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WB-140/35/FB 14% (wb140-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WB-140/35/FB 14% (wb140-il)
Reynolds number: 1,000,000
Max Cl/Cd: 74.91 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-wb140-il-1000000-n5.txt
Download as CSV file: xf-wb140-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WB-140/35/FB 14%                                
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8644   0.08498   0.08164  -0.0503   0.7157   0.0060
 -16.000  -1.0464   0.04676   0.04298  -0.0806   0.7160   0.0054
 -15.750  -1.0808   0.03880   0.03478  -0.0876   0.7158   0.0053
 -15.500  -1.0921   0.03566   0.03149  -0.0879   0.7157   0.0054
 -15.250  -1.0977   0.03363   0.02932  -0.0862   0.7155   0.0055
 -15.000  -1.0947   0.03199   0.02755  -0.0848   0.7153   0.0056
 -14.750  -1.0860   0.03051   0.02594  -0.0838   0.7151   0.0057
 -14.500  -1.0742   0.02918   0.02449  -0.0830   0.7149   0.0058
 -14.250  -1.0602   0.02796   0.02315  -0.0823   0.7147   0.0059
 -14.000  -1.0444   0.02684   0.02191  -0.0816   0.7145   0.0061
 -13.750  -1.0271   0.02582   0.02077  -0.0810   0.7143   0.0062
 -13.500  -1.0085   0.02487   0.01971  -0.0805   0.7139   0.0063
 -13.250  -0.9888   0.02401   0.01874  -0.0801   0.7133   0.0064
 -13.000  -0.9689   0.02312   0.01773  -0.0797   0.7127   0.0066
 -12.750  -0.9485   0.02224   0.01674  -0.0793   0.7121   0.0069
 -12.500  -0.9266   0.02149   0.01592  -0.0790   0.7115   0.0072
 -12.250  -0.9040   0.02083   0.01519  -0.0787   0.7110   0.0075
 -12.000  -0.8806   0.02022   0.01451  -0.0786   0.7105   0.0079
 -11.750  -0.8568   0.01965   0.01386  -0.0784   0.7101   0.0082
 -11.500  -0.8326   0.01910   0.01323  -0.0783   0.7097   0.0085
 -11.250  -0.8081   0.01858   0.01263  -0.0782   0.7094   0.0089
 -11.000  -0.7832   0.01809   0.01204  -0.0781   0.7091   0.0091
 -10.750  -0.7581   0.01760   0.01151  -0.0781   0.7089   0.0098
 -10.500  -0.7320   0.01724   0.01112  -0.0781   0.7086   0.0105
 -10.250  -0.7058   0.01691   0.01077  -0.0782   0.7078   0.0112
 -10.000  -0.6795   0.01659   0.01040  -0.0783   0.7068   0.0119
  -9.500  -0.6267   0.01590   0.00957  -0.0785   0.7052   0.0130
  -9.250  -0.5994   0.01564   0.00933  -0.0787   0.7048   0.0137
  -9.000  -0.5719   0.01543   0.00912  -0.0789   0.7043   0.0144
  -8.750  -0.5444   0.01521   0.00889  -0.0791   0.7037   0.0151
  -8.500  -0.5169   0.01499   0.00865  -0.0793   0.7030   0.0159
  -8.250  -0.4893   0.01476   0.00839  -0.0795   0.7023   0.0166
  -8.000  -0.4616   0.01455   0.00814  -0.0798   0.7016   0.0170
  -7.750  -0.4341   0.01430   0.00784  -0.0800   0.7007   0.0174
  -7.500  -0.4070   0.01394   0.00745  -0.0801   0.6995   0.0181
  -7.250  -0.3792   0.01373   0.00723  -0.0804   0.6984   0.0187
  -7.000  -0.3513   0.01354   0.00703  -0.0806   0.6973   0.0194
  -6.750  -0.3234   0.01333   0.00680  -0.0809   0.6964   0.0201
  -6.500  -0.2955   0.01311   0.00653  -0.0811   0.6956   0.0207
  -6.250  -0.2675   0.01291   0.00630  -0.0813   0.6948   0.0214
