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WASP (smoothed) (waspsm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: WASP (smoothed) (waspsm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 115.78 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-waspsm-il-1000000.txt
Download as CSV file: xf-waspsm-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500  -0.4615   0.09316   0.09151  -0.0211   1.0000   0.0140
  -9.250  -0.6816   0.03375   0.03160  -0.0573   1.0000   0.0094
  -9.000  -0.6950   0.02716   0.02442  -0.0556   1.0000   0.0095
  -8.750  -0.6900   0.02463   0.02160  -0.0531   1.0000   0.0097
  -8.500  -0.6629   0.02236   0.01902  -0.0546   0.9987   0.0100
  -8.250  -0.6328   0.02063   0.01701  -0.0562   0.9970   0.0102
  -8.000  -0.6078   0.01712   0.01298  -0.0574   0.9948   0.0106
  -7.750  -0.5790   0.01577   0.01148  -0.0582   0.9918   0.0111
  -7.500  -0.5472   0.01506   0.01068  -0.0593   0.9886   0.0115
  -7.250  -0.5172   0.01438   0.00991  -0.0600   0.9845   0.0119
  -7.000  -0.4862   0.01366   0.00908  -0.0608   0.9807   0.0123
  -6.750  -0.4536   0.01293   0.00825  -0.0619   0.9778   0.0128
  -6.500  -0.4236   0.01233   0.00756  -0.0624   0.9733   0.0133
  -6.250  -0.3900   0.01189   0.00704  -0.0636   0.9702   0.0137
  -6.000  -0.3568   0.01066   0.00567  -0.0650   0.9677   0.0149
  -5.750  -0.3200   0.01029   0.00527  -0.0669   0.9648   0.0160
  -5.500  -0.2827   0.00999   0.00494  -0.0690   0.9607   0.0173
  -5.250  -0.2418   0.00972   0.00462  -0.0719   0.9572   0.0183
  -5.000  -0.2015   0.00898   0.00381  -0.0747   0.9530   0.0205
  -4.750  -0.1681   0.00875   0.00355  -0.0759   0.9444   0.0222
  -4.500  -0.1337   0.00856   0.00331  -0.0772   0.9364   0.0235
  -4.250  -0.1046   0.00816   0.00285  -0.0774   0.9256   0.0262
  -4.000  -0.0771   0.00800   0.00266  -0.0772   0.9135   0.0286
  -3.750  -0.0493   0.00786   0.00248  -0.0770   0.9003   0.0305
  -3.500  -0.0230   0.00759   0.00216  -0.0764   0.8853   0.0356
  -3.250   0.0037   0.00749   0.00200  -0.0760   0.8687   0.0394
  -2.750   0.0545   0.00719   0.00162  -0.0745   0.8316   0.0580
  -2.500   0.0794   0.00709   0.00149  -0.0737   0.8122   0.0727
  -2.250   0.1041   0.00700   0.00138  -0.0728   0.7931   0.0921
  -2.000   0.1287   0.00690   0.00129  -0.0719   0.7747   0.1174
  -1.750   0.1532   0.00679   0.00121  -0.0711   0.7562   0.1490
  -1.500   0.1774   0.00666   0.00115  -0.0702   0.7372   0.1922
  -1.250   0.2012   0.00653   0.00110  -0.0692   0.7177   0.2446
  -1.000   0.2251   0.00640   0.00107  -0.0683   0.6989   0.3026
  -0.750   0.2487   0.00624   0.00105  -0.0673   0.6795   0.3729
  -0.500   0.2720   0.00610   0.00104  -0.0663   0.6591   0.4491
  -0.250   0.2952   0.00598   0.00105  -0.0652   0.6389   0.5246
   0.000   0.3178   0.00583   0.00107  -0.0640   0.6191   0.6079
   0.250   0.3370   0.00555   0.00110  -0.0619   0.6000   0.7345
   0.500   0.4478   0.00526   0.00123  -0.0810   0.5657   0.9978
   0.750   0.4799   0.00539   0.00125  -0.0819   0.5440   1.0000
   1.000   0.5053   0.00552   0.00128  -0.0813   0.5242   1.0000
   1.250   0.5307   0.00566   0.00131  -0.0807   0.5059   1.0000
   1.500   0.5564   0.00578   0.00135  -0.0801   0.4885   1.0000
   1.750   0.5822   0.00591   0.00140  -0.0795   0.4725   1.0000
   2.000   0.6079   0.00604   0.00145  -0.0790   0.4572   1.0000
   2.250   0.6336   0.00617   0.00152  -0.0784   0.4418   1.0000
   2.500   0.6593   0.00631   0.00159  -0.0779   0.4278   1.0000
   2.750   0.6850   0.00645   0.00166  -0.0774   0.4145   1.0000
   3.000   0.7106   0.00659   0.00174  -0.0768   0.4004   1.0000
   3.250   0.7362   0.00674   0.00184  -0.0763   0.3865   1.0000
   3.500   0.7619   0.00689   0.00193  -0.0757   0.3737   1.0000
