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NREL's S832 Airfoil (s832-nr) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NREL's S832 Airfoil (s832-nr)
Reynolds number: 500,000
Max Cl/Cd: 126.01 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s832-nr-500000.txt
Download as CSV file: xf-s832-nr-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750   0.0188   0.08673   0.08339  -0.1268   0.8019   0.0109
  -9.500   0.0236   0.08390   0.08057  -0.1280   0.7985   0.0111
  -9.250   0.0282   0.08115   0.07781  -0.1291   0.7953   0.0112
  -9.000   0.0320   0.07826   0.07489  -0.1304   0.7923   0.0115
  -8.750   0.0355   0.07542   0.07206  -0.1317   0.7893   0.0116
  -8.500   0.0382   0.07251   0.06918  -0.1331   0.7859   0.0118
  -8.250   0.0391   0.06936   0.06605  -0.1347   0.7824   0.0123
  -8.000   0.0390   0.06627   0.06294  -0.1366   0.7792   0.0122
  -7.750   0.0343   0.06294   0.05961  -0.1391   0.7758   0.0123
  -7.500   0.0251   0.06012   0.05680  -0.1396   0.7720   0.0125
  -7.250   0.0237   0.05711   0.05375  -0.1403   0.7687   0.0127
  -7.000   0.0260   0.05400   0.05055  -0.1410   0.7658   0.0131
  -6.750   0.0328   0.05087   0.04726  -0.1414   0.7632   0.0135
  -6.500   0.0435   0.04782   0.04406  -0.1411   0.7605   0.0138
  -6.250   0.0524   0.02761   0.02396  -0.1325   0.7511   0.0140
  -6.000   0.0570   0.02447   0.02073  -0.1319   0.7489   0.0144
  -5.750   0.0679   0.02217   0.01836  -0.1314   0.7466   0.0147
  -5.500   0.0802   0.01995   0.01606  -0.1307   0.7440   0.0152
  -5.250   0.0947   0.01772   0.01370  -0.1301   0.7415   0.0158
  -5.000   0.1108   0.01546   0.01125  -0.1293   0.7392   0.0169
  -4.750   0.1353   0.01404   0.00945  -0.1277   0.7371   0.0187
  -4.500   0.1457   0.01051   0.00562  -0.1265   0.7352   0.0195
  -4.250   0.1648   0.00919   0.00421  -0.1263   0.7331   0.0204
  -4.000   0.1855   0.00811   0.00302  -0.1258   0.7308   0.0218
  -3.750   0.2128   0.00807   0.00264  -0.1246   0.7284   0.0254
  -3.500   0.2439   0.01882   0.01264  -0.1300   0.7319   0.0176
  -3.250   0.2687   0.01702   0.01060  -0.1292   0.7296   0.0171
  -3.000   0.2950   0.01562   0.00900  -0.1287   0.7274   0.0170
  -2.750   0.3209   0.01375   0.00687  -0.1278   0.7254   0.0150
  -2.500   0.3462   0.01295   0.00596  -0.1273   0.7234   0.0148
  -2.250   0.3713   0.01237   0.00532  -0.1269   0.7216   0.0154
  -2.000   0.3971   0.01201   0.00488  -0.1267   0.7196   0.0168
  -1.750   0.4206   0.01157   0.00444  -0.1260   0.7174   0.0206
  -1.500   0.4457   0.01130   0.00424  -0.1258   0.7151   0.0404
  -1.250   0.4721   0.01118   0.00415  -0.1258   0.7129   0.0589
  -1.000   0.4977   0.01085   0.00395  -0.1258   0.7110   0.1052
  -0.750   0.5046   0.00897   0.00411  -0.1226   0.7090   0.7900
  -0.500   0.5289   0.00917   0.00431  -0.1215   0.7073   0.8324
  -0.250   0.5535   0.00941   0.00451  -0.1206   0.7056   0.8528
   0.000   0.5757   0.00955   0.00467  -0.1193   0.7034   0.8659
   0.250   0.5976   0.00969   0.00482  -0.1179   0.7011   0.8783
   0.500   0.6210   0.00982   0.00493  -0.1170   0.6989   0.8892
   0.750   0.6436   0.00989   0.00499  -0.1158   0.6970   0.8963
   1.000   0.6694   0.00997   0.00503  -0.1156   0.6953   0.9038
   1.250   0.6961   0.01000   0.00502  -0.1156   0.6937   0.9069
   1.500   0.7250   0.01006   0.00503  -0.1161   0.6921   0.9090
   1.750   0.7513   0.01014   0.00510  -0.1163   0.6901   0.9116
   2.000   0.7765   0.01020   0.00518  -0.1162   0.6878   0.9148
   2.250   0.8034   0.01027   0.00525  -0.1165   0.6857   0.9179
   2.500   0.8291   0.01030   0.00529  -0.1164   0.6838   0.9203
   2.750   0.8559   0.01035   0.00534  -0.1166   0.6820   0.9229
   3.000   0.8838   0.01039   0.00538  -0.1170   0.6803   0.9257
   3.250   0.9129   0.01046   0.00543  -0.1177   0.6787   0.9286
   3.500   0.9420   0.01059   0.00554  -0.1184   0.6770   0.9318
   3.750   0.9633   0.01066   0.00569  -0.1175   0.6749   0.9354
   4.000   0.9862   0.01074   0.00585  -0.1169   0.6726   0.9392
