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WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 77-W-343 AIRFOIL (fx77w343-il)
Reynolds number: 200,000
Max Cl/Cd: 20.76 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx77w343-il-200000-n5.txt
Download as CSV file: xf-fx77w343-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.8591   0.10767   0.09894  -0.0176   0.5010   0.0444
 -18.500  -0.8537   0.10485   0.09609  -0.0188   0.4984   0.0449
 -18.250  -0.8484   0.10204   0.09323  -0.0199   0.4958   0.0455
 -18.000  -0.8417   0.09943   0.09055  -0.0209   0.4933   0.0462
 -17.750  -0.8345   0.09690   0.08795  -0.0218   0.4910   0.0469
 -17.500  -0.8271   0.09440   0.08536  -0.0226   0.4889   0.0476
 -17.250  -0.8194   0.09197   0.08287  -0.0234   0.4869   0.0483
 -17.000  -0.8115   0.08953   0.08038  -0.0243   0.4851   0.0490
 -16.750  -0.8027   0.08725   0.07807  -0.0250   0.4834   0.0499
 -16.500  -0.7928   0.08512   0.07590  -0.0256   0.4815   0.0508
 -16.250  -0.7825   0.08304   0.07377  -0.0262   0.4796   0.0519
 -16.000  -0.7721   0.08099   0.07168  -0.0267   0.4776   0.0529
 -15.750  -0.7607   0.07908   0.06972  -0.0272   0.4756   0.0540
 -15.500  -0.7488   0.07725   0.06782  -0.0277   0.4737   0.0552
 -15.250  -0.7364   0.07548   0.06595  -0.0281   0.4719   0.0565
 -15.000  -0.7246   0.07369   0.06410  -0.0285   0.4703   0.0576
 -14.750  -0.7124   0.07195   0.06229  -0.0288   0.4687   0.0587
 -14.500  -0.6998   0.07028   0.06052  -0.0291   0.4673   0.0600
 -14.250  -0.6860   0.06872   0.05886  -0.0294   0.4660   0.0613
 -14.000  -0.6740   0.06702   0.05713  -0.0297   0.4649   0.0624
 -13.750  -0.6622   0.06531   0.05539  -0.0299   0.4637   0.0637
 -13.500  -0.6494   0.06372   0.05375  -0.0301   0.4626   0.0652
 -13.250  -0.6349   0.06232   0.05228  -0.0303   0.4613   0.0668
 -13.000  -0.6249   0.06055   0.05051  -0.0303   0.4602   0.0680
 -12.750  -0.6136   0.05891   0.04884  -0.0304   0.4591   0.0695
 -12.500  -0.6010   0.05740   0.04728  -0.0305   0.4579   0.0710
 -12.250  -0.5882   0.05593   0.04578  -0.0305   0.4568   0.0724
 -12.000  -0.5766   0.05440   0.04423  -0.0305   0.4557   0.0739
 -11.750  -0.5642   0.05295   0.04276  -0.0304   0.4547   0.0756
 -11.500  -0.5510   0.05159   0.04139  -0.0304   0.4537   0.0775
 -11.250  -0.5379   0.05026   0.04006  -0.0303   0.4527   0.0798
 -11.000  -0.5247   0.04896   0.03877  -0.0302   0.4518   0.0826
 -10.750  -0.5111   0.04772   0.03753  -0.0301   0.4509   0.0871
 -10.500  -0.4957   0.04666   0.03642  -0.0300   0.4499   0.0929
 -10.250  -0.4797   0.04567   0.03538  -0.0299   0.4490   0.0981
 -10.000  -0.4636   0.04471   0.03436  -0.0298   0.4480   0.1028
  -9.750  -0.4507   0.04357   0.03320  -0.0295   0.4471   0.1073
  -9.500  -0.4383   0.04241   0.03207  -0.0292   0.4464   0.1123
  -9.250  -0.4269   0.04121   0.03095  -0.0287   0.4458   0.1190
  -9.000  -0.4164   0.04003   0.02985  -0.0280   0.4452   0.1320
  -8.750  -0.4016   0.03913   0.02896  -0.0276   0.4445   0.1435
  -8.500  -0.3906   0.03803   0.02789  -0.0270   0.4438   0.1528
  -8.250  -0.3848   0.03665   0.02665  -0.0259   0.4431   0.1646
  -8.000  -0.3785   0.03534   0.02545  -0.0247   0.4424   0.1875
  -7.750  -0.3704   0.03415   0.02432  -0.0236   0.4415   0.2023
  -7.500  -0.3704   0.03257   0.02289  -0.0218   0.4407   0.2194
  -7.250  -0.3735   0.03113   0.02155  -0.0192   0.4399   0.2451
