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NREL's S807 Airfoil (s807-nr) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: NREL's S807 Airfoil (s807-nr)
Reynolds number: 1,000,000
Max Cl/Cd: 101.66 at α=8.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s807-nr-1000000-n5.txt
Download as CSV file: xf-s807-nr-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0601   0.10385   0.09991  -0.0386   1.0000   0.0095
 -19.500  -1.0636   0.10028   0.09628  -0.0396   1.0000   0.0096
 -19.250  -1.0683   0.09665   0.09258  -0.0406   1.0000   0.0096
 -19.000  -1.0702   0.09340   0.08927  -0.0414   1.0000   0.0097
 -18.750  -1.0704   0.09045   0.08626  -0.0420   1.0000   0.0098
 -18.500  -1.0705   0.08756   0.08331  -0.0426   1.0000   0.0099
 -18.250  -1.0705   0.08472   0.08042  -0.0431   1.0000   0.0100
 -18.000  -1.0708   0.08188   0.07751  -0.0435   1.0000   0.0101
 -17.750  -1.0694   0.07929   0.07487  -0.0438   1.0000   0.0102
 -17.500  -1.0693   0.07656   0.07208  -0.0441   1.0000   0.0102
 -17.250  -1.0692   0.07390   0.06937  -0.0444   1.0000   0.0104
 -17.000  -1.0699   0.07115   0.06657  -0.0446   1.0000   0.0105
 -16.750  -1.0701   0.06856   0.06393  -0.0447   1.0000   0.0106
 -16.500  -1.0696   0.06604   0.06136  -0.0447   1.0000   0.0107
 -16.250  -1.0673   0.06381   0.05910  -0.0446   1.0000   0.0109
 -16.000  -1.0647   0.06165   0.05691  -0.0445   1.0000   0.0111
 -15.750  -1.0622   0.05948   0.05469  -0.0443   1.0000   0.0112
 -15.500  -1.0577   0.05760   0.05279  -0.0440   1.0000   0.0113
 -15.250  -1.0551   0.05553   0.05067  -0.0436   1.0000   0.0115
 -15.000  -1.0506   0.05369   0.04880  -0.0432   1.0000   0.0116
 -14.750  -1.0467   0.05184   0.04691  -0.0427   1.0000   0.0117
 -14.500  -1.0425   0.05002   0.04506  -0.0422   1.0000   0.0120
 -14.250  -1.0357   0.04835   0.04336  -0.0419   0.9999   0.0122
 -14.000  -1.0268   0.04654   0.04150  -0.0423   0.9996   0.0123
 -13.750  -1.0171   0.04478   0.03970  -0.0427   0.9993   0.0125
 -13.500  -1.0063   0.04320   0.03809  -0.0429   0.9989   0.0127
 -13.250  -0.9964   0.04154   0.03639  -0.0432   0.9985   0.0129
 -13.000  -0.9862   0.03991   0.03473  -0.0435   0.9980   0.0130
 -12.750  -0.9787   0.03809   0.03287  -0.0437   0.9973   0.0133
 -12.500  -0.9691   0.03632   0.03107  -0.0444   0.9965   0.0135
 -12.250  -0.9595   0.03473   0.02945  -0.0446   0.9957   0.0137
 -12.000  -0.9491   0.03318   0.02788  -0.0450   0.9949   0.0140
 -11.750  -0.9374   0.03172   0.02639  -0.0454   0.9942   0.0143
 -11.500  -0.9249   0.03023   0.02488  -0.0461   0.9935   0.0146
 -11.250  -0.9135   0.02890   0.02352  -0.0462   0.9926   0.0149
 -11.000  -0.9060   0.02754   0.02213  -0.0455   0.9910   0.0152
 -10.750  -0.8961   0.02622   0.02077  -0.0452   0.9892   0.0155
 -10.500  -0.8794   0.02491   0.01944  -0.0462   0.9871   0.0158
 -10.250  -0.8556   0.02357   0.01807  -0.0485   0.9849   0.0161
 -10.000  -0.8175   0.02200   0.01648  -0.0538   0.9825   0.0171
  -9.750  -0.8080   0.02067   0.01512  -0.0534   0.9782   0.0174
  -9.500  -0.7849   0.01927   0.01370  -0.0554   0.9736   0.0181
  -9.250  -0.7489   0.01798   0.01239  -0.0595   0.9712   0.0191
  -9.000  -0.7105   0.01670   0.01109  -0.0643   0.9697   0.0206
  -8.750  -0.6938   0.01552   0.00988  -0.0649   0.9648   0.0220
  -8.500  -0.6672   0.01467   0.00902  -0.0663   0.9604   0.0250
