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DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il)
Reynolds number: 1,000,000
Max Cl/Cd: 92.64 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-du84132v-il-1000000.txt
Download as CSV file: xf-du84132v-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.000  -0.3140   0.10015   0.09849  -0.0552   0.9966   0.0251
 -11.750  -0.6422   0.04976   0.04741  -0.0851   0.9972   0.0199
 -11.500  -0.6425   0.04534   0.04275  -0.0919   0.9940   0.0200
 -11.250  -0.6489   0.04068   0.03789  -0.0961   0.9890   0.0200
 -11.000  -0.6534   0.03569   0.03251  -0.1015   0.9823   0.0202
 -10.750  -0.6372   0.03339   0.03004  -0.1033   0.9787   0.0202
 -10.500  -0.6186   0.03178   0.02830  -0.1042   0.9739   0.0201
 -10.250  -0.5996   0.02903   0.02530  -0.1060   0.9708   0.0201
 -10.000  -0.5763   0.02651   0.02255  -0.1080   0.9688   0.0202
  -9.750  -0.5478   0.02468   0.02054  -0.1102   0.9675   0.0202
  -9.500  -0.5280   0.02304   0.01873  -0.1101   0.9615   0.0202
  -9.250  -0.5029   0.02067   0.01625  -0.1111   0.9574   0.0198
  -9.000  -0.4716   0.01943   0.01485  -0.1129   0.9543   0.0198
  -8.750  -0.4428   0.01923   0.01453  -0.1136   0.9485   0.0201
  -8.500  -0.4191   0.01747   0.01260  -0.1138   0.9409   0.0203
  -8.250  -0.3893   0.01661   0.01166  -0.1147   0.9356   0.0202
  -8.000  -0.3642   0.01566   0.01062  -0.1146   0.9280   0.0203
  -7.750  -0.3356   0.01467   0.00954  -0.1152   0.9219   0.0204
  -7.500  -0.3099   0.01414   0.00895  -0.1151   0.9145   0.0203
  -7.250  -0.2827   0.01352   0.00825  -0.1152   0.9073   0.0203
  -7.000  -0.2578   0.01299   0.00768  -0.1149   0.8992   0.0202
  -6.750  -0.2327   0.01239   0.00701  -0.1146   0.8910   0.0202
  -6.500  -0.2090   0.01176   0.00632  -0.1140   0.8828   0.0203
  -6.250  -0.1845   0.01123   0.00573  -0.1136   0.8749   0.0204
  -6.000  -0.1604   0.01067   0.00512  -0.1131   0.8677   0.0207
  -5.750  -0.1352   0.01026   0.00465  -0.1128   0.8602   0.0210
  -5.500  -0.1093   0.00992   0.00425  -0.1125   0.8535   0.0214
  -5.250  -0.0833   0.00963   0.00393  -0.1122   0.8462   0.0217
  -5.000  -0.0568   0.00939   0.00363  -0.1121   0.8394   0.0222
  -4.750  -0.0305   0.00914   0.00337  -0.1118   0.8311   0.0226
  -4.500  -0.0041   0.00894   0.00312  -0.1115   0.8215   0.0230
  -4.250   0.0220   0.00877   0.00289  -0.1111   0.8093   0.0234
  -4.000   0.0482   0.00862   0.00268  -0.1108   0.7966   0.0238
  -3.750   0.0745   0.00848   0.00249  -0.1104   0.7812   0.0242
  -3.250   0.1264   0.00828   0.00213  -0.1095   0.7560   0.0268
  -3.000   0.1531   0.00817   0.00203  -0.1093   0.7463   0.0314
  -2.750   0.1802   0.00808   0.00197  -0.1091   0.7368   0.0453
  -2.250   0.2340   0.00795   0.00178  -0.1087   0.7141   0.0564
  -2.000   0.2606   0.00787   0.00171  -0.1085   0.7035   0.0657
  -1.750   0.2867   0.00756   0.00161  -0.1083   0.6927   0.1394
  -1.500   0.3131   0.00744   0.00155  -0.1081   0.6761   0.1701
  -1.250   0.3384   0.00726   0.00149  -0.1077   0.6615   0.2351
  -0.750   0.3882   0.00681   0.00142  -0.1070   0.6215   0.4074
  -0.500   0.4138   0.00672   0.00141  -0.1067   0.6035   0.4584
  -0.250   0.4389   0.00651   0.00139  -0.1063   0.5827   0.5466
   0.000   0.4631   0.00636   0.00149  -0.1057   0.5665   0.6563
   0.250   0.4892   0.00647   0.00161  -0.1052   0.5519   0.6939
   0.500   0.5159   0.00660   0.00171  -0.1049   0.5390   0.7089
   0.750   0.5426   0.00673   0.00179  -0.1046   0.5270   0.7188
   1.250   0.5961   0.00701   0.00196  -0.1040   0.5041   0.7333
   1.500   0.6222   0.00718   0.00210  -0.1035   0.4935   0.7405
   1.750   0.6484   0.00738   0.00224  -0.1031   0.4802   0.7484
   2.000   0.6744   0.00754   0.00235  -0.1027   0.4518   0.7532
   2.250   0.6977   0.00787   0.00252  -0.1017   0.4180   0.7571
   2.500   0.7207   0.00822   0.00272  -0.1008   0.3878   0.7610
   2.750   0.7452   0.00852   0.00292  -0.1001   0.3694   0.7654
   3.000   0.7699   0.00875   0.00308  -0.0995   0.3514   0.7688
   3.250   0.7944   0.00898   0.00326  -0.0988   0.3311   0.7714
