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NREL's S802 Airfoil (s802-nr) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NREL's S802 Airfoil (s802-nr)
Reynolds number: 1,000,000
Max Cl/Cd: 132.52 at α=2.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s802-nr-1000000-n5.txt
Download as CSV file: xf-s802-nr-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NREL's S802 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.7156   0.03819   0.03590  -0.1071   0.9893   0.0070
 -12.250  -0.7018   0.03545   0.03307  -0.1114   0.9863   0.0072
 -12.000  -0.7102   0.03151   0.02892  -0.1143   0.9775   0.0072
 -11.250  -0.6676   0.02574   0.02269  -0.1176   0.9512   0.0076
 -11.000  -0.6404   0.02392   0.02067  -0.1202   0.9445   0.0078
 -10.750  -0.6066   0.02200   0.01852  -0.1241   0.9380   0.0080
 -10.500  -0.5657   0.02029   0.01657  -0.1290   0.9328   0.0083
 -10.250  -0.5263   0.01879   0.01482  -0.1333   0.9223   0.0085
 -10.000  -0.4912   0.01783   0.01365  -0.1360   0.9068   0.0088
  -9.750  -0.4639   0.01708   0.01268  -0.1368   0.8884   0.0089
  -9.500  -0.4422   0.01610   0.01148  -0.1366   0.8707   0.0091
  -9.250  -0.4198   0.01545   0.01068  -0.1363   0.8554   0.0093
  -9.000  -0.3964   0.01501   0.01012  -0.1360   0.8419   0.0095
  -8.500  -0.3474   0.01441   0.00934  -0.1354   0.8184   0.0100
  -8.250  -0.3229   0.01399   0.00882  -0.1351   0.8089   0.0103
  -8.000  -0.2983   0.01355   0.00826  -0.1349   0.8000   0.0105
  -7.750  -0.2732   0.01307   0.00768  -0.1347   0.7922   0.0108
  -7.500  -0.2480   0.01264   0.00714  -0.1345   0.7846   0.0110
  -7.250  -0.2221   0.01222   0.00663  -0.1344   0.7779   0.0113
  -7.000  -0.1961   0.01186   0.00618  -0.1343   0.7712   0.0116
  -6.750  -0.1696   0.01157   0.00582  -0.1343   0.7653   0.0118
  -6.500  -0.1429   0.01129   0.00547  -0.1343   0.7590   0.0121
  -6.000  -0.0902   0.01040   0.00445  -0.1343   0.7480   0.0129
  -5.750  -0.0630   0.01013   0.00413  -0.1344   0.7428   0.0133
  -5.250  -0.0081   0.00965   0.00355  -0.1345   0.7341   0.0140
  -5.000   0.0196   0.00941   0.00328  -0.1347   0.7298   0.0144
  -4.750   0.0473   0.00921   0.00303  -0.1348   0.7257   0.0148
  -4.500   0.0751   0.00904   0.00281  -0.1349   0.7218   0.0153
  -4.250   0.1033   0.00888   0.00263  -0.1350   0.7181   0.0157
  -4.000   0.1314   0.00866   0.00237  -0.1352   0.7141   0.0166
  -3.750   0.1595   0.00850   0.00218  -0.1354   0.7105   0.0174
  -3.500   0.1875   0.00837   0.00202  -0.1355   0.7073   0.0182
  -3.250   0.2161   0.00825   0.00189  -0.1357   0.7045   0.0192
  -3.000   0.2446   0.00814   0.00177  -0.1359   0.7014   0.0202
  -2.750   0.2730   0.00803   0.00165  -0.1361   0.6983   0.0236
  -2.500   0.3014   0.00785   0.00155  -0.1364   0.6952   0.0437
  -2.250   0.3297   0.00769   0.00147  -0.1366   0.6922   0.0711
  -2.000   0.3586   0.00748   0.00140  -0.1370   0.6897   0.1121
  -1.750   0.3874   0.00733   0.00134  -0.1374   0.6871   0.1479
  -1.500   0.4162   0.00713   0.00130  -0.1378   0.6844   0.2006
  -1.250   0.4450   0.00694   0.00127  -0.1383   0.6816   0.2602
  -1.000   0.4739   0.00672   0.00125  -0.1388   0.6789   0.3388
  -0.750   0.5034   0.00633   0.00124  -0.1396   0.6765   0.4744
  -0.500   0.5330   0.00598   0.00127  -0.1403   0.6739   0.6061
  -0.250   0.5616   0.00592   0.00133  -0.1405   0.6704   0.6598
   0.000   0.5897   0.00594   0.00138  -0.1405   0.6660   0.6829
   0.250   0.6176   0.00600   0.00142  -0.1405   0.6613   0.6975
   0.500   0.6460   0.00603   0.00145  -0.1406   0.6561   0.7084
   0.750   0.6737   0.00608   0.00150  -0.1406   0.6499   0.7170
   1.000   0.7016   0.00613   0.00153  -0.1406   0.6436   0.7246
   1.250   0.7292   0.00618   0.00158  -0.1405   0.6362   0.7313
   1.500   0.7568   0.00625   0.00163  -0.1405   0.6290   0.7379
   1.750   0.7842   0.00631   0.00169  -0.1404   0.6207   0.7431
   2.000   0.8115   0.00638   0.00175  -0.1403   0.6113   0.7487
   2.250   0.8383   0.00648   0.00181  -0.1401   0.5990   0.7546
   2.500   0.8647   0.00657   0.00189  -0.1398   0.5847   0.7596
   2.750   0.8905   0.00672   0.00198  -0.1394   0.5632   0.7634
   3.000   0.9143   0.00698   0.00209  -0.1386   0.5289   0.7663