  -8.250  -0.6335   0.01385   0.00823  -0.0689   0.9578   0.0313
  -8.000  -0.5963   0.01300   0.00744  -0.0722   0.9556   0.0439
  -7.750  -0.5872   0.01250   0.00696  -0.0692   0.9461   0.0510
  -7.500  -0.5560   0.01186   0.00637  -0.0707   0.9410   0.0633
  -7.000  -0.5054   0.01055   0.00523  -0.0713   0.9129   0.1037
  -6.750  -0.4435   0.00952   0.00413  -0.0796   0.8200   0.1635
  -6.500  -0.4272   0.00918   0.00364  -0.0781   0.7331   0.2095
  -6.250  -0.4067   0.00852   0.00304  -0.0778   0.6730   0.2764
  -6.000  -0.3825   0.00803   0.00262  -0.0779   0.6231   0.3373
  -5.750  -0.3564   0.00794   0.00247  -0.0778   0.5784   0.3680
  -5.500  -0.3293   0.00797   0.00239  -0.0778   0.5384   0.3842
  -5.250  -0.3016   0.00801   0.00233  -0.0778   0.5063   0.3974
  -5.000  -0.2734   0.00806   0.00230  -0.0780   0.4812   0.4136
  -4.750  -0.2448   0.00811   0.00230  -0.0781   0.4607   0.4247
  -4.500  -0.2160   0.00819   0.00228  -0.0782   0.4428   0.4300
  -4.250  -0.1872   0.00825   0.00223  -0.0784   0.4271   0.4318
  -4.000  -0.1584   0.00827   0.00218  -0.0785   0.4130   0.4337
  -3.750  -0.1294   0.00830   0.00214  -0.0787   0.4004   0.4356
  -3.500  -0.1005   0.00833   0.00211  -0.0789   0.3890   0.4371
  -3.250  -0.0715   0.00837   0.00208  -0.0791   0.3781   0.4386
  -3.000  -0.0423   0.00839   0.00206  -0.0793   0.3704   0.4402
  -2.750  -0.0132   0.00843   0.00204  -0.0795   0.3623   0.4420
  -2.500   0.0160   0.00847   0.00202  -0.0797   0.3560   0.4436
  -2.250   0.0452   0.00850   0.00201  -0.0798   0.3495   0.4451
  -2.000   0.0742   0.00855   0.00200  -0.0800   0.3431   0.4463
  -1.750   0.1035   0.00858   0.00199  -0.0802   0.3383   0.4474
  -1.500   0.1327   0.00861   0.00199  -0.0804   0.3325   0.4488
  -1.250   0.1617   0.00866   0.00199  -0.0806   0.3266   0.4504
  -1.000   0.1909   0.00868   0.00200  -0.0808   0.3223   0.4520
  -0.750   0.2201   0.00871   0.00202  -0.0810   0.3181   0.4536
  -0.500   0.2492   0.00876   0.00204  -0.0811   0.3138   0.4555
   0.000   0.3074   0.00887   0.00210  -0.0815   0.3065   0.4590
   0.250   0.3365   0.00891   0.00213  -0.0816   0.3034   0.4605
   0.500   0.3655   0.00897   0.00216  -0.0818   0.3000   0.4619
   0.750   0.3944   0.00903   0.00220  -0.0819   0.2965   0.4632
   1.000   0.4232   0.00911   0.00225  -0.0820   0.2925   0.4645
   1.250   0.4523   0.00915   0.00230  -0.0822   0.2901   0.4663
   1.500   0.4813   0.00919   0.00235  -0.0823   0.2874   0.4681
   1.750   0.5102   0.00925   0.00241  -0.0825   0.2847   0.4698
   2.000   0.5390   0.00932   0.00248  -0.0826   0.2820   0.4716
   2.250   0.5676   0.00940   0.00255  -0.0827   0.2792   0.4736
   2.500   0.5962   0.00950   0.00263  -0.0827   0.2763   0.4756
   2.750   0.6249   0.00956   0.00271  -0.0828   0.2746   0.4774
   3.000   0.6536   0.00963   0.00279  -0.0829   0.2729   0.4789
   3.250   0.6822   0.00971   0.00287  -0.0829   0.2709   0.4802
   3.500   0.7108   0.00978   0.00296  -0.0830   0.2684   0.4822
   3.750   0.7392   0.00987   0.00305  -0.0831   0.2658   0.4841
   4.000   0.7675   0.00996   0.00316  -0.0831   0.2634   0.4861
   4.250   0.7956   0.01007   0.00328  -0.0831   0.2610   0.4880
   4.500   0.8238   0.01017   0.00340  -0.0831   0.2592   0.4900
   4.750   0.8522   0.01026   0.00351  -0.0831   0.2578   0.4920
