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WORTMANN FX 75-193 (fx75193-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: WORTMANN FX 75-193 (fx75193-il)
Reynolds number: 100,000
Max Cl/Cd: 23.4 at α=12.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fx75193-il-100000.txt
Download as CSV file: xf-fx75193-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WORTMANN FX 75-193                              
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.3214   0.12186   0.11739  -0.0934   0.9458   0.1329
 -10.750  -0.2947   0.12058   0.11608  -0.0882   0.9446   0.1343
 -10.500  -0.2923   0.11950   0.11502  -0.0847   0.9430   0.1365
 -10.250  -0.3005   0.11775   0.11331  -0.0826   0.9411   0.1398
 -10.000  -0.4091   0.11310   0.10888  -0.0851   0.9420   0.1452
  -9.750  -0.3520   0.11246   0.10819  -0.0799   0.9399   0.1475
  -9.500  -0.5148   0.12959   0.12578  -0.0316   1.0000   0.1299
  -9.250  -0.5542   0.12346   0.11976  -0.0348   1.0000   0.1340
  -9.000  -0.5393   0.12234   0.11863  -0.0316   1.0000   0.1363
  -8.750  -0.5459   0.11954   0.11586  -0.0308   1.0000   0.1397
  -8.500  -0.6489   0.10992   0.10633  -0.0378   1.0000   0.1448
  -8.250  -0.5984   0.10972   0.10617  -0.0328   1.0000   0.1484
  -8.000  -0.6041   0.10705   0.10352  -0.0315   1.0000   0.1514
  -7.750  -0.6472   0.10162   0.09813  -0.0322   1.0000   0.1546
  -7.500  -0.7018   0.09739   0.09391  -0.0303   1.0000   0.1553
  -7.250  -0.7670   0.09256   0.08892  -0.0298   1.0000   0.1572
  -7.000  -0.8307   0.06680   0.06098  -0.0334   0.9987   0.0703
  -6.750  -0.8053   0.06795   0.06264  -0.0355   0.9945   0.0868
  -6.500  -0.7896   0.05473   0.04748  -0.0351   0.9919   0.0521
  -6.250  -0.7694   0.05199   0.04444  -0.0352   0.9874   0.0510
  -6.000  -0.7418   0.04938   0.04131  -0.0363   0.9822   0.0497
  -5.750  -0.7104   0.04796   0.03943  -0.0376   0.9788   0.0494
  -5.500  -0.6884   0.04611   0.03733  -0.0371   0.9711   0.0497
  -5.250  -0.6571   0.04520   0.03618  -0.0381   0.9661   0.0510
  -5.000  -0.6270   0.04499   0.03567  -0.0387   0.9632   0.0526
  -4.750  -0.6084   0.04357   0.03435  -0.0376   0.9537   0.0550
  -4.500  -0.5776   0.04358   0.03434  -0.0387   0.9493   0.0603
  -4.250  -0.5596   0.04286   0.03365  -0.0377   0.9413   0.0668
  -4.000  -0.5328   0.04235   0.03325  -0.0379   0.9345   0.0778
  -3.750  -0.5036   0.04223   0.03344  -0.0391   0.9311   0.1045
  -3.500  -0.4918   0.04108   0.03248  -0.0375   0.9210   0.1294
  -3.250  -0.4633   0.04084   0.03269  -0.0389   0.9153   0.1795
  -2.750  -0.4434   0.04335   0.03777  -0.0293   0.8983   0.6612
  -2.500  -0.4159   0.04710   0.04131  -0.0266   0.8939   0.6936
  -2.250  -0.4191   0.04700   0.04119  -0.0198   0.8819   0.7049
  -2.000  -0.3950   0.04902   0.04306  -0.0174   0.8763   0.7229
  -1.750  -0.3920   0.04929   0.04325  -0.0127   0.8685   0.7348
  -1.500  -0.3789   0.05012   0.04397  -0.0087   0.8605   0.7520
  -1.250  -0.3612   0.05203   0.04580  -0.0045   0.8566   0.7764
  -1.000  -0.3716   0.05134   0.04511   0.0029   0.8469   0.7919
  -0.750  -0.3628   0.05203   0.04574   0.0086   0.8403   0.8183
  -0.500  -0.3434   0.05378   0.04740   0.0130   0.8371   0.8444
  -0.250  -0.3601   0.05194   0.04554   0.0198   0.8273   0.8559
   0.000  -0.3386   0.05237   0.04584   0.0208   0.8217   0.8692
   0.250  -0.2986   0.05406   0.04736   0.0179   0.8187   0.8738
   0.500  -0.3114   0.05221   0.04548   0.0227   0.8085   0.8779
   0.750  -0.2819   0.05286   0.04597   0.0209   0.8035   0.8820
   1.000  -0.2406   0.05477   0.04773   0.0175   0.8008   0.8854
   1.250  -0.2543   0.05284   0.04579   0.0222   0.7906   0.8880
   1.500  -0.2214   0.05367   0.04650   0.0200   0.7860   0.8897
   2.000  -0.1939   0.05408   0.04677   0.0206   0.7746   0.8940
   2.250  -0.1595   0.05500   0.04759   0.0182   0.7690   0.8964
   2.500  -0.1201   0.05691   0.04938   0.0148   0.7663   0.8978
   2.750  -0.1300   0.05591   0.04839   0.0179   0.7589   0.8995
   3.000  -0.0941   0.05689   0.04928   0.0153   0.7528   0.9007
   3.250  -0.0662   0.05824   0.05057   0.0136   0.7498   0.9022
