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NREL's S832 Airfoil (s832-nr) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NREL's S832 Airfoil (s832-nr)
Reynolds number: 200,000
Max Cl/Cd: 67.2 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s832-nr-200000-n5.txt
Download as CSV file: xf-s832-nr-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NREL's S832 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
  ------ -------- --------- --------- -------- -------- --------
 -10.000   0.0048   0.09321   0.08864  -0.1243   0.8106   0.0183
  -9.750   0.0075   0.09037   0.08579  -0.1261   0.8071   0.0184
  -9.500   0.0099   0.08738   0.08280  -0.1280   0.8037   0.0186
  -9.250   0.0131   0.08440   0.07984  -0.1297   0.7998   0.0186
  -9.000   0.0149   0.08118   0.07663  -0.1317   0.7962   0.0187
  -8.750   0.0179   0.07808   0.07352  -0.1335   0.7930   0.0187
  -8.500   0.0193   0.07480   0.07024  -0.1358   0.7899   0.0187
  -8.250   0.0165   0.07123   0.06669  -0.1386   0.7855   0.0188
  -8.000   0.0141   0.06835   0.06379  -0.1395   0.7817   0.0188
  -7.750   0.0105   0.06584   0.06121  -0.1395   0.7784   0.0188
  -7.500   0.0108   0.06289   0.05819  -0.1398   0.7755   0.0188
  -7.250   0.0128   0.06005   0.05529  -0.1398   0.7720   0.0188
  -7.000   0.0169   0.05722   0.05236  -0.1395   0.7688   0.0188
  -6.500   0.0239   0.04989   0.04487  -0.1382   0.7636   0.0135
  -6.250   0.0309   0.04764   0.04256  -0.1375   0.7607   0.0128
  -6.000   0.0391   0.04486   0.03965  -0.1367   0.7573   0.0122
  -5.750   0.0489   0.04172   0.03631  -0.1355   0.7544   0.0113
  -5.250   0.0753   0.03484   0.02879  -0.1324   0.7498   0.0105
  -5.000   0.0935   0.03328   0.02704  -0.1319   0.7479   0.0112
  -4.750   0.1106   0.03137   0.02492  -0.1305   0.7447   0.0124
  -4.500   0.1292   0.02860   0.02176  -0.1286   0.7418   0.0133
  -4.250   0.1490   0.02642   0.01926  -0.1274   0.7393   0.0131
  -4.000   0.1713   0.02436   0.01686  -0.1264   0.7371   0.0129
  -3.750   0.1957   0.02243   0.01456  -0.1256   0.7354   0.0128
  -3.500   0.2219   0.02079   0.01256  -0.1250   0.7338   0.0128
  -3.250   0.2446   0.01954   0.01110  -0.1240   0.7311   0.0130
  -3.000   0.2682   0.01852   0.00990  -0.1231   0.7284   0.0134
  -2.750   0.2917   0.01763   0.00891  -0.1223   0.7260   0.0142
  -2.500   0.3156   0.01703   0.00828  -0.1218   0.7238   0.0152
  -2.250   0.3403   0.01653   0.00769  -0.1213   0.7219   0.0177
  -2.000   0.3661   0.01619   0.00733  -0.1212   0.7203   0.0233
  -1.750   0.3885   0.01592   0.00706  -0.1205   0.7180   0.0315
  -1.500   0.4098   0.01573   0.00688  -0.1196   0.7153   0.0442
  -1.250   0.4327   0.01552   0.00664  -0.1190   0.7129   0.0591
  -1.000   0.4566   0.01525   0.00643  -0.1186   0.7107   0.0886
  -0.750   0.4589   0.01329   0.00664  -0.1142   0.7085   0.7309
  -0.500   0.4785   0.01346   0.00687  -0.1118   0.7068   0.8182
  -0.250   0.4988   0.01367   0.00701  -0.1096   0.7052   0.8522
   0.000   0.5120   0.01397   0.00732  -0.1065   0.7021   0.8744
   0.250   0.5270   0.01419   0.00753  -0.1036   0.6995   0.8915
   0.500   0.5444   0.01433   0.00764  -0.1011   0.6973   0.9067
   0.750   0.5664   0.01441   0.00764  -0.1000   0.6953   0.9170
   1.000   0.5947   0.01442   0.00756  -0.1004   0.6936   0.9196
   1.250   0.6245   0.01443   0.00748  -0.1012   0.6922   0.9218
   1.500   0.6487   0.01456   0.00757  -0.1009   0.6901   0.9252
   1.750   0.6655   0.01480   0.00782  -0.0993   0.6870   0.9305
   2.000   0.6880   0.01496   0.00798  -0.0988   0.6845   0.9345
   2.250   0.7139   0.01507   0.00808  -0.0989   0.6824   0.9381
   2.500   0.7415   0.01514   0.00812  -0.0993   0.6806   0.9417
   2.750   0.7705   0.01519   0.00813  -0.0999   0.6790   0.9454
   3.000   0.8025   0.01524   0.00816  -0.1012   0.6778   0.9482
   3.250   0.8241   0.01555   0.00852  -0.1007   0.6752   0.9536
   3.500   0.8422   0.01591   0.00895  -0.0996   0.6718   0.9606
   3.750   0.8705   0.01613   0.00920  -0.1004   0.6693   0.9648
