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NREL's S802 Airfoil (s802-nr) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: NREL's S802 Airfoil (s802-nr)
Reynolds number: 200,000
Max Cl/Cd: 85.66 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s802-nr-200000-n5.txt
Download as CSV file: xf-s802-nr-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.3590   0.12178   0.11807  -0.0476   1.0000   0.0259
 -11.000  -0.3592   0.11824   0.11457  -0.0480   1.0000   0.0259
 -10.750  -0.3600   0.11476   0.11113  -0.0483   1.0000   0.0259
 -10.500  -0.3569   0.11037   0.10674  -0.0465   1.0000   0.0201
 -10.250  -0.3571   0.10779   0.10421  -0.0458   1.0000   0.0198
 -10.000  -0.3483   0.10356   0.09999  -0.0488   0.9982   0.0195
  -9.750  -0.3376   0.09857   0.09500  -0.0534   0.9951   0.0194
  -9.500  -0.3321   0.09208   0.08852  -0.0592   0.9909   0.0199
  -9.250  -0.3272   0.08509   0.08154  -0.0659   0.9858   0.0201
  -9.000  -0.3200   0.08025   0.07672  -0.0701   0.9790   0.0200
  -8.750  -0.3137   0.07503   0.07152  -0.0750   0.9706   0.0197
  -8.500  -0.3139   0.06865   0.06516  -0.0810   0.9575   0.0195
  -8.250  -0.3200   0.05937   0.05587  -0.0920   0.9401   0.0192
  -8.000  -0.3224   0.04764   0.04378  -0.1053   0.9254   0.0188
  -7.750  -0.3147   0.03890   0.03447  -0.1127   0.9151   0.0187
  -7.500  -0.2959   0.03245   0.02730  -0.1174   0.9071   0.0190
  -7.250  -0.2720   0.02823   0.02238  -0.1200   0.8993   0.0197
  -7.000  -0.2425   0.02534   0.01892  -0.1224   0.8930   0.0207
  -6.750  -0.2119   0.02344   0.01676  -0.1243   0.8869   0.0213
  -6.500  -0.1815   0.02181   0.01485  -0.1256   0.8798   0.0218
  -6.250  -0.1483   0.02035   0.01311  -0.1273   0.8742   0.0224
  -6.000  -0.1197   0.01919   0.01174  -0.1279   0.8662   0.0231
  -5.750  -0.0876   0.01811   0.01046  -0.1291   0.8602   0.0239
  -5.500  -0.0599   0.01739   0.00956  -0.1293   0.8526   0.0253
  -5.250  -0.0302   0.01653   0.00857  -0.1299   0.8465   0.0264
  -5.000  -0.0029   0.01577   0.00777  -0.1302   0.8401   0.0273
  -4.750   0.0252   0.01518   0.00712  -0.1305   0.8338   0.0283
  -4.500   0.0545   0.01466   0.00650  -0.1311   0.8286   0.0297
  -4.250   0.0812   0.01423   0.00599  -0.1311   0.8220   0.0313
  -4.000   0.1100   0.01381   0.00550  -0.1315   0.8166   0.0341
  -3.750   0.1383   0.01349   0.00512  -0.1318   0.8115   0.0385
  -3.500   0.1658   0.01313   0.00474  -0.1319   0.8062   0.0450
  -3.250   0.1946   0.01275   0.00440  -0.1323   0.8017   0.0651
  -3.000   0.2234   0.01236   0.00415  -0.1329   0.7977   0.1115
  -2.750   0.2505   0.01196   0.00400  -0.1333   0.7926   0.1816
  -2.500   0.2787   0.01141   0.00388  -0.1340   0.7881   0.2979
  -2.250   0.3074   0.01077   0.00381  -0.1348   0.7844   0.4632
  -2.000   0.3314   0.01048   0.00406  -0.1339   0.7803   0.6118
  -1.750   0.3564   0.01058   0.00427  -0.1330   0.7762   0.6810
  -1.500   0.3833   0.01071   0.00437  -0.1325   0.7724   0.7151
  -1.250   0.4114   0.01084   0.00440  -0.1324   0.7692   0.7362
  -1.000   0.4377   0.01096   0.00449  -0.1319   0.7652   0.7525
  -0.750   0.4636   0.01107   0.00458  -0.1314   0.7614   0.7658
  -0.500   0.4899   0.01118   0.00466  -0.1309   0.7579   0.7775
  -0.250   0.5173   0.01128   0.00471  -0.1307   0.7548   0.7885
   0.000   0.5441   0.01139   0.00478  -0.1304   0.7515   0.7992
   0.250   0.5686   0.01149   0.00490  -0.1295   0.7476   0.8077
   0.500   0.5954   0.01158   0.00497  -0.1293   0.7440   0.8167
   0.750   0.6213   0.01165   0.00504  -0.1287   0.7406   0.8241
   1.000   0.6496   0.01174   0.00509  -0.1288   0.7376   0.8315
   1.250   0.6736   0.01181   0.00521  -0.1280   0.7330   0.8371
   1.500   0.7007   0.01188   0.00528  -0.1279   0.7285   0.8426
   1.750   0.7289   0.01194   0.00531  -0.1280   0.7244   0.8469
   2.000   0.7546   0.01200   0.00541  -0.1276   0.7194   0.8507
   2.250   0.7807   0.01205   0.00549  -0.1272   0.7135   0.8548
   2.500   0.8098   0.01209   0.00549  -0.1275   0.7078   0.8587
   2.750   0.8337   0.01213   0.00560  -0.1267   0.6996   0.8623
   3.000   0.8609   0.01213   0.00557  -0.1264   0.6922   0.8658
   3.250   0.8847   0.01216   0.00567  -0.1256   0.6825   0.8700