   4.250   1.0111   0.01082   0.00596  -0.1168   0.6703   0.9432
   4.500   1.0375   0.01088   0.00605  -0.1170   0.6683   0.9470
   4.750   1.0640   0.01092   0.00611  -0.1171   0.6665   0.9508
   5.000   1.0927   0.01097   0.00618  -0.1176   0.6646   0.9548
   5.250   1.1154   0.01098   0.00625  -0.1170   0.6606   0.9603
   5.500   1.1390   0.01068   0.00598  -0.1163   0.6530   0.9656
   5.750   1.1627   0.01049   0.00580  -0.1156   0.6451   0.9722
   6.000   1.1923   0.01044   0.00580  -0.1165   0.6395   0.9769
   6.250   1.2263   0.01045   0.00582  -0.1183   0.6358   0.9808
   6.500   1.2556   0.01054   0.00603  -0.1193   0.6308   0.9870
   6.750   1.2880   0.01057   0.00612  -0.1210   0.6250   0.9930
   7.000   1.3167   0.01061   0.00620  -0.1218   0.6191   1.0000
   7.250   1.3289   0.01067   0.00634  -0.1193   0.6128   1.0000
   7.500   1.3508   0.01072   0.00641  -0.1187   0.6062   1.0000
   7.750   1.3610   0.01085   0.00664  -0.1157   0.5980   1.0000
   8.000   1.3749   0.01101   0.00683  -0.1135   0.5891   1.0000
   8.250   1.3880   0.01122   0.00705  -0.1112   0.5789   1.0000
   8.500   1.3958   0.01156   0.00742  -0.1079   0.5653   1.0000
   8.750   1.4022   0.01201   0.00792  -0.1046   0.5490   1.0000
   9.000   1.4055   0.01265   0.00854  -0.1008   0.5271   1.0000
   9.250   1.3990   0.01372   0.00949  -0.0957   0.4938   1.0000
   9.500   1.3818   0.01549   0.01103  -0.0893   0.4493   1.0000
   9.750   1.3611   0.01775   0.01306  -0.0830   0.4059   1.0000
  10.000   1.3396   0.02035   0.01541  -0.0771   0.3621   1.0000
  10.250   1.3253   0.02279   0.01766  -0.0726   0.3249   1.0000
  10.500   1.3130   0.02527   0.01996  -0.0686   0.2874   1.0000
  10.750   1.3052   0.02761   0.02213  -0.0653   0.2547   1.0000
  11.000   1.2994   0.02990   0.02426  -0.0625   0.2234   1.0000
  11.250   1.2963   0.03210   0.02631  -0.0601   0.1943   1.0000
  11.750   1.2984   0.03605   0.03006  -0.0563   0.1476   1.0000
  12.000   1.2976   0.03825   0.03210  -0.0544   0.1214   1.0000
  12.250   1.3042   0.03991   0.03373  -0.0532   0.1080   1.0000
  12.500   1.3094   0.04172   0.03549  -0.0520   0.0937   1.0000
  12.750   1.3130   0.04368   0.03735  -0.0507   0.0763   1.0000
  13.000   1.3200   0.04543   0.03910  -0.0497   0.0674   1.0000
  13.250   1.3245   0.04739   0.04099  -0.0486   0.0528   1.0000
  13.500   1.3288   0.04942   0.04295  -0.0476   0.0410   1.0000
  13.750   1.3345   0.05136   0.04486  -0.0468   0.0327   1.0000
  14.000   1.3395   0.05339   0.04688  -0.0459   0.0254   1.0000
  14.250   1.3448   0.05546   0.04895  -0.0452   0.0204   1.0000
  14.500   1.3526   0.05731   0.05087  -0.0446   0.0178   1.0000
  14.750   1.3580   0.05942   0.05299  -0.0440   0.0139   1.0000
  15.000   1.3614   0.06179   0.05538  -0.0434   0.0105   1.0000
  15.250   1.3605   0.06467   0.05825  -0.0426   0.0053   1.0000
  15.500   1.3563   0.06808   0.06175  -0.0417   0.0028   1.0000
  15.750   1.3607   0.07054   0.06432  -0.0414   0.0028   1.0000
  16.000   1.3578   0.07392   0.06781  -0.0410   0.0020   1.0000
  16.250   1.3573   0.07708   0.07110  -0.0407   0.0019   1.0000
  16.500   1.3571   0.08027   0.07444  -0.0406   0.0017   1.0000
  16.750   1.3572   0.08350   0.07778  -0.0406   0.0017   1.0000
  17.000   1.3566   0.08689   0.08130  -0.0408   0.0016   1.0000
  17.250   1.3534   0.09065   0.08520  -0.0410   0.0014   1.0000
  17.500   1.3515   0.09434   0.08901  -0.0415   0.0015   1.0000
  17.750   1.3477   0.09836   0.09316  -0.0421   0.0014   1.0000
  18.000   1.3426   0.10265   0.09758  -0.0429   0.0013   1.0000
  18.250   1.3381   0.10693   0.10199  -0.0438   0.0013   1.0000
  18.500   1.3310   0.11170   0.10689  -0.0450   0.0012   1.0000
  18.750   1.3270   0.11604   0.11136  -0.0463   0.0012   1.0000
  19.000   1.3212   0.12073   0.11618  -0.0479   0.0012   1.0000
  19.250   1.3147   0.12564   0.12123  -0.0496   0.0012   1.0000
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