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DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: DELFT DU84-132V3 AIRFOIL (MEASURED) (du84132v-il)
Reynolds number: 500,000
Max Cl/Cd: 82.01 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-du84132v-il-500000.txt
Download as CSV file: xf-du84132v-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.3881   0.11446   0.11201  -0.0425   1.0000   0.0365
 -11.500  -0.3885   0.11148   0.10905  -0.0426   1.0000   0.0370
 -11.250  -0.3904   0.10836   0.10596  -0.0428   1.0000   0.0377
 -11.000  -0.3491   0.08892   0.08672  -0.0564   0.9966   0.0411
 -10.750  -0.3362   0.08579   0.08358  -0.0578   0.9952   0.0414
 -10.500  -0.3259   0.08199   0.07979  -0.0601   0.9939   0.0417
 -10.250  -0.3162   0.07806   0.07586  -0.0626   0.9925   0.0421
 -10.000  -0.3118   0.07323   0.07103  -0.0655   0.9900   0.0425
  -9.750  -0.3114   0.06708   0.06488  -0.0698   0.9873   0.0429
  -9.500  -0.3605   0.04863   0.04632  -0.0861   0.9835   0.0435
  -9.250  -0.3940   0.04031   0.03780  -0.0941   0.9759   0.0436
  -9.000  -0.4017   0.03504   0.03231  -0.0993   0.9692   0.0441
  -8.750  -0.3991   0.03093   0.02797  -0.1017   0.9632   0.0450
  -8.500  -0.3914   0.02815   0.02463  -0.1039   0.9567   0.0476
  -8.250  -0.3690   0.02582   0.02190  -0.1063   0.9541   0.0479
  -8.000  -0.4052   0.02348   0.01800  -0.1062   0.9531   0.0292
  -7.750  -0.3827   0.02139   0.01581  -0.1059   0.9480   0.0286
  -7.500  -0.3557   0.01967   0.01394  -0.1063   0.9439   0.0282
  -7.250  -0.3241   0.01816   0.01230  -0.1075   0.9411   0.0279
  -7.000  -0.2906   0.01687   0.01091  -0.1089   0.9386   0.0277
  -6.750  -0.2624   0.01589   0.00986  -0.1092   0.9339   0.0277
  -6.500  -0.2353   0.01504   0.00894  -0.1092   0.9279   0.0278
  -6.250  -0.2036   0.01422   0.00807  -0.1102   0.9237   0.0279
  -6.000  -0.1745   0.01355   0.00735  -0.1107   0.9185   0.0282
  -5.750  -0.1481   0.01300   0.00675  -0.1105   0.9118   0.0285
  -5.500  -0.1167   0.01244   0.00612  -0.1114   0.9067   0.0288
  -5.250  -0.0912   0.01201   0.00566  -0.1111   0.8990   0.0291
  -5.000  -0.0638   0.01145   0.00506  -0.1112   0.8919   0.0299
  -4.750  -0.0364   0.01109   0.00466  -0.1112   0.8848   0.0308
  -4.500  -0.0093   0.01081   0.00436  -0.1110   0.8769   0.0318
  -4.250   0.0192   0.01056   0.00408  -0.1112   0.8698   0.0331
  -4.000   0.0461   0.01034   0.00383  -0.1109   0.8612   0.0351
  -3.750   0.0745   0.01018   0.00365  -0.1110   0.8534   0.0396
  -3.500   0.1014   0.00996   0.00340  -0.1108   0.8444   0.0471
  -3.250   0.1280   0.00968   0.00311  -0.1105   0.8357   0.0590
  -3.000   0.1542   0.00932   0.00289  -0.1103   0.8264   0.0952
  -2.750   0.1791   0.00889   0.00272  -0.1100   0.8164   0.1675
  -2.500   0.2053   0.00852   0.00256  -0.1099   0.8069   0.2380
  -2.250   0.2310   0.00814   0.00241  -0.1097   0.7957   0.3130
  -2.000   0.2562   0.00778   0.00231  -0.1094   0.7827   0.4035
  -1.750   0.2821   0.00748   0.00219  -0.1091   0.7704   0.4689
  -1.500   0.3074   0.00715   0.00211  -0.1088   0.7593   0.5684
  -1.250   0.3322   0.00709   0.00233  -0.1079   0.7490   0.6628
  -1.000   0.3587   0.00722   0.00245  -0.1073   0.7369   0.6938
  -0.750   0.3851   0.00737   0.00256  -0.1068   0.7238   0.7148
  -0.500   0.4116   0.00757   0.00270  -0.1062   0.7131   0.7295
  -0.250   0.4382   0.00773   0.00282  -0.1057   0.7024   0.7378
   0.000   0.4646   0.00791   0.00295  -0.1052   0.6901   0.7468
   0.250   0.4902   0.00808   0.00308  -0.1045   0.6758   0.7535
   0.500   0.5151   0.00831   0.00323  -0.1036   0.6610   0.7601
   0.750   0.5404   0.00849   0.00332  -0.1029   0.6424   0.7670
   1.000   0.5639   0.00870   0.00346  -0.1017   0.6240   0.7715
   1.250   0.5884   0.00891   0.00358  -0.1008   0.6096   0.7769
   1.750   0.6380   0.00924   0.00385  -0.0992   0.5817   0.7886
   2.000   0.6624   0.00946   0.00401  -0.0983   0.5691   0.7962
   2.250   0.6860   0.00959   0.00411  -0.0972   0.5565   0.8014
   2.500   0.7099   0.00973   0.00421  -0.0963   0.5430   0.8056
   2.750   0.7348   0.00987   0.00430  -0.0957   0.5288   0.8090
