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FX S 02/1-158 AIRFOIL (fxs21158-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX S 02/1-158 AIRFOIL (fxs21158-il)
Reynolds number: 200,000
Max Cl/Cd: 72.12 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxs21158-il-200000-n5.txt
Download as CSV file: xf-fxs21158-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.4192   0.08012   0.07703  -0.0498   0.9320   0.0130
 -10.750  -0.4968   0.05859   0.05527  -0.0655   0.9284   0.0114
 -10.500  -0.4959   0.04778   0.04383  -0.0834   0.8449   0.0121
 -10.250  -0.5100   0.04215   0.03771  -0.0886   0.7903   0.0127
 -10.000  -0.5294   0.03765   0.03267  -0.0897   0.7569   0.0139
  -9.750  -0.5325   0.03426   0.02858  -0.0894   0.7314   0.0154
  -9.500  -0.5230   0.03264   0.02671  -0.0891   0.7092   0.0161
  -9.250  -0.5059   0.03218   0.02612  -0.0888   0.6888   0.0170
  -9.000  -0.4879   0.03175   0.02551  -0.0886   0.6717   0.0182
  -8.750  -0.4695   0.03108   0.02458  -0.0884   0.6572   0.0202
  -8.500  -0.4511   0.02989   0.02303  -0.0880   0.6439   0.0217
  -8.250  -0.4318   0.02876   0.02155  -0.0877   0.6318   0.0229
  -7.750  -0.3897   0.02725   0.01982  -0.0877   0.6107   0.0265
  -7.500  -0.3670   0.02634   0.01868  -0.0875   0.6021   0.0280
  -7.250  -0.3438   0.02527   0.01736  -0.0872   0.5940   0.0290
  -7.000  -0.3201   0.02403   0.01589  -0.0868   0.5866   0.0294
  -6.750  -0.2959   0.02297   0.01462  -0.0865   0.5796   0.0298
  -6.500  -0.2714   0.02200   0.01350  -0.0861   0.5729   0.0302
  -6.250  -0.2467   0.02118   0.01253  -0.0858   0.5665   0.0306
  -6.000  -0.2219   0.02043   0.01165  -0.0854   0.5610   0.0310
  -5.750  -0.1969   0.01976   0.01084  -0.0851   0.5556   0.0314
  -5.500  -0.1717   0.01917   0.01014  -0.0849   0.5512   0.0317
  -5.250  -0.1478   0.01827   0.00919  -0.0847   0.5469   0.0331
  -5.000  -0.1225   0.01765   0.00852  -0.0847   0.5423   0.0344
  -4.750  -0.0965   0.01714   0.00792  -0.0847   0.5380   0.0354
  -4.500  -0.0701   0.01669   0.00734  -0.0848   0.5343   0.0362
  -4.250  -0.0429   0.01626   0.00681  -0.0850   0.5299   0.0374
  -4.000  -0.0154   0.01590   0.00634  -0.0852   0.5258   0.0389
  -3.750   0.0122   0.01561   0.00591  -0.0854   0.5223   0.0412
  -3.500   0.0400   0.01532   0.00551  -0.0855   0.5193   0.0459
  -3.250   0.0680   0.01498   0.00518  -0.0858   0.5158   0.0612
  -3.000   0.0957   0.01448   0.00481  -0.0863   0.5125   0.1135
  -2.750   0.1210   0.01318   0.00460  -0.0873   0.5096   0.4022
  -2.500   0.1495   0.01332   0.00463  -0.0873   0.5071   0.4412
  -2.250   0.1777   0.01358   0.00485  -0.0873   0.5048   0.4726
  -2.000   0.2060   0.01384   0.00506  -0.0872   0.5021   0.4946
  -1.750   0.2341   0.01401   0.00519  -0.0871   0.4995   0.5060
  -1.500   0.2627   0.01409   0.00515  -0.0872   0.4970   0.5125
  -1.250   0.2908   0.01414   0.00514  -0.0873   0.4948   0.5156
  -1.000   0.3192   0.01419   0.00510  -0.0874   0.4928   0.5183
  -0.750   0.3477   0.01426   0.00508  -0.0875   0.4909   0.5210
  -0.500   0.3762   0.01430   0.00507  -0.0877   0.4887   0.5236
  -0.250   0.4048   0.01437   0.00508  -0.0879   0.4865   0.5271
   0.000   0.4328   0.01443   0.00515  -0.0880   0.4843   0.5305
   0.250   0.4609   0.01452   0.00520  -0.0881   0.4820   0.5348
   0.500   0.4892   0.01461   0.00523  -0.0882   0.4797   0.5395
   0.750   0.5174   0.01472   0.00527  -0.0883   0.4777   0.5432
   1.000   0.5453   0.01479   0.00537  -0.0884   0.4751   0.5461
   1.250   0.5733   0.01486   0.00546  -0.0885   0.4725   0.5487
   1.500   0.6013   0.01492   0.00552  -0.0886   0.4696   0.5510
   1.750   0.6294   0.01500   0.00558  -0.0888   0.4670   0.5533
   2.000   0.6575   0.01510   0.00563  -0.0889   0.4647   0.5556
   2.250   0.6856   0.01522   0.00572  -0.0891   0.4627   0.5577
   2.500   0.7131   0.01529   0.00589  -0.0891   0.4603   0.5601
   2.750   0.7407   0.01540   0.00607  -0.0892   0.4579   0.5627
   3.000   0.7684   0.01551   0.00622  -0.0893   0.4556   0.5655
   3.250   0.7961   0.01562   0.00636  -0.0894   0.4534   0.5683
