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WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il)
Reynolds number: 100,000
Max Cl/Cd: 1.75 at α=-2.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx77w343-il-100000-n5.txt
Download as CSV file: xf-fx77w343-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 77-W-343 AIRFOIL                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.8224   0.12384   0.11511  -0.0181   0.5745   0.0602
 -19.500  -0.8301   0.11883   0.10981  -0.0208   0.5701   0.0611
 -19.250  -0.8290   0.11530   0.10607  -0.0225   0.5656   0.0620
 -19.000  -0.8181   0.11326   0.10402  -0.0235   0.5596   0.0627
 -18.750  -0.8102   0.11080   0.10148  -0.0246   0.5544   0.0636
 -18.500  -0.8039   0.10810   0.09865  -0.0258   0.5499   0.0646
 -18.250  -0.7986   0.10529   0.09565  -0.0269   0.5463   0.0657
 -18.000  -0.7947   0.10226   0.09240  -0.0281   0.5429   0.0667
 -17.750  -0.7790   0.10102   0.09121  -0.0285   0.5386   0.0676
 -17.500  -0.7659   0.09940   0.08957  -0.0290   0.5350   0.0686
 -17.000  -0.7442   0.09552   0.08548  -0.0302   0.5289   0.0711
 -16.750  -0.7324   0.09375   0.08360  -0.0307   0.5264   0.0723
 -16.500  -0.7184   0.09230   0.08217  -0.0311   0.5238   0.0733
 -16.250  -0.7059   0.09063   0.08050  -0.0315   0.5212   0.0746
 -16.000  -0.6937   0.08890   0.07872  -0.0320   0.5187   0.0760
 -15.750  -0.6811   0.08723   0.07700  -0.0324   0.5163   0.0775
 -15.500  -0.6696   0.08550   0.07528  -0.0328   0.5142   0.0789
 -15.250  -0.6585   0.08369   0.07344  -0.0333   0.5121   0.0805
 -15.000  -0.6464   0.08200   0.07166  -0.0336   0.5102   0.0825
 -14.750  -0.6350   0.08027   0.06989  -0.0340   0.5084   0.0843
 -14.500  -0.6230   0.07860   0.06815  -0.0344   0.5066   0.0865
 -14.250  -0.6094   0.07711   0.06658  -0.0347   0.5047   0.0891
 -14.000  -0.5970   0.07548   0.06498  -0.0350   0.5027   0.0915
 -13.750  -0.5828   0.07406   0.06350  -0.0353   0.5006   0.0948
 -13.500  -0.5700   0.07257   0.06201  -0.0355   0.4986   0.0979
 -13.250  -0.5560   0.07119   0.06057  -0.0357   0.4967   0.1020
 -13.000  -0.5447   0.06963   0.05904  -0.0358   0.4951   0.1056
 -12.750  -0.5324   0.06817   0.05757  -0.0359   0.4935   0.1100
 -12.500  -0.5221   0.06655   0.05600  -0.0359   0.4921   0.1143
 -12.250  -0.5112   0.06499   0.05447  -0.0360   0.4908   0.1195
 -12.000  -0.5002   0.06347   0.05298  -0.0360   0.4895   0.1261
 -11.750  -0.4879   0.06209   0.05157  -0.0360   0.4883   0.1350
 -11.500  -0.4754   0.06077   0.05021  -0.0359   0.4872   0.1447
 -11.250  -0.4649   0.05935   0.04881  -0.0358   0.4862   0.1543
 -11.000  -0.4566   0.05774   0.04733  -0.0356   0.4852   0.1649
 -10.750  -0.4478   0.05618   0.04589  -0.0354   0.4841   0.1807
 -10.500  -0.4368   0.05482   0.04459  -0.0352   0.4829   0.1982
 -10.250  -0.4307   0.05323   0.04319  -0.0347   0.4819   0.2142
 -10.000  -0.4237   0.05173   0.04184  -0.0343   0.4807   0.2373
  -9.750  -0.4155   0.05041   0.04067  -0.0337   0.4796   0.2593
  -9.500  -0.4073   0.04930   0.03980  -0.0329   0.4785   0.2843