  -6.000  -0.2393   0.01273   0.00608  -0.0816   0.6940   0.0220
  -5.750  -0.2111   0.01254   0.00586  -0.0819   0.6933   0.0224
  -5.500  -0.1829   0.01237   0.00565  -0.0821   0.6925   0.0227
  -5.250  -0.1545   0.01224   0.00549  -0.0824   0.6917   0.0230
  -5.000  -0.1261   0.01208   0.00531  -0.0827   0.6910   0.0232
  -4.750  -0.0977   0.01178   0.00494  -0.0830   0.6905   0.0238
  -4.500  -0.0692   0.01156   0.00468  -0.0832   0.6897   0.0245
  -4.250  -0.0405   0.01138   0.00448  -0.0836   0.6887   0.0252
  -4.000  -0.0118   0.01122   0.00431  -0.0839   0.6874   0.0260
  -3.750   0.0170   0.01108   0.00416  -0.0842   0.6860   0.0267
  -3.500   0.0458   0.01095   0.00402  -0.0845   0.6846   0.0273
  -3.250   0.0746   0.01083   0.00389  -0.0849   0.6830   0.0278
  -3.000   0.1035   0.01072   0.00378  -0.0852   0.6814   0.0284
  -2.750   0.1323   0.01062   0.00366  -0.0856   0.6798   0.0289
  -2.500   0.1611   0.01053   0.00356  -0.0859   0.6781   0.0293
  -2.250   0.1901   0.01042   0.00345  -0.0863   0.6756   0.0297
  -2.000   0.2191   0.01028   0.00333  -0.0867   0.6712   0.0301
  -1.750   0.2481   0.01015   0.00322  -0.0870   0.6658   0.0305
  -1.500   0.2772   0.01003   0.00311  -0.0874   0.6595   0.0316
  -1.250   0.3063   0.00991   0.00301  -0.0878   0.6468   0.0357
  -1.000   0.3349   0.00990   0.00310  -0.0880   0.6242   0.0911
  -0.750   0.3617   0.00977   0.00302  -0.0881   0.6056   0.1302
  -0.500   0.3892   0.00976   0.00296  -0.0883   0.5919   0.1331
  -0.250   0.4170   0.00977   0.00294  -0.0885   0.5792   0.1356
   0.000   0.4444   0.00981   0.00293  -0.0887   0.5595   0.1378
   0.250   0.4703   0.00997   0.00295  -0.0886   0.5221   0.1398
   0.500   0.4960   0.01017   0.00301  -0.0884   0.4892   0.1406
   1.000   0.5488   0.01055   0.00318  -0.0883   0.4372   0.1432
   1.250   0.5759   0.01074   0.00330  -0.0884   0.4210   0.1453
   1.500   0.6030   0.01088   0.00340  -0.0884   0.4089   0.1476
   1.750   0.6304   0.01095   0.00346  -0.0886   0.3993   0.1486
   2.000   0.6571   0.01107   0.00353  -0.0886   0.3853   0.1485
   2.250   0.6832   0.01122   0.00362  -0.0885   0.3630   0.1485
   2.500   0.7077   0.01150   0.00376  -0.0882   0.3293   0.1484
   2.750   0.7331   0.01170   0.00388  -0.0880   0.3095   0.1484
   3.000   0.7588   0.01186   0.00400  -0.0879   0.2932   0.1484
   3.500   0.8091   0.01224   0.00428  -0.0874   0.2650   0.1483
   3.750   0.8351   0.01236   0.00440  -0.0873   0.2611   0.1483
   4.000   0.8610   0.01247   0.00452  -0.0872   0.2576   0.1482
   4.250   0.8865   0.01261   0.00467  -0.0870   0.2522   0.1483
   4.500   0.9127   0.01269   0.00479  -0.0869   0.2479   0.1484
   4.750   0.9377   0.01284   0.00495  -0.0867   0.2408   0.1485
   5.000   0.9628   0.01298   0.00509  -0.0864   0.2313   0.1485
   5.250   0.9863   0.01321   0.00527  -0.0859   0.2140   0.1485
   5.500   1.0091   0.01347   0.00547  -0.0853   0.1978   0.1485
   5.750   1.0300   0.01383   0.00574  -0.0843   0.1757   0.1484
   6.000   1.0479   0.01434   0.00610  -0.0829   0.1477   0.1484
   6.250   1.0663   0.01479   0.00646  -0.0815   0.1291   0.1484
