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WORTMANN FX 082-512 AIRFOIL (fx082512-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 082-512 AIRFOIL (fx082512-il)
Reynolds number: 500,000
Max Cl/Cd: 75.3 at α=-0.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx082512-il-500000-n5.txt
Download as CSV file: xf-fx082512-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.6609   0.16358   0.16100  -0.0216   1.0000   0.0074
 -17.250  -0.6861   0.15230   0.14963  -0.0264   1.0000   0.0075
 -17.000  -0.7022   0.14404   0.14131  -0.0300   1.0000   0.0074
 -16.750  -0.7222   0.13509   0.13227  -0.0339   1.0000   0.0075
 -16.500  -0.7410   0.12667   0.12376  -0.0376   1.0000   0.0075
 -16.250  -0.7594   0.11868   0.11567  -0.0411   1.0000   0.0075
 -16.000  -0.7745   0.11171   0.10861  -0.0442   1.0000   0.0074
 -15.750  -0.7906   0.10483   0.10162  -0.0474   1.0000   0.0075
 -15.500  -0.8040   0.09878   0.09547  -0.0501   1.0000   0.0075
 -15.250  -0.8143   0.09353   0.09013  -0.0523   1.0000   0.0075
 -15.000  -0.8279   0.08802   0.08456  -0.0547   1.0000   0.0077
 -14.750  -0.8367   0.08348   0.07995  -0.0565   1.0000   0.0077
 -14.500  -0.8461   0.07905   0.07545  -0.0581   1.0000   0.0078
 -14.250  -0.8541   0.07501   0.07134  -0.0595   1.0000   0.0079
 -14.000  -0.8617   0.07127   0.06754  -0.0605   1.0000   0.0079
 -13.750  -0.8694   0.06771   0.06391  -0.0614   1.0000   0.0080
 -13.500  -0.8751   0.06446   0.06062  -0.0622   0.9999   0.0082
 -13.250  -0.8704   0.06076   0.05684  -0.0657   0.9988   0.0083
 -13.000  -0.8633   0.05757   0.05358  -0.0689   0.9974   0.0086
 -12.750  -0.8563   0.05434   0.05027  -0.0723   0.9958   0.0088
 -12.500  -0.8465   0.05148   0.04734  -0.0757   0.9943   0.0091
 -12.250  -0.8410   0.04870   0.04449  -0.0781   0.9916   0.0094
 -12.000  -0.8357   0.04583   0.04153  -0.0810   0.9886   0.0095
 -11.750  -0.8247   0.04334   0.03894  -0.0842   0.9862   0.0099
 -11.500  -0.8244   0.04093   0.03647  -0.0853   0.9810   0.0101
 -11.250  -0.8118   0.03833   0.03378  -0.0888   0.9771   0.0103
 -11.000  -0.7922   0.03440   0.02976  -0.0962   0.9744   0.0109
 -10.750  -0.7828   0.03136   0.02665  -0.0998   0.9681   0.0113
 -10.500  -0.7557   0.02824   0.02345  -0.1066   0.9653   0.0120
 -10.250  -0.7226   0.02541   0.02050  -0.1138   0.9638   0.0127
 -10.000  -0.6866   0.02279   0.01774  -0.1208   0.9629   0.0138
  -9.750  -0.6492   0.02051   0.01530  -0.1271   0.9623   0.0152
  -9.500  -0.6122   0.01882   0.01350  -0.1322   0.9617   0.0181
  -9.250  -0.5855   0.01775   0.01234  -0.1339   0.9586   0.0204
  -9.000  -0.5544   0.01679   0.01132  -0.1363   0.9567   0.0253
  -8.750  -0.5220   0.01596   0.01054  -0.1387   0.9552   0.0362
  -8.500  -0.4906   0.01556   0.01013  -0.1402   0.9537   0.0443
  -8.250  -0.4590   0.01527   0.00981  -0.1414   0.9524   0.0491
  -8.000  -0.4268   0.01495   0.00946  -0.1429   0.9513   0.0523
  -7.750  -0.3945   0.01471   0.00917  -0.1442   0.9503   0.0553
  -7.500  -0.3618   0.01447   0.00885  -0.1455   0.9494   0.0576
  -7.250  -0.3278   0.01400   0.00833  -0.1475   0.9487   0.0603
