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WASP (smoothed) (waspsm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: WASP (smoothed) (waspsm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.06 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-waspsm-il-1000000-n5.txt
Download as CSV file: xf-waspsm-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: WASP (smoothed)                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.9535   0.03419   0.03172  -0.0644   1.0000   0.0057
 -12.000  -0.9503   0.03064   0.02793  -0.0644   1.0000   0.0058
 -11.750  -0.9403   0.02820   0.02529  -0.0639   1.0000   0.0059
 -11.500  -0.9271   0.02628   0.02317  -0.0631   1.0000   0.0060
 -11.250  -0.9115   0.02475   0.02149  -0.0623   1.0000   0.0061
 -11.000  -0.8946   0.02343   0.02004  -0.0613   1.0000   0.0062
 -10.750  -0.8770   0.02226   0.01873  -0.0603   1.0000   0.0063
 -10.500  -0.8591   0.02118   0.01753  -0.0591   1.0000   0.0065
 -10.250  -0.8412   0.02017   0.01639  -0.0578   1.0000   0.0066
 -10.000  -0.8147   0.01908   0.01515  -0.0584   0.9992   0.0068
  -9.750  -0.7859   0.01803   0.01394  -0.0593   0.9977   0.0069
  -9.500  -0.7570   0.01710   0.01287  -0.0601   0.9956   0.0071
  -9.000  -0.7068   0.01554   0.01108  -0.0597   0.9816   0.0073
  -8.750  -0.6780   0.01487   0.01029  -0.0602   0.9767   0.0074
  -8.500  -0.6489   0.01396   0.00925  -0.0609   0.9730   0.0077
  -8.250  -0.6175   0.01326   0.00845  -0.0619   0.9700   0.0080
  -8.000  -0.5840   0.01270   0.00783  -0.0633   0.9674   0.0084
  -7.750  -0.5491   0.01221   0.00727  -0.0650   0.9644   0.0087
  -7.500  -0.5128   0.01174   0.00673  -0.0670   0.9607   0.0091
  -7.250  -0.4736   0.01127   0.00619  -0.0696   0.9574   0.0096
  -7.000  -0.4324   0.01084   0.00568  -0.0727   0.9541   0.0100
  -6.750  -0.3950   0.01043   0.00520  -0.0749   0.9478   0.0105
  -6.500  -0.3584   0.01002   0.00474  -0.0769   0.9403   0.0113
  -6.250  -0.3273   0.00977   0.00445  -0.0776   0.9309   0.0121
  -6.000  -0.2967   0.00954   0.00415  -0.0782   0.9207   0.0130
  -5.750  -0.2675   0.00934   0.00388  -0.0784   0.9087   0.0136
  -5.500  -0.2402   0.00906   0.00354  -0.0782   0.8945   0.0146
  -5.250  -0.2135   0.00886   0.00328  -0.0778   0.8781   0.0157
  -5.000  -0.1874   0.00871   0.00304  -0.0773   0.8593   0.0167
  -4.750  -0.1617   0.00859   0.00282  -0.0767   0.8396   0.0177
  -4.500  -0.1366   0.00847   0.00260  -0.0759   0.8201   0.0187
  -4.250  -0.1116   0.00833   0.00241  -0.0751   0.8008   0.0207
  -4.000  -0.0865   0.00824   0.00224  -0.0744   0.7821   0.0226
  -3.750  -0.0613   0.00818   0.00208  -0.0736   0.7634   0.0240
  -3.500  -0.0365   0.00807   0.00192  -0.0728   0.7452   0.0276
  -3.250  -0.0111   0.00801   0.00178  -0.0721   0.7267   0.0304
  -3.000   0.0141   0.00793   0.00165  -0.0714   0.7084   0.0348
  -2.750   0.0393   0.00789   0.00154  -0.0707   0.6891   0.0393
  -2.500   0.0644   0.00783   0.00144  -0.0700   0.6706   0.0469
  -2.250   0.0898   0.00778   0.00135  -0.0693   0.6517   0.0547
  -2.000   0.1153   0.00774   0.00127  -0.0687   0.6328   0.0644
  -1.750   0.1406   0.00770   0.00120  -0.0680   0.6140   0.0777
  -1.500   0.1657   0.00765   0.00114  -0.0673   0.5954   0.0975
  -1.250   0.1909   0.00759   0.00109  -0.0667   0.5758   0.1232
  -1.000   0.2162   0.00755   0.00106  -0.0660   0.5576   0.1489
  -0.750   0.2414   0.00750   0.00103  -0.0654   0.5400   0.1814
  -0.500   0.2665   0.00745   0.00101  -0.0647   0.5223   0.2171
  -0.250   0.2916   0.00740   0.00101  -0.0641   0.5053   0.2580
   0.000   0.3167   0.00732   0.00101  -0.0635   0.4904   0.3077
   0.250   0.3413   0.00721   0.00103  -0.0628   0.4760   0.3741
   0.500   0.3661   0.00713   0.00106  -0.0621   0.4610   0.4350
   0.750   0.3910   0.00708   0.00110  -0.0614   0.4464   0.4900
   1.000   0.4156   0.00702   0.00114  -0.0606   0.4318   0.5507
   1.250   0.4394   0.00691   0.00120  -0.0597   0.4180   0.6271
   1.500   0.4616   0.00674   0.00126  -0.0584   0.4051   0.7207
   2.000   0.6010   0.00656   0.00151  -0.0778   0.3664   1.0000
   2.250   0.6267   0.00669   0.00158  -0.0772   0.3537   1.0000
