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WORTMANN FX 082-512 AIRFOIL (fx082512-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 082-512 AIRFOIL (fx082512-il)
Reynolds number: 500,000
Max Cl/Cd: 83.67 at α=0.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx082512-il-500000.txt
Download as CSV file: xf-fx082512-il-500000.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 =     0.500 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.7323   0.11199   0.10929  -0.0456   1.0000   0.0162
 -15.250  -0.7707   0.10032   0.09746  -0.0516   1.0000   0.0160
 -15.000  -0.7945   0.09228   0.08927  -0.0558   1.0000   0.0160
 -14.750  -0.8134   0.08562   0.08248  -0.0590   1.0000   0.0160
 -14.500  -0.8277   0.08011   0.07685  -0.0615   1.0000   0.0161
 -14.250  -0.8382   0.07550   0.07213  -0.0634   1.0000   0.0162
 -14.000  -0.8506   0.07085   0.06736  -0.0652   1.0000   0.0163
 -13.750  -0.8593   0.06702   0.06342  -0.0665   1.0000   0.0164
 -13.500  -0.8672   0.06363   0.05993  -0.0672   1.0000   0.0164
 -13.250  -0.8823   0.05987   0.05607  -0.0674   1.0000   0.0166
 -13.000  -0.8942   0.05692   0.05304  -0.0668   1.0000   0.0169
 -12.750  -0.9034   0.05449   0.05057  -0.0660   1.0000   0.0170
 -12.500  -0.9144   0.05218   0.04822  -0.0649   1.0000   0.0172
 -12.250  -0.9261   0.05004   0.04604  -0.0634   1.0000   0.0174
 -12.000  -0.9400   0.04800   0.04399  -0.0615   1.0000   0.0176
 -11.750  -0.9595   0.04618   0.04213  -0.0584   1.0000   0.0176
 -11.500  -0.9501   0.04352   0.03941  -0.0621   0.9968   0.0181
 -11.250  -0.9301   0.04078   0.03659  -0.0674   0.9939   0.0188
 -11.000  -0.9098   0.03807   0.03378  -0.0723   0.9903   0.0195
 -10.750  -0.8833   0.03544   0.03100  -0.0780   0.9879   0.0203
 -10.500  -0.8513   0.03235   0.02780  -0.0857   0.9863   0.0215
 -10.250  -0.8259   0.02938   0.02478  -0.0914   0.9825   0.0225
 -10.000  -0.7910   0.02687   0.02217  -0.0980   0.9808   0.0239
  -9.750  -0.7532   0.02465   0.01979  -0.1044   0.9797   0.0255
  -9.500  -0.7120   0.02211   0.01717  -0.1119   0.9791   0.0285
  -9.250  -0.6752   0.02115   0.01611  -0.1156   0.9782   0.0314
  -9.000  -0.6373   0.02008   0.01504  -0.1197   0.9776   0.0358
  -8.750  -0.6006   0.01944   0.01433  -0.1228   0.9770   0.0406
  -8.500  -0.5757   0.01922   0.01413  -0.1227   0.9737   0.0445
  -8.250  -0.5445   0.01906   0.01388  -0.1239   0.9716   0.0483
  -8.000  -0.5102   0.01856   0.01338  -0.1262   0.9703   0.0524
  -7.750  -0.4759   0.01838   0.01313  -0.1280   0.9690   0.0559
  -7.500  -0.4409   0.01836   0.01302  -0.1298   0.9680   0.0582
  -7.250  -0.4035   0.01733   0.01196  -0.1332   0.9674   0.0624
  -7.000  -0.3671   0.01694   0.01154  -0.1356   0.9668   0.0655
  -6.750  -0.3411   0.01661   0.01116  -0.1357   0.9633   0.0681
  -6.500  -0.3096   0.01634   0.01083  -0.1369   0.9610   0.0702
