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NREL's S807 Airfoil (s807-nr) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NREL's S807 Airfoil (s807-nr)
Reynolds number: 500,000
Max Cl/Cd: 83.85 at α=9.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s807-nr-500000-n5.txt
Download as CSV file: xf-s807-nr-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.9582   0.11799   0.11361  -0.0348   1.0000   0.0119
 -19.500  -0.9612   0.11421   0.10975  -0.0362   1.0000   0.0120
 -19.250  -0.9644   0.11045   0.10591  -0.0375   1.0000   0.0121
 -19.000  -0.9664   0.10692   0.10230  -0.0386   1.0000   0.0123
 -18.750  -0.9683   0.10347   0.09878  -0.0396   1.0000   0.0124
 -18.500  -0.9693   0.10020   0.09542  -0.0405   1.0000   0.0125
 -18.250  -0.9701   0.09699   0.09213  -0.0413   1.0000   0.0127
 -18.000  -0.9704   0.09395   0.08902  -0.0420   1.0000   0.0128
 -17.750  -0.9701   0.09097   0.08595  -0.0426   1.0000   0.0129
 -17.500  -0.9692   0.08816   0.08308  -0.0431   1.0000   0.0130
 -17.250  -0.9706   0.08516   0.08004  -0.0436   1.0000   0.0132
 -17.000  -0.9702   0.08241   0.07725  -0.0440   1.0000   0.0134
 -16.750  -0.9697   0.07966   0.07446  -0.0443   1.0000   0.0136
 -16.500  -0.9684   0.07709   0.07184  -0.0445   1.0000   0.0136
 -16.250  -0.9659   0.07464   0.06936  -0.0448   1.0000   0.0140
 -16.000  -0.9638   0.07222   0.06690  -0.0449   1.0000   0.0142
 -15.750  -0.9608   0.06996   0.06459  -0.0449   1.0000   0.0144
 -15.500  -0.9579   0.06769   0.06227  -0.0448   1.0000   0.0146
 -15.250  -0.9549   0.06550   0.06003  -0.0447   1.0000   0.0148
 -15.000  -0.9512   0.06343   0.05791  -0.0445   1.0000   0.0150
 -14.750  -0.9481   0.06131   0.05574  -0.0443   1.0000   0.0152
 -14.500  -0.9444   0.05932   0.05370  -0.0439   1.0000   0.0154
 -14.250  -0.9402   0.05740   0.05173  -0.0435   1.0000   0.0156
 -14.000  -0.9363   0.05548   0.04977  -0.0431   1.0000   0.0158
 -13.750  -0.9311   0.05375   0.04798  -0.0425   1.0000   0.0160
 -13.500  -0.9297   0.05168   0.04589  -0.0420   1.0000   0.0162
 -13.250  -0.9289   0.04961   0.04380  -0.0413   1.0000   0.0165
 -13.000  -0.9263   0.04777   0.04193  -0.0406   1.0000   0.0168
 -12.750  -0.9230   0.04603   0.04016  -0.0398   1.0000   0.0172
 -12.500  -0.9199   0.04434   0.03844  -0.0389   1.0000   0.0174
 -12.250  -0.9171   0.04268   0.03675  -0.0379   1.0000   0.0177
 -12.000  -0.9140   0.04113   0.03517  -0.0368   1.0000   0.0181
 -11.750  -0.9122   0.03959   0.03360  -0.0355   1.0000   0.0185
 -11.500  -0.9111   0.03804   0.03201  -0.0341   1.0000   0.0188
 -11.250  -0.9098   0.03659   0.03052  -0.0325   1.0000   0.0191
 -11.000  -0.9095   0.03510   0.02899  -0.0309   1.0000   0.0193
 -10.750  -0.9114   0.03357   0.02744  -0.0289   1.0000   0.0196
 -10.500  -0.9159   0.03197   0.02581  -0.0267   1.0000   0.0200
 -10.250  -0.9208   0.03045   0.02426  -0.0242   1.0000   0.0202
 -10.000  -0.9141   0.02886   0.02265  -0.0241   0.9987   0.0209
  -9.750  -0.8998   0.02738   0.02114  -0.0251   0.9961   0.0215
  -9.500  -0.8838   0.02594   0.01966  -0.0266   0.9934   0.0224
  -9.250  -0.8660   0.02440   0.01808  -0.0283   0.9889   0.0236
  -9.000  -0.8289   0.02269   0.01636  -0.0337   0.9841   0.0259
