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NREL's S832 Airfoil (s832-nr) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NREL's S832 Airfoil (s832-nr)
Reynolds number: 500,000
Max Cl/Cd: 118.92 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s832-nr-500000-n5.txt
Download as CSV file: xf-s832-nr-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.750   0.0376   0.08761   0.08420  -0.1110   0.7553   0.0076
 -10.500   0.0422   0.08451   0.08110  -0.1121   0.7531   0.0078
 -10.250   0.0462   0.08123   0.07781  -0.1132   0.7509   0.0078
 -10.000   0.0501   0.07807   0.07463  -0.1143   0.7489   0.0078
  -9.750   0.0537   0.07479   0.07135  -0.1155   0.7469   0.0079
  -9.500   0.0568   0.07139   0.06796  -0.1167   0.7448   0.0080
  -9.250   0.0596   0.06806   0.06464  -0.1178   0.7426   0.0080
  -9.000   0.0615   0.06460   0.06119  -0.1190   0.7403   0.0082
  -8.750   0.0634   0.06126   0.05785  -0.1202   0.7381   0.0082
  -8.500   0.0643   0.05786   0.05444  -0.1215   0.7359   0.0082
  -8.250   0.0637   0.05435   0.05093  -0.1228   0.7337   0.0084
  -8.000   0.0627   0.05082   0.04742  -0.1245   0.7314   0.0082
  -7.750   0.0593   0.04716   0.04379  -0.1266   0.7289   0.0081
  -7.500   0.0501   0.04337   0.04000  -0.1296   0.7263   0.0081
  -7.000   0.0112   0.05079   0.04702  -0.1385   0.7275   0.0071
  -6.750   0.0288   0.03293   0.02936  -0.1305   0.7194   0.0066
  -6.500   0.0314   0.02966   0.02602  -0.1303   0.7169   0.0062
  -6.250   0.0236   0.04019   0.03601  -0.1363   0.7204   0.0047
  -6.000   0.0341   0.03709   0.03274  -0.1353   0.7182   0.0046
  -5.750   0.0467   0.03411   0.02958  -0.1342   0.7156   0.0045
  -5.500   0.0605   0.03087   0.02611  -0.1328   0.7131   0.0045
  -5.250   0.0750   0.02727   0.02221  -0.1309   0.7108   0.0045
  -5.000   0.0864   0.02090   0.01520  -0.1274   0.7087   0.0047
  -4.750   0.1052   0.01719   0.01091  -0.1256   0.7068   0.0050
  -4.500   0.1299   0.01627   0.00979  -0.1253   0.7050   0.0053
  -4.250   0.1550   0.01520   0.00853  -0.1250   0.7030   0.0055
  -4.000   0.1806   0.01450   0.00769  -0.1248   0.7008   0.0060
  -3.750   0.2065   0.01394   0.00699  -0.1246   0.6985   0.0068
  -3.500   0.2322   0.01337   0.00628  -0.1243   0.6963   0.0071
  -3.250   0.2570   0.01270   0.00550  -0.1239   0.6943   0.0071
  -3.000   0.2812   0.01208   0.00479  -0.1234   0.6924   0.0074
  -2.750   0.3061   0.01166   0.00432  -0.1231   0.6905   0.0077
  -2.500   0.3314   0.01136   0.00399  -0.1229   0.6885   0.0081
  -2.250   0.3571   0.01109   0.00368  -0.1227   0.6865   0.0089
  -2.000   0.3829   0.01085   0.00340  -0.1226   0.6844   0.0104
  -1.750   0.4089   0.01064   0.00318  -0.1225   0.6824   0.0150
  -1.500   0.4353   0.01050   0.00306  -0.1225   0.6804   0.0264
  -1.250   0.4620   0.01038   0.00299  -0.1226   0.6785   0.0428
  -1.000   0.4888   0.01027   0.00288  -0.1227   0.6767   0.0567
  -0.750   0.5149   0.01012   0.00282  -0.1228   0.6747   0.0883
  -0.500   0.5261   0.00823   0.00280  -0.1209   0.6726   0.7135
  -0.250   0.5505   0.00823   0.00294  -0.1202   0.6706   0.7846
   0.000   0.5764   0.00830   0.00302  -0.1199   0.6687   0.8080
   0.250   0.6026   0.00839   0.00308  -0.1196   0.6669   0.8260
   0.500   0.6288   0.00847   0.00313  -0.1194   0.6651   0.8383
   0.750   0.6559   0.00856   0.00317  -0.1195   0.6634   0.8472
   1.000   0.6818   0.00863   0.00324  -0.1193   0.6614   0.8539
   1.250   0.7091   0.00868   0.00328  -0.1195   0.6594   0.8571
   1.500   0.7367   0.00873   0.00331  -0.1199   0.6575   0.8596
   1.750   0.7637   0.00878   0.00335  -0.1200   0.6556   0.8615
   2.000   0.7908   0.00883   0.00340  -0.1202   0.6538   0.8635
   2.250   0.8182   0.00889   0.00344  -0.1205   0.6520   0.8656
   2.500   0.8459   0.00896   0.00348  -0.1208   0.6502   0.8681
   2.750   0.8734   0.00904   0.00355  -0.1212   0.6485   0.8709
   3.000   0.9000   0.00911   0.00366  -0.1213   0.6465   0.8737
   3.250   0.9261   0.00918   0.00376  -0.1214   0.6446   0.8759