  -7.000  -0.2936   0.01359   0.00788  -0.1493   0.9480   0.0630
  -6.750  -0.2600   0.01331   0.00755  -0.1509   0.9474   0.0664
  -6.500  -0.2335   0.01308   0.00726  -0.1510   0.9443   0.0683
  -6.250  -0.2037   0.01275   0.00687  -0.1518   0.9419   0.0692
  -6.000  -0.1721   0.01243   0.00649  -0.1529   0.9401   0.0700
  -5.750  -0.1394   0.01210   0.00609  -0.1542   0.9386   0.0707
  -5.500  -0.1053   0.01164   0.00559  -0.1560   0.9374   0.0725
  -5.250  -0.0714   0.01128   0.00518  -0.1576   0.9363   0.0742
  -5.000  -0.0372   0.01095   0.00483  -0.1592   0.9352   0.0762
  -4.750  -0.0027   0.01067   0.00450  -0.1608   0.9342   0.0783
  -4.500   0.0320   0.01040   0.00419  -0.1624   0.9333   0.0800
  -4.250   0.0676   0.01010   0.00387  -0.1643   0.9324   0.0826
  -4.000   0.1037   0.00982   0.00357  -0.1662   0.9316   0.0863
  -3.750   0.1303   0.00967   0.00342  -0.1661   0.9276   0.0916
  -3.500   0.1687   0.00857   0.00282  -0.1696   0.9261   0.2489
  -3.250   0.2007   0.00845   0.00276  -0.1705   0.9228   0.2754
  -3.000   0.2372   0.00831   0.00263  -0.1722   0.9191   0.2866
  -2.750   0.2782   0.00815   0.00245  -0.1749   0.9163   0.2935
  -2.500   0.3103   0.00810   0.00241  -0.1758   0.9115   0.2985
  -2.250   0.3405   0.00807   0.00236  -0.1761   0.9050   0.3033
  -2.000   0.3782   0.00800   0.00229  -0.1782   0.9012   0.3074
  -1.750   0.4142   0.00796   0.00226  -0.1799   0.8956   0.3109
  -1.500   0.4449   0.00793   0.00223  -0.1803   0.8868   0.3137
  -1.250   0.4811   0.00790   0.00217  -0.1820   0.8771   0.3169
  -1.000   0.5170   0.00788   0.00212  -0.1836   0.8663   0.3191
  -0.750   0.5502   0.00785   0.00209  -0.1846   0.8498   0.3213
  -0.500   0.5827   0.00790   0.00206  -0.1854   0.8210   0.3244
  -0.250   0.6114   0.00812   0.00205  -0.1853   0.7710   0.3272
   0.000   0.6291   0.00859   0.00214  -0.1828   0.6967   0.3297
   0.250   0.6403   0.00927   0.00235  -0.1790   0.6030   0.3317
   0.500   0.6516   0.01015   0.00265  -0.1756   0.4835   0.3333
   0.750   0.6652   0.01123   0.00308  -0.1729   0.3363   0.3345
   1.000   0.6842   0.01203   0.00342  -0.1713   0.2317   0.3357
   1.250   0.7017   0.01304   0.00389  -0.1695   0.0943   0.3369
   1.500   0.7273   0.01323   0.00408  -0.1690   0.0876   0.3383
   1.750   0.7529   0.01344   0.00428  -0.1685   0.0835   0.3397
   2.000   0.7787   0.01361   0.00447  -0.1680   0.0814   0.3412
   2.250   0.8043   0.01379   0.00469  -0.1675   0.0793   0.3428
   2.500   0.8296   0.01401   0.00491  -0.1669   0.0775   0.3444
   2.750   0.8545   0.01426   0.00517  -0.1662   0.0758   0.3461
   3.000   0.8791   0.01453   0.00546  -0.1655   0.0742   0.3477
   3.250   0.9044   0.01472   0.00570  -0.1650   0.0730   0.3494
   3.500   0.9294   0.01494   0.00598  -0.1643   0.0718   0.3511
   3.750   0.9541   0.01518   0.00627  -0.1636   0.0702   0.3528
   4.000   0.9789   0.01539   0.00653  -0.1630   0.0672   0.3546
   4.250   1.0025   0.01571   0.00685  -0.1621   0.0635   0.3564
   4.500   1.0267   0.01594   0.00713  -0.1614   0.0615   0.3583
   4.750   1.0513   0.01610   0.00735  -0.1606   0.0591   0.3602