  -9.250  -0.3969   0.04833   0.03896  -0.0322   0.4774   0.3115
  -9.000  -0.3749   0.04856   0.03948  -0.0316   0.4762   0.3378
  -8.750  -0.3551   0.04850   0.03954  -0.0311   0.4750   0.3662
  -8.500  -0.3201   0.04976   0.04095  -0.0312   0.4737   0.3865
  -8.250  -0.2858   0.05094   0.04221  -0.0314   0.4725   0.4028
  -8.000  -0.2769   0.04992   0.04115  -0.0307   0.4716   0.4220
  -7.750  -0.2734   0.04850   0.03966  -0.0296   0.4707   0.4398
  -7.500  -0.2360   0.04986   0.04098  -0.0300   0.4694   0.4474
  -7.250  -0.2230   0.04926   0.04031  -0.0293   0.4684   0.4606
  -7.000  -0.1948   0.04994   0.04091  -0.0292   0.4672   0.4687
  -6.750  -0.1870   0.04907   0.03995  -0.0282   0.4664   0.4816
  -6.250  -0.1601   0.04860   0.03953  -0.0268   0.4642   0.5008
  -6.000  -0.1268   0.04988   0.04084  -0.0274   0.4625   0.5046
  -5.750  -0.1345   0.04884   0.03982  -0.0247   0.4611   0.5177
  -5.500  -0.0956   0.05046   0.04144  -0.0256   0.4589   0.5210
  -5.250  -0.0608   0.05174   0.04271  -0.0262   0.4568   0.5254
  -5.000  -0.0769   0.05071   0.04168  -0.0222   0.4557   0.5380
  -4.750  -0.0343   0.05228   0.04322  -0.0235   0.4540   0.5415
  -4.500  -0.0582   0.05083   0.04174  -0.0193   0.4531   0.5562
  -4.250  -0.0175   0.05244   0.04332  -0.0201   0.4518   0.5587
  -4.000   0.0173   0.05361   0.04444  -0.0206   0.4507   0.5624
  -3.750   0.0067   0.05242   0.04320  -0.0183   0.4499   0.5756
  -3.500   0.0419   0.05357   0.04429  -0.0186   0.4489   0.5778
  -3.000   0.0699   0.05328   0.04386  -0.0179   0.4473   0.5926
  -2.750   0.0921   0.05412   0.04471  -0.0177   0.4461   0.5949
  -2.500   0.0988   0.05632   0.04718  -0.0167   0.4435   0.5969
  -2.250   0.0851   0.05946   0.05062  -0.0142   0.4398   0.6002
  -2.000   0.0250   0.06233   0.05374  -0.0109   0.4347   0.6115
  -1.750   0.0247   0.06412   0.05557  -0.0084   0.4323   0.6132
  -1.500   0.0369   0.06499   0.05641  -0.0069   0.4308   0.6156
  -1.000   0.0643   0.06444   0.05567  -0.0084   0.4285   0.6296
  -0.750   0.0846   0.06485   0.05602  -0.0072   0.4277   0.6311
   2.250  -0.0479   0.10572   0.09737  -0.0033   0.3803   0.6619
   2.500  -0.0258   0.10683   0.09842  -0.0056   0.3787   0.6651
   2.750   0.0051   0.10776   0.09921  -0.0100   0.3773   0.6695
   3.000   0.0251   0.10856   0.09999  -0.0101   0.3763   0.6707
   3.250   0.0469   0.10929   0.10068  -0.0103   0.3754   0.6720
   3.500   0.0699   0.10997   0.10132  -0.0106   0.3746   0.6734
   4.000   0.0449   0.11780   0.10931  -0.0111   0.3651   0.6761
   4.250   0.0621   0.11909   0.11057  -0.0119   0.3629   0.6780
   4.500   0.0832   0.12014   0.11158  -0.0130   0.3612   0.6802
   4.750   0.1071   0.12112   0.11252  -0.0145   0.3600   0.6826
   5.000   0.1332   0.12212   0.11345  -0.0165   0.3591   0.6852
   5.250   0.1627   0.12311   0.11436  -0.0191   0.3583   0.6882
   5.500   0.1919   0.12405   0.11522  -0.0214   0.3576   0.6908
   6.000   0.1618   0.13262   0.12399  -0.0223   0.3489   0.6928
   6.250   0.1753   0.13435   0.12573  -0.0229   0.3474   0.6943
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