   3.500   0.8239   0.01574   0.00650  -0.0895   0.4511   0.5710
   3.750   0.8514   0.01583   0.00663  -0.0896   0.4489   0.5736
   4.000   0.8783   0.01594   0.00684  -0.0896   0.4460   0.5767
   4.250   0.9052   0.01604   0.00704  -0.0895   0.4425   0.5803
   4.500   0.9322   0.01609   0.00716  -0.0895   0.4384   0.5840
   4.750   0.9591   0.01611   0.00717  -0.0894   0.4343   0.5872
   5.000   0.9850   0.01613   0.00736  -0.0892   0.4280   0.5906
   5.250   1.0113   0.01612   0.00739  -0.0890   0.4221   0.5947
   5.500   1.0375   0.01620   0.00755  -0.0888   0.4170   0.5992
   5.750   1.0635   0.01631   0.00780  -0.0887   0.4127   0.6033
   6.000   1.0896   0.01641   0.00799  -0.0885   0.4088   0.6083
   6.250   1.1158   0.01654   0.00817  -0.0883   0.4057   0.6144
   6.500   1.1416   0.01669   0.00851  -0.0882   0.4021   0.6203
   6.750   1.1672   0.01686   0.00887  -0.0880   0.3981   0.6277
   7.000   1.1917   0.01690   0.00900  -0.0875   0.3902   0.6353
   7.500   1.2333   0.01710   0.00919  -0.0855   0.3321   0.6542
   7.750   1.2452   0.01792   0.00973  -0.0835   0.2766   0.6658
   8.000   1.2440   0.01971   0.01115  -0.0800   0.1944   0.6793
   8.250   1.2470   0.02111   0.01245  -0.0770   0.1632   0.6976
   8.500   1.2445   0.02256   0.01387  -0.0734   0.1294   0.7246
   9.000   1.2296   0.02534   0.01692  -0.0653   0.0857   1.0000
   9.250   1.2263   0.02723   0.01882  -0.0631   0.0610   1.0000
   9.500   1.2219   0.02955   0.02114  -0.0616   0.0558   1.0000
   9.750   1.2191   0.03208   0.02371  -0.0608   0.0499   1.0000
  10.000   1.2249   0.03402   0.02577  -0.0603   0.0408   1.0000
  10.250   1.2197   0.03712   0.02891  -0.0599   0.0365   1.0000
  10.500   1.2147   0.04032   0.03215  -0.0597   0.0323   1.0000
  10.750   1.2137   0.04316   0.03506  -0.0595   0.0298   1.0000
  11.000   1.2102   0.04631   0.03827  -0.0594   0.0266   1.0000
  11.250   1.2068   0.04949   0.04150  -0.0593   0.0238   1.0000
  11.500   1.2107   0.05191   0.04403  -0.0593   0.0193   1.0000
  11.750   1.2079   0.05507   0.04721  -0.0593   0.0125   1.0000
  12.000   1.2047   0.05831   0.05048  -0.0594   0.0095   1.0000
  12.250   1.2029   0.06153   0.05378  -0.0596   0.0077   1.0000
  12.500   1.2034   0.06456   0.05686  -0.0599   0.0071   1.0000
  12.750   1.2045   0.06760   0.05999  -0.0601   0.0066   1.0000
  13.000   1.2063   0.07061   0.06309  -0.0605   0.0063   1.0000
  13.250   1.2077   0.07372   0.06629  -0.0609   0.0059   1.0000
  13.500   1.2096   0.07683   0.06950  -0.0614   0.0056   1.0000
  13.750   1.2103   0.08014   0.07289  -0.0620   0.0052   1.0000
  14.000   1.2105   0.08357   0.07640  -0.0626   0.0049   1.0000
  14.250   1.2108   0.08705   0.07996  -0.0633   0.0046   1.0000
  14.500   1.2126   0.09038   0.08340  -0.0641   0.0045   1.0000
  14.750   1.2146   0.09369   0.08681  -0.0649   0.0041   1.0000
  15.000   1.2163   0.09711   0.09034  -0.0657   0.0041   1.0000
  15.250   1.2175   0.10064   0.09398  -0.0666   0.0039   1.0000
  15.500   1.2192   0.10412   0.09755  -0.0676   0.0038   1.0000
  15.750   1.2203   0.10774   0.10132  -0.0687   0.0038   1.0000
  16.000   1.2212   0.11142   0.10510  -0.0698   0.0037   1.0000
  16.250   1.2222   0.11510   0.10889  -0.0710   0.0036   1.0000
  16.500   1.2235   0.11878   0.11267  -0.0723   0.0036   1.0000
  16.750   1.2241   0.12259   0.11658  -0.0736   0.0035   1.0000
  17.000   1.2253   0.12631   0.12041  -0.0750   0.0035   1.0000
  17.250   1.2265   0.13005   0.12425  -0.0765   0.0034   1.0000
  17.500   1.2273   0.13387   0.12818  -0.0781   0.0034   1.0000
  17.750   1.2282   0.13767   0.13209  -0.0797   0.0033   1.0000
  18.000   1.2289   0.14154   0.13605  -0.0814   0.0033   1.0000
  18.250   1.2303   0.14532   0.13994  -0.0832   0.0032   1.0000
  18.500   1.2313   0.14916   0.14389  -0.0850   0.0032   1.0000
  18.750   1.2317   0.15318   0.14802  -0.0870   0.0032   1.0000
  19.000   1.2323   0.15717   0.15213  -0.0891   0.0032   1.0000
  19.250   1.2317   0.16141   0.15649  -0.0914   0.0031   1.0000
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