   3.750   0.7875   0.00703   0.00204  -0.0752   0.3606   1.0000
   4.000   0.8130   0.00720   0.00215  -0.0746   0.3470   1.0000
   4.250   0.8384   0.00736   0.00227  -0.0741   0.3342   1.0000
   4.500   0.8638   0.00753   0.00240  -0.0735   0.3219   1.0000
   4.750   0.8890   0.00771   0.00254  -0.0730   0.3092   1.0000
   5.000   0.9140   0.00791   0.00270  -0.0724   0.2955   1.0000
   5.250   0.9390   0.00811   0.00286  -0.0717   0.2823   1.0000
   5.500   0.9637   0.00834   0.00303  -0.0711   0.2683   1.0000
   5.750   0.9879   0.00860   0.00322  -0.0704   0.2481   1.0000
   6.000   1.0112   0.00894   0.00345  -0.0696   0.2257   1.0000
   6.250   1.0351   0.00923   0.00367  -0.0688   0.2074   1.0000
   6.500   1.0589   0.00954   0.00391  -0.0680   0.1905   1.0000
   6.750   1.0827   0.00983   0.00415  -0.0673   0.1767   1.0000
   7.000   1.1064   0.01014   0.00442  -0.0665   0.1637   1.0000
   7.250   1.1298   0.01046   0.00469  -0.0657   0.1499   1.0000
   7.500   1.1527   0.01083   0.00499  -0.0649   0.1348   1.0000
   7.750   1.1750   0.01125   0.00533  -0.0639   0.1182   1.0000
   8.000   1.1966   0.01173   0.00572  -0.0629   0.0983   1.0000
   8.250   1.2148   0.01250   0.00629  -0.0613   0.0670   1.0000
   8.500   1.2322   0.01335   0.00697  -0.0596   0.0408   1.0000
   8.750   1.2513   0.01405   0.00759  -0.0582   0.0285   1.0000
   9.000   1.2717   0.01460   0.00813  -0.0569   0.0229   1.0000
   9.250   1.2920   0.01516   0.00872  -0.0557   0.0193   1.0000
   9.500   1.3124   0.01569   0.00927  -0.0545   0.0171   1.0000
   9.750   1.3302   0.01644   0.01007  -0.0529   0.0150   1.0000
  10.000   1.3511   0.01689   0.01056  -0.0518   0.0143   1.0000
  10.250   1.3709   0.01740   0.01112  -0.0505   0.0133   1.0000
  10.500   1.3893   0.01800   0.01175  -0.0491   0.0124   1.0000
  10.750   1.4033   0.01894   0.01278  -0.0470   0.0114   1.0000
  11.000   1.4188   0.01970   0.01362  -0.0451   0.0110   1.0000
  11.250   1.4358   0.02030   0.01428  -0.0436   0.0106   1.0000
  11.500   1.4512   0.02098   0.01503  -0.0418   0.0102   1.0000
  11.750   1.4642   0.02170   0.01581  -0.0396   0.0098   1.0000
  12.000   1.4744   0.02243   0.01660  -0.0369   0.0094   1.0000
  12.250   1.4836   0.02324   0.01747  -0.0343   0.0091   1.0000
  12.500   1.4893   0.02431   0.01861  -0.0314   0.0087   1.0000
  12.750   1.4864   0.02601   0.02043  -0.0279   0.0083   1.0000
  13.000   1.4847   0.02780   0.02234  -0.0250   0.0081   1.0000
  13.250   1.4937   0.02894   0.02357  -0.0235   0.0079   1.0000
  13.500   1.4995   0.03041   0.02513  -0.0219   0.0077   1.0000
  13.750   1.5032   0.03217   0.02699  -0.0205   0.0075   1.0000
  14.000   1.5056   0.03420   0.02911  -0.0194   0.0074   1.0000
  14.250   1.5068   0.03648   0.03150  -0.0186   0.0072   1.0000
  14.500   1.5067   0.03907   0.03419  -0.0182   0.0070   1.0000
  14.750   1.5056   0.04196   0.03718  -0.0181   0.0069   1.0000
  15.000   1.5028   0.04519   0.04052  -0.0183   0.0067   1.0000
  15.250   1.4987   0.04878   0.04421  -0.0189   0.0066   1.0000
  15.500   1.4924   0.05279   0.04835  -0.0198   0.0065   1.0000
  15.750   1.4839   0.05723   0.05289  -0.0210   0.0064   1.0000
  16.000   1.4733   0.06212   0.05791  -0.0225   0.0063   1.0000
  16.250   1.4604   0.06743   0.06333  -0.0242   0.0063   1.0000
  16.500   1.4460   0.07313   0.06915  -0.0262   0.0062   1.0000
  16.750   1.4304   0.07913   0.07527  -0.0284   0.0062   1.0000
  17.000   1.4140   0.08534   0.08159  -0.0307   0.0061   1.0000
  17.250   1.3973   0.09174   0.08810  -0.0331   0.0061   1.0000
  17.500   1.3803   0.09827   0.09475  -0.0357   0.0060   1.0000
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