   4.000   0.9008   0.01627   0.00937  -0.1016   0.6674   0.9693
   4.250   0.9329   0.01639   0.00951  -0.1030   0.6658   0.9738
   4.500   0.9685   0.01647   0.00962  -0.1052   0.6645   0.9771
   4.750   1.0047   0.01653   0.00971  -0.1074   0.6633   0.9807
   5.000   1.0195   0.01727   0.01060  -0.1064   0.6584   0.9988
   5.250   1.0290   0.01760   0.01099  -0.1036   0.6549   1.0000
   5.500   1.0524   0.01773   0.01116  -0.1034   0.6527   1.0000
   5.750   1.0821   0.01776   0.01123  -0.1042   0.6509   1.0000
   6.000   1.1171   0.01767   0.01119  -0.1059   0.6493   1.0000
   6.250   1.0954   0.01871   0.01232  -0.0978   0.6411   1.0000
   6.500   1.1325   0.01823   0.01188  -0.0995   0.6373   1.0000
   6.750   1.1355   0.01858   0.01229  -0.0956   0.6287   1.0000
   7.000   1.1793   0.01755   0.01124  -0.0980   0.6210   1.0000
   7.250   1.1683   0.01856   0.01236  -0.0922   0.6115   1.0000
   7.500   1.1929   0.01847   0.01232  -0.0919   0.6053   1.0000
   7.750   1.1946   0.01931   0.01326  -0.0883   0.5970   1.0000
   8.000   1.2092   0.01969   0.01372  -0.0867   0.5894   1.0000
   8.250   1.2229   0.02012   0.01422  -0.0850   0.5809   1.0000
   8.500   1.2248   0.02119   0.01540  -0.0819   0.5702   1.0000
   8.750   1.2340   0.02192   0.01621  -0.0798   0.5585   1.0000
   9.000   1.2429   0.02271   0.01707  -0.0777   0.5448   1.0000
   9.250   1.2528   0.02345   0.01786  -0.0757   0.5277   1.0000
   9.500   1.2660   0.02398   0.01839  -0.0741   0.5048   1.0000
   9.750   1.2808   0.02426   0.01852  -0.0724   0.4637   1.0000
  10.000   1.2809   0.02547   0.01942  -0.0691   0.4143   1.0000
  10.250   1.2701   0.02761   0.02126  -0.0650   0.3696   1.0000
  10.500   1.2598   0.02995   0.02339  -0.0613   0.3314   1.0000
  10.750   1.2512   0.03238   0.02562  -0.0582   0.2969   1.0000
  11.000   1.2431   0.03490   0.02797  -0.0554   0.2626   1.0000
  11.250   1.2395   0.03723   0.03017  -0.0531   0.2341   1.0000
  11.500   1.2376   0.03952   0.03234  -0.0512   0.2081   1.0000
  12.000   1.2391   0.04385   0.03651  -0.0480   0.1629   1.0000
  12.250   1.2416   0.04597   0.03858  -0.0467   0.1438   1.0000
  12.500   1.2454   0.04801   0.04059  -0.0456   0.1274   1.0000
  12.750   1.2502   0.05000   0.04255  -0.0446   0.1120   1.0000
  13.000   1.2552   0.05202   0.04456  -0.0437   0.0977   1.0000
  13.250   1.2604   0.05405   0.04658  -0.0428   0.0850   1.0000
  13.500   1.2653   0.05615   0.04867  -0.0421   0.0726   1.0000
  13.750   1.2704   0.05828   0.05080  -0.0413   0.0621   1.0000
  14.000   1.2750   0.06046   0.05300  -0.0407   0.0529   1.0000
  14.250   1.2791   0.06278   0.05532  -0.0400   0.0448   1.0000
  14.500   1.2845   0.06497   0.05760  -0.0395   0.0382   1.0000
  14.750   1.2887   0.06736   0.06005  -0.0390   0.0332   1.0000
  15.000   1.2915   0.06994   0.06266  -0.0386   0.0280   1.0000
  15.250   1.2955   0.07242   0.06525  -0.0382   0.0240   1.0000
  15.500   1.2963   0.07533   0.06820  -0.0379   0.0205   1.0000
  15.750   1.3003   0.07790   0.07090  -0.0377   0.0172   1.0000
  16.000   1.3004   0.08100   0.07403  -0.0377   0.0146   1.0000
  16.250   1.3041   0.08370   0.07684  -0.0377   0.0116   1.0000
  16.500   1.3047   0.08681   0.08004  -0.0378   0.0094   1.0000
  16.750   1.3047   0.09008   0.08343  -0.0380   0.0080   1.0000
  17.000   1.3026   0.09372   0.08718  -0.0384   0.0071   1.0000
  17.250   1.3024   0.09713   0.09075  -0.0388   0.0056   1.0000
  17.500   1.2997   0.10101   0.09479  -0.0395   0.0054   1.0000
  17.750   1.2950   0.10523   0.09915  -0.0403   0.0048   1.0000
  18.000   1.2955   0.10871   0.10276  -0.0413   0.0036   1.0000
  18.250   1.2910   0.11303   0.10722  -0.0425   0.0034   1.0000
  18.500   1.2852   0.11769   0.11206  -0.0439   0.0028   1.0000
  18.750   1.2796   0.12240   0.11695  -0.0455   0.0028   1.0000
  19.000   1.2739   0.12721   0.12193  -0.0474   0.0026   1.0000
  19.250   1.2674   0.13229   0.12718  -0.0496   0.0025   1.0000
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