  -6.250  -0.2738   0.01569   0.01010  -0.1393   0.9598   0.0734
  -6.000  -0.2368   0.01503   0.00942  -0.1420   0.9587   0.0769
  -5.750  -0.2004   0.01459   0.00892  -0.1443   0.9577   0.0796
  -5.500  -0.1634   0.01419   0.00846  -0.1466   0.9569   0.0819
  -5.250  -0.1264   0.01382   0.00803  -0.1489   0.9561   0.0837
  -5.000  -0.0894   0.01352   0.00766  -0.1510   0.9554   0.0852
  -4.750  -0.0603   0.01311   0.00720  -0.1517   0.9521   0.0889
  -4.500  -0.0280   0.01275   0.00680  -0.1529   0.9495   0.0930
  -4.250   0.0069   0.01243   0.00644  -0.1546   0.9478   0.0974
  -4.000   0.0425   0.01212   0.00610  -0.1564   0.9464   0.1059
  -3.750   0.0833   0.01105   0.00561  -0.1604   0.9461   0.2751
  -3.500   0.1184   0.01108   0.00563  -0.1617   0.9448   0.2966
  -3.250   0.1542   0.01110   0.00568  -0.1632   0.9437   0.3071
  -3.000   0.1907   0.01111   0.00562  -0.1649   0.9428   0.3142
  -2.750   0.2178   0.01109   0.00565  -0.1645   0.9378   0.3188
  -2.500   0.2534   0.01093   0.00548  -0.1658   0.9343   0.3235
  -2.250   0.2908   0.01075   0.00527  -0.1676   0.9325   0.3274
  -2.000   0.3281   0.01050   0.00505  -0.1694   0.9313   0.3311
  -1.750   0.3676   0.01028   0.00488  -0.1715   0.9300   0.3356
  -1.500   0.4141   0.00984   0.00445  -0.1751   0.9285   0.3390
  -1.250   0.4393   0.00976   0.00438  -0.1742   0.9215   0.3412
  -1.000   0.4777   0.00955   0.00415  -0.1762   0.9182   0.3434
  -0.750   0.5226   0.00918   0.00380  -0.1797   0.9152   0.3459
  -0.500   0.5562   0.00899   0.00366  -0.1806   0.9073   0.3484
  -0.250   0.6042   0.00883   0.00355  -0.1846   0.8985   0.3533
   0.000   0.6358   0.00874   0.00343  -0.1849   0.8799   0.3568
   0.250   0.6681   0.00864   0.00326  -0.1855   0.8546   0.3586
   0.500   0.7013   0.00864   0.00313  -0.1863   0.8214   0.3598
   0.750   0.7288   0.00871   0.00300  -0.1859   0.7688   0.3616
   1.000   0.7442   0.00918   0.00306  -0.1828   0.6846   0.3630
   1.250   0.7465   0.01019   0.00337  -0.1772   0.5437   0.3641
   1.500   0.7485   0.01191   0.00403  -0.1722   0.3223   0.3652
   1.750   0.7585   0.01355   0.00471  -0.1691   0.1103   0.3665
   2.000   0.7831   0.01383   0.00496  -0.1684   0.0992   0.3682
   2.250   0.8077   0.01412   0.00525  -0.1676   0.0930   0.3701
   2.500   0.8331   0.01433   0.00549  -0.1670   0.0909   0.3722
   2.750   0.8579   0.01458   0.00577  -0.1663   0.0885   0.3741
   3.000   0.8823   0.01488   0.00608  -0.1655   0.0858   0.3756
   3.250   0.9063   0.01516   0.00641  -0.1647   0.0827   0.3778
   3.500   0.9280   0.01567   0.00697  -0.1635   0.0792   0.3797
   3.750   0.9523   0.01593   0.00728  -0.1627   0.0769   0.3817
   4.000   0.9767   0.01616   0.00756  -0.1619   0.0742   0.3839
   4.250   1.0003   0.01646   0.00790  -0.1610   0.0713   0.3861
   4.500   1.0227   0.01684   0.00829  -0.1599   0.0683   0.3883
