0397   0.0359   1.0000
  18.500   1.3607   0.11003   0.10512  -0.0420   0.0349   1.0000
  18.750   1.3591   0.11407   0.10922  -0.0439   0.0338   1.0000
  19.000   1.3687   0.11588   0.11092  -0.0439   0.0321   1.0000
  19.250   1.3521   0.12285   0.11817  -0.0480   0.0316   1.0000
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