   2.500   0.6525   0.00683   0.00165  -0.0767   0.3419   1.0000
   2.750   0.6785   0.00695   0.00172  -0.0762   0.3312   1.0000
   3.000   0.7042   0.00709   0.00181  -0.0757   0.3191   1.0000
   3.250   0.7298   0.00724   0.00191  -0.0752   0.3069   1.0000
   3.500   0.7554   0.00740   0.00201  -0.0747   0.2963   1.0000
   3.750   0.7809   0.00756   0.00212  -0.0741   0.2847   1.0000
   4.000   0.8063   0.00773   0.00224  -0.0736   0.2723   1.0000
   4.250   0.8318   0.00789   0.00238  -0.0730   0.2613   1.0000
   4.500   0.8572   0.00807   0.00251  -0.0725   0.2515   1.0000
   5.000   0.9075   0.00845   0.00281  -0.0713   0.2291   1.0000
   5.250   0.9325   0.00865   0.00299  -0.0708   0.2185   1.0000
   5.500   0.9574   0.00886   0.00317  -0.0701   0.2079   1.0000
   5.750   0.9811   0.00918   0.00338  -0.0694   0.1881   1.0000
   6.000   1.0041   0.00955   0.00364  -0.0685   0.1654   1.0000
   6.250   1.0275   0.00990   0.00390  -0.0677   0.1472   1.0000
   6.500   1.0507   0.01025   0.00416  -0.0668   0.1312   1.0000
   6.750   1.0743   0.01057   0.00443  -0.0660   0.1182   1.0000
   7.000   1.0976   0.01091   0.00473  -0.0652   0.1049   1.0000
   7.250   1.1198   0.01135   0.00507  -0.0643   0.0873   1.0000
   7.500   1.1400   0.01197   0.00554  -0.0630   0.0617   1.0000
   7.750   1.1602   0.01259   0.00604  -0.0617   0.0419   1.0000
   8.000   1.1817   0.01307   0.00648  -0.0606   0.0318   1.0000
   8.250   1.2036   0.01352   0.00691  -0.0596   0.0255   1.0000
   8.500   1.2254   0.01397   0.00734  -0.0586   0.0209   1.0000
   8.750   1.2476   0.01436   0.00775  -0.0577   0.0182   1.0000
   9.000   1.2689   0.01483   0.00821  -0.0567   0.0154   1.0000
   9.250   1.2908   0.01523   0.00865  -0.0557   0.0139   1.0000
   9.500   1.3119   0.01568   0.00912  -0.0546   0.0124   1.0000
   9.750   1.3324   0.01619   0.00964  -0.0535   0.0111   1.0000
  10.000   1.3534   0.01662   0.01012  -0.0524   0.0105   1.0000
  10.250   1.3738   0.01709   0.01062  -0.0513   0.0098   1.0000
  10.500   1.3933   0.01761   0.01117  -0.0500   0.0091   1.0000
  10.750   1.4116   0.01820   0.01181  -0.0486   0.0084   1.0000
  11.000   1.4298   0.01878   0.01243  -0.0472   0.0080   1.0000
  11.250   1.4480   0.01932   0.01303  -0.0458   0.0077   1.0000
  11.500   1.4652   0.01990   0.01367  -0.0443   0.0074   1.0000
  11.750   1.4814   0.02052   0.01435  -0.0426   0.0071   1.0000
  12.000   1.4960   0.02118   0.01506  -0.0407   0.0068   1.0000
  12.250   1.5073   0.02186   0.01581  -0.0382   0.0065   1.0000
  12.500   1.5172   0.02261   0.01662  -0.0356   0.0063   1.0000
  12.750   1.5255   0.02351   0.01757  -0.0330   0.0060   1.0000
  13.000   1.5318   0.02458   0.01873  -0.0304   0.0057   1.0000
  13.250   1.5414   0.02550   0.01972  -0.0284   0.0056   1.0000
  13.500   1.5500   0.02654   0.02084  -0.0264   0.0054   1.0000
  13.750   1.5573   0.02774   0.02213  -0.0246   0.0053   1.0000
  14.000   1.5635   0.02910   0.02357  -0.0229   0.0052   1.0000
  14.250   1.5686   0.03064   0.02521  -0.0214   0.0050   1.0000
  14.500   1.5726   0.03239   0.02705  -0.0201   0.0049   1.0000
  14.750   1.5756   0.03435   0.02911  -0.0191   0.0048   1.0000
  15.000   1.5773   0.03658   0.03143  -0.0184   0.0046   1.0000
  15.250   1.5777   0.03909   0.03405  -0.0179   0.0045   1.0000
  15.500   1.5765   0.04194   0.03699  -0.0178   0.0044   1.0000
  15.750   1.5735   0.04515   0.04031  -0.0180   0.0043   1.0000
  16.000   1.5685   0.04877   0.04404  -0.0186   0.0043   1.0000
  16.250   1.5611   0.05287   0.04825  -0.0194   0.0042   1.0000
  16.500   1.5511   0.05747   0.05298  -0.0207   0.0041   1.0000
  16.750   1.5389   0.06255   0.05818  -0.0222   0.0041   1.0000
  17.000   1.5241   0.06815   0.06391  -0.0241   0.0040   1.0000
  17.250   1.5073   0.07421   0.07011  -0.0263   0.0040   1.0000
  17.500   1.4886   0.08070   0.07673  -0.0287   0.0040   1.0000
  17.750   1.4687   0.08752   0.08368  -0.0313   0.0039   1.0000
  18.000   1.4480   0.09465   0.09093  -0.0342   0.0039   1.0000
  18.250   1.4269   0.10189   0.09830  -0.0372   0.0039   1.0000
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