   3.250   0.7843   0.01015   0.00444  -0.0945   0.4998   0.8144
   3.500   0.8079   0.01025   0.00452  -0.0937   0.4841   0.8169
   3.750   0.8321   0.01036   0.00460  -0.0929   0.4634   0.8196
   4.000   0.8533   0.01059   0.00469  -0.0917   0.4342   0.8221
   4.250   0.8750   0.01086   0.00485  -0.0906   0.4036   0.8246
   4.500   0.8961   0.01121   0.00505  -0.0895   0.3834   0.8273
   4.750   0.9181   0.01146   0.00523  -0.0885   0.3666   0.8295
   5.000   0.9399   0.01165   0.00539  -0.0874   0.3512   0.8318
   5.250   0.9622   0.01185   0.00556  -0.0864   0.3359   0.8343
   5.750   1.0068   0.01231   0.00592  -0.0845   0.3090   0.8384
   6.000   1.0292   0.01255   0.00614  -0.0837   0.2983   0.8398
   6.250   1.0504   0.01283   0.00637  -0.0826   0.2860   0.8410
   6.500   1.0712   0.01309   0.00658  -0.0815   0.2712   0.8422
   6.750   1.0909   0.01338   0.00682  -0.0801   0.2604   0.8434
   7.000   1.1108   0.01361   0.00705  -0.0788   0.2510   0.8446
   7.250   1.1289   0.01391   0.00732  -0.0771   0.2406   0.8459
   7.500   1.1490   0.01415   0.00756  -0.0759   0.2253   0.8473
   7.750   1.1658   0.01456   0.00787  -0.0741   0.1997   0.8489
   8.000   1.1791   0.01515   0.00831  -0.0718   0.1687   0.8509
   8.250   1.1899   0.01588   0.00888  -0.0692   0.1454   0.8530
   8.500   1.2048   0.01642   0.00939  -0.0673   0.1351   0.8550
   9.000   1.2362   0.01746   0.01039  -0.0638   0.1103   0.8580
   9.250   1.2502   0.01807   0.01094  -0.0618   0.1014   0.8595
   9.500   1.2651   0.01859   0.01147  -0.0601   0.0963   0.8612
   9.750   1.2791   0.01917   0.01208  -0.0582   0.0922   0.8630
  10.000   1.2919   0.01984   0.01276  -0.0563   0.0883   0.8649
  10.250   1.3055   0.02048   0.01346  -0.0545   0.0853   0.8668
  10.500   1.3211   0.02102   0.01409  -0.0530   0.0831   0.8688
  10.750   1.3349   0.02169   0.01482  -0.0514   0.0804   0.8708
  11.000   1.3464   0.02253   0.01569  -0.0496   0.0770   0.8729
  11.250   1.3540   0.02360   0.01680  -0.0474   0.0733   0.8753
  11.500   1.3704   0.02413   0.01745  -0.0463   0.0711   0.8781
  11.750   1.3840   0.02485   0.01825  -0.0449   0.0676   0.8813
  12.000   1.3940   0.02584   0.01926  -0.0432   0.0637   0.8846
  12.250   1.4064   0.02671   0.02021  -0.0419   0.0595   0.8882
  12.500   1.4184   0.02766   0.02118  -0.0406   0.0536   0.8932
  12.750   1.4290   0.02882   0.02236  -0.0395   0.0481   0.9004
  13.000   1.4372   0.03033   0.02390  -0.0385   0.0436   0.9148
  13.250   1.4435   0.03216   0.02580  -0.0378   0.0407   1.0000
  13.500   1.4411   0.03454   0.02821  -0.0362   0.0381   1.0000
  13.750   1.4466   0.03635   0.03013  -0.0352   0.0367   1.0000
  14.000   1.4492   0.03848   0.03235  -0.0342   0.0353   1.0000
  14.250   1.4489   0.04097   0.03492  -0.0334   0.0339   1.0000
  14.500   1.4429   0.04412   0.03814  -0.0326   0.0326   1.0000
  14.750   1.4443   0.04669   0.04080  -0.0322   0.0317   1.0000
  15.000   1.4531   0.04853   0.04274  -0.0320   0.0305   1.0000
  15.250   1.4578   0.05086   0.04517  -0.0319   0.0292   1.0000
  15.500   1.4605   0.05349   0.04787  -0.0320   0.0283   1.0000
  15.750   1.4605   0.05652   0.05097  -0.0322   0.0275   1.0000
  16.000   1.4569   0.06010   0.05463  -0.0326   0.0269   1.0000
  16.250   1.4597   0.06296   0.05760  -0.0330   0.0262   1.0000
  16.500   1.4616   0.06600   0.06074  -0.0336   0.0254   1.0000
  16.750   1.4626   0.06922   0.06406  -0.0343   0.0248   1.0000
  17.000   1.4623   0.07272   0.06763  -0.0352   0.0240   1.0000
  17.250   1.4595   0.07663   0.07162  -0.0363   0.0235   1.0000
  17.500   1.4535   0.08109   0.07615  -0.0377   0.0229   1.0000
  17.750   1.4463   0.08584   0.08101  -0.0393   0.0223   1.0000
  18.000   1.4426   0.09018   0.08547  -0.0409   0.0218   1.0000
  18.250   1.4378   0.09478   0.09018  -0.0428   0.0213   1.0000
  18.500   1.4323   0.09958   0.09509  -0.0448   0.0207   1.0000
  18.750   1.4257   0.10464   0.10026  -0.0470   0.0202   1.0000
  19.000   1.4174   0.11005   0.10575  -0.0495   0.0196   1.0000
  19.250   1.4072   0.11582   0.11160  -0.0523   0.0191   1.0000
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