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FX S 02-196 AIRFOIL (fxs02196-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: FX S 02-196 AIRFOIL (fxs02196-il)
Reynolds number: 200,000
Max Cl/Cd: 55.99 at α=4°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fxs02196-il-200000-n5.txt
Download as CSV file: xf-fxs02196-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.5031   0.08969   0.08557  -0.0766   1.0000   0.0174
 -15.000  -0.5415   0.07921   0.07484  -0.0831   1.0000   0.0173
 -14.750  -0.5681   0.07196   0.06738  -0.0872   1.0000   0.0173
 -14.500  -0.5885   0.06516   0.06033  -0.0917   0.9762   0.0175
 -14.250  -0.5970   0.05825   0.05298  -0.0997   0.9388   0.0179
 -14.000  -0.6057   0.05188   0.04602  -0.1073   0.9128   0.0183
 -13.750  -0.5910   0.04881   0.04280  -0.1108   0.8903   0.0188
 -13.500  -0.5792   0.04651   0.04033  -0.1126   0.8688   0.0192
 -13.250  -0.5712   0.04441   0.03807  -0.1137   0.8498   0.0199
 -13.000  -0.5674   0.04217   0.03555  -0.1144   0.8334   0.0204
 -12.750  -0.5679   0.03988   0.03293  -0.1143   0.8177   0.0210
 -12.500  -0.5544   0.03860   0.03160  -0.1139   0.8043   0.0214
 -12.250  -0.5438   0.03741   0.03035  -0.1135   0.7918   0.0219
 -12.000  -0.5338   0.03612   0.02893  -0.1130   0.7797   0.0224
 -11.750  -0.5224   0.03490   0.02755  -0.1125   0.7690   0.0229
 -11.500  -0.5108   0.03366   0.02613  -0.1117   0.7579   0.0234
 -11.250  -0.4982   0.03266   0.02506  -0.1111   0.7482   0.0239
 -11.000  -0.4856   0.03176   0.02410  -0.1104   0.7385   0.0243
 -10.750  -0.4736   0.03092   0.02317  -0.1098   0.7299   0.0248
 -10.500  -0.4601   0.03006   0.02222  -0.1091   0.7211   0.0253
 -10.250  -0.4463   0.02924   0.02126  -0.1083   0.7132   0.0260
 -10.000  -0.4330   0.02849   0.02045  -0.1077   0.7055   0.0267
  -9.750  -0.4180   0.02777   0.01965  -0.1069   0.6976   0.0271
  -9.500  -0.4024   0.02706   0.01884  -0.1060   0.6907   0.0275
  -9.250  -0.3871   0.02636   0.01807  -0.1052   0.6837   0.0282
  -9.000  -0.3709   0.02565   0.01727  -0.1041   0.6769   0.0286
  -8.750  -0.3558   0.02494   0.01646  -0.1030   0.6710   0.0288
  -8.500  -0.3417   0.02423   0.01570  -0.1018   0.6653   0.0290
  -8.250  -0.3299   0.02356   0.01497  -0.1003   0.6595   0.0292
  -8.000  -0.3194   0.02295   0.01429  -0.0986   0.6544   0.0294
  -7.750  -0.3056   0.02233   0.01360  -0.0975   0.6499   0.0297
  -7.500  -0.2900   0.02173   0.01296  -0.0966   0.6452   0.0300
  -7.250  -0.2733   0.02116   0.01234  -0.0957   0.6404   0.0305
  -7.000  -0.2556   0.02062   0.01172  -0.0949   0.6359   0.0309
  -6.750  -0.2367   0.02012   0.01113  -0.0943   0.6319   0.0315
  -6.500  -0.2165   0.01966   0.01057  -0.0938   0.6284   0.0322
  -6.250  -0.1950   0.01922   0.01007  -0.0934   0.6245   0.0329
  -6.000  -0.1729   0.01878   0.00957  -0.0932   0.6207   0.0338
  -5.750  -0.1496   0.01842   0.00912  -0.0930   0.6171   0.0352
  -5.500  -0.1256   0.01809   0.00870  -0.0929   0.6138   0.0368
  -5.250  -0.1014   0.01773   0.00824  -0.0929   0.6108   0.0385
