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WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: WORTMANN FX 05-H-126 AIRFOIL (fx05h126-il)
Reynolds number: 100,000
Max Cl/Cd: 24.34 at α=11°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx05h126-il-100000-n5.txt
Download as CSV file: xf-fx05h126-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 05-H-126 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
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.3695   0.10377   0.09850  -0.0039   0.6523   0.0585
  -8.500  -0.3675   0.10041   0.09516  -0.0066   0.6513   0.0604
  -8.250  -0.3717   0.09710   0.09189  -0.0110   0.6504   0.0623
  -8.000  -0.3844   0.09385   0.08868  -0.0173   0.6495   0.0631
  -7.750  -0.3902   0.09029   0.08505  -0.0225   0.6485   0.0635
  -7.500  -0.3893   0.08655   0.08121  -0.0265   0.6470   0.0637
  -7.250  -0.3843   0.08253   0.07710  -0.0291   0.6454   0.0638
  -7.000  -0.3706   0.07697   0.07164  -0.0293   0.6438   0.0646
  -6.750  -0.3587   0.07315   0.06779  -0.0301   0.6422   0.0652
  -6.500  -0.3522   0.06412   0.05837  -0.0335   0.6411   0.0425
  -6.250  -0.3361   0.06163   0.05589  -0.0334   0.6398   0.0405
  -6.000  -0.3230   0.05800   0.05210  -0.0344   0.6386   0.0395
  -5.750  -0.3085   0.05427   0.04810  -0.0352   0.6375   0.0395
  -5.500  -0.2924   0.05073   0.04426  -0.0356   0.6364   0.0397
  -5.250  -0.2751   0.04744   0.04065  -0.0357   0.6354   0.0391
  -5.000  -0.2567   0.04418   0.03704  -0.0354   0.6344   0.0381
  -4.750  -0.2368   0.04107   0.03349  -0.0349   0.6333   0.0372
  -4.500  -0.2139   0.03831   0.03034  -0.0350   0.6313   0.0366
  -4.250  -0.1902   0.03599   0.02758  -0.0348   0.6293   0.0363
  -4.000  -0.1657   0.03406   0.02526  -0.0345   0.6275   0.0363
  -3.750  -0.1404   0.03260   0.02349  -0.0344   0.6260   0.0370
  -3.500  -0.1146   0.03148   0.02208  -0.0342   0.6246   0.0388
  -3.250  -0.0881   0.03033   0.02061  -0.0340   0.6233   0.0400
  -3.000  -0.0613   0.02920   0.01920  -0.0337   0.6221   0.0405
  -2.750  -0.0343   0.02822   0.01801  -0.0334   0.6209   0.0410
  -2.500  -0.0076   0.02739   0.01699  -0.0330   0.6198   0.0418
  -2.250   0.0183   0.02661   0.01614  -0.0326   0.6187   0.0427
  -2.000   0.0456   0.02637   0.01597  -0.0335   0.6160   0.0444
  -1.750   0.0720   0.02630   0.01594  -0.0340   0.6139   0.0481
  -1.500   0.0977   0.02620   0.01577  -0.0341   0.6118   0.0516
  -1.250   0.1220   0.02594   0.01552  -0.0338   0.6098   0.0547
  -1.000   0.1468   0.02578   0.01528  -0.0334   0.6080   0.0599
  -0.750   0.1717   0.02559   0.01505  -0.0329   0.6066   0.0694
  -0.500   0.1966   0.02522   0.01485  -0.0325   0.6054   0.1118
   0.250   0.3740   0.02380   0.01572  -0.0526   0.5987   1.0000
   0.500   0.3975   0.02433   0.01615  -0.0527   0.5956   1.0000
   0.750   0.4206   0.02468   0.01637  -0.0522   0.5933   1.0000
   1.000   0.4436   0.02494   0.01651  -0.0515   0.5915   1.0000
   1.250   0.4668   0.02512   0.01657  -0.0506   0.5900   1.0000
   1.500   0.4901   0.02529   0.01663  -0.0496   0.5888   1.0000
   1.750   0.5108   0.02697   0.01837  -0.0515   0.5819   1.0000
   2.000   0.5328   0.02752   0.01887  -0.0511   0.5790   1.0000
   2.250   0.5556   0.02781   0.01910  -0.0504   0.5769   1.0000
   2.500   0.5788   0.02801   0.01924  -0.0495   0.5753   1.0000
   2.750   0.6025   0.02816   0.01932  -0.0486   0.5741   1.0000
   3.250   0.6375   0.03070   0.02193  -0.0491   0.5627   1.0000
   3.500   0.6606   0.03092   0.02214  -0.0483   0.5609   1.0000
   3.750   0.6847   0.03101   0.02220  -0.0473   0.5595   1.0000
   4.250   0.7133   0.03369   0.02499  -0.0470   0.5472   1.0000
