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NREL's S807 Airfoil (s807-nr) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NREL's S807 Airfoil (s807-nr)
Reynolds number: 100,000
Max Cl/Cd: 40.34 at α=10.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s807-nr-100000-n5.txt
Download as CSV file: xf-s807-nr-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NREL's S807 Airfoil                             
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.7169   0.13211   0.12602  -0.0327   1.0000   0.0313
 -17.250  -0.7597   0.11919   0.11283  -0.0397   1.0000   0.0310
 -17.000  -0.7860   0.11061   0.10402  -0.0439   1.0000   0.0310
 -16.750  -0.8052   0.10381   0.09700  -0.0470   1.0000   0.0311
 -16.500  -0.8196   0.09809   0.09107  -0.0492   1.0000   0.0312
 -16.250  -0.8301   0.09320   0.08598  -0.0509   1.0000   0.0314
 -16.000  -0.8376   0.08889   0.08147  -0.0521   1.0000   0.0317
 -15.750  -0.8422   0.08510   0.07749  -0.0528   1.0000   0.0321
 -15.500  -0.8441   0.08177   0.07396  -0.0533   1.0000   0.0325
 -15.250  -0.8425   0.07899   0.07103  -0.0533   1.0000   0.0330
 -15.000  -0.8355   0.07714   0.06920  -0.0530   1.0000   0.0338
 -14.750  -0.8296   0.07513   0.06717  -0.0528   1.0000   0.0345
 -14.500  -0.8250   0.07299   0.06496  -0.0526   1.0000   0.0354
 -14.250  -0.8193   0.07097   0.06284  -0.0523   1.0000   0.0365
 -14.000  -0.8109   0.06930   0.06107  -0.0516   1.0000   0.0375
 -13.750  -0.8011   0.06784   0.05948  -0.0507   1.0000   0.0385
 -13.500  -0.7895   0.06675   0.05841  -0.0496   1.0000   0.0394
 -13.250  -0.7800   0.06546   0.05715  -0.0487   1.0000   0.0406
 -13.000  -0.7706   0.06417   0.05585  -0.0478   1.0000   0.0419
 -12.750  -0.7617   0.06284   0.05448  -0.0468   1.0000   0.0437
 -12.500  -0.7517   0.06166   0.05320  -0.0458   1.0000   0.0456
 -12.250  -0.7450   0.06024   0.05186  -0.0449   1.0000   0.0475
 -12.000  -0.7379   0.05883   0.05047  -0.0439   1.0000   0.0497
 -11.750  -0.7302   0.05754   0.04914  -0.0428   1.0000   0.0527
 -11.500  -0.7250   0.05606   0.04770  -0.0417   1.0000   0.0555
 -11.250  -0.7207   0.05450   0.04616  -0.0406   1.0000   0.0588
 -11.000  -0.7168   0.05293   0.04458  -0.0394   1.0000   0.0635
 -10.750  -0.7164   0.05110   0.04282  -0.0383   1.0000   0.0687
 -10.500  -0.7163   0.04935   0.04112  -0.0370   1.0000   0.0755
 -10.250  -0.7178   0.04754   0.03936  -0.0355   1.0000   0.0841
 -10.000  -0.7224   0.04557   0.03750  -0.0340   1.0000   0.0938
  -9.750  -0.7282   0.04359   0.03561  -0.0322   1.0000   0.1049
  -9.500  -0.7365   0.04154   0.03368  -0.0302   1.0000   0.1180
  -9.250  -0.7479   0.03942   0.03168  -0.0278   1.0000   0.1324
  -9.000  -0.7633   0.03723   0.02962  -0.0250   1.0000   0.1476
  -8.750  -0.7836   0.03506   0.02756  -0.0214   1.0000   0.1612
  -8.500  -0.8072   0.03287   0.02546  -0.0173   1.0000   0.1727
  -8.250  -0.8245   0.02986   0.02258  -0.0158   1.0000   0.1939
  -8.000  -0.8329   0.02619   0.01918  -0.0170   1.0000   0.2375
