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WORTMANN FX 77-W-258 AIRFOIL (fx77w258-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 77-W-258 AIRFOIL (fx77w258-il)
Reynolds number: 100,000
Max Cl/Cd: 10.51 at α=2°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx77w258-il-100000-n5.txt
Download as CSV file: xf-fx77w258-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 77-W-258 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.5747   0.13649   0.12962  -0.0145   0.5725   0.0384
 -17.000  -0.6573   0.11427   0.10702  -0.0281   0.5800   0.0373
 -16.750  -0.6920   0.10372   0.09616  -0.0344   0.5798   0.0371
 -16.500  -0.7129   0.09625   0.08839  -0.0387   0.5775   0.0372
 -16.250  -0.7277   0.09017   0.08202  -0.0418   0.5746   0.0375
 -16.000  -0.7392   0.08487   0.07645  -0.0444   0.5712   0.0379
 -15.750  -0.7482   0.08012   0.07143  -0.0464   0.5675   0.0383
 -15.500  -0.7452   0.07728   0.06853  -0.0475   0.5628   0.0388
 -15.250  -0.7420   0.07455   0.06571  -0.0484   0.5586   0.0394
 -15.000  -0.7397   0.07176   0.06278  -0.0493   0.5550   0.0400
 -14.750  -0.7374   0.06900   0.05985  -0.0500   0.5518   0.0407
 -14.500  -0.7349   0.06629   0.05697  -0.0505   0.5483   0.0414
 -14.250  -0.7320   0.06368   0.05413  -0.0509   0.5450   0.0422
 -14.000  -0.7228   0.06191   0.05236  -0.0511   0.5415   0.0428
 -13.750  -0.7140   0.06015   0.05053  -0.0511   0.5384   0.0434
 -13.500  -0.7052   0.05841   0.04869  -0.0511   0.5356   0.0441
 -13.250  -0.6954   0.05677   0.04691  -0.0510   0.5332   0.0449
 -13.000  -0.6843   0.05517   0.04518  -0.0509   0.5307   0.0457
 -12.750  -0.6720   0.05369   0.04361  -0.0507   0.5281   0.0464
 -12.500  -0.6598   0.05234   0.04225  -0.0505   0.5256   0.0471
 -12.250  -0.6468   0.05106   0.04092  -0.0503   0.5231   0.0477
 -12.000  -0.6331   0.04982   0.03961  -0.0500   0.5208   0.0485
 -11.750  -0.6187   0.04864   0.03835  -0.0497   0.5186   0.0493
 -11.500  -0.6038   0.04752   0.03712  -0.0493   0.5164   0.0502
 -11.250  -0.5897   0.04642   0.03595  -0.0489   0.5143   0.0511
 -11.000  -0.5753   0.04539   0.03484  -0.0486   0.5124   0.0522
 -10.750  -0.5599   0.04439   0.03379  -0.0483   0.5102   0.0537
 -10.500  -0.5439   0.04343   0.03278  -0.0479   0.5080   0.0554
 -10.250  -0.5286   0.04246   0.03180  -0.0476   0.5059   0.0574
 -10.000  -0.5115   0.04162   0.03087  -0.0472   0.5039   0.0599
  -9.750  -0.4961   0.04070   0.02994  -0.0468   0.5021   0.0622
  -9.500  -0.4792   0.03989   0.02905  -0.0463   0.5004   0.0652
  -9.250  -0.4644   0.03897   0.02812  -0.0458   0.4987   0.0679
  -9.000  -0.4487   0.03812   0.02723  -0.0452   0.4972   0.0710
  -8.750  -0.4338   0.03725   0.02635  -0.0446   0.4958   0.0740
  -8.500  -0.4185   0.03643   0.02553  -0.0440   0.4944   0.0774
  -8.250  -0.4025   0.03568   0.02477  -0.0434   0.4932   0.0816
  -8.000  -0.3860   0.03500   0.02409  -0.0428   0.4919   0.0873
  -7.500  -0.3521   0.03376   0.02287  -0.0416   0.4894   0.1029
  -7.250  -0.3379   0.03312   0.02231  -0.0407   0.4881   0.1110
  -7.000  -0.3255   0.03248   0.02183  -0.0396   0.4868   0.1214
  -6.750  -0.3127   0.03197   0.02141  -0.0383   0.4854   0.1401
  -6.500  -0.3024   0.03141   0.02099  -0.0368   0.4842   0.1589
  -6.250  -0.2911   0.03074   0.02051  -0.0358   0.4829   0.1886