   3.500   0.9521   0.00925   0.00386  -0.1214   0.6426   0.8782
   3.750   0.9783   0.00932   0.00396  -0.1214   0.6405   0.8808
   4.000   1.0048   0.00940   0.00407  -0.1216   0.6385   0.8837
   4.250   1.0320   0.00949   0.00417  -0.1219   0.6369   0.8867
   4.750   1.0837   0.00967   0.00445  -0.1219   0.6330   0.8923
   5.000   1.1079   0.00976   0.00461  -0.1216   0.6306   0.8955
   5.250   1.1306   0.00982   0.00472  -0.1210   0.6260   0.8991
   5.750   1.1631   0.00987   0.00480  -0.1168   0.6040   0.9085
   6.000   1.1778   0.00995   0.00490  -0.1144   0.5949   0.9145
   6.250   1.1951   0.01005   0.00507  -0.1127   0.5894   0.9200
   6.500   1.2102   0.01019   0.00527  -0.1105   0.5826   0.9270
   6.750   1.2256   0.01035   0.00549  -0.1084   0.5756   0.9353
   7.000   1.2399   0.01053   0.00573  -0.1061   0.5672   0.9475
   7.250   1.2584   0.01077   0.00603  -0.1049   0.5556   0.9651
   7.500   1.2786   0.01109   0.00637  -0.1044   0.5412   1.0000
   7.750   1.2879   0.01160   0.00683  -0.1016   0.5227   1.0000
   8.000   1.2908   0.01236   0.00752  -0.0979   0.4952   1.0000
   8.250   1.2808   0.01372   0.00868  -0.0924   0.4541   1.0000
   8.500   1.2655   0.01556   0.01030  -0.0864   0.4114   1.0000
   8.750   1.2530   0.01752   0.01207  -0.0814   0.3726   1.0000
   9.000   1.2424   0.01957   0.01394  -0.0769   0.3355   1.0000
   9.250   1.2373   0.02144   0.01566  -0.0734   0.3042   1.0000
   9.500   1.2314   0.02346   0.01753  -0.0700   0.2706   1.0000
   9.750   1.2279   0.02544   0.01936  -0.0670   0.2396   1.0000
  10.000   1.2278   0.02726   0.02106  -0.0646   0.2124   1.0000
  10.250   1.2309   0.02893   0.02264  -0.0626   0.1895   1.0000
  10.500   1.2336   0.03066   0.02428  -0.0606   0.1673   1.0000
  10.750   1.2384   0.03230   0.02584  -0.0589   0.1473   1.0000
  11.000   1.2444   0.03389   0.02736  -0.0574   0.1304   1.0000
  11.500   1.2585   0.03700   0.03039  -0.0548   0.1023   1.0000
  11.750   1.2654   0.03861   0.03196  -0.0536   0.0883   1.0000
  12.000   1.2700   0.04044   0.03369  -0.0523   0.0700   1.0000
  12.250   1.2787   0.04197   0.03523  -0.0513   0.0616   1.0000
  12.500   1.2870   0.04355   0.03680  -0.0504   0.0532   1.0000
  12.750   1.2923   0.04542   0.03861  -0.0493   0.0409   1.0000
  13.000   1.3026   0.04691   0.04014  -0.0486   0.0374   1.0000
  13.250   1.3070   0.04892   0.04208  -0.0476   0.0270   1.0000
  13.500   1.3125   0.05087   0.04400  -0.0467   0.0196   1.0000
  13.750   1.3191   0.05275   0.04588  -0.0460   0.0143   1.0000
  14.000   1.3246   0.05478   0.04792  -0.0452   0.0098   1.0000
  14.250   1.3323   0.05664   0.04982  -0.0446   0.0076   1.0000
  14.500   1.3411   0.05841   0.05167  -0.0442   0.0070   1.0000
  14.750   1.3470   0.06049   0.05378  -0.0436   0.0048   1.0000
  15.000   1.3543   0.06247   0.05584  -0.0432   0.0039   1.0000
  15.250   1.3590   0.06477   0.05819  -0.0428   0.0023   1.0000
  15.500   1.3631   0.06716   0.06065  -0.0423   0.0013   1.0000
  15.750   1.3701   0.06927   0.06286  -0.0421   0.0013   1.0000
  16.000   1.3726   0.07194   0.06560  -0.0417   0.0008   1.0000
  16.250   1.3768   0.07446   0.06823  -0.0416   0.0007   1.0000
  16.500   1.3777   0.07740   0.07130  -0.0414   0.0005   1.0000
  16.750   1.3819   0.08000   0.07400  -0.0414   0.0005   1.0000
  17.000   1.3838   0.08294   0.07707  -0.0414   0.0004   1.0000
  17.250   1.3845   0.08608   0.08033  -0.0415   0.0003   1.0000
  17.500   1.3872   0.08901   0.08337  -0.0418   0.0004   1.0000
  17.750   1.3875   0.09227   0.08676  -0.0422   0.0003   1.0000
  18.000   1.3848   0.09604   0.09068  -0.0427   0.0003   1.0000
  18.250   1.3843   0.09955   0.09433  -0.0433   0.0003   1.0000
  18.500   1.3803   0.10368   0.09860  -0.0441   0.0002   1.0000
  18.750   1.3788   0.10744   0.10249  -0.0450   0.0003   1.0000
  19.000   1.3759   0.11150   0.10668  -0.0461   0.0002   1.0000
  19.250   1.3710   0.11594   0.11126  -0.0475   0.0002   1.0000
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