   4.750   1.0406   0.01770   0.00918  -0.1580   0.0647   0.3902
   5.000   1.0662   0.01770   0.00925  -0.1575   0.0626   0.3928
   5.250   1.0907   0.01782   0.00944  -0.1568   0.0594   0.3958
   5.500   1.1145   0.01800   0.00964  -0.1560   0.0561   0.3987
   5.750   1.1350   0.01851   0.01018  -0.1546   0.0521   0.4016
   6.000   1.1614   0.01843   0.01014  -0.1542   0.0480   0.4047
   6.250   1.1840   0.01872   0.01038  -0.1532   0.0430   0.4074
   6.500   1.2094   0.01878   0.01052  -0.1526   0.0388   0.4110
   6.750   1.2303   0.01925   0.01096  -0.1513   0.0345   0.4145
   7.000   1.2522   0.01960   0.01137  -0.1501   0.0315   0.4183
   7.250   1.2712   0.02021   0.01196  -0.1485   0.0286   0.4219
   7.500   1.2902   0.02087   0.01274  -0.1468   0.0269   0.4261
   7.750   1.3095   0.02147   0.01342  -0.1452   0.0253   0.4310
   8.000   1.3276   0.02216   0.01415  -0.1434   0.0240   0.4364
   8.250   1.3407   0.02347   0.01554  -0.1409   0.0225   0.4418
   8.500   1.3601   0.02411   0.01632  -0.1394   0.0217   0.4489
   8.750   1.3787   0.02485   0.01716  -0.1379   0.0206   0.4568
   9.000   1.3965   0.02565   0.01806  -0.1362   0.0197   0.4674
   9.250   1.4134   0.02659   0.01911  -0.1345   0.0190   0.4817
   9.500   1.4283   0.02823   0.02089  -0.1327   0.0182   0.5040
   9.750   1.4472   0.02963   0.02259  -0.1315   0.0176   0.5603
  10.000   1.4704   0.03060   0.02418  -0.1311   0.0171   0.7735
  10.250   1.4748   0.03128   0.02519  -0.1268   0.0168   1.0000
  10.500   1.4899   0.03258   0.02661  -0.1250   0.0162   1.0000
  10.750   1.5036   0.03384   0.02797  -0.1230   0.0157   1.0000
  11.000   1.5160   0.03512   0.02933  -0.1209   0.0153   1.0000
  11.250   1.5269   0.03646   0.03073  -0.1188   0.0148   1.0000
  11.500   1.5363   0.03862   0.03300  -0.1167   0.0144   1.0000
  11.750   1.5408   0.04205   0.03671  -0.1142   0.0140   1.0000
  12.000   1.5458   0.04391   0.03879  -0.1115   0.0138   1.0000
  12.250   1.5482   0.04631   0.04142  -0.1088   0.0137   1.0000
  12.500   1.5480   0.04895   0.04429  -0.1061   0.0135   1.0000
  12.750   1.5443   0.05203   0.04763  -0.1034   0.0133   1.0000
  13.000   1.5377   0.05545   0.05130  -0.1009   0.0131   1.0000
  13.250   1.5266   0.05952   0.05564  -0.0986   0.0130   1.0000
  13.500   1.5124   0.06408   0.06047  -0.0967   0.0129   1.0000
  13.750   1.4956   0.06911   0.06576  -0.0955   0.0128   1.0000
  14.000   1.4738   0.07518   0.07211  -0.0952   0.0127   1.0000
  14.250   1.4465   0.08256   0.07979  -0.0962   0.0128   1.0000
  14.500   1.4124   0.09187   0.08940  -0.0991   0.0129   1.0000
  14.750   1.3785   0.10226   0.10007  -0.1041   0.0130   1.0000
  15.000   1.3358   0.11628   0.11439  -0.1130   0.0131   1.0000
  15.250   1.2376   0.15194   0.15045  -0.1386   0.0140   1.0000
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