  -7.750  -0.8224   0.02536   0.01911  -0.0160   1.0000   0.3190
  -7.500  -0.8005   0.02584   0.01977  -0.0148   1.0000   0.3731
  -7.250  -0.7794   0.02525   0.01905  -0.0156   1.0000   0.4034
  -7.000  -0.7560   0.02580   0.01951  -0.0148   1.0000   0.4225
  -6.750  -0.7334   0.02595   0.01953  -0.0143   1.0000   0.4355
  -6.500  -0.7106   0.02567   0.01907  -0.0147   1.0000   0.4482
  -6.250  -0.6884   0.02761   0.02111  -0.0108   1.0000   0.4538
  -6.000  -0.6470   0.02871   0.02208  -0.0127   0.9942   0.4663
  -5.750  -0.6029   0.03045   0.02381  -0.0132   0.9868   0.4710
  -5.500  -0.5609   0.02921   0.02231  -0.0186   0.9792   0.4811
  -5.250  -0.5199   0.02963   0.02267  -0.0201   0.9711   0.4832
  -5.000  -0.4827   0.02964   0.02261  -0.0216   0.9623   0.4858
  -4.750  -0.4425   0.02928   0.02214  -0.0242   0.9536   0.4894
  -4.500  -0.4067   0.02736   0.01997  -0.0290   0.9417   0.4974
  -3.750  -0.3154   0.02630   0.01879  -0.0299   0.8940   0.5033
  -3.500  -0.2865   0.02562   0.01804  -0.0305   0.8718   0.5064
  -3.250  -0.2484   0.02443   0.01667  -0.0337   0.8495   0.5111
  -3.000  -0.2056   0.02351   0.01558  -0.0371   0.8212   0.5147
  -2.750  -0.1473   0.02309   0.01499  -0.0422   0.7833   0.5162
  -2.500  -0.0809   0.02279   0.01435  -0.0491   0.7253   0.5180
  -2.250  -0.0376   0.02272   0.01392  -0.0519   0.6663   0.5202
  -2.000  -0.0052   0.02265   0.01352  -0.0530   0.6199   0.5229
  -1.750   0.0247   0.02240   0.01298  -0.0541   0.5834   0.5262
  -1.500   0.0556   0.02193   0.01218  -0.0559   0.5533   0.5300
  -1.250   0.0841   0.02184   0.01191  -0.0563   0.5287   0.5318
  -1.000   0.1115   0.02188   0.01183  -0.0562   0.5083   0.5334
  -0.750   0.1389   0.02192   0.01175  -0.0562   0.4912   0.5353
  -0.500   0.1666   0.02193   0.01164  -0.0564   0.4769   0.5375
  -0.250   0.1949   0.02189   0.01147  -0.0567   0.4647   0.5401
   0.000   0.2238   0.02177   0.01125  -0.0574   0.4533   0.5428
   0.250   0.2534   0.02164   0.01096  -0.0583   0.4434   0.5458
   0.500   0.2828   0.02153   0.01074  -0.0592   0.4337   0.5485
   0.750   0.3099   0.02162   0.01078  -0.0590   0.4256   0.5501
   1.000   0.3372   0.02170   0.01086  -0.0590   0.4178   0.5521
   1.250   0.3650   0.02183   0.01090  -0.0591   0.4117   0.5544
   1.500   0.3934   0.02188   0.01096  -0.0594   0.4051   0.5570
   1.750   0.4223   0.02192   0.01095  -0.0599   0.3990   0.5598
   2.000   0.4520   0.02199   0.01089  -0.0606   0.3938   0.5628
   2.250   0.4817   0.02201   0.01090  -0.0614   0.3877   0.5657
   2.500   0.5089   0.02215   0.01108  -0.0613   0.3824   0.5674
   2.750   0.5364   0.02234   0.01125  -0.0613   0.3780   0.5696
   3.000   0.5643   0.02252   0.01147  -0.0614   0.3738   0.5722
   3.250   0.5925   0.02269   0.01170  -0.0616   0.3693   0.5752
   3.500   0.6214   0.02287   0.01187  -0.0621   0.3652   0.5785
   3.750   0.6513   0.02305   0.01197  -0.0628   0.3614   0.5819
   4.000   0.6790   0.02327   0.01225  -0.0629   0.3576   0.5842
   4.250   0.7057   0.02350   0.01260  -0.0628   0.3534   0.5864