  -8.750  -0.7886   0.02102   0.01467  -0.0394   0.9786   0.0294
  -8.500  -0.7497   0.01925   0.01291  -0.0450   0.9724   0.0361
  -8.250  -0.7052   0.01772   0.01140  -0.0513   0.9692   0.0482
  -8.000  -0.6835   0.01659   0.01031  -0.0520   0.9616   0.0602
  -7.750  -0.6517   0.01552   0.00932  -0.0546   0.9580   0.0786
  -7.250  -0.5986   0.01342   0.00751  -0.0574   0.9492   0.1403
  -7.000  -0.5694   0.01220   0.00652  -0.0594   0.9443   0.1914
  -6.500  -0.5147   0.00970   0.00472  -0.0625   0.9310   0.3475
  -6.250  -0.4871   0.00939   0.00452  -0.0626   0.9223   0.3811
  -6.000  -0.4595   0.00920   0.00433  -0.0625   0.9106   0.3962
  -5.750  -0.4260   0.00899   0.00409  -0.0635   0.8925   0.4069
  -5.500  -0.3281   0.00878   0.00371  -0.0774   0.8432   0.4339
  -5.250  -0.2914   0.00916   0.00367  -0.0789   0.7487   0.4420
  -5.000  -0.2687   0.00945   0.00360  -0.0778   0.6798   0.4452
  -4.750  -0.2449   0.00967   0.00351  -0.0769   0.6236   0.4473
  -4.500  -0.2199   0.00981   0.00343  -0.0763   0.5765   0.4488
  -4.250  -0.1938   0.00993   0.00337  -0.0759   0.5382   0.4505
  -4.000  -0.1668   0.01002   0.00332  -0.0758   0.5083   0.4522
  -3.750  -0.1393   0.01010   0.00327  -0.0757   0.4842   0.4537
  -3.500  -0.1115   0.01016   0.00321  -0.0757   0.4640   0.4552
  -3.000  -0.0550   0.01028   0.00311  -0.0758   0.4313   0.4587
  -2.750  -0.0265   0.01033   0.00306  -0.0759   0.4177   0.4605
  -2.500   0.0020   0.01038   0.00301  -0.0760   0.4054   0.4620
  -2.250   0.0304   0.01044   0.00297  -0.0761   0.3940   0.4634
  -2.000   0.0592   0.01046   0.00294  -0.0762   0.3849   0.4648
  -1.750   0.0875   0.01050   0.00293  -0.0763   0.3766   0.4662
  -1.500   0.1163   0.01052   0.00293  -0.0764   0.3695   0.4677
  -1.250   0.1449   0.01057   0.00293  -0.0765   0.3624   0.4692
  -1.000   0.1736   0.01062   0.00295  -0.0766   0.3566   0.4710
  -0.750   0.2024   0.01067   0.00296  -0.0767   0.3507   0.4729
  -0.500   0.2309   0.01074   0.00298  -0.0768   0.3446   0.4747
  -0.250   0.2596   0.01080   0.00299  -0.0769   0.3394   0.4763
   0.000   0.2884   0.01085   0.00301  -0.0771   0.3343   0.4779
   0.250   0.3170   0.01092   0.00303  -0.0772   0.3295   0.4794
   0.500   0.3453   0.01100   0.00307  -0.0772   0.3253   0.4809
   0.750   0.3741   0.01103   0.00312  -0.0774   0.3219   0.4825
   1.000   0.4028   0.01108   0.00318  -0.0774   0.3181   0.4841
   1.250   0.4312   0.01115   0.00325  -0.0775   0.3144   0.4858
   1.500   0.4595   0.01125   0.00333  -0.0775   0.3109   0.4878
   1.750   0.4878   0.01134   0.00341  -0.0776   0.3076   0.4898
   2.000   0.5165   0.01141   0.00348  -0.0777   0.3046   0.4919
   2.250   0.5450   0.01149   0.00356  -0.0777   0.3012   0.4937
   2.500   0.5733   0.01159   0.00364  -0.0778   0.2981   0.4955
   2.750   0.6013   0.01170   0.00373  -0.0778   0.2952   0.4971
   3.000   0.6292   0.01181   0.00385  -0.0777   0.2925   0.4988
   3.250   0.6575   0.01189   0.00397  -0.0778   0.2904   0.5007
   3.500   0.6858   0.01198   0.00410  -0.0778   0.2882   0.5025
   3.750   0.7140   0.01208   0.00423  -0.0778   0.2858   0.5045
   4.000   0.7419   0.01219   0.00436  -0.0778   0.2832   0.5067
