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CLARK-Y 11.7% smoothed (clarkysm-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: CLARK-Y 11.7% smoothed (clarkysm-il)
Reynolds number: 1,000,000
Max Cl/Cd: 106.23 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-clarkysm-il-1000000-n5.txt
Download as CSV file: xf-clarkysm-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: CLARK-Y 11.7% 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.6696   0.10205   0.09987  -0.0482   1.0000   0.0094
 -15.000  -1.0206   0.03735   0.03431  -0.0940   1.0000   0.0082
 -14.500  -1.0729   0.03154   0.02824  -0.0887   1.0000   0.0082
 -14.250  -1.0719   0.02959   0.02616  -0.0874   0.9986   0.0083
 -14.000  -1.0534   0.02770   0.02413  -0.0887   0.9960   0.0085
 -13.750  -1.0330   0.02622   0.02253  -0.0895   0.9935   0.0086
 -13.500  -1.0146   0.02487   0.02108  -0.0896   0.9904   0.0087
 -13.250  -0.9924   0.02371   0.01982  -0.0901   0.9876   0.0089
 -13.000  -0.9683   0.02263   0.01862  -0.0908   0.9853   0.0091
 -12.750  -0.9424   0.02163   0.01752  -0.0916   0.9836   0.0093
 -12.500  -0.9214   0.02075   0.01654  -0.0912   0.9797   0.0094
 -12.250  -0.8976   0.01993   0.01563  -0.0913   0.9763   0.0096
 -12.000  -0.8715   0.01911   0.01471  -0.0917   0.9738   0.0099
 -11.750  -0.8431   0.01839   0.01390  -0.0925   0.9718   0.0100
 -11.500  -0.8160   0.01772   0.01314  -0.0930   0.9690   0.0102
 -11.250  -0.7921   0.01690   0.01223  -0.0928   0.9641   0.0105
 -11.000  -0.7626   0.01618   0.01145  -0.0938   0.9611   0.0109
 -10.750  -0.7314   0.01557   0.01078  -0.0950   0.9585   0.0112
 -10.500  -0.7023   0.01503   0.01017  -0.0956   0.9545   0.0115
 -10.250  -0.6743   0.01453   0.00960  -0.0960   0.9489   0.0119
 -10.000  -0.6436   0.01403   0.00903  -0.0969   0.9443   0.0122
  -9.750  -0.6154   0.01358   0.00851  -0.0972   0.9384   0.0125
  -9.500  -0.5875   0.01318   0.00802  -0.0974   0.9314   0.0128
  -9.250  -0.5603   0.01271   0.00748  -0.0975   0.9247   0.0133
  -9.000  -0.5347   0.01231   0.00703  -0.0972   0.9165   0.0138
  -8.750  -0.5083   0.01198   0.00664  -0.0970   0.9091   0.0143
  -8.500  -0.4828   0.01168   0.00629  -0.0965   0.9006   0.0149
  -8.250  -0.4570   0.01141   0.00595  -0.0961   0.8929   0.0155
  -8.000  -0.4317   0.01116   0.00562  -0.0956   0.8842   0.0159
  -7.750  -0.4068   0.01084   0.00525  -0.0950   0.8762   0.0167
  -7.500  -0.3818   0.01058   0.00494  -0.0944   0.8676   0.0175
  -7.250  -0.3565   0.01035   0.00467  -0.0939   0.8597   0.0183
  -7.000  -0.3311   0.01015   0.00440  -0.0933   0.8511   0.0192
  -6.750  -0.3058   0.00992   0.00413  -0.0927   0.8431   0.0203
  -6.500  -0.2806   0.00972   0.00389  -0.0921   0.8345   0.0217
  -6.250  -0.2549   0.00954   0.00367  -0.0916   0.8265   0.0231
  -6.000  -0.2296   0.00937   0.00344  -0.0910   0.8180   0.0245
  -5.750  -0.2039   0.00919   0.00324  -0.0905   0.8099   0.0262
  -5.500  -0.1783   0.00906   0.00305  -0.0899   0.8014   0.0280
  -5.250  -0.1525   0.00889   0.00287  -0.0894   0.7928   0.0304
  -5.000  -0.1269   0.00876   0.00271  -0.0889   0.7844   0.0331
