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NREL's S803 Airfoil (s803-nr) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NREL's S803 Airfoil (s803-nr)
Reynolds number: 1,000,000
Max Cl/Cd: 124.01 at α=3°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s803-nr-1000000-n5.txt
Download as CSV file: xf-s803-nr-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NREL's S803 Airfoil                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.8342   0.04188   0.03951  -0.0851   0.9984   0.0067
 -12.750  -0.8375   0.03538   0.03277  -0.0945   0.9952   0.0068
 -12.500  -0.8356   0.03092   0.02810  -0.1006   0.9904   0.0069
 -12.250  -0.8129   0.02862   0.02565  -0.1049   0.9875   0.0070
 -12.000  -0.7844   0.02776   0.02474  -0.1071   0.9861   0.0072
 -11.750  -0.7569   0.02633   0.02320  -0.1099   0.9848   0.0073
 -11.500  -0.7301   0.02598   0.02285  -0.1107   0.9829   0.0075
 -11.250  -0.7123   0.02457   0.02131  -0.1111   0.9784   0.0076
 -11.000  -0.6865   0.02329   0.01990  -0.1128   0.9756   0.0078
 -10.750  -0.6585   0.02203   0.01851  -0.1146   0.9736   0.0080
 -10.500  -0.6400   0.02094   0.01728  -0.1142   0.9680   0.0082
 -10.250  -0.6154   0.01974   0.01593  -0.1150   0.9634   0.0084
 -10.000  -0.5894   0.01864   0.01468  -0.1159   0.9593   0.0086
  -9.750  -0.5670   0.01780   0.01372  -0.1156   0.9518   0.0088
  -9.250  -0.5068   0.01618   0.01185  -0.1181   0.9414   0.0091
  -9.000  -0.4721   0.01501   0.01054  -0.1206   0.9368   0.0094
  -8.750  -0.4320   0.01435   0.00981  -0.1238   0.9327   0.0098
  -8.500  -0.3883   0.01383   0.00923  -0.1277   0.9263   0.0101
  -8.250  -0.3438   0.01332   0.00863  -0.1318   0.9167   0.0104
  -8.000  -0.3055   0.01279   0.00796  -0.1345   0.8999   0.0107
  -7.750  -0.2746   0.01233   0.00736  -0.1355   0.8801   0.0111
  -7.500  -0.2473   0.01196   0.00683  -0.1357   0.8610   0.0113
  -7.250  -0.2214   0.01162   0.00635  -0.1355   0.8434   0.0116
  -7.000  -0.1956   0.01132   0.00593  -0.1353   0.8270   0.0119
  -6.750  -0.1698   0.01107   0.00556  -0.1351   0.8113   0.0121
  -6.500  -0.1438   0.01082   0.00521  -0.1348   0.7965   0.0123
  -6.250  -0.1182   0.01034   0.00462  -0.1347   0.7827   0.0129
  -6.000  -0.0916   0.01008   0.00429  -0.1347   0.7700   0.0133
  -5.750  -0.0647   0.00985   0.00399  -0.1346   0.7588   0.0137
  -5.500  -0.0376   0.00963   0.00370  -0.1346   0.7484   0.0141
  -5.000   0.0171   0.00923   0.00316  -0.1346   0.7281   0.0149
  -4.750   0.0445   0.00907   0.00293  -0.1346   0.7187   0.0153
  -4.500   0.0721   0.00892   0.00272  -0.1346   0.7091   0.0157
  -4.250   0.1001   0.00878   0.00252  -0.1347   0.7010   0.0162
  -4.000   0.1279   0.00859   0.00229  -0.1348   0.6930   0.0173
  -3.750   0.1561   0.00845   0.00212  -0.1349   0.6859   0.0182
  -3.500   0.1842   0.00835   0.00197  -0.1350   0.6786   0.0191
  -3.250   0.2124   0.00826   0.00184  -0.1351   0.6718   0.0201
