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FX S 02-196 AIRFOIL (fxs02196-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: FX S 02-196 AIRFOIL (fxs02196-il)
Reynolds number: 100,000
Max Cl/Cd: 37.48 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxs02196-il-100000-n5.txt
Download as CSV file: xf-fxs02196-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX S 02-196 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
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.3198   0.11434   0.10950  -0.0666   1.0000   0.0317
 -13.500  -0.3480   0.09947   0.09462  -0.0751   0.9794   0.0318
 -13.000  -0.4645   0.06815   0.06258  -0.0994   0.9397   0.0296
 -12.750  -0.4609   0.06358   0.05780  -0.1052   0.9192   0.0304
 -12.250  -0.4777   0.05440   0.04793  -0.1130   0.8791   0.0314
 -12.000  -0.4913   0.05087   0.04401  -0.1142   0.8601   0.0321
 -11.750  -0.5073   0.04779   0.04048  -0.1142   0.8430   0.0327
 -11.500  -0.4974   0.04646   0.03910  -0.1140   0.8294   0.0337
 -11.250  -0.4984   0.04465   0.03704  -0.1132   0.8165   0.0349
 -11.000  -0.5033   0.04264   0.03470  -0.1118   0.8039   0.0356
 -10.750  -0.5096   0.04090   0.03251  -0.1095   0.7935   0.0363
 -10.500  -0.4921   0.03946   0.03105  -0.1090   0.7834   0.0371
 -10.250  -0.4782   0.03810   0.02949  -0.1081   0.7750   0.0381
 -10.000  -0.4628   0.03663   0.02780  -0.1073   0.7660   0.0388
  -9.750  -0.4420   0.03519   0.02612  -0.1068   0.7579   0.0393
  -9.500  -0.4179   0.03390   0.02458  -0.1064   0.7511   0.0398
  -9.250  -0.3901   0.03276   0.02333  -0.1064   0.7432   0.0403
  -9.000  -0.3600   0.03178   0.02234  -0.1064   0.7366   0.0410
  -8.750  -0.3342   0.03099   0.02149  -0.1059   0.7308   0.0416
  -8.500  -0.3122   0.03030   0.02077  -0.1051   0.7236   0.0424
  -8.250  -0.2927   0.02964   0.02005  -0.1040   0.7172   0.0431
  -8.000  -0.2760   0.02901   0.01932  -0.1028   0.7120   0.0441
  -7.750  -0.2648   0.02836   0.01872  -0.1012   0.7053   0.0450
  -7.500  -0.2539   0.02773   0.01807  -0.0997   0.6989   0.0461
  -7.250  -0.2410   0.02708   0.01733  -0.0984   0.6937   0.0473
  -7.000  -0.2277   0.02646   0.01664  -0.0971   0.6889   0.0484
  -6.750  -0.2139   0.02589   0.01607  -0.0960   0.6833   0.0496
  -6.500  -0.1984   0.02535   0.01547  -0.0950   0.6784   0.0511
  -6.250  -0.1813   0.02482   0.01486  -0.0942   0.6743   0.0532
  -6.000  -0.1625   0.02432   0.01421  -0.0935   0.6708   0.0567
  -5.750  -0.1435   0.02390   0.01369  -0.0928   0.6665   0.0621
  -5.500  -0.1244   0.02344   0.01315  -0.0923   0.6621   0.0689
  -5.250  -0.1059   0.02279   0.01256  -0.0919   0.6581   0.0777
  -5.000  -0.0849   0.02224   0.01201  -0.0917   0.6546   0.1059
  -4.750  -0.0644   0.02141   0.01134  -0.0918   0.6516   0.1535
  -4.500  -0.0455   0.02007   0.01050  -0.0924   0.6490   0.2666
  -4.250  -0.0256   0.01983   0.01108  -0.0917   0.6452   0.3974
  -4.000   0.0012   0.01988   0.01103  -0.0919   0.6415   0.4467
  -3.750   0.0281   0.02004   0.01112  -0.0919   0.6380   0.4663
  -3.500   0.0562   0.02009   0.01098  -0.0923   0.6348   0.4820
  -3.250   0.0843   0.02020   0.01096  -0.0925   0.6320   0.4941
  -3.000   0.1129   0.02031   0.01093  -0.0927   0.6297   0.5060
  -2.750   0.1396   0.02053   0.01109  -0.0928   0.6269   0.5176
  -2.500   0.1648   0.02085   0.01143  -0.0924   0.6239   0.5278
  -2.250   0.1915   0.02110   0.01158  -0.0926   0.6210   0.5399
  -2.000   0.2169   0.02138   0.01189  -0.0921   0.6182   0.5472
  -1.750   0.2443   0.02151   0.01194  -0.0923   0.6155   0.5540
  -1.500   0.2728   0.02158   0.01187  -0.0928   0.6131   0.5603
  -1.250   0.2999   0.02175   0.01202  -0.0926   0.6110   0.5653
  -1.000   0.3281   0.02198   0.01218  -0.0927   0.6092   0.5756
  -0.750   0.3528   0.02238   0.01263  -0.0920   0.6073   0.5863
  -0.500   0.3759   0.02283   0.01312  -0.0916   0.6047   0.5977
  -0.250   0.3981   0.02323   0.01361  -0.0908   0.6021   0.6043
   0.000   0.4217   0.02356   0.01397  -0.0904   0.5997   0.6098
   0.250   0.4473   0.02381   0.01419  -0.0906   0.5974   0.6162
