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FX S 02/1-158 AIRFOIL (fxs21158-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: FX S 02/1-158 AIRFOIL (fxs21158-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.14 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-fxs21158-il-1000000.txt
Download as CSV file: xf-fxs21158-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX S 02/1-158 AIRFOIL                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.7557   0.07002   0.06797  -0.0460   1.0000   0.0024
 -14.000  -0.7858   0.06066   0.05844  -0.0524   1.0000   0.0024
 -13.750  -0.8124   0.05320   0.05080  -0.0574   1.0000   0.0024
 -13.500  -0.8237   0.04843   0.04591  -0.0604   1.0000   0.0024
 -13.250  -0.8429   0.04287   0.04015  -0.0637   1.0000   0.0024
 -13.000  -0.8480   0.03928   0.03645  -0.0657   1.0000   0.0024
 -12.750  -0.8539   0.03569   0.03272  -0.0676   1.0000   0.0024
 -12.500  -0.8538   0.03296   0.02988  -0.0689   1.0000   0.0024
 -12.250  -0.8622   0.02967   0.02643  -0.0700   1.0000   0.0024
 -12.000  -0.8635   0.02729   0.02394  -0.0708   1.0000   0.0024
 -11.750  -0.8321   0.02454   0.02095  -0.0768   0.9616   0.0024
 -11.500  -0.7353   0.02138   0.01726  -0.0953   0.8834   0.0025
 -11.250  -0.7244   0.02062   0.01611  -0.0938   0.8047   0.0025
 -11.000  -0.7120   0.01976   0.01496  -0.0924   0.7605   0.0026
 -10.750  -0.6960   0.01900   0.01397  -0.0913   0.7264   0.0026
 -10.500  -0.6771   0.01834   0.01313  -0.0906   0.6994   0.0026
 -10.250  -0.6577   0.01763   0.01224  -0.0900   0.6769   0.0027
 -10.000  -0.6367   0.01697   0.01142  -0.0895   0.6579   0.0027
  -9.750  -0.6146   0.01637   0.01067  -0.0890   0.6392   0.0028
  -9.500  -0.5929   0.01566   0.00977  -0.0886   0.6214   0.0032
  -9.250  -0.5699   0.01507   0.00904  -0.0882   0.6068   0.0036
  -9.000  -0.5460   0.01453   0.00838  -0.0880   0.5933   0.0039
  -8.750  -0.5221   0.01392   0.00768  -0.0878   0.5806   0.0051
  -8.500  -0.4964   0.01362   0.00747  -0.0877   0.5680   0.0093
  -8.250  -0.4685   0.01369   0.00754  -0.0878   0.5572   0.0119
  -8.000  -0.4405   0.01380   0.00761  -0.0878   0.5478   0.0137
  -7.750  -0.4116   0.01402   0.00783  -0.0879   0.5400   0.0147
  -7.500  -0.3833   0.01418   0.00795  -0.0879   0.5334   0.0151
  -7.250  -0.3540   0.01445   0.00820  -0.0881   0.5277   0.0154
  -7.000  -0.3314   0.01335   0.00698  -0.0879   0.5227   0.0169
  -6.750  -0.3043   0.01316   0.00677  -0.0880   0.5181   0.0180
  -6.500  -0.2764   0.01305   0.00666  -0.0882   0.5136   0.0190
  -6.250  -0.2490   0.01289   0.00645  -0.0883   0.5092   0.0199
  -6.000  -0.2215   0.01276   0.00628  -0.0883   0.5052   0.0209
  -5.750  -0.1934   0.01266   0.00615  -0.0884   0.5017   0.0218
  -5.500  -0.1655   0.01255   0.00599  -0.0885   0.4977   0.0223
  -5.250  -0.1379   0.01241   0.00579  -0.0886   0.4931   0.0227
  -5.000  -0.1122   0.01157   0.00484  -0.0886   0.4891   0.0237
  -4.750  -0.0849   0.01114   0.00434  -0.0888   0.4843   0.0251
  -4.500  -0.0573   0.01090   0.00403  -0.0889   0.4798   0.0261
  -4.250  -0.0293   0.01067   0.00372  -0.0890   0.4762   0.0264
  -4.000  -0.0009   0.01043   0.00343  -0.0892   0.4734   0.0267
  -3.750   0.0275   0.01022   0.00318  -0.0893   0.4705   0.0270
  -3.500   0.0558   0.01006   0.00295  -0.0895   0.4673   0.0274
  -3.250   0.0841   0.00994   0.00277  -0.0896   0.4644   0.0282
  -3.000   0.1126   0.00982   0.00260  -0.0897   0.4619   0.0290
  -2.750   0.1414   0.00969   0.00244  -0.0899   0.4600   0.0300
  -2.500   0.1703   0.00958   0.00230  -0.0901   0.4578   0.0317
  -2.250   0.1989   0.00934   0.00212  -0.0903   0.4552   0.0676
  -2.000   0.2274   0.00912   0.00199  -0.0906   0.4526   0.1076
  -1.750   0.2552   0.00875   0.00182  -0.0909   0.4487   0.1931
  -1.500   0.2823   0.00786   0.00155  -0.0915   0.4459   0.3860
  -1.250   0.3111   0.00779   0.00157  -0.0917   0.4425   0.4269
  -1.000   0.3400   0.00781   0.00157  -0.0918   0.4394   0.4398
  -0.750   0.3687   0.00784   0.00159  -0.0920   0.4369   0.4503
