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WORTMANN FX 082-512 AIRFOIL (fx082512-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 082-512 AIRFOIL (fx082512-il)
Reynolds number: 200,000
Max Cl/Cd: 60.18 at α=1.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx082512-il-200000-n5.txt
Download as CSV file: xf-fx082512-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 082-512 AIRFOIL                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6885   0.09974   0.09570  -0.0504   1.0000   0.0153
 -13.750  -0.7133   0.09121   0.08701  -0.0545   1.0000   0.0151
 -13.500  -0.7306   0.08487   0.08058  -0.0573   1.0000   0.0153
 -13.250  -0.7453   0.07937   0.07496  -0.0595   1.0000   0.0153
 -13.000  -0.7576   0.07462   0.07012  -0.0613   1.0000   0.0155
 -12.750  -0.7688   0.07038   0.06581  -0.0626   1.0000   0.0158
 -12.500  -0.7793   0.06657   0.06190  -0.0634   1.0000   0.0159
 -12.250  -0.7893   0.06317   0.05844  -0.0639   1.0000   0.0162
 -12.000  -0.7999   0.06011   0.05532  -0.0639   1.0000   0.0165
 -11.750  -0.8107   0.05732   0.05247  -0.0635   1.0000   0.0168
 -11.500  -0.8223   0.05472   0.04983  -0.0627   1.0000   0.0171
 -11.250  -0.8345   0.05238   0.04743  -0.0614   1.0000   0.0174
 -11.000  -0.8495   0.05021   0.04522  -0.0594   1.0000   0.0176
 -10.750  -0.8470   0.04747   0.04237  -0.0618   0.9968   0.0181
 -10.500  -0.8376   0.04459   0.03937  -0.0653   0.9933   0.0190
 -10.250  -0.8233   0.04171   0.03635  -0.0693   0.9893   0.0197
 -10.000  -0.8026   0.03889   0.03336  -0.0742   0.9862   0.0208
  -9.750  -0.7809   0.03636   0.03065  -0.0785   0.9832   0.0219
  -9.500  -0.7557   0.03287   0.02711  -0.0854   0.9795   0.0248
  -9.250  -0.7238   0.03029   0.02445  -0.0916   0.9774   0.0284
  -9.000  -0.6881   0.02797   0.02205  -0.0979   0.9759   0.0332
  -8.750  -0.6512   0.02640   0.02036  -0.1031   0.9748   0.0407
  -8.500  -0.6185   0.02548   0.01927  -0.1063   0.9730   0.0479
  -8.250  -0.5881   0.02467   0.01830  -0.1086   0.9705   0.0531
  -8.000  -0.5559   0.02409   0.01747  -0.1110   0.9683   0.0583
  -7.750  -0.5228   0.02321   0.01653  -0.1138   0.9665   0.0627
  -7.500  -0.4889   0.02260   0.01576  -0.1162   0.9649   0.0673
  -7.250  -0.4544   0.02201   0.01497  -0.1187   0.9635   0.0717
  -7.000  -0.4197   0.02132   0.01425  -0.1213   0.9623   0.0760
  -6.750  -0.3871   0.02079   0.01360  -0.1231   0.9607   0.0791
  -6.500  -0.3591   0.02023   0.01299  -0.1240   0.9575   0.0813
  -6.250  -0.3269   0.01962   0.01236  -0.1259   0.9553   0.0835
  -6.000  -0.2929   0.01910   0.01179  -0.1279   0.9533   0.0854
  -5.750  -0.2579   0.01864   0.01124  -0.1301   0.9516   0.0874
  -5.500  -0.2218   0.01814   0.01065  -0.1326   0.9501   0.0897
  -5.250  -0.1849   0.01762   0.01004  -0.1353   0.9489   0.0930
  -5.000  -0.1481   0.01721   0.00952  -0.1377   0.9478   0.0964
  -4.750  -0.1147   0.01675   0.00898  -0.1395   0.9457   0.1003
  -4.500  -0.0855   0.01638   0.00854  -0.1403   0.9420   0.1063
  -4.250  -0.0445   0.01512   0.00786  -0.1449   0.9410   0.2470
  -4.000  -0.0132   0.01517   0.00789  -0.1456   0.9381   0.2792
  -3.750   0.0199   0.01524   0.00791  -0.1466   0.9357   0.2938
  -3.500   0.0541   0.01526   0.00785  -0.1479   0.9339   0.3028
  -3.250   0.0889   0.01530   0.00786  -0.1492   0.9323   0.3095
  -3.000   0.1171   0.01537   0.00788  -0.1493   0.9286   0.3153
  -2.750   0.1443   0.01543   0.00789  -0.1492   0.9239   0.3206
  -2.500   0.1759   0.01546   0.00794  -0.1499   0.9209   0.3246
  -2.250   0.2097   0.01540   0.00785  -0.1511   0.9187   0.3286
  -2.000   0.2450   0.01529   0.00766  -0.1526   0.9170   0.3328
  -1.750   0.2803   0.01516   0.00756  -0.1540   0.9155   0.3354
  -1.500   0.3031   0.01527   0.00773  -0.1530   0.9089   0.3386
  -1.250   0.3361   0.01513   0.00760  -0.1538   0.9043   0.3428