  -3.000   0.2406   0.00817   0.00172  -0.1352   0.6646   0.0224
  -2.750   0.2688   0.00805   0.00161  -0.1354   0.6583   0.0307
  -2.500   0.2975   0.00786   0.00151  -0.1357   0.6522   0.0584
  -2.250   0.3259   0.00769   0.00143  -0.1359   0.6466   0.0933
  -2.000   0.3547   0.00753   0.00137  -0.1363   0.6415   0.1318
  -1.750   0.3834   0.00737   0.00132  -0.1366   0.6359   0.1755
  -1.250   0.4412   0.00701   0.00124  -0.1374   0.6257   0.2909
  -1.000   0.4707   0.00668   0.00121  -0.1382   0.6210   0.4027
  -0.750   0.5001   0.00632   0.00123  -0.1388   0.6164   0.5474
  -0.500   0.5287   0.00629   0.00129  -0.1390   0.6121   0.5910
  -0.250   0.5572   0.00632   0.00132  -0.1391   0.6074   0.6065
   0.000   0.5853   0.00636   0.00136  -0.1391   0.6027   0.6201
   0.250   0.6134   0.00642   0.00139  -0.1391   0.5976   0.6298
   0.500   0.6416   0.00646   0.00144  -0.1392   0.5911   0.6373
   0.750   0.6692   0.00655   0.00148  -0.1391   0.5838   0.6451
   1.000   0.6972   0.00659   0.00153  -0.1391   0.5760   0.6520
   1.250   0.7247   0.00668   0.00159  -0.1390   0.5680   0.6588
   1.500   0.7525   0.00674   0.00165  -0.1389   0.5594   0.6660
   1.750   0.7799   0.00683   0.00172  -0.1388   0.5502   0.6737
   2.000   0.8072   0.00693   0.00178  -0.1387   0.5399   0.6791
   2.250   0.8347   0.00700   0.00186  -0.1386   0.5301   0.6831
   2.500   0.8619   0.00711   0.00194  -0.1385   0.5189   0.6862
   2.750   0.8887   0.00723   0.00202  -0.1383   0.5041   0.6891
   3.000   0.9152   0.00738   0.00211  -0.1380   0.4870   0.6917
   3.250   0.9409   0.00759   0.00223  -0.1376   0.4631   0.6945
   3.500   0.9649   0.00793   0.00241  -0.1370   0.4224   0.6974
   3.750   0.9873   0.00841   0.00267  -0.1360   0.3747   0.7003
   4.000   1.0095   0.00893   0.00297  -0.1351   0.3275   0.7034
   4.250   1.0314   0.00946   0.00329  -0.1341   0.2811   0.7063
   4.500   1.0537   0.00994   0.00359  -0.1332   0.2423   0.7094
   4.750   1.0771   0.01033   0.00387  -0.1325   0.2148   0.7129
   5.000   1.0998   0.01075   0.00416  -0.1317   0.1863   0.7167
   5.250   1.1226   0.01116   0.00447  -0.1309   0.1616   0.7203
   5.500   1.1454   0.01156   0.00477  -0.1301   0.1410   0.7238
   5.750   1.1681   0.01194   0.00508  -0.1292   0.1226   0.7276
   6.000   1.1910   0.01230   0.00538  -0.1284   0.1079   0.7318
   6.250   1.2137   0.01267   0.00570  -0.1276   0.0949   0.7363
   6.500   1.2362   0.01303   0.00603  -0.1267   0.0842   0.7409
   6.750   1.2590   0.01335   0.00635  -0.1259   0.0763   0.7463
   7.000   1.2816   0.01368   0.00667  -0.1251   0.0695   0.7519
   7.250   1.3031   0.01407   0.00704  -0.1240   0.0618   0.7572
   7.500   1.3253   0.01439   0.00738  -0.1231   0.0568   0.7635
   7.750   1.3461   0.01478   0.00777  -0.1220   0.0516   0.7699
   8.000   1.3676   0.01511   0.00813  -0.1210   0.0482   0.7770