  -5.000  -0.0761   0.01746   0.00785  -0.0929   0.6079   0.0403
  -4.750  -0.0509   0.01711   0.00747  -0.0930   0.6046   0.0420
  -4.500  -0.0250   0.01683   0.00716  -0.0932   0.6012   0.0443
  -4.250   0.0013   0.01658   0.00690  -0.0933   0.5976   0.0465
  -4.000   0.0278   0.01632   0.00666  -0.0936   0.5941   0.0502
  -3.750   0.0553   0.01624   0.00647  -0.0938   0.5908   0.0623
  -3.500   0.0829   0.01617   0.00629  -0.0940   0.5876   0.0668
  -3.250   0.1104   0.01607   0.00616  -0.0942   0.5844   0.0693
  -3.000   0.1379   0.01592   0.00603  -0.0945   0.5807   0.0733
  -2.750   0.1649   0.01566   0.00583  -0.0948   0.5759   0.0913
  -2.500   0.1925   0.01563   0.00568  -0.0949   0.5704   0.1007
  -2.250   0.2201   0.01558   0.00555  -0.0951   0.5649   0.1051
  -2.000   0.2473   0.01544   0.00544  -0.0953   0.5586   0.1108
  -1.750   0.2747   0.01526   0.00527  -0.0956   0.5524   0.1426
  -1.500   0.3023   0.01508   0.00509  -0.0959   0.5477   0.1629
  -1.250   0.3302   0.01473   0.00493  -0.0966   0.5438   0.2227
  -0.750   0.3865   0.01395   0.00494  -0.0982   0.5364   0.4520
  -0.500   0.4147   0.01400   0.00503  -0.0984   0.5333   0.4729
  -0.250   0.4430   0.01407   0.00506  -0.0987   0.5301   0.4856
   0.000   0.4711   0.01415   0.00509  -0.0989   0.5271   0.4948
   0.250   0.4994   0.01422   0.00513  -0.0992   0.5240   0.5023
   0.500   0.5268   0.01427   0.00527  -0.0993   0.5190   0.5126
   0.750   0.5541   0.01434   0.00538  -0.0993   0.5133   0.5258
   1.000   0.5810   0.01444   0.00543  -0.0993   0.5073   0.5371
   1.250   0.6082   0.01450   0.00551  -0.0994   0.5018   0.5425
   1.500   0.6354   0.01457   0.00561  -0.0995   0.4973   0.5463
   1.750   0.6627   0.01466   0.00569  -0.0996   0.4936   0.5508
   2.000   0.6899   0.01476   0.00576  -0.0997   0.4898   0.5575
   2.250   0.7160   0.01487   0.00589  -0.0995   0.4852   0.5658
   2.500   0.7424   0.01499   0.00606  -0.0995   0.4787   0.5762
   2.750   0.7674   0.01511   0.00619  -0.0992   0.4703   0.5838
   3.000   0.7924   0.01524   0.00635  -0.0989   0.4624   0.5909
   3.250   0.8182   0.01536   0.00650  -0.0988   0.4528   0.5962
   3.500   0.8433   0.01549   0.00663  -0.0986   0.4430   0.6003
   3.750   0.8672   0.01562   0.00678  -0.0981   0.4290   0.6038
   4.000   0.8874   0.01585   0.00693  -0.0971   0.4076   0.6074
   4.250   0.8950   0.01652   0.00728  -0.0941   0.3526   0.6107
   4.500   0.9033   0.01725   0.00784  -0.0914   0.3131   0.6142
   4.750   0.9075   0.01801   0.00846  -0.0881   0.2901   0.6177
   5.000   0.9165   0.01857   0.00900  -0.0855   0.2759   0.6209
   5.500   0.9221   0.02046   0.01079  -0.0792   0.2289   0.6277
   5.750   0.9304   0.02130   0.01163  -0.0772   0.2207   0.6318
   6.000   0.9458   0.02188   0.01226  -0.0760   0.2140   0.6365
   6.250   0.9531   0.02288   0.01328  -0.0741   0.1897   0.6407
   6.500   0.9586   0.02404   0.01446  -0.0722   0.1839   0.6448
   6.750   0.9642   0.02529   0.01573  -0.0704   0.1770   0.6495