  -6.000  -0.2804   0.02992   0.01993  -0.0349   0.4814   0.2207
  -5.750  -0.2688   0.02906   0.01932  -0.0342   0.4798   0.2669
  -5.500  -0.2564   0.02820   0.01878  -0.0335   0.4783   0.3243
  -5.250  -0.2403   0.02771   0.01875  -0.0325   0.4768   0.3949
  -5.000  -0.2135   0.02896   0.02051  -0.0297   0.4753   0.4672
  -4.750  -0.1813   0.03067   0.02234  -0.0275   0.4738   0.5097
  -4.500  -0.1528   0.03149   0.02309  -0.0269   0.4724   0.5361
  -4.250  -0.1291   0.03147   0.02290  -0.0275   0.4711   0.5620
  -3.750  -0.0790   0.03216   0.02349  -0.0286   0.4676   0.5972
  -3.500  -0.0515   0.03323   0.02457  -0.0277   0.4657   0.6050
  -3.250  -0.0267   0.03343   0.02468  -0.0285   0.4638   0.6190
  -3.000  -0.0002   0.03438   0.02562  -0.0274   0.4618   0.6264
  -2.750   0.0250   0.03477   0.02591  -0.0277   0.4600   0.6389
  -2.500   0.0510   0.03572   0.02685  -0.0261   0.4583   0.6446
  -2.250   0.0765   0.03578   0.02678  -0.0272   0.4568   0.6573
  -2.000   0.1015   0.03657   0.02755  -0.0255   0.4555   0.6610
  -1.750   0.1269   0.03718   0.02811  -0.0244   0.4543   0.6660
  -1.500   0.1523   0.03737   0.02820  -0.0246   0.4532   0.6744
  -1.250   0.1780   0.03747   0.02819  -0.0250   0.4521   0.6806
  -1.000   0.2032   0.03784   0.02850  -0.0242   0.4511   0.6835
  -0.750   0.2237   0.03853   0.02924  -0.0236   0.4495   0.6872
  -0.500   0.2409   0.03938   0.03021  -0.0236   0.4472   0.6920
  -0.250   0.2601   0.04008   0.03095  -0.0249   0.4448   0.6979
   0.000   0.2779   0.04085   0.03176  -0.0252   0.4424   0.7011
   0.250   0.2943   0.04166   0.03261  -0.0246   0.4402   0.7030
   0.500   0.3122   0.04236   0.03332  -0.0241   0.4383   0.7050
   0.750   0.3311   0.04299   0.03394  -0.0238   0.4366   0.7075
   1.000   0.3515   0.04352   0.03445  -0.0237   0.4351   0.7105
   1.250   0.3756   0.04382   0.03469  -0.0240   0.4338   0.7139
   1.500   0.4035   0.04395   0.03472  -0.0250   0.4327   0.7177
   1.750   0.4357   0.04398   0.03462  -0.0270   0.4316   0.7216
   2.000   0.4633   0.04407   0.03463  -0.0274   0.4307   0.7232
   2.500   0.2375   0.06797   0.05954  -0.0226   0.4005   0.7278
   4.500   0.3336   0.08285   0.07426  -0.0293   0.3784   0.7414
   4.750   0.3574   0.08381   0.07516  -0.0305   0.3770   0.7436
   5.000   0.3802   0.08459   0.07591  -0.0310   0.3758   0.7450
   5.250   0.4037   0.08521   0.07650  -0.0314   0.3749   0.7460
   5.500   0.4282   0.08577   0.07703  -0.0317   0.3741   0.7470
   6.000   0.3918   0.09592   0.08737  -0.0336   0.3617   0.7492
   6.250   0.4093   0.09729   0.08872  -0.0341   0.3601   0.7505
   6.500   0.4301   0.09835   0.08976  -0.0347   0.3587   0.7516
   6.750   0.4541   0.09906   0.09045  -0.0352   0.3576   0.7526
   7.000   0.4794   0.09962   0.09098  -0.0358   0.3566   0.7537
   7.500   0.4678   0.10693   0.09838  -0.0378   0.3441   0.7554
   7.750   0.4891   0.10789   0.09933  -0.0385   0.3424   0.7564
   8.000   0.5123   0.10867   0.10009  -0.0392   0.3410   0.7575
   8.250   0.5361   0.10939   0.10078  -0.0398   0.3400   0.7586
   8.500   0.5606   0.11009   0.10147  -0.0404   0.3392   0.7597
   9.000   0.5388   0.11927   0.11079  -0.0431   0.3275   0.7612
   9.250   0.5584   0.12055   0.11207  -0.0440   0.3258   0.7623
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