   4.500   0.7329   0.02375   0.01293  -0.0628   0.3497   0.5890
   4.750   0.7608   0.02403   0.01325  -0.0630   0.3465   0.5922
   5.000   0.7897   0.02433   0.01354  -0.0634   0.3436   0.5959
   5.250   0.8185   0.02466   0.01391  -0.0639   0.3404   0.6000
   5.500   0.8437   0.02497   0.01441  -0.0635   0.3365   0.6024
   5.750   0.8695   0.02530   0.01486  -0.0633   0.3330   0.6053
   6.000   0.8963   0.02564   0.01529  -0.0632   0.3300   0.6084
   6.250   0.9243   0.02600   0.01567  -0.0634   0.3273   0.6120
   6.500   0.9520   0.02641   0.01612  -0.0637   0.3243   0.6162
   6.750   0.9757   0.02684   0.01679  -0.0632   0.3205   0.6194
   7.000   0.9998   0.02726   0.01739  -0.0627   0.3169   0.6228
   7.250   1.0254   0.02765   0.01789  -0.0625   0.3135   0.6269
   7.500   1.0528   0.02801   0.01827  -0.0626   0.3103   0.6315
   7.750   1.0778   0.02847   0.01885  -0.0624   0.3068   0.6355
   8.000   1.0985   0.02895   0.01960  -0.0614   0.3022   0.6389
   8.250   1.1217   0.02932   0.02012  -0.0608   0.2978   0.6431
   8.500   1.1480   0.02960   0.02043  -0.0607   0.2939   0.6482
   8.750   1.1706   0.03006   0.02104  -0.0601   0.2898   0.6530
   9.000   1.1890   0.03057   0.02183  -0.0588   0.2846   0.6574
   9.250   1.2116   0.03085   0.02223  -0.0581   0.2798   0.6628
   9.500   1.2379   0.03102   0.02237  -0.0580   0.2755   0.6687
   9.750   1.2511   0.03163   0.02335  -0.0560   0.2694   0.6731
  10.000   1.2707   0.03187   0.02372  -0.0548   0.2638   0.6788
  10.250   1.2928   0.03205   0.02394  -0.0541   0.2587   0.6856
  10.500   1.3040   0.03265   0.02487  -0.0518   0.2520   0.6911
  10.750   1.3221   0.03280   0.02511  -0.0505   0.2461   0.6983
  11.000   1.3340   0.03333   0.02586  -0.0484   0.2396   0.7052
  11.250   1.3449   0.03374   0.02646  -0.0462   0.2327   0.7125
  11.500   1.3542   0.03413   0.02699  -0.0437   0.2263   0.7206
  11.750   1.3585   0.03486   0.02797  -0.0408   0.2185   0.7286
  12.000   1.3650   0.03549   0.02873  -0.0383   0.2114   0.7382
  12.250   1.3673   0.03647   0.02993  -0.0357   0.2028   0.7486
  12.500   1.3685   0.03760   0.03124  -0.0332   0.1946   0.7598
  12.750   1.3676   0.03889   0.03265  -0.0308   0.1862   0.7728
  13.000   1.3620   0.04078   0.03476  -0.0287   0.1774   0.7877
  13.250   1.3535   0.04292   0.03701  -0.0268   0.1698   0.8058
  13.500   1.3389   0.04589   0.04020  -0.0254   0.1624   0.8301
  13.750   1.3180   0.04926   0.04373  -0.0240   0.1571   0.8787
  14.000   1.2916   0.05449   0.04916  -0.0250   0.1518   1.0000
  14.250   1.2673   0.06096   0.05569  -0.0278   0.1462   1.0000
  14.500   1.2415   0.06812   0.06294  -0.0312   0.1410   1.0000
  14.750   1.2160   0.07548   0.07039  -0.0347   0.1352   1.0000
  15.000   1.2015   0.08115   0.07601  -0.0373   0.1295   1.0000
  15.250   1.1808   0.08810   0.08308  -0.0406   0.1237   1.0000
  15.500   1.1743   0.09262   0.08752  -0.0427   0.1180   1.0000
  15.750   1.1603   0.09880   0.09379  -0.0457   0.1126   1.0000
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