   6.500   1.0771   0.01562   0.00705  -0.0789   0.0824   0.1484
   6.750   1.0753   0.01681   0.00796  -0.0738   0.0223   0.1484
   7.000   1.0892   0.01721   0.00836  -0.0715   0.0156   0.1484
   7.250   1.1080   0.01755   0.00873  -0.0703   0.0135   0.1484
   7.500   1.1274   0.01791   0.00915  -0.0692   0.0124   0.1484
   7.750   1.1460   0.01833   0.00961  -0.0680   0.0114   0.1484
   8.000   1.1640   0.01879   0.01012  -0.0668   0.0103   0.1485
   8.250   1.1816   0.01929   0.01067  -0.0655   0.0096   0.1485
   8.500   1.2001   0.01974   0.01116  -0.0645   0.0092   0.1485
   8.750   1.2178   0.02023   0.01169  -0.0633   0.0086   0.1485
   9.000   1.2351   0.02076   0.01228  -0.0622   0.0081   0.1486
   9.250   1.2516   0.02134   0.01291  -0.0610   0.0077   0.1486
   9.500   1.2675   0.02198   0.01359  -0.0597   0.0073   0.1487
   9.750   1.2817   0.02275   0.01441  -0.0583   0.0068   0.1488
  10.000   1.2958   0.02354   0.01527  -0.0569   0.0065   0.1489
  10.250   1.3110   0.02428   0.01606  -0.0558   0.0064   0.1490
  10.500   1.3254   0.02507   0.01692  -0.0546   0.0062   0.1491
  10.750   1.3393   0.02593   0.01784  -0.0534   0.0060   0.1492
  11.250   1.3660   0.02778   0.01981  -0.0511   0.0055   0.1497
  11.500   1.3788   0.02876   0.02085  -0.0500   0.0053   0.1500
  11.750   1.3912   0.02980   0.02194  -0.0490   0.0051   0.1504
  12.000   1.4028   0.03092   0.02313  -0.0479   0.0049   0.1509
  12.250   1.4130   0.03218   0.02445  -0.0467   0.0047   0.1514
  12.500   1.4207   0.03367   0.02601  -0.0455   0.0046   0.1523
  12.750   1.4250   0.03552   0.02796  -0.0441   0.0044   0.1536
  13.000   1.4334   0.03705   0.02957  -0.0431   0.0043   0.1548
  13.250   1.4409   0.03869   0.03129  -0.0422   0.0043   0.1558
  13.500   1.4475   0.04041   0.03310  -0.0412   0.0042   0.1690
  13.750   1.4539   0.04219   0.03496  -0.0404   0.0041   0.1709
  14.000   1.4583   0.04417   0.03703  -0.0395   0.0040   0.1716
  14.250   1.4618   0.04629   0.03923  -0.0385   0.0040   0.1721
  14.500   1.4648   0.04849   0.04153  -0.0377   0.0039   0.1726
  14.750   1.4662   0.05094   0.04407  -0.0370   0.0038   0.1732
  15.000   1.4672   0.05353   0.04675  -0.0364   0.0038   0.1735
  15.250   1.4675   0.05626   0.04958  -0.0359   0.0037   0.1739
  15.500   1.4664   0.05925   0.05267  -0.0356   0.0036   0.1742
  15.750   1.4649   0.06240   0.05590  -0.0354   0.0036   0.1746
  16.250   1.4598   0.06924   0.06294  -0.0355   0.0035   0.1751
  16.500   1.4556   0.07302   0.06682  -0.0359   0.0034   0.1751
  16.750   1.4500   0.07711   0.07102  -0.0365   0.0034   0.1751
  17.000   1.4436   0.08143   0.07544  -0.0372   0.0033   0.1751
  17.250   1.4364   0.08593   0.08004  -0.0381   0.0033   0.1751
  17.500   1.4279   0.09068   0.08489  -0.0392   0.0033   0.1751
  17.750   1.4195   0.09552   0.08984  -0.0405   0.0032   0.1751
  18.000   1.4086   0.10082   0.09525  -0.0420   0.0032   0.1751
  18.250   1.3984   0.10609   0.10063  -0.0437   0.0032   0.1751
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