  -4.750  -0.1010   0.00862   0.00255  -0.0884   0.7757   0.0359
  -4.500  -0.0752   0.00851   0.00241  -0.0878   0.7670   0.0388
  -4.250  -0.0493   0.00840   0.00228  -0.0873   0.7575   0.0420
  -4.000  -0.0234   0.00829   0.00215  -0.0868   0.7485   0.0461
  -3.500   0.0282   0.00812   0.00193  -0.0857   0.7284   0.0545
  -3.250   0.0537   0.00807   0.00183  -0.0851   0.7151   0.0583
  -3.000   0.0785   0.00801   0.00174  -0.0844   0.6982   0.0644
  -2.750   0.1037   0.00798   0.00165  -0.0837   0.6828   0.0691
  -2.500   0.1292   0.00792   0.00158  -0.0831   0.6707   0.0765
  -2.250   0.1548   0.00788   0.00151  -0.0825   0.6595   0.0839
  -2.000   0.1807   0.00782   0.00145  -0.0820   0.6484   0.0931
  -1.750   0.2063   0.00777   0.00139  -0.0815   0.6368   0.1046
  -1.500   0.2316   0.00771   0.00134  -0.0809   0.6256   0.1213
  -1.250   0.2569   0.00764   0.00130  -0.0803   0.6145   0.1418
  -1.000   0.2822   0.00757   0.00127  -0.0797   0.6024   0.1696
  -0.750   0.3072   0.00752   0.00126  -0.0790   0.5895   0.1974
  -0.500   0.3321   0.00747   0.00125  -0.0784   0.5772   0.2272
  -0.250   0.3571   0.00744   0.00125  -0.0777   0.5652   0.2548
   0.000   0.3822   0.00741   0.00126  -0.0771   0.5521   0.2836
   0.250   0.4066   0.00738   0.00128  -0.0764   0.5372   0.3199
   0.500   0.4308   0.00733   0.00130  -0.0756   0.5230   0.3650
   0.750   0.4544   0.00726   0.00134  -0.0747   0.5088   0.4227
   1.000   0.4775   0.00716   0.00138  -0.0737   0.4952   0.4942
   1.250   0.4990   0.00700   0.00144  -0.0725   0.4816   0.5870
   1.500   0.5154   0.00668   0.00152  -0.0700   0.4681   0.7378
   1.750   0.5320   0.00643   0.00163  -0.0673   0.4527   0.8705
   2.000   0.5877   0.00657   0.00183  -0.0735   0.4299   0.9443
   2.250   0.6382   0.00680   0.00196  -0.0786   0.4108   0.9608
   2.750   0.7045   0.00718   0.00218  -0.0810   0.3803   0.9788
   3.000   0.7346   0.00737   0.00230  -0.0816   0.3657   0.9852
   3.250   0.7690   0.00758   0.00243  -0.0831   0.3504   0.9916
   3.750   0.8472   0.00810   0.00273  -0.0884   0.3122   1.0000
   4.000   0.8675   0.00829   0.00286  -0.0869   0.2991   1.0000
   4.250   0.8879   0.00849   0.00299  -0.0854   0.2861   1.0000
   4.500   0.9095   0.00864   0.00311  -0.0841   0.2784   1.0000
   4.750   0.9305   0.00881   0.00325  -0.0827   0.2704   1.0000
   5.000   0.9519   0.00897   0.00338  -0.0814   0.2620   1.0000
   5.250   0.9725   0.00917   0.00354  -0.0799   0.2521   1.0000
   5.500   0.9936   0.00936   0.00369  -0.0786   0.2434   1.0000
   5.750   1.0145   0.00955   0.00385  -0.0772   0.2350   1.0000
   6.000   1.0345   0.00978   0.00403  -0.0756   0.2244   1.0000
   6.250   1.0554   0.00997   0.00420  -0.0743   0.2153   1.0000
   6.500   1.0750   0.01022   0.00440  -0.0727   0.2030   1.0000
   6.750   1.0942   0.01050   0.00462  -0.0710   0.1900   1.0000
   7.000   1.1117   0.01085   0.00488  -0.0691   0.1715   1.0000
   7.250   1.1260   0.01136   0.00525  -0.0666   0.1443   1.0000
   7.500   1.1373   0.01202   0.00572  -0.0637   0.1130   1.0000