   5.000   0.8804   0.01035   0.00363  -0.0831   0.2560   0.4940
   5.250   0.9084   0.01045   0.00375  -0.0831   0.2538   0.4958
   5.500   0.9363   0.01056   0.00386  -0.0830   0.2506   0.4977
   5.750   0.9639   0.01069   0.00400  -0.0830   0.2463   0.5000
   6.000   0.9915   0.01082   0.00415  -0.0829   0.2432   0.5022
   6.250   1.0195   0.01091   0.00429  -0.0829   0.2410   0.5044
   6.500   1.0472   0.01102   0.00443  -0.0828   0.2378   0.5066
   6.750   1.0744   0.01116   0.00457  -0.0826   0.2335   0.5087
   7.000   1.1012   0.01135   0.00475  -0.0824   0.2288   0.5107
   7.250   1.1287   0.01146   0.00490  -0.0823   0.2260   0.5125
   7.500   1.1558   0.01160   0.00506  -0.0821   0.2216   0.5145
   7.750   1.1823   0.01178   0.00524  -0.0819   0.2158   0.5174
   8.000   1.2090   0.01195   0.00544  -0.0817   0.2096   0.5202
   8.250   1.2347   0.01219   0.00566  -0.0814   0.2005   0.5229
   8.500   1.2606   0.01240   0.00588  -0.0810   0.1926   0.5254
   8.750   1.2855   0.01270   0.00614  -0.0805   0.1827   0.5277
   9.000   1.3093   0.01308   0.00646  -0.0799   0.1685   0.5298
   9.250   1.3315   0.01357   0.00688  -0.0791   0.1510   0.5321
   9.500   1.3530   0.01411   0.00735  -0.0781   0.1348   0.5349
   9.750   1.3740   0.01466   0.00784  -0.0771   0.1208   0.5377
  10.000   1.3947   0.01520   0.00834  -0.0760   0.1087   0.5408
  10.250   1.4152   0.01572   0.00883  -0.0749   0.0984   0.5439
  10.500   1.4347   0.01627   0.00935  -0.0736   0.0885   0.5467
  10.750   1.4529   0.01688   0.00992  -0.0722   0.0783   0.5495
  11.000   1.4698   0.01748   0.01050  -0.0705   0.0695   0.5528
  11.250   1.4847   0.01805   0.01106  -0.0685   0.0624   0.5560
  11.500   1.4994   0.01861   0.01163  -0.0665   0.0564   0.5593
  11.750   1.5130   0.01925   0.01226  -0.0643   0.0511   0.5625
  12.000   1.5263   0.01989   0.01291  -0.0621   0.0464   0.5653
  12.250   1.5391   0.02057   0.01360  -0.0600   0.0421   0.5692
  12.500   1.5506   0.02130   0.01436  -0.0578   0.0385   0.5735
  12.750   1.5629   0.02200   0.01510  -0.0557   0.0359   0.5781
  13.000   1.5740   0.02277   0.01591  -0.0536   0.0336   0.5819
  13.250   1.5837   0.02363   0.01681  -0.0514   0.0316   0.5863
  13.500   1.5939   0.02448   0.01773  -0.0494   0.0301   0.5910
  13.750   1.6018   0.02549   0.01879  -0.0472   0.0284   0.5956
  14.000   1.6075   0.02667   0.02002  -0.0450   0.0269   0.5999
  14.250   1.6143   0.02783   0.02127  -0.0432   0.0259   0.6051
  14.500   1.6190   0.02922   0.02274  -0.0414   0.0248   0.6111
  14.750   1.6208   0.03090   0.02449  -0.0396   0.0238   0.6166
  15.000   1.6203   0.03292   0.02660  -0.0382   0.0228   0.6230
  15.250   1.6197   0.03515   0.02893  -0.0372   0.0220   0.6297
  15.500   1.6175   0.03776   0.03165  -0.0367   0.0214   0.6360
  15.750   1.6125   0.04097   0.03498  -0.0367   0.0207   0.6429
  16.000   1.6044   0.04488   0.03901  -0.0374   0.0201   0.6494
  16.250   1.5919   0.04973   0.04399  -0.0388   0.0194   0.6554
  16.500   1.5768   0.05527   0.04968  -0.0408   0.0190   0.6618
  16.750   1.5586   0.06143   0.05598  -0.0432   0.0186   0.6674
  17.000   1.5394   0.06783   0.06254  -0.0458   0.0184   0.6731
  17.250   1.5183   0.07457   0.06943  -0.0485   0.0182   0.6787
  17.500   1.4963   0.08155   0.07655  -0.0515   0.0180   0.6842
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