   7.000   0.9748   0.02632   0.01681  -0.0693   0.1728   0.6550
   7.250   0.9830   0.02756   0.01810  -0.0680   0.1673   0.6605
   7.500   0.9954   0.02854   0.01918  -0.0671   0.1602   0.6663
   7.750   0.9988   0.03022   0.02087  -0.0656   0.1394   0.6728
   8.000   1.0040   0.03185   0.02251  -0.0645   0.1354   0.6800
   8.250   1.0105   0.03338   0.02410  -0.0634   0.1317   0.6871
   8.500   1.0187   0.03485   0.02565  -0.0626   0.1279   0.6958
   8.750   1.0260   0.03643   0.02729  -0.0617   0.1239   0.7044
   9.000   1.0349   0.03791   0.02887  -0.0610   0.1201   0.7145
   9.250   1.0494   0.03895   0.03005  -0.0606   0.1019   0.7259
   9.500   1.0485   0.04132   0.03241  -0.0595   0.0953   0.7382
   9.750   1.0541   0.04318   0.03432  -0.0588   0.0923   0.7523
  10.000   1.0614   0.04490   0.03612  -0.0582   0.0901   0.7694
  10.250   1.0679   0.04668   0.03800  -0.0575   0.0878   0.7911
  10.500   1.0761   0.04820   0.03967  -0.0567   0.0862   0.8206
  11.000   1.0908   0.05085   0.04267  -0.0547   0.0827   1.0000
  11.250   1.1015   0.05258   0.04445  -0.0546   0.0804   1.0000
  11.500   1.1138   0.05416   0.04610  -0.0546   0.0780   1.0000
  11.750   1.1292   0.05546   0.04752  -0.0547   0.0659   1.0000
  12.000   1.1327   0.05797   0.04999  -0.0546   0.0631   1.0000
  12.250   1.1391   0.06023   0.05222  -0.0546   0.0605   1.0000
  12.500   1.1453   0.06254   0.05453  -0.0546   0.0586   1.0000
  12.750   1.1521   0.06482   0.05684  -0.0547   0.0571   1.0000
  13.000   1.1592   0.06710   0.05916  -0.0548   0.0559   1.0000
  13.250   1.1665   0.06938   0.06150  -0.0549   0.0548   1.0000
  13.500   1.1747   0.07161   0.06381  -0.0551   0.0535   1.0000
  13.750   1.1817   0.07398   0.06626  -0.0554   0.0522   1.0000
  14.000   1.1869   0.07663   0.06898  -0.0557   0.0508   1.0000
  14.250   1.1927   0.07923   0.07165  -0.0560   0.0495   1.0000
  14.500   1.2024   0.08135   0.07388  -0.0563   0.0479   1.0000
  14.750   1.2107   0.08367   0.07630  -0.0567   0.0460   1.0000
  15.000   1.2180   0.08613   0.07885  -0.0571   0.0445   1.0000
  15.250   1.2269   0.08840   0.08122  -0.0576   0.0425   1.0000
  15.500   1.2351   0.09078   0.08369  -0.0581   0.0405   1.0000
  15.750   1.2426   0.09325   0.08622  -0.0586   0.0393   1.0000
  16.000   1.2494   0.09583   0.08886  -0.0592   0.0383   1.0000
  16.250   1.2553   0.09857   0.09165  -0.0599   0.0376   1.0000
  16.500   1.2615   0.10127   0.09440  -0.0607   0.0369   1.0000
  16.750   1.2673   0.10403   0.09720  -0.0614   0.0362   1.0000
  17.000   1.2718   0.10703   0.10025  -0.0623   0.0357   1.0000
  17.250   1.2760   0.11005   0.10334  -0.0632   0.0352   1.0000
  17.500   1.2804   0.11304   0.10640  -0.0642   0.0348   1.0000
  17.750   1.2842   0.11613   0.10957  -0.0652   0.0345   1.0000
  18.000   1.2880   0.11923   0.11273  -0.0663   0.0341   1.0000
  18.250   1.2920   0.12227   0.11582  -0.0674   0.0337   1.0000
  18.500   1.2958   0.12534   0.11895  -0.0686   0.0334   1.0000
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