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SD7037-092-88 (sd7037-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: SD7037-092-88 (sd7037-il)
Reynolds number: 100,000
Max Cl/Cd: 55.22 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sd7037-il-100000.txt
Download as CSV file: xf-sd7037-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7037-092-88                                   
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.3686   0.10006   0.09510  -0.0296   1.0000   0.0930
  -8.500  -0.3794   0.09810   0.09326  -0.0325   1.0000   0.0956
  -8.250  -0.4023   0.09686   0.09218  -0.0353   1.0000   0.0964
  -8.000  -0.3760   0.09132   0.08660  -0.0316   1.0000   0.0999
  -7.750  -0.3715   0.08876   0.08408  -0.0303   1.0000   0.1033
  -7.500  -0.3792   0.08661   0.08203  -0.0297   1.0000   0.1065
  -7.250  -0.3982   0.08494   0.08049  -0.0297   1.0000   0.1090
  -7.000  -0.4259   0.08260   0.07822  -0.0374   1.0000   0.1108
  -6.750  -0.4203   0.07861   0.07433  -0.0330   1.0000   0.1127
  -6.500  -0.4133   0.07635   0.07210  -0.0286   1.0000   0.1157
  -6.250  -0.4144   0.07385   0.06964  -0.0280   1.0000   0.1194
  -6.000  -0.4263   0.06939   0.06505  -0.0365   1.0000   0.1265
  -5.750  -0.4192   0.06686   0.06265  -0.0317   1.0000   0.1288
  -5.500  -0.4139   0.06448   0.06029  -0.0301   1.0000   0.1338
  -5.250  -0.4096   0.06041   0.05609  -0.0337   1.0000   0.1428
  -5.000  -0.3997   0.05743   0.05288  -0.0368   1.0000   0.1559
  -4.750  -0.3913   0.05461   0.05022  -0.0337   1.0000   0.1587
  -4.500  -0.3785   0.05163   0.04710  -0.0351   1.0000   0.1723
  -4.250  -0.3277   0.03733   0.03108  -0.0453   1.0000   0.0841
  -4.000  -0.2997   0.03241   0.02553  -0.0456   1.0000   0.0669
  -3.750  -0.2747   0.02936   0.02209  -0.0458   1.0000   0.0639
  -3.500  -0.2493   0.02723   0.01949  -0.0458   1.0000   0.0644
  -3.250  -0.2239   0.02543   0.01727  -0.0454   1.0000   0.0652
  -3.000  -0.1990   0.02382   0.01531  -0.0449   1.0000   0.0655
  -2.750  -0.1746   0.02257   0.01378  -0.0443   1.0000   0.0669
  -2.500  -0.1468   0.02145   0.01246  -0.0443   0.9987   0.0699
  -2.250  -0.1029   0.02040   0.01144  -0.0475   0.9919   0.0836
  -2.000  -0.0590   0.01914   0.01046  -0.0507   0.9853   0.1222
  -1.750  -0.0223   0.01694   0.01005  -0.0532   0.9786   0.4425
  -1.500   0.0069   0.01593   0.01047  -0.0513   0.9720   0.8662
  -1.250   0.0622   0.01597   0.01016  -0.0569   0.9612   1.0000
  -1.000   0.1053   0.01625   0.01010  -0.0602   0.9501   1.0000
  -0.750   0.1501   0.01649   0.01008  -0.0637   0.9394   1.0000
  -0.500   0.1991   0.01667   0.01003  -0.0678   0.9302   1.0000
  -0.250   0.2384   0.01676   0.00995  -0.0701   0.9177   1.0000
   0.000   0.2790   0.01681   0.00986  -0.0724   0.9057   1.0000
   0.250   0.3241   0.01677   0.00970  -0.0755   0.8954   1.0000
   0.500   0.3721   0.01660   0.00943  -0.0789   0.8862   1.0000
   0.750   0.4085   0.01648   0.00924  -0.0801   0.8732   1.0000
   1.000   0.4446   0.01630   0.00901  -0.0810   0.8604   1.0000
   1.250   0.4799   0.01608   0.00874  -0.0817   0.8475   1.0000
   1.500   0.5142   0.01582   0.00845  -0.0820   0.8344   1.0000
   1.750   0.5469   0.01555   0.00816  -0.0820   0.8204   1.0000
   2.000   0.5779   0.01531   0.00788  -0.0817   0.8052   1.0000
