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FX S 02/1-158 AIRFOIL (fxs21158-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: FX S 02/1-158 AIRFOIL (fxs21158-il)
Reynolds number: 1,000,000
Max Cl/Cd: 76.02 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxs21158-il-1000000-n5.txt
Download as CSV file: xf-fxs21158-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.7830   0.07273   0.07055  -0.0451   1.0000   0.0012
 -14.500  -0.8349   0.05986   0.05743  -0.0539   1.0000   0.0012
 -14.250  -0.8556   0.05349   0.05091  -0.0580   1.0000   0.0012
 -14.000  -0.8670   0.04787   0.04513  -0.0626   0.9990   0.0012
 -13.750  -0.7996   0.03864   0.03528  -0.0889   0.8859   0.0012
 -13.500  -0.7883   0.03602   0.03209  -0.0926   0.7699   0.0012
 -13.250  -0.7933   0.03313   0.02895  -0.0935   0.7344   0.0012
 -13.000  -0.7904   0.03117   0.02680  -0.0938   0.7049   0.0012
 -12.750  -0.7888   0.02914   0.02459  -0.0939   0.6814   0.0012
 -12.500  -0.7847   0.02745   0.02275  -0.0938   0.6648   0.0012
 -12.250  -0.7861   0.02555   0.02069  -0.0932   0.6504   0.0013
 -12.000  -0.7841   0.02420   0.01921  -0.0923   0.6345   0.0013
 -11.750  -0.7730   0.02309   0.01794  -0.0915   0.6193   0.0013
 -11.250  -0.7416   0.02127   0.01586  -0.0903   0.5963   0.0013
 -11.000  -0.7233   0.02047   0.01493  -0.0898   0.5852   0.0014
 -10.750  -0.7037   0.01974   0.01407  -0.0894   0.5732   0.0014
 -10.500  -0.6832   0.01904   0.01324  -0.0890   0.5612   0.0014
 -10.250  -0.6616   0.01842   0.01251  -0.0886   0.5515   0.0014
 -10.000  -0.6403   0.01765   0.01161  -0.0882   0.5433   0.0016
  -9.750  -0.6177   0.01704   0.01088  -0.0880   0.5360   0.0016
  -9.500  -0.5946   0.01641   0.01014  -0.0877   0.5297   0.0018
  -9.250  -0.5707   0.01586   0.00950  -0.0875   0.5230   0.0019
  -9.000  -0.5462   0.01535   0.00889  -0.0874   0.5166   0.0020
  -8.750  -0.5216   0.01482   0.00828  -0.0873   0.5102   0.0022
  -8.500  -0.4963   0.01439   0.00776  -0.0872   0.5044   0.0023
  -8.250  -0.4705   0.01398   0.00727  -0.0871   0.4993   0.0025
  -8.000  -0.4444   0.01361   0.00683  -0.0871   0.4939   0.0026
  -7.750  -0.4182   0.01322   0.00636  -0.0871   0.4898   0.0031
  -7.500  -0.3921   0.01277   0.00586  -0.0871   0.4862   0.0042
  -7.250  -0.3652   0.01249   0.00567  -0.0873   0.4828   0.0101
  -7.000  -0.3375   0.01238   0.00556  -0.0873   0.4798   0.0122
  -6.750  -0.3098   0.01225   0.00539  -0.0874   0.4770   0.0133
  -6.500  -0.2818   0.01213   0.00526  -0.0875   0.4751   0.0143
  -6.250  -0.2537   0.01204   0.00516  -0.0877   0.4729   0.0149
  -6.000  -0.2254   0.01202   0.00513  -0.0878   0.4706   0.0153
  -5.750  -0.1978   0.01178   0.00484  -0.0879   0.4683   0.0159
  -5.500  -0.1704   0.01143   0.00442  -0.0880   0.4657   0.0166
  -5.250  -0.1428   0.01119   0.00412  -0.0882   0.4625   0.0173
  -5.000  -0.1146   0.01097   0.00387  -0.0883   0.4591   0.0180
  -4.750  -0.0864   0.01081   0.00369  -0.0885   0.4535   0.0190
  -4.500  -0.0584   0.01067   0.00349  -0.0886   0.4485   0.0197
  -4.250  -0.0300   0.01048   0.00325  -0.0888   0.4454   0.0199
  -4.000  -0.0015   0.01031   0.00304  -0.0890   0.4414   0.0201
  -3.750   0.0269   0.01017   0.00285  -0.0891   0.4377   0.0204
  -3.500   0.0553   0.01006   0.00268  -0.0893   0.4338   0.0208
  -3.250   0.0839   0.00994   0.00251  -0.0894   0.4309   0.0211
  -3.000   0.1125   0.00983   0.00237  -0.0896   0.4279   0.0214
  -2.750   0.1411   0.00975   0.00225  -0.0897   0.4252   0.0218
  -2.500   0.1697   0.00968   0.00214  -0.0899   0.4224   0.0223
  -2.250   0.1982   0.00961   0.00204  -0.0901   0.4195   0.0256
  -2.000   0.2269   0.00948   0.00194  -0.0903   0.4170   0.0387
  -1.750   0.2553   0.00936   0.00185  -0.0905   0.4120   0.0642
  -1.500   0.2837   0.00935   0.00180  -0.0906   0.4067   0.0686
  -1.250   0.3123   0.00929   0.00175  -0.0908   0.4027   0.0773
  -1.000   0.3409   0.00921   0.00170  -0.0910   0.3991   0.1020