   8.500   1.4069   0.01589   0.00896  -0.1183   0.0404   0.7941
   8.750   1.4255   0.01623   0.00935  -0.1167   0.0384   0.8045
   9.000   1.4423   0.01664   0.00980  -0.1149   0.0358   0.8167
   9.250   1.4581   0.01710   0.01031  -0.1129   0.0329   0.8310
   9.500   1.4752   0.01747   0.01076  -0.1111   0.0316   0.8483
   9.750   1.4906   0.01789   0.01126  -0.1091   0.0297   0.8725
  10.000   1.4999   0.01821   0.01173  -0.1058   0.0275   1.0000
  10.250   1.5149   0.01878   0.01232  -0.1039   0.0254   1.0000
  10.500   1.5305   0.01934   0.01291  -0.1022   0.0239   1.0000
  10.750   1.5446   0.01997   0.01357  -0.1003   0.0224   1.0000
  11.000   1.5579   0.02069   0.01430  -0.0983   0.0210   1.0000
  11.250   1.5715   0.02139   0.01505  -0.0964   0.0200   1.0000
  11.500   1.5850   0.02211   0.01582  -0.0946   0.0192   1.0000
  11.750   1.5975   0.02291   0.01666  -0.0928   0.0183   1.0000
  12.000   1.6089   0.02381   0.01759  -0.0909   0.0171   1.0000
  12.250   1.6193   0.02482   0.01864  -0.0890   0.0160   1.0000
  12.500   1.6307   0.02578   0.01966  -0.0873   0.0153   1.0000
  12.750   1.6414   0.02683   0.02077  -0.0857   0.0144   1.0000
  13.000   1.6509   0.02802   0.02199  -0.0840   0.0134   1.0000
  13.250   1.6593   0.02933   0.02334  -0.0824   0.0125   1.0000
  13.500   1.6684   0.03064   0.02471  -0.0809   0.0118   1.0000
  13.750   1.6769   0.03204   0.02618  -0.0796   0.0111   1.0000
  14.000   1.6842   0.03360   0.02779  -0.0782   0.0102   1.0000
  14.250   1.6901   0.03534   0.02959  -0.0769   0.0094   1.0000
  14.500   1.6971   0.03704   0.03136  -0.0758   0.0089   1.0000
  14.750   1.7028   0.03891   0.03329  -0.0748   0.0082   1.0000
  15.000   1.7074   0.04095   0.03540  -0.0738   0.0075   1.0000
  15.250   1.7110   0.04316   0.03768  -0.0729   0.0069   1.0000
  15.500   1.7152   0.04537   0.03997  -0.0722   0.0065   1.0000
  15.750   1.7181   0.04781   0.04248  -0.0716   0.0059   1.0000
  16.000   1.7197   0.05044   0.04519  -0.0711   0.0055   1.0000
  16.250   1.7203   0.05328   0.04812  -0.0707   0.0050   1.0000
  16.500   1.7219   0.05609   0.05103  -0.0705   0.0048   1.0000
  16.750   1.7224   0.05912   0.05415  -0.0705   0.0045   1.0000
  17.000   1.7219   0.06237   0.05750  -0.0706   0.0043   1.0000
  17.250   1.7203   0.06584   0.06106  -0.0709   0.0041   1.0000
  17.500   1.7175   0.06958   0.06490  -0.0713   0.0039   1.0000
  17.750   1.7137   0.07359   0.06902  -0.0720   0.0037   1.0000
  18.000   1.7087   0.07789   0.07342  -0.0729   0.0035   1.0000
  18.250   1.7028   0.08243   0.07807  -0.0741   0.0034   1.0000
  18.500   1.6974   0.08701   0.08278  -0.0754   0.0034   1.0000
  18.750   1.6906   0.09195   0.08784  -0.0770   0.0033   1.0000
  19.000   1.6829   0.09716   0.09318  -0.0789   0.0032   1.0000
  19.250   1.6738   0.10274   0.09888  -0.0811   0.0032   1.0000
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