   3.500   0.8183   0.00926   0.00344  -0.0981   0.3106   0.7741
   3.750   0.8429   0.00951   0.00362  -0.0974   0.2973   0.7779
   4.000   0.8674   0.00974   0.00379  -0.0968   0.2829   0.7803
   4.250   0.8920   0.00999   0.00396  -0.0962   0.2690   0.7822
   4.500   0.9162   0.01016   0.00410  -0.0956   0.2599   0.7843
   4.750   0.9407   0.01033   0.00426  -0.0950   0.2526   0.7860
   5.000   0.9650   0.01051   0.00443  -0.0943   0.2452   0.7876
   5.250   0.9894   0.01069   0.00459  -0.0937   0.2368   0.7891
   5.500   1.0126   0.01093   0.00477  -0.0929   0.2196   0.7906
   5.750   1.0325   0.01135   0.00502  -0.0916   0.1899   0.7923
   6.000   1.0485   0.01198   0.00542  -0.0896   0.1493   0.7942
   6.250   1.0690   0.01235   0.00572  -0.0883   0.1392   0.7961
   6.500   1.0910   0.01261   0.00597  -0.0873   0.1308   0.7977
   6.750   1.1107   0.01285   0.00619  -0.0858   0.1218   0.7993
   7.000   1.1256   0.01330   0.00651  -0.0836   0.0978   0.8005
   7.250   1.1445   0.01358   0.00678  -0.0820   0.0924   0.8016
   7.500   1.1629   0.01390   0.00707  -0.0804   0.0868   0.8028
   7.750   1.1830   0.01415   0.00734  -0.0791   0.0844   0.8039
   8.000   1.2021   0.01445   0.00766  -0.0776   0.0813   0.8054
   8.250   1.2204   0.01478   0.00800  -0.0760   0.0784   0.8069
   8.500   1.2385   0.01514   0.00836  -0.0744   0.0750   0.8084
   8.750   1.2574   0.01546   0.00870  -0.0730   0.0732   0.8097
   9.000   1.2772   0.01572   0.00901  -0.0718   0.0722   0.8108
   9.250   1.2963   0.01603   0.00934  -0.0704   0.0707   0.8118
   9.500   1.3145   0.01638   0.00971  -0.0690   0.0682   0.8127
   9.750   1.3312   0.01679   0.01012  -0.0674   0.0653   0.8139
  10.000   1.3473   0.01721   0.01056  -0.0657   0.0622   0.8153
  10.250   1.3651   0.01756   0.01096  -0.0643   0.0600   0.8166
  10.500   1.3795   0.01810   0.01146  -0.0625   0.0526   0.8179
  10.750   1.3919   0.01875   0.01206  -0.0604   0.0451   0.8192
  11.000   1.4040   0.01943   0.01273  -0.0584   0.0424   0.8205
  11.250   1.4158   0.02016   0.01346  -0.0563   0.0402   0.8219
  11.500   1.4276   0.02090   0.01423  -0.0544   0.0381   0.8233
  11.750   1.4413   0.02155   0.01495  -0.0528   0.0369   0.8247
  12.000   1.4526   0.02236   0.01582  -0.0510   0.0354   0.8262
  12.250   1.4606   0.02341   0.01690  -0.0488   0.0335   0.8275
  12.500   1.4708   0.02436   0.01790  -0.0471   0.0319   0.8285
  12.750   1.4853   0.02501   0.01862  -0.0458   0.0304   0.8302
  13.000   1.4971   0.02588   0.01953  -0.0444   0.0282   0.8317
  13.250   1.5067   0.02692   0.02061  -0.0428   0.0263   0.8333
  13.500   1.5161   0.02801   0.02173  -0.0413   0.0244   0.8348
  13.750   1.5240   0.02926   0.02299  -0.0398   0.0229   0.8363
  14.000   1.5317   0.03056   0.02434  -0.0384   0.0220   0.8379
  14.250   1.5384   0.03200   0.02584  -0.0370   0.0212   0.8394
  14.500   1.5442   0.03357   0.02746  -0.0358   0.0205   0.8409
  14.750   1.5487   0.03530   0.02925  -0.0346   0.0199   0.8424
  15.000   1.5511   0.03731   0.03131  -0.0334   0.0190   0.8437
  15.250   1.5533   0.03941   0.03350  -0.0324   0.0185   0.8456
  15.500   1.5592   0.04122   0.03540  -0.0317   0.0182   0.8477
  15.750   1.5628   0.04331   0.03759  -0.0311   0.0179   0.8496
  16.000   1.5661   0.04553   0.03990  -0.0306   0.0173   0.8517
  16.250   1.5673   0.04805   0.04250  -0.0303   0.0169   0.8538
  16.500   1.5668   0.05087   0.04541  -0.0301   0.0164   0.8559
  16.750   1.5652   0.05393   0.04855  -0.0301   0.0160   0.8579
  17.000   1.5603   0.05751   0.05223  -0.0304   0.0155   0.8603
  17.250   1.5534   0.06148   0.05632  -0.0309   0.0151   0.8633
  17.500   1.5567   0.06420   0.05916  -0.0314   0.0149   0.8673
  17.750   1.5588   0.06711   0.06219  -0.0319   0.0144   0.8723
  18.000   1.5585   0.07025   0.06549  -0.0325   0.0140   0.8876
  18.250   1.5657   0.07435   0.06979  -0.0357   0.0134   0.9526
  18.500   1.5591   0.07846   0.07398  -0.0367   0.0129   1.0000
  18.750   1.5507   0.08326   0.07888  -0.0383   0.0125   1.0000
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