  -0.750   0.3695   0.00915   0.00166  -0.0912   0.3958   0.1146
  -0.500   0.3979   0.00904   0.00161  -0.0914   0.3925   0.1523
  -0.250   0.4264   0.00891   0.00157  -0.0917   0.3899   0.1951
   0.000   0.4547   0.00865   0.00149  -0.0920   0.3866   0.2645
   0.250   0.4823   0.00816   0.00143  -0.0924   0.3819   0.4116
   0.500   0.5106   0.00819   0.00149  -0.0925   0.3759   0.4362
   0.750   0.5391   0.00825   0.00152  -0.0926   0.3704   0.4411
   1.000   0.5671   0.00834   0.00157  -0.0927   0.3614   0.4458
   1.250   0.5945   0.00851   0.00166  -0.0927   0.3465   0.4507
   1.500   0.6197   0.00891   0.00185  -0.0924   0.3036   0.4538
   1.750   0.6410   0.00974   0.00232  -0.0916   0.2286   0.4569
   2.000   0.6649   0.01028   0.00267  -0.0911   0.1806   0.4599
   2.250   0.6919   0.01048   0.00282  -0.0911   0.1708   0.4626
   2.500   0.7193   0.01062   0.00294  -0.0911   0.1650   0.4648
   2.750   0.7450   0.01095   0.00318  -0.0909   0.1385   0.4673
   3.000   0.7714   0.01119   0.00336  -0.0907   0.1270   0.4696
   3.250   0.7980   0.01139   0.00355  -0.0906   0.1186   0.4729
   3.500   0.8251   0.01154   0.00370  -0.0906   0.1149   0.4759
   3.750   0.8504   0.01187   0.00396  -0.0903   0.0932   0.4786
   4.000   0.8772   0.01204   0.00412  -0.0903   0.0913   0.4810
   4.250   0.9037   0.01223   0.00430  -0.0902   0.0888   0.4832
   4.500   0.9301   0.01240   0.00450  -0.0901   0.0864   0.4877
   4.750   0.9562   0.01260   0.00472  -0.0899   0.0818   0.4925
   5.000   0.9796   0.01305   0.00508  -0.0894   0.0571   0.4968
   5.250   1.0049   0.01330   0.00533  -0.0891   0.0512   0.4995
   5.500   1.0301   0.01355   0.00561  -0.0889   0.0405   0.5023
   5.750   1.0528   0.01399   0.00600  -0.0882   0.0280   0.5051
   6.000   1.0773   0.01428   0.00629  -0.0879   0.0239   0.5077
   6.250   1.1018   0.01454   0.00657  -0.0875   0.0219   0.5102
   6.750   1.1442   0.01550   0.00752  -0.0858   0.0025   0.5168
   7.000   1.1665   0.01587   0.00793  -0.0851   0.0021   0.5211
   7.250   1.1884   0.01624   0.00834  -0.0844   0.0018   0.5251
   7.500   1.2096   0.01662   0.00876  -0.0835   0.0017   0.5282
   7.750   1.2299   0.01702   0.00921  -0.0826   0.0017   0.5314
   8.000   1.2493   0.01746   0.00969  -0.0815   0.0016   0.5350
   8.250   1.2673   0.01792   0.01022  -0.0802   0.0015   0.5386
   8.750   1.2951   0.01894   0.01135  -0.0763   0.0014   0.5464
   9.000   1.3042   0.01954   0.01202  -0.0736   0.0013   0.5513
   9.250   1.3116   0.02026   0.01280  -0.0708   0.0013   0.5560
   9.500   1.3168   0.02112   0.01374  -0.0681   0.0012   0.5609
   9.750   1.3204   0.02220   0.01490  -0.0656   0.0012   0.5664
  10.250   1.3228   0.02527   0.01814  -0.0616   0.0011   0.5779
  10.500   1.3240   0.02720   0.02016  -0.0603   0.0011   0.5844
  10.750   1.3244   0.02941   0.02249  -0.0594   0.0011   0.5921
  11.250   1.3156   0.03520   0.02851  -0.0579   0.0009   0.6105
  11.500   1.3208   0.03725   0.03064  -0.0576   0.0010   0.6232
  11.750   1.3118   0.04078   0.03430  -0.0571   0.0009   0.6359
  12.000   1.3031   0.04435   0.03801  -0.0567   0.0009   0.6518
  12.250   1.2899   0.04844   0.04226  -0.0565   0.0008   0.6724
  12.500   1.2878   0.05132   0.04532  -0.0563   0.0008   0.7167
  13.000   1.2964   0.05722   0.05187  -0.0588   0.0008   1.0000
  13.250   1.2961   0.06032   0.05504  -0.0590   0.0008   1.0000
  13.500   1.2954   0.06350   0.05828  -0.0593   0.0008   1.0000
  13.750   1.2958   0.06664   0.06148  -0.0596   0.0008   1.0000
  14.000   1.2964   0.06978   0.06469  -0.0600   0.0008   1.0000
  14.250   1.2970   0.07301   0.06798  -0.0605   0.0008   1.0000
  14.500   1.2975   0.07627   0.07131  -0.0611   0.0008   1.0000
  14.750   1.2981   0.07962   0.07474  -0.0617   0.0007   1.0000
  15.000   1.2990   0.08295   0.07813  -0.0624   0.0008   1.0000
  15.250   1.2989   0.08648   0.08172  -0.0631   0.0008   1.0000
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