   3.500  -0.0637   0.05780   0.05014   0.0153   0.7410   0.9040
   3.750  -0.0152   0.05949   0.05174   0.0115   0.7356   0.9061
   4.000  -0.0223   0.05915   0.05142   0.0141   0.7282   0.9085
   4.250   0.0260   0.06051   0.05271   0.0103   0.7212   0.9100
   4.500   0.0670   0.05816   0.05026   0.0096   0.6840   0.9113
   4.750   0.1162   0.05844   0.05049   0.0064   0.6770   0.9131
   5.000   0.1221   0.05896   0.05101   0.0073   0.6665   0.9151
   5.250   0.1677   0.05928   0.05130   0.0044   0.6612   0.9168
   5.500   0.1694   0.06025   0.05231   0.0055   0.6526   0.9183
   5.750   0.2052   0.06064   0.05270   0.0035   0.6466   0.9197
   6.000   0.2213   0.06139   0.05346   0.0034   0.6375   0.9213
   6.250   0.2503   0.06192   0.05401   0.0020   0.6311   0.9233
   6.500   0.3008   0.06205   0.05416  -0.0010   0.6275   0.9255
   6.750   0.2952   0.06338   0.05553   0.0004   0.6157   0.9272
   7.000   0.3415   0.06348   0.05566  -0.0023   0.6114   0.9288
   7.250   0.3430   0.06495   0.05717  -0.0016   0.6002   0.9301
   7.500   0.3818   0.06524   0.05750  -0.0038   0.5951   0.9315
   7.750   0.4310   0.06522   0.05755  -0.0067   0.5924   0.9332
   8.000   0.4180   0.06747   0.05987  -0.0052   0.5795   0.9349
   8.250   0.4639   0.06734   0.05981  -0.0076   0.5758   0.9374
   8.500   0.4620   0.06938   0.06192  -0.0070   0.5638   0.9394
   8.750   0.5040   0.06928   0.06192  -0.0091   0.5589   0.9417
   9.000   0.5554   0.06857   0.06129  -0.0117   0.5560   0.9438
   9.250   0.5502   0.07092   0.06373  -0.0111   0.5418   0.9453
   9.750   0.5903   0.07338   0.06641  -0.0132   0.5251   0.9498
  10.000   0.6385   0.07262   0.06579  -0.0155   0.5215   0.9535
  10.250   0.6343   0.07577   0.06904  -0.0157   0.5082   0.9565
  10.500   0.6796   0.07518   0.06862  -0.0179   0.5039   0.9610
  10.750   0.7338   0.07349   0.06710  -0.0201   0.5009   0.9682
  11.250   0.7283   0.07884   0.07264  -0.0197   0.4731   1.0000
  11.500   0.7717   0.07761   0.07158  -0.0209   0.4679   1.0000
  11.750   0.8173   0.07559   0.06973  -0.0218   0.4617   1.0000
  12.000   0.9399   0.06317   0.05763  -0.0233   0.4642   1.0000
  12.250   0.9499   0.06391   0.05850  -0.0227   0.4487   1.0000
  12.500   1.0485   0.05295   0.04777  -0.0231   0.4378   1.0000
  12.750   1.1113   0.04750   0.04232  -0.0236   0.4078   1.0000
  13.000   1.1091   0.04975   0.04463  -0.0224   0.3800   1.0000
  13.250   1.1154   0.05111   0.04584  -0.0214   0.3393   1.0000
  13.500   1.1109   0.05369   0.04813  -0.0201   0.2857   1.0000
  13.750   1.0940   0.05775   0.05173  -0.0187   0.2200   1.0000
  14.000   1.0703   0.06292   0.05638  -0.0176   0.1614   1.0000
  14.250   1.0488   0.06822   0.06123  -0.0170   0.1211   1.0000
  14.500   1.0340   0.07300   0.06570  -0.0167   0.0964   1.0000
  14.750   1.0290   0.07676   0.06927  -0.0166   0.0820   1.0000
  15.000   1.0329   0.07944   0.07184  -0.0164   0.0709   1.0000
  15.250   1.0462   0.08094   0.07320  -0.0162   0.0632   1.0000
  15.500   1.0669   0.08167   0.07385  -0.0159   0.0575   1.0000
  15.750   1.0911   0.08218   0.07429  -0.0159   0.0530   1.0000
  16.000   1.1232   0.08198   0.07395  -0.0158   0.0497   1.0000
  16.250   1.1544   0.08235   0.07445  -0.0158   0.0475   1.0000
  16.500   1.1968   0.08206   0.07410  -0.0161   0.0458   1.0000
  16.750   1.2329   0.08306   0.07524  -0.0166   0.0448   1.0000
  17.000   1.2519   0.08546   0.07794  -0.0169   0.0444   1.0000
  17.250   1.2635   0.08850   0.08128  -0.0173   0.0441   1.0000
  17.500   1.2699   0.09194   0.08501  -0.0177   0.0441   1.0000
  17.750   1.2718   0.09574   0.08910  -0.0182   0.0442   1.0000
  18.000   1.2695   0.09989   0.09353  -0.0188   0.0443   1.0000
  18.250   1.2640   0.10432   0.09822  -0.0197   0.0445   1.0000
  18.500   1.2564   0.10896   0.10312  -0.0209   0.0447   1.0000
  18.750   1.2507   0.11358   0.10795  -0.0222   0.0450   1.0000
  19.000   1.2486   0.11806   0.11261  -0.0236   0.0453   1.0000
  19.250   1.1751   0.12937   0.12453  -0.0287   0.0464   1.0000
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