  -0.500   0.3974   0.00789   0.00161  -0.0921   0.4344   0.4563
  -0.250   0.4262   0.00791   0.00163  -0.0923   0.4326   0.4611
   0.000   0.4552   0.00794   0.00165  -0.0925   0.4305   0.4655
   0.250   0.4839   0.00798   0.00168  -0.0926   0.4281   0.4720
   0.500   0.5126   0.00804   0.00174  -0.0928   0.4255   0.4798
   0.750   0.5413   0.00810   0.00176  -0.0929   0.4232   0.4824
   1.000   0.5696   0.00815   0.00180  -0.0930   0.4203   0.4852
   1.250   0.5984   0.00817   0.00183  -0.0932   0.4168   0.4884
   1.500   0.6269   0.00821   0.00186  -0.0934   0.4114   0.4912
   1.750   0.6550   0.00830   0.00191  -0.0935   0.4064   0.4938
   2.000   0.6836   0.00835   0.00195  -0.0936   0.4038   0.4959
   2.250   0.7123   0.00839   0.00199  -0.0938   0.4007   0.4978
   2.500   0.7406   0.00842   0.00204  -0.0940   0.3970   0.5004
   2.750   0.7688   0.00848   0.00211  -0.0941   0.3929   0.5031
   3.000   0.7970   0.00854   0.00217  -0.0942   0.3892   0.5056
   3.250   0.8254   0.00859   0.00224  -0.0943   0.3843   0.5083
   3.500   0.8535   0.00867   0.00230  -0.0945   0.3783   0.5106
   3.750   0.8815   0.00875   0.00238  -0.0946   0.3713   0.5127
   4.250   0.9364   0.00896   0.00258  -0.0946   0.3548   0.5194
   4.500   0.9631   0.00916   0.00274  -0.0946   0.3420   0.5238
   4.750   0.9826   0.01006   0.00325  -0.0935   0.2733   0.5271
   5.000   0.9954   0.01155   0.00424  -0.0916   0.1717   0.5308
   5.250   1.0169   0.01218   0.00471  -0.0908   0.1337   0.5337
   5.500   1.0373   0.01288   0.00526  -0.0899   0.0928   0.5368
   5.750   1.0614   0.01324   0.00558  -0.0894   0.0841   0.5401
   6.000   1.0869   0.01345   0.00582  -0.0892   0.0784   0.5434
   6.250   1.1074   0.01405   0.00631  -0.0883   0.0515   0.5470
   6.500   1.1320   0.01430   0.00660  -0.0879   0.0468   0.5516
   6.750   1.1513   0.01495   0.00718  -0.0868   0.0270   0.5554
   7.000   1.1744   0.01526   0.00753  -0.0863   0.0230   0.5603
   7.250   1.1970   0.01558   0.00789  -0.0856   0.0190   0.5655
   7.500   1.2125   0.01637   0.00861  -0.0840   0.0041   0.5699
   7.750   1.2328   0.01678   0.00907  -0.0830   0.0035   0.5748
   8.000   1.2523   0.01721   0.00955  -0.0819   0.0031   0.5806
   8.250   1.2706   0.01767   0.01009  -0.0806   0.0029   0.5869
   8.500   1.2871   0.01816   0.01067  -0.0791   0.0028   0.5944
   8.750   1.2993   0.01870   0.01128  -0.0768   0.0027   0.6029
   9.000   1.3069   0.01933   0.01200  -0.0739   0.0025   0.6137
   9.250   1.3132   0.02006   0.01283  -0.0709   0.0024   0.6270
   9.500   1.3150   0.02105   0.01394  -0.0677   0.0023   0.6435
   9.750   1.3182   0.02210   0.01513  -0.0652   0.0023   0.6692
  10.000   1.3186   0.02345   0.01668  -0.0628   0.0023   0.7147
  10.250   1.3203   0.02506   0.01891  -0.0618   0.0022   1.0000
  10.500   1.3219   0.02716   0.02109  -0.0609   0.0022   1.0000
  10.750   1.3214   0.02968   0.02369  -0.0602   0.0021   1.0000
  11.000   1.3210   0.03234   0.02644  -0.0598   0.0021   1.0000
  11.250   1.3147   0.03567   0.02988  -0.0594   0.0021   1.0000
  11.500   1.3170   0.03817   0.03243  -0.0591   0.0021   1.0000
  11.750   1.3113   0.04151   0.03586  -0.0588   0.0021   1.0000
  12.000   1.3071   0.04474   0.03917  -0.0587   0.0021   1.0000
  12.250   1.3010   0.04818   0.04269  -0.0585   0.0021   1.0000
  12.500   1.2984   0.05128   0.04586  -0.0584   0.0021   1.0000
  12.750   1.2946   0.05457   0.04923  -0.0584   0.0021   1.0000
  13.000   1.2924   0.05781   0.05254  -0.0586   0.0021   1.0000
  13.250   1.2895   0.06125   0.05605  -0.0588   0.0021   1.0000
  13.500   1.2905   0.06424   0.05910  -0.0591   0.0021   1.0000
  13.750   1.2875   0.06783   0.06277  -0.0594   0.0021   1.0000
  14.000   1.2876   0.07107   0.06608  -0.0598   0.0021   1.0000
  14.250   1.2865   0.07450   0.06959  -0.0603   0.0022   1.0000
  14.500   1.2876   0.07771   0.07287  -0.0608   0.0022   1.0000
  14.750   1.2855   0.08139   0.07664  -0.0613   0.0023   1.0000
  15.000   1.2876   0.08452   0.07985  -0.0619   0.0023   1.0000
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