   3.250   0.9337   0.00754   0.00235  -0.1371   0.4650   0.7689
   3.500   0.9539   0.00809   0.00265  -0.1357   0.4106   0.7711
   3.750   0.9750   0.00857   0.00293  -0.1346   0.3655   0.7734
   4.000   0.9952   0.00910   0.00324  -0.1333   0.3170   0.7757
   4.250   1.0153   0.00963   0.00355  -0.1320   0.2718   0.7780
   4.500   1.0371   0.01004   0.00383  -0.1310   0.2403   0.7804
   4.750   1.0586   0.01046   0.00411  -0.1299   0.2109   0.7829
   5.000   1.0796   0.01090   0.00441  -0.1288   0.1823   0.7851
   5.250   1.1013   0.01127   0.00470  -0.1278   0.1607   0.7873
   5.500   1.1223   0.01166   0.00501  -0.1266   0.1402   0.7895
   5.750   1.1434   0.01204   0.00531  -0.1255   0.1221   0.7920
   6.000   1.1645   0.01241   0.00562  -0.1244   0.1073   0.7949
   6.250   1.1855   0.01277   0.00593  -0.1233   0.0952   0.7978
   6.500   1.2064   0.01313   0.00625  -0.1221   0.0855   0.8004
   6.750   1.2266   0.01348   0.00657  -0.1209   0.0770   0.8030
   7.000   1.2461   0.01378   0.00688  -0.1194   0.0704   0.8060
   7.250   1.2637   0.01416   0.00724  -0.1176   0.0628   0.8093
   7.500   1.2824   0.01450   0.00758  -0.1161   0.0580   0.8128
   7.750   1.3000   0.01490   0.00797  -0.1144   0.0527   0.8162
   8.000   1.3187   0.01524   0.00834  -0.1128   0.0496   0.8202
   8.250   1.3358   0.01566   0.00877  -0.1111   0.0454   0.8248
   8.500   1.3532   0.01609   0.00921  -0.1094   0.0419   0.8294
   8.750   1.3709   0.01648   0.00965  -0.1078   0.0396   0.8340
   9.000   1.3872   0.01696   0.01014  -0.1061   0.0369   0.8395
   9.250   1.4032   0.01747   0.01068  -0.1043   0.0340   0.8453
   9.500   1.4198   0.01792   0.01119  -0.1026   0.0326   0.8518
   9.750   1.4358   0.01843   0.01174  -0.1009   0.0308   0.8594
  10.000   1.4500   0.01902   0.01237  -0.0990   0.0286   0.8685
  10.250   1.4643   0.01961   0.01302  -0.0972   0.0266   0.8802
  10.500   1.4780   0.02016   0.01365  -0.0952   0.0249   0.8995
  10.750   1.4886   0.02067   0.01429  -0.0927   0.0234   1.0000
  11.000   1.5021   0.02146   0.01510  -0.0910   0.0217   1.0000
  11.250   1.5164   0.02221   0.01589  -0.0895   0.0208   1.0000
  11.500   1.5306   0.02298   0.01671  -0.0880   0.0199   1.0000
  11.750   1.5439   0.02383   0.01759  -0.0865   0.0188   1.0000
  12.000   1.5564   0.02477   0.01855  -0.0850   0.0177   1.0000
  12.250   1.5680   0.02579   0.01960  -0.0834   0.0165   1.0000
  12.500   1.5809   0.02674   0.02062  -0.0821   0.0157   1.0000
  12.750   1.5929   0.02778   0.02171  -0.0807   0.0148   1.0000
  13.000   1.6039   0.02893   0.02289  -0.0793   0.0138   1.0000
  13.250   1.6141   0.03017   0.02416  -0.0779   0.0129   1.0000
  13.500   1.6249   0.03139   0.02544  -0.0766   0.0122   1.0000
  13.750   1.6350   0.03269   0.02680  -0.0754   0.0114   1.0000
  14.000   1.6439   0.03413   0.02828  -0.0742   0.0105   1.0000
  14.250   1.6521   0.03566   0.02986  -0.0729   0.0097   1.0000
  14.500   1.6607   0.03718   0.03146  -0.0718   0.0091   1.0000
  14.750   1.6684   0.03884   0.03318  -0.0708   0.0084   1.0000
  15.000   1.6745   0.04068   0.03507  -0.0697   0.0077   1.0000
  15.250   1.6808   0.04255   0.03701  -0.0688   0.0071   1.0000
  15.500   1.6867   0.04450   0.03904  -0.0679   0.0065   1.0000
  15.750   1.6913   0.04665   0.04125  -0.0671   0.0060   1.0000
  16.000   1.6943   0.04902   0.04369  -0.0663   0.0054   1.0000
  16.250   1.6981   0.05136   0.04611  -0.0657   0.0051   1.0000
  16.500   1.7014   0.05382   0.04866  -0.0652   0.0048   1.0000
  16.750   1.7036   0.05648   0.05142  -0.0648   0.0045   1.0000
  17.000   1.7044   0.05939   0.05442  -0.0645   0.0042   1.0000
  17.250   1.7041   0.06249   0.05762  -0.0644   0.0040   1.0000
  17.500   1.7028   0.06584   0.06106  -0.0645   0.0038   1.0000
  18.000   1.6985   0.07308   0.06852  -0.0651   0.0035   1.0000
  18.250   1.6955   0.07696   0.07251  -0.0658   0.0035   1.0000
  18.500   1.6912   0.08115   0.07682  -0.0666   0.0034   1.0000
  18.750   1.6857   0.08565   0.08145  -0.0678   0.0033   1.0000
  19.000   1.6789   0.09053   0.08645  -0.0693   0.0032   1.0000
  19.250   1.6704   0.09582   0.09187  -0.0711   0.0031   1.0000
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