   0.500   0.4733   0.02399   0.01435  -0.0906   0.5949   0.6213
   0.750   0.4993   0.02411   0.01447  -0.0904   0.5925   0.6250
   1.000   0.5283   0.02412   0.01443  -0.0908   0.5902   0.6280
   1.250   0.5592   0.02407   0.01430  -0.0916   0.5881   0.6306
   1.500   0.5810   0.02440   0.01467  -0.0913   0.5846   0.6333
   1.750   0.6009   0.02478   0.01509  -0.0908   0.5802   0.6363
   2.000   0.6257   0.02495   0.01525  -0.0910   0.5763   0.6394
   2.250   0.6520   0.02496   0.01527  -0.0909   0.5729   0.6416
   2.500   0.6810   0.02491   0.01521  -0.0912   0.5702   0.6442
   2.750   0.7130   0.02477   0.01501  -0.0919   0.5677   0.6471
   3.000   0.7302   0.02522   0.01556  -0.0908   0.5634   0.6502
   3.250   0.7470   0.02563   0.01606  -0.0897   0.5581   0.6537
   3.500   0.7748   0.02546   0.01586  -0.0898   0.5528   0.6576
   3.750   0.8118   0.02485   0.01514  -0.0910   0.5481   0.6612
   4.000   0.8296   0.02509   0.01548  -0.0897   0.5426   0.6644
   4.250   0.8439   0.02548   0.01600  -0.0881   0.5366   0.6681
   4.500   0.8692   0.02544   0.01597  -0.0879   0.5319   0.6726
   4.750   0.9027   0.02511   0.01559  -0.0888   0.5279   0.6776
   5.000   0.9214   0.02536   0.01592  -0.0877   0.5230   0.6821
   5.250   0.9267   0.02606   0.01680  -0.0849   0.5170   0.6866
   5.500   0.9456   0.02624   0.01704  -0.0839   0.5119   0.6921
   5.750   0.9755   0.02603   0.01683  -0.0842   0.5078   0.6988
   6.000   0.9876   0.02646   0.01738  -0.0823   0.5031   0.7043
   6.250   0.9769   0.02767   0.01878  -0.0775   0.4974   0.7101
   6.500   0.9870   0.02828   0.01947  -0.0756   0.4924   0.7174
   6.750   1.0154   0.02801   0.01923  -0.0756   0.4881   0.7246
   7.000   1.0160   0.02917   0.02053  -0.0729   0.4835   0.7321
   7.250   0.9788   0.03296   0.02451  -0.0678   0.4753   0.7403
   7.500   0.9935   0.03352   0.02518  -0.0668   0.4703   0.7491
   7.750   1.0237   0.03305   0.02478  -0.0668   0.4670   0.7603
   8.000   0.9552   0.04046   0.03241  -0.0620   0.4494   0.7685
   8.500   0.9383   0.04650   0.03875  -0.0592   0.4297   0.7951
   8.750   0.9247   0.05019   0.04260  -0.0579   0.4178   0.8121
   9.000   0.9368   0.05080   0.04338  -0.0566   0.4122   0.8416
   9.250   0.9289   0.05327   0.04606  -0.0546   0.4020   0.8969
   9.500   0.9364   0.05466   0.04754  -0.0541   0.3935   1.0000
   9.750   0.9384   0.05738   0.05032  -0.0542   0.3823   1.0000
  10.000   0.9539   0.05852   0.05149  -0.0543   0.3737   1.0000
  10.250   0.9682   0.05976   0.05277  -0.0543   0.3639   1.0000
  10.500   0.9990   0.05891   0.05189  -0.0542   0.3551   1.0000
  10.750   1.0203   0.05920   0.05217  -0.0541   0.3430   1.0000
  11.000   1.0425   0.05937   0.05232  -0.0539   0.3309   1.0000
  11.250   1.0545   0.06081   0.05377  -0.0538   0.3137   1.0000
  11.500   1.0818   0.06014   0.05293  -0.0534   0.2953   1.0000
  11.750   1.0990   0.06072   0.05336  -0.0529   0.2792   1.0000
  12.000   1.1041   0.06305   0.05571  -0.0528   0.2562   1.0000
  12.500   1.1146   0.06727   0.05960  -0.0523   0.2211   1.0000
  12.750   1.1210   0.06966   0.06207  -0.0524   0.1979   1.0000
  13.000   1.1201   0.07270   0.06494  -0.0524   0.1822   1.0000
  13.250   1.1222   0.07553   0.06770  -0.0525   0.1697   1.0000
  13.500   1.1292   0.07793   0.07018  -0.0528   0.1482   1.0000
  13.750   1.1260   0.08153   0.07359  -0.0531   0.1347   1.0000
  14.000   1.1275   0.08463   0.07664  -0.0535   0.1252   1.0000
  14.250   1.1361   0.08692   0.07908  -0.0538   0.1102   1.0000
  14.500   1.1363   0.09029   0.08236  -0.0544   0.0974   1.0000
  14.750   1.1367   0.09370   0.08568  -0.0550   0.0914   1.0000
  15.000   1.1370   0.09715   0.08910  -0.0557   0.0866   1.0000
  15.250   1.1427   0.09990   0.09197  -0.0563   0.0807   1.0000
  15.500   1.1509   0.10233   0.09457  -0.0568   0.0739   1.0000
  15.750   1.1567   0.10512   0.09744  -0.0575   0.0683   1.0000
  16.000   1.1602   0.10823   0.10056  -0.0584   0.0651   1.0000
  16.250   1.1635   0.11139   0.10371  -0.0593   0.0629   1.0000
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