   3.500   0.9113   0.01220   0.00572  -0.1253   0.6734   0.8741
   3.750   0.9361   0.01220   0.00575  -0.1246   0.6631   0.8775
   4.000   0.9594   0.01223   0.00584  -0.1237   0.6513   0.8819
   4.250   0.9839   0.01227   0.00592  -0.1230   0.6391   0.8866
   4.500   1.0077   0.01232   0.00602  -0.1221   0.6256   0.8910
   4.750   1.0302   0.01236   0.00611  -0.1210   0.6096   0.8957
   5.000   1.0525   0.01243   0.00619  -0.1198   0.5887   0.9017
   5.250   1.0724   0.01252   0.00627  -0.1182   0.5591   0.9082
   5.500   1.0892   0.01274   0.00634  -0.1159   0.5116   0.9161
   5.750   1.0993   0.01326   0.00655  -0.1124   0.4533   0.9272
   6.000   1.1072   0.01399   0.00698  -0.1088   0.3947   0.9487
   6.250   1.1179   0.01485   0.00756  -0.1061   0.3389   1.0000
   6.500   1.1286   0.01576   0.00822  -0.1036   0.2926   1.0000
   6.750   1.1394   0.01665   0.00891  -0.1010   0.2528   1.0000
   7.000   1.1511   0.01753   0.00962  -0.0987   0.2185   1.0000
   7.250   1.1634   0.01840   0.01034  -0.0966   0.1893   1.0000
   7.500   1.1763   0.01926   0.01109  -0.0946   0.1650   1.0000
   7.750   1.1894   0.02013   0.01186  -0.0926   0.1446   1.0000
   8.000   1.2023   0.02101   0.01269  -0.0907   0.1281   1.0000
   8.250   1.2155   0.02190   0.01353  -0.0889   0.1140   1.0000
   8.500   1.2289   0.02279   0.01440  -0.0872   0.1022   1.0000
   8.750   1.2426   0.02368   0.01530  -0.0856   0.0927   1.0000
   9.000   1.2552   0.02465   0.01628  -0.0839   0.0846   1.0000
   9.250   1.2677   0.02567   0.01731  -0.0823   0.0774   1.0000
   9.500   1.2803   0.02670   0.01840  -0.0807   0.0722   1.0000
   9.750   1.2926   0.02777   0.01952  -0.0792   0.0670   1.0000
  10.000   1.3028   0.02904   0.02079  -0.0775   0.0627   1.0000
  10.250   1.3158   0.03012   0.02197  -0.0762   0.0588   1.0000
  10.500   1.3268   0.03138   0.02330  -0.0748   0.0554   1.0000
  10.750   1.3347   0.03292   0.02486  -0.0732   0.0524   1.0000
  11.000   1.3466   0.03418   0.02624  -0.0719   0.0500   1.0000
  11.250   1.3578   0.03552   0.02768  -0.0707   0.0473   1.0000
  11.500   1.3673   0.03701   0.02924  -0.0695   0.0450   1.0000
  11.750   1.3738   0.03883   0.03109  -0.0681   0.0430   1.0000
  12.000   1.3834   0.04042   0.03280  -0.0670   0.0413   1.0000
  12.250   1.3933   0.04200   0.03453  -0.0659   0.0394   1.0000
  12.500   1.4022   0.04368   0.03632  -0.0650   0.0375   1.0000
  12.750   1.4096   0.04553   0.03825  -0.0640   0.0360   1.0000
  13.000   1.4140   0.04776   0.04052  -0.0630   0.0345   1.0000
  13.250   1.4213   0.04973   0.04264  -0.0622   0.0332   1.0000
  13.500   1.4289   0.05170   0.04477  -0.0614   0.0317   1.0000
  13.750   1.4354   0.05381   0.04701  -0.0608   0.0302   1.0000
  14.000   1.4405   0.05608   0.04941  -0.0603   0.0290   1.0000
  14.250   1.4432   0.05868   0.05209  -0.0599   0.0278   1.0000
  14.500   1.4454   0.06143   0.05496  -0.0595   0.0266   1.0000
  14.750   1.4498   0.06401   0.05774  -0.0592   0.0254   1.0000
  15.000   1.4525   0.06683   0.06072  -0.0591   0.0241   1.0000
  15.250   1.4540   0.06986   0.06389  -0.0592   0.0231   1.0000
  15.500   1.4538   0.07316   0.06730  -0.0596   0.0222   1.0000
  15.750   1.4504   0.07701   0.07124  -0.0601   0.0214   1.0000
  16.000   1.4488   0.08080   0.07522  -0.0607   0.0206   1.0000
  16.250   1.4466   0.08479   0.07943  -0.0615   0.0197   1.0000
  16.500   1.4431   0.08906   0.08389  -0.0626   0.0189   1.0000
  16.750   1.4385   0.09362   0.08863  -0.0641   0.0182   1.0000
  17.000   1.4330   0.09849   0.09364  -0.0660   0.0176   1.0000
  17.250   1.4259   0.10377   0.09906  -0.0682   0.0171   1.0000
  17.500   1.4172   0.10951   0.10492  -0.0708   0.0167   1.0000
  17.750   1.4074   0.11561   0.11119  -0.0738   0.0163   1.0000
  18.000   1.3970   0.12204   0.11785  -0.0771   0.0159   1.0000
  18.250   1.3853   0.12893   0.12495  -0.0809   0.0156   1.0000
  18.500   1.3727   0.13621   0.13244  -0.0852   0.0153   1.0000
  18.750   1.3591   0.14396   0.14038  -0.0901   0.0150   1.0000
  19.000   1.3440   0.15228   0.14888  -0.0955   0.0148   1.0000
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