   7.750   1.1518   0.01247   0.00608  -0.0612   0.0978   1.0000
   8.000   1.1660   0.01285   0.00642  -0.0587   0.0884   1.0000
   8.250   1.1821   0.01316   0.00672  -0.0565   0.0825   1.0000
   8.500   1.1973   0.01353   0.00706  -0.0543   0.0758   1.0000
   8.750   1.2146   0.01384   0.00738  -0.0524   0.0720   1.0000
   9.000   1.2308   0.01422   0.00774  -0.0504   0.0677   1.0000
   9.250   1.2480   0.01456   0.00810  -0.0487   0.0642   1.0000
   9.500   1.2656   0.01491   0.00846  -0.0470   0.0618   1.0000
   9.750   1.2825   0.01530   0.00886  -0.0453   0.0591   1.0000
  10.000   1.2982   0.01577   0.00931  -0.0435   0.0553   1.0000
  10.250   1.3158   0.01614   0.00972  -0.0420   0.0537   1.0000
  10.500   1.3327   0.01657   0.01017  -0.0405   0.0516   1.0000
  10.750   1.3483   0.01707   0.01068  -0.0388   0.0490   1.0000
  11.000   1.3633   0.01762   0.01123  -0.0371   0.0460   1.0000
  11.250   1.3798   0.01810   0.01174  -0.0356   0.0446   1.0000
  11.500   1.3951   0.01865   0.01232  -0.0341   0.0425   1.0000
  11.750   1.4095   0.01928   0.01297  -0.0325   0.0405   1.0000
  12.000   1.4231   0.01997   0.01367  -0.0309   0.0384   1.0000
  12.250   1.4378   0.02060   0.01434  -0.0295   0.0370   1.0000
  12.500   1.4515   0.02132   0.01509  -0.0280   0.0351   1.0000
  12.750   1.4632   0.02218   0.01596  -0.0264   0.0329   1.0000
  13.000   1.4756   0.02302   0.01684  -0.0250   0.0315   1.0000
  13.250   1.4877   0.02391   0.01777  -0.0236   0.0296   1.0000
  13.500   1.4984   0.02492   0.01880  -0.0222   0.0279   1.0000
  13.750   1.5076   0.02606   0.01997  -0.0208   0.0259   1.0000
  14.000   1.5174   0.02720   0.02116  -0.0195   0.0242   1.0000
  14.250   1.5257   0.02849   0.02248  -0.0181   0.0227   1.0000
  14.500   1.5330   0.02988   0.02391  -0.0169   0.0213   1.0000
  14.750   1.5405   0.03132   0.02541  -0.0158   0.0201   1.0000
  15.000   1.5459   0.03296   0.02710  -0.0146   0.0187   1.0000
  15.250   1.5504   0.03475   0.02892  -0.0136   0.0174   1.0000
  15.500   1.5552   0.03657   0.03081  -0.0127   0.0163   1.0000
  15.750   1.5593   0.03852   0.03283  -0.0120   0.0156   1.0000
  16.000   1.5604   0.04082   0.03518  -0.0112   0.0145   1.0000
  16.250   1.5621   0.04313   0.03756  -0.0107   0.0136   1.0000
  16.500   1.5633   0.04559   0.04009  -0.0103   0.0130   1.0000
  16.750   1.5638   0.04820   0.04278  -0.0101   0.0125   1.0000
  17.000   1.5607   0.05125   0.04590  -0.0099   0.0117   1.0000
  17.250   1.5592   0.05426   0.04899  -0.0100   0.0113   1.0000
  17.500   1.5567   0.05745   0.05227  -0.0102   0.0108   1.0000
  17.750   1.5532   0.06085   0.05575  -0.0106   0.0105   1.0000
  18.000   1.5480   0.06449   0.05949  -0.0111   0.0101   1.0000
  18.250   1.5424   0.06830   0.06339  -0.0118   0.0099   1.0000
  18.500   1.5344   0.07253   0.06771  -0.0127   0.0095   1.0000
  18.750   1.5253   0.07696   0.07224  -0.0137   0.0093   1.0000
  19.000   1.5148   0.08165   0.07703  -0.0149   0.0089   1.0000
  19.250   1.5050   0.08634   0.08183  -0.0163   0.0088   1.0000
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