   5.000   1.0756   0.01628   0.00756  -0.1599   0.0562   0.3621
   5.250   1.0989   0.01652   0.00780  -0.1590   0.0532   0.3637
   5.500   1.1232   0.01668   0.00804  -0.1582   0.0496   0.3659
   5.750   1.1470   0.01687   0.00825  -0.1574   0.0443   0.3681
   6.000   1.1700   0.01713   0.00849  -0.1564   0.0355   0.3706
   6.250   1.1911   0.01758   0.00891  -0.1552   0.0267   0.3733
   6.500   1.2115   0.01808   0.00941  -0.1537   0.0219   0.3760
   6.750   1.2317   0.01860   0.00997  -0.1522   0.0182   0.3785
   7.250   1.2724   0.01957   0.01110  -0.1493   0.0155   0.3834
   7.500   1.2918   0.02016   0.01174  -0.1478   0.0143   0.3862
   7.750   1.3101   0.02086   0.01251  -0.1460   0.0131   0.3892
   8.000   1.3287   0.02152   0.01325  -0.1443   0.0123   0.3925
   8.250   1.3476   0.02211   0.01392  -0.1427   0.0117   0.3957
   8.500   1.3660   0.02274   0.01467  -0.1411   0.0111   0.3990
   8.750   1.3841   0.02342   0.01543  -0.1394   0.0105   0.4033
   9.000   1.4015   0.02416   0.01625  -0.1377   0.0100   0.4082
   9.250   1.4178   0.02502   0.01718  -0.1358   0.0096   0.4133
   9.500   1.4314   0.02615   0.01842  -0.1336   0.0091   0.4190
   9.750   1.4477   0.02700   0.01939  -0.1318   0.0089   0.4262
  10.000   1.4635   0.02791   0.02044  -0.1299   0.0086   0.4338
  10.250   1.4784   0.02890   0.02156  -0.1280   0.0084   0.4438
  10.500   1.4931   0.02991   0.02270  -0.1261   0.0081   0.4568
  10.750   1.5075   0.03094   0.02391  -0.1243   0.0078   0.4754
  11.000   1.5216   0.03200   0.02513  -0.1226   0.0075   0.5053
  11.250   1.5361   0.03309   0.02642  -0.1210   0.0072   0.5613
  11.500   1.5508   0.03430   0.02793  -0.1197   0.0070   0.6685
  11.750   1.5532   0.03512   0.02927  -0.1159   0.0069   1.0000
  12.000   1.5593   0.03693   0.03119  -0.1134   0.0067   1.0000
  12.250   1.5648   0.03885   0.03324  -0.1110   0.0065   1.0000
  12.500   1.5723   0.04057   0.03512  -0.1089   0.0064   1.0000
  12.750   1.5782   0.04248   0.03718  -0.1068   0.0063   1.0000
  13.000   1.5822   0.04462   0.03948  -0.1047   0.0062   1.0000
  13.250   1.5848   0.04694   0.04196  -0.1027   0.0061   1.0000
  13.500   1.5862   0.04942   0.04460  -0.1008   0.0060   1.0000
  13.750   1.5855   0.05222   0.04758  -0.0991   0.0059   1.0000
  14.000   1.5837   0.05521   0.05074  -0.0975   0.0058   1.0000
  14.250   1.5799   0.05854   0.05425  -0.0963   0.0057   1.0000
  14.500   1.5747   0.06219   0.05808  -0.0953   0.0057   1.0000
  14.750   1.5681   0.06620   0.06226  -0.0948   0.0056   1.0000
  15.000   1.5579   0.07093   0.06719  -0.0948   0.0056   1.0000
  15.250   1.5489   0.07575   0.07218  -0.0953   0.0055   1.0000
  15.500   1.5362   0.08145   0.07807  -0.0966   0.0055   1.0000
  15.750   1.5228   0.08762   0.08444  -0.0986   0.0054   1.0000
  16.000   1.5032   0.09541   0.09244  -0.1018   0.0054   1.0000
  16.250   1.4839   0.10376   0.10100  -0.1061   0.0054   1.0000
  16.500   1.4602   0.11377   0.11123  -0.1119   0.0054   1.0000
  16.750   1.4332   0.12546   0.12315  -0.1195   0.0054   1.0000
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