  -7.000  -0.3852   0.02980   0.02029  -0.0153   0.4391   0.2611
  -6.750  -0.3881   0.02799   0.01866  -0.0139   0.4383   0.2917
  -6.500  -0.3738   0.02630   0.01715  -0.0156   0.4373   0.3290
  -6.250  -0.3499   0.02485   0.01603  -0.0186   0.4362   0.3882
  -6.000  -0.3203   0.02437   0.01577  -0.0204   0.4349   0.4415
  -5.750  -0.2901   0.02447   0.01607  -0.0211   0.4338   0.4692
  -5.500  -0.2580   0.02449   0.01611  -0.0225   0.4327   0.4929
  -5.250  -0.2269   0.02488   0.01656  -0.0229   0.4319   0.5071
  -5.000  -0.1956   0.02530   0.01701  -0.0235   0.4311   0.5184
  -4.750  -0.1649   0.02602   0.01778  -0.0233   0.4303   0.5258
  -4.500  -0.1327   0.02629   0.01800  -0.0245   0.4294   0.5348
  -4.250  -0.1007   0.02668   0.01834  -0.0255   0.4285   0.5427
  -4.000  -0.0646   0.02619   0.01767  -0.0291   0.4274   0.5559
  -3.750  -0.0339   0.02674   0.01826  -0.0295   0.4268   0.5591
  -3.500  -0.0025   0.02714   0.01868  -0.0303   0.4261   0.5629
  -3.250   0.0301   0.02729   0.01882  -0.0319   0.4253   0.5682
  -3.000   0.0650   0.02710   0.01857  -0.0347   0.4244   0.5754
  -2.750   0.0951   0.02765   0.01915  -0.0351   0.4235   0.5774
  -2.500   0.1255   0.02820   0.01973  -0.0357   0.4226   0.5801
  -2.250   0.1564   0.02870   0.02025  -0.0365   0.4216   0.5838
  -2.000   0.1899   0.02888   0.02039  -0.0386   0.4206   0.5909
  -1.750   0.2210   0.02935   0.02085  -0.0397   0.4196   0.5952
  -1.500   0.2501   0.03004   0.02158  -0.0399   0.4186   0.5981
  -1.250   0.2800   0.03062   0.02216  -0.0405   0.4177   0.6023
  -1.000   0.3165   0.03052   0.02195  -0.0439   0.4167   0.6114
  -0.750   0.3447   0.03111   0.02256  -0.0440   0.4158   0.6131
  -0.500   0.3735   0.03156   0.02302  -0.0444   0.4148   0.6149
  -0.250   0.4029   0.03194   0.02338  -0.0450   0.4139   0.6170
   0.000   0.4333   0.03219   0.02360  -0.0460   0.4130   0.6199
   0.250   0.4665   0.03223   0.02355  -0.0480   0.4121   0.6243
   0.500   0.5033   0.03203   0.02321  -0.0513   0.4113   0.6297
   0.750   0.5323   0.03232   0.02348  -0.0519   0.4106   0.6308
   1.000   0.5614   0.03266   0.02380  -0.0525   0.4098   0.6319
   1.250   0.5903   0.03307   0.02417  -0.0533   0.4091   0.6332
   1.500   0.6155   0.03360   0.02480  -0.0538   0.4082   0.6346
   1.750   0.6393   0.03422   0.02551  -0.0543   0.4070   0.6361
   2.000   0.6619   0.03489   0.02628  -0.0547   0.4057   0.6378
   2.250   0.6836   0.03560   0.02708  -0.0552   0.4042   0.6399
   2.500   0.7045   0.03632   0.02786  -0.0557   0.4028   0.6423
   2.750   0.7255   0.03700   0.02858  -0.0565   0.4013   0.6450
   3.000   0.7475   0.03762   0.02919  -0.0577   0.3999   0.6480
   3.250   0.7645   0.03835   0.02996  -0.0576   0.3986   0.6495
   3.500   0.7780   0.03912   0.03078  -0.0568   0.3974   0.6505
   3.750   0.7905   0.03984   0.03154  -0.0558   0.3962   0.6515
   4.000   0.7979   0.04059   0.03233  -0.0540   0.3951   0.6525
   4.250   0.8046   0.04133   0.03309  -0.0523   0.3941   0.6536
   4.500   0.8247   0.04177   0.03351  -0.0523   0.3933   0.6549
   4.750   0.8503   0.04204   0.03374  -0.0528   0.3926   0.6565
   5.000   0.8777   0.04228   0.03394  -0.0536   0.3919   0.6582
   6.500   0.3991   0.11206   0.10503  -0.0452   0.3302   0.6634
   6.750   0.4206   0.11304   0.10597  -0.0464   0.3293   0.6651
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