   4.500   0.7373   0.03379   0.02509  -0.0461   0.5456   1.0000
   4.750   0.7627   0.03373   0.02503  -0.0451   0.5443   1.0000
   5.250   0.7869   0.03643   0.02786  -0.0443   0.5311   1.0000
   5.500   0.8131   0.03629   0.02775  -0.0434   0.5298   1.0000
   6.000   0.8114   0.04067   0.03222  -0.0418   0.5098   1.0000
   6.250   0.8273   0.04130   0.03289  -0.0407   0.5052   1.0000
   6.500   0.8532   0.04123   0.03290  -0.0400   0.5030   1.0000
   6.750   0.8799   0.04108   0.03282  -0.0393   0.5012   1.0000
   7.000   0.8682   0.04338   0.03514  -0.0370   0.4899   1.0000
   7.250   0.8889   0.04362   0.03546  -0.0361   0.4864   1.0000
   7.500   0.8901   0.04516   0.03705  -0.0345   0.4768   1.0000
   7.750   0.9124   0.04504   0.03703  -0.0336   0.4721   1.0000
   8.000   0.9234   0.04568   0.03774  -0.0324   0.4630   1.0000
   8.500   0.9633   0.04533   0.03757  -0.0303   0.4483   1.0000
   9.000   0.9887   0.04631   0.03876  -0.0282   0.4282   1.0000
   9.250   1.0144   0.04539   0.03795  -0.0272   0.4203   1.0000
   9.500   1.0264   0.04601   0.03865  -0.0262   0.4078   1.0000
   9.750   1.0420   0.04631   0.03904  -0.0252   0.3954   1.0000
  10.000   1.0611   0.04630   0.03915  -0.0243   0.3831   1.0000
  10.250   1.0816   0.04614   0.03907  -0.0233   0.3690   1.0000
  10.500   1.1010   0.04603   0.03901  -0.0222   0.3510   1.0000
  10.750   1.1177   0.04620   0.03917  -0.0211   0.3274   1.0000
  11.000   1.1320   0.04650   0.03937  -0.0198   0.2945   1.0000
  11.250   1.1395   0.04748   0.04010  -0.0184   0.2575   1.0000
  11.500   1.1385   0.04958   0.04195  -0.0173   0.2221   1.0000
  11.750   1.1348   0.05219   0.04433  -0.0164   0.1926   1.0000
  12.000   1.1314   0.05493   0.04690  -0.0158   0.1689   1.0000
  12.250   1.1300   0.05758   0.04944  -0.0152   0.1504   1.0000
  12.500   1.1307   0.06008   0.05188  -0.0148   0.1354   1.0000
  12.750   1.1334   0.06242   0.05420  -0.0144   0.1232   1.0000
  13.000   1.1374   0.06463   0.05641  -0.0140   0.1136   1.0000
  13.250   1.1407   0.06692   0.05867  -0.0136   0.1059   1.0000
  13.500   1.1476   0.06885   0.06068  -0.0132   0.0990   1.0000
  13.750   1.1517   0.07107   0.06286  -0.0129   0.0927   1.0000
  14.000   1.1566   0.07336   0.06523  -0.0128   0.0855   1.0000
  14.250   1.1590   0.07596   0.06783  -0.0128   0.0784   1.0000
  14.500   1.1601   0.07889   0.07081  -0.0131   0.0714   1.0000
  14.750   1.1626   0.08166   0.07367  -0.0134   0.0649   1.0000
  15.000   1.1650   0.08449   0.07660  -0.0137   0.0598   1.0000
  15.250   1.1668   0.08745   0.07963  -0.0141   0.0548   1.0000
  15.500   1.1688   0.09048   0.08284  -0.0146   0.0497   1.0000
  15.750   1.1669   0.09409   0.08646  -0.0154   0.0457   1.0000
  16.000   1.1685   0.09726   0.08983  -0.0159   0.0406   1.0000
  16.250   1.1659   0.10114   0.09376  -0.0169   0.0374   1.0000
  16.500   1.1653   0.10469   0.09742  -0.0176   0.0335   1.0000
  16.750   1.1628   0.10871   0.10153  -0.0189   0.0307   1.0000
  17.000   1.1596   0.11280   0.10566  -0.0201   0.0288   1.0000
  17.250   1.1588   0.11657   0.10960  -0.0211   0.0264   1.0000
  17.500   1.1559   0.12082   0.11395  -0.0227   0.0248   1.0000
  17.750   1.1529   0.12508   0.11829  -0.0243   0.0238   1.0000
  18.000   1.1510   0.12915   0.12247  -0.0257   0.0228   1.0000
  18.250   1.1494   0.13325   0.12676  -0.0272   0.0219   1.0000
  18.500   1.1466   0.13769   0.13137  -0.0290   0.0212   1.0000
  18.750   1.1422   0.14259   0.13645  -0.0312   0.0205   1.0000
  19.000   1.1375   0.14765   0.14166  -0.0337   0.0201   1.0000
  19.250   1.1321   0.15303   0.14718  -0.0365   0.0196   1.0000
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