   4.250   0.7697   0.01232   0.00450  -0.0778   0.2806   0.5090
   4.500   0.7972   0.01247   0.00464  -0.0777   0.2780   0.5113
   4.750   0.8245   0.01265   0.00480  -0.0775   0.2757   0.5133
   5.000   0.8525   0.01274   0.00496  -0.0775   0.2741   0.5153
   5.250   0.8804   0.01285   0.00513  -0.0775   0.2721   0.5173
   5.500   0.9080   0.01297   0.00531  -0.0774   0.2697   0.5195
   5.750   0.9355   0.01310   0.00549  -0.0773   0.2672   0.5217
   6.000   0.9626   0.01326   0.00567  -0.0772   0.2647   0.5240
   6.250   0.9892   0.01344   0.00585  -0.0769   0.2614   0.5264
   6.500   1.0163   0.01359   0.00604  -0.0768   0.2581   0.5287
   6.750   1.0436   0.01371   0.00622  -0.0766   0.2549   0.5311
   7.000   1.0705   0.01385   0.00641  -0.0765   0.2516   0.5337
   7.250   1.0969   0.01401   0.00662  -0.0762   0.2480   0.5364
   7.500   1.1226   0.01423   0.00684  -0.0758   0.2440   0.5390
   7.750   1.1496   0.01435   0.00705  -0.0757   0.2404   0.5417
   8.000   1.1760   0.01451   0.00726  -0.0754   0.2362   0.5445
   8.250   1.2014   0.01471   0.00748  -0.0750   0.2315   0.5470
   8.500   1.2269   0.01491   0.00772  -0.0746   0.2269   0.5495
   8.750   1.2528   0.01507   0.00795  -0.0743   0.2206   0.5524
   9.000   1.2770   0.01533   0.00822  -0.0737   0.2136   0.5556
   9.250   1.3022   0.01553   0.00849  -0.0733   0.2064   0.5591
   9.500   1.3257   0.01583   0.00879  -0.0726   0.1979   0.5626
  10.000   1.3708   0.01654   0.00951  -0.0710   0.1744   0.5689
  10.250   1.3901   0.01710   0.01001  -0.0698   0.1580   0.5722
  10.500   1.4076   0.01775   0.01061  -0.0683   0.1421   0.5758
  10.750   1.4229   0.01842   0.01124  -0.0664   0.1283   0.5794
  11.250   1.4501   0.01987   0.01266  -0.0623   0.1055   0.5868
  11.500   1.4637   0.02058   0.01340  -0.0602   0.0963   0.5913
  11.750   1.4761   0.02135   0.01418  -0.0581   0.0884   0.5960
  12.250   1.4972   0.02307   0.01595  -0.0536   0.0737   0.6046
  12.500   1.5058   0.02404   0.01695  -0.0513   0.0674   0.6095
  12.750   1.5122   0.02515   0.01808  -0.0488   0.0616   0.6144
  13.000   1.5192   0.02624   0.01923  -0.0466   0.0566   0.6193
  13.250   1.5224   0.02760   0.02064  -0.0442   0.0521   0.6249
  13.500   1.5274   0.02891   0.02203  -0.0422   0.0486   0.6312
  13.750   1.5281   0.03060   0.02378  -0.0401   0.0453   0.6373
  14.000   1.5296   0.03235   0.02563  -0.0385   0.0430   0.6443
  14.250   1.5293   0.03441   0.02780  -0.0371   0.0410   0.6513
  14.500   1.5254   0.03700   0.03050  -0.0362   0.0392   0.6584
  14.750   1.5190   0.04014   0.03377  -0.0359   0.0377   0.6658
  15.000   1.5134   0.04359   0.03736  -0.0363   0.0365   0.6732
  15.250   1.5045   0.04779   0.04172  -0.0373   0.0353   0.6813
  15.500   1.4917   0.05286   0.04695  -0.0391   0.0343   0.6888
  15.750   1.4757   0.05863   0.05288  -0.0413   0.0336   0.6967
  16.000   1.4567   0.06498   0.05939  -0.0438   0.0329   0.7041
  16.250   1.4366   0.07157   0.06614  -0.0465   0.0324   0.7120
  16.500   1.4167   0.07816   0.07288  -0.0493   0.0319   0.7202
  16.750   1.4002   0.08439   0.07926  -0.0520   0.0313   0.7299
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