  -1.000   0.3773   0.01468   0.00712  -0.1561   0.9005   0.3466
  -0.750   0.4088   0.01444   0.00690  -0.1566   0.8933   0.3497
  -0.500   0.4397   0.01429   0.00683  -0.1570   0.8874   0.3526
  -0.250   0.4777   0.01400   0.00660  -0.1588   0.8835   0.3557
   0.000   0.5053   0.01386   0.00649  -0.1585   0.8744   0.3577
   0.250   0.5426   0.01353   0.00618  -0.1601   0.8674   0.3597
   0.500   0.5729   0.01331   0.00598  -0.1603   0.8549   0.3616
   0.750   0.6088   0.01301   0.00568  -0.1616   0.8406   0.3634
   1.000   0.6545   0.01255   0.00522  -0.1647   0.8147   0.3652
   1.250   0.7106   0.01225   0.00479  -0.1700   0.7617   0.3673
   1.500   0.7498   0.01246   0.00463  -0.1718   0.6786   0.3693
   1.750   0.7689   0.01304   0.00476  -0.1697   0.5890   0.3711
   2.000   0.7756   0.01407   0.00512  -0.1652   0.4587   0.3728
   2.250   0.7842   0.01524   0.00564  -0.1616   0.3316   0.3747
   2.500   0.7919   0.01687   0.00634  -0.1582   0.1402   0.3766
   2.750   0.8122   0.01754   0.00681  -0.1568   0.1081   0.3787
   3.000   0.8358   0.01790   0.00716  -0.1560   0.1014   0.3806
   3.250   0.8594   0.01822   0.00755  -0.1551   0.0977   0.3823
   3.500   0.8831   0.01853   0.00796  -0.1543   0.0947   0.3842
   3.750   0.9057   0.01893   0.00842  -0.1533   0.0920   0.3863
   4.000   0.9280   0.01932   0.00888  -0.1522   0.0894   0.3885
   4.250   0.9498   0.01973   0.00938  -0.1510   0.0869   0.3909
   4.500   0.9703   0.02022   0.00992  -0.1496   0.0849   0.3934
   4.750   0.9897   0.02083   0.01054  -0.1480   0.0830   0.3959
   5.000   1.0117   0.02121   0.01104  -0.1469   0.0790   0.3986
   5.250   1.0313   0.02183   0.01168  -0.1455   0.0744   0.4013
   5.500   1.0545   0.02209   0.01212  -0.1446   0.0701   0.4044
   5.750   1.0762   0.02251   0.01263  -0.1435   0.0658   0.4077
   6.000   1.0967   0.02307   0.01324  -0.1422   0.0617   0.4109
   6.250   1.1201   0.02329   0.01361  -0.1413   0.0566   0.4141
   6.500   1.1432   0.02352   0.01400  -0.1405   0.0512   0.4174
   6.750   1.1668   0.02371   0.01431  -0.1397   0.0444   0.4213
   7.000   1.1890   0.02407   0.01472  -0.1387   0.0376   0.4256
   7.500   1.2280   0.02537   0.01603  -0.1359   0.0280   0.4348
   7.750   1.2457   0.02628   0.01709  -0.1342   0.0256   0.4404
   8.250   1.2807   0.02826   0.01932  -0.1308   0.0216   0.4530
   8.500   1.2966   0.02952   0.02069  -0.1290   0.0196   0.4606
   8.750   1.3117   0.03114   0.02253  -0.1271   0.0182   0.4689
   9.250   1.3477   0.03382   0.02568  -0.1242   0.0168   0.4954
   9.500   1.3653   0.03533   0.02746  -0.1228   0.0161   0.5179
   9.750   1.3817   0.03680   0.02922  -0.1213   0.0153   0.5563
  10.000   1.3965   0.03814   0.03088  -0.1196   0.0146   0.6307
  10.250   1.4030   0.03902   0.03227  -0.1163   0.0140   0.8283
  10.750   1.4140   0.04229   0.03586  -0.1104   0.0131   1.0000
  11.000   1.4180   0.04534   0.03916  -0.1079   0.0127   1.0000
  11.250   1.4236   0.04780   0.04187  -0.1056   0.0124   1.0000
  11.500   1.4260   0.05056   0.04491  -0.1032   0.0122   1.0000
  11.750   1.4248   0.05367   0.04836  -0.1006   0.0121   1.0000
  12.000   1.4200   0.05712   0.05211  -0.0982   0.0119   1.0000
  12.250   1.4111   0.06106   0.05635  -0.0959   0.0117   1.0000
  12.500   1.3986   0.06547   0.06108  -0.0940   0.0116   1.0000
  12.750   1.3829   0.07041   0.06632  -0.0927   0.0116   1.0000
  13.000   1.3633   0.07613   0.07234  -0.0922   0.0115   1.0000
  13.250   1.3412   0.08257   0.07906  -0.0929   0.0115   1.0000
  13.500   1.3165   0.08994   0.08671  -0.0949   0.0115   1.0000
  13.750   1.2893   0.09861   0.09564  -0.0988   0.0116   1.0000
  14.000   1.2588   0.10922   0.10651  -0.1050   0.0117   1.0000
  14.250   1.2228   0.12335   0.12086  -0.1148   0.0119   1.0000
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