   2.250   0.6077   0.01509   0.00763  -0.0811   0.7890   1.0000
   2.500   0.6370   0.01489   0.00741  -0.0804   0.7718   1.0000
   2.750   0.6661   0.01473   0.00718  -0.0796   0.7540   1.0000
   3.000   0.6930   0.01470   0.00710  -0.0787   0.7338   1.0000
   3.250   0.7195   0.01472   0.00709  -0.0777   0.7123   1.0000
   3.500   0.7464   0.01477   0.00706  -0.0768   0.6910   1.0000
   3.750   0.7716   0.01493   0.00716  -0.0757   0.6674   1.0000
   4.000   0.7970   0.01511   0.00727  -0.0747   0.6439   1.0000
   4.250   0.8223   0.01533   0.00743  -0.0737   0.6200   1.0000
   4.500   0.8464   0.01561   0.00766  -0.0727   0.5946   1.0000
   4.750   0.8708   0.01592   0.00789  -0.0716   0.5698   1.0000
   5.000   0.8951   0.01625   0.00813  -0.0706   0.5447   1.0000
   5.250   0.9183   0.01663   0.00850  -0.0695   0.5182   1.0000
   5.500   0.9414   0.01705   0.00885  -0.0684   0.4919   1.0000
   5.750   0.9645   0.01751   0.00923  -0.0674   0.4662   1.0000
   6.000   0.9872   0.01800   0.00965  -0.0663   0.4403   1.0000
   6.250   1.0091   0.01853   0.01016  -0.0651   0.4136   1.0000
   6.500   1.0308   0.01910   0.01069  -0.0640   0.3876   1.0000
   6.750   1.0525   0.01974   0.01125  -0.0629   0.3630   1.0000
   7.000   1.0735   0.02040   0.01188  -0.0617   0.3383   1.0000
   7.250   1.0941   0.02112   0.01260  -0.0606   0.3142   1.0000
   7.500   1.1147   0.02191   0.01326  -0.0594   0.2920   1.0000
   7.750   1.1340   0.02269   0.01410  -0.0581   0.2689   1.0000
   8.000   1.1537   0.02358   0.01490  -0.0570   0.2484   1.0000
   8.250   1.1719   0.02446   0.01588  -0.0555   0.2273   1.0000
   8.500   1.1903   0.02544   0.01682  -0.0542   0.2082   1.0000
   8.750   1.2081   0.02655   0.01792  -0.0529   0.1897   1.0000
   9.000   1.2245   0.02769   0.01915  -0.0513   0.1716   1.0000
   9.250   1.2391   0.02878   0.02028  -0.0496   0.1540   1.0000
   9.500   1.2507   0.02985   0.02125  -0.0477   0.1365   1.0000
   9.750   1.2582   0.03082   0.02238  -0.0452   0.1191   1.0000
  10.000   1.2656   0.03211   0.02374  -0.0428   0.1030   1.0000
  10.250   1.2704   0.03365   0.02529  -0.0402   0.0881   1.0000
  10.500   1.2730   0.03549   0.02714  -0.0372   0.0755   1.0000
  10.750   1.2785   0.03785   0.02956  -0.0347   0.0653   1.0000
  11.000   1.2878   0.04047   0.03223  -0.0329   0.0584   1.0000
  11.250   1.2943   0.04253   0.03443  -0.0309   0.0533   1.0000
  11.500   1.3059   0.04547   0.03739  -0.0297   0.0493   1.0000
  11.750   1.3113   0.04823   0.04051  -0.0277   0.0472   1.0000
  12.000   1.3151   0.05123   0.04381  -0.0259   0.0455   1.0000
  12.250   1.3153   0.05437   0.04722  -0.0241   0.0444   1.0000
  12.500   1.3122   0.05770   0.05082  -0.0226   0.0436   1.0000
  12.750   1.3058   0.06128   0.05465  -0.0212   0.0429   1.0000
  13.000   1.2955   0.06527   0.05891  -0.0203   0.0426   1.0000
  13.250   1.2811   0.06974   0.06365  -0.0200   0.0425   1.0000
  13.500   1.2617   0.07485   0.06906  -0.0206   0.0427   1.0000
  13.750   1.2378   0.08088   0.07539  -0.0223   0.0429   1.0000
  14.000   1.2050   0.08863   0.08347  -0.0261   0.0436   1.0000
  14.250   1.1631   0.09897   0.09413  -0.0327   0.0449   1.0000
  14.500   1.1201   0.11143   0.10682  -0.0414   0.0463   1.0000
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