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SD7062 (14%) (sd7062-il) Xfoil prediction polar at RE=50,000 Ncrit=5


Details Polar file
Airfoil: SD7062 (14%) (sd7062-il)
Reynolds number: 50,000
Max Cl/Cd: 32.14 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sd7062-il-50000-n5.txt
Download as CSV file: xf-sd7062-il-50000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SD7062 (14%)                                    
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.050 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500  -0.2807   0.10122   0.09419  -0.0436   1.0000   0.0631
  -9.250  -0.2836   0.09780   0.09087  -0.0442   1.0000   0.0620
  -9.000  -0.2904   0.09425   0.08744  -0.0449   1.0000   0.0609
  -8.750  -0.3029   0.09041   0.08374  -0.0456   1.0000   0.0596
  -8.500  -0.3381   0.08451   0.07802  -0.0479   1.0000   0.0575
  -8.250  -0.3556   0.08241   0.07606  -0.0460   1.0000   0.0572
  -8.000  -0.3788   0.08068   0.07447  -0.0435   1.0000   0.0569
  -7.750  -0.3997   0.07780   0.07169  -0.0433   0.9982   0.0564
  -7.500  -0.3919   0.06968   0.06342  -0.0542   0.9835   0.0558
  -7.250  -0.3859   0.06241   0.05584  -0.0629   0.9696   0.0557
  -7.000  -0.3763   0.05607   0.04906  -0.0693   0.9567   0.0560
  -6.750  -0.3633   0.05083   0.04326  -0.0735   0.9443   0.0567
  -6.500  -0.3446   0.04634   0.03807  -0.0766   0.9333   0.0576
  -6.250  -0.3139   0.04353   0.03505  -0.0793   0.9255   0.0588
  -6.000  -0.2893   0.04108   0.03228  -0.0804   0.9151   0.0597
  -5.750  -0.2546   0.03852   0.02934  -0.0830   0.9082   0.0612
  -5.500  -0.2284   0.03656   0.02702  -0.0835   0.8978   0.0631
  -5.250  -0.1928   0.03452   0.02451  -0.0853   0.8908   0.0666
  -5.000  -0.1669   0.03338   0.02336  -0.0854   0.8803   0.0700
  -4.750  -0.1316   0.03191   0.02162  -0.0865   0.8731   0.0743
  -4.500  -0.1060   0.03082   0.02045  -0.0861   0.8625   0.0784
  -4.250  -0.0720   0.02973   0.01919  -0.0869   0.8551   0.0868
  -4.000  -0.0480   0.02890   0.01839  -0.0863   0.8441   0.0960
  -3.750  -0.0151   0.02786   0.01730  -0.0870   0.8367   0.1135
  -3.500   0.0078   0.02706   0.01665  -0.0864   0.8253   0.1377
  -3.250   0.0408   0.02595   0.01577  -0.0874   0.8180   0.1923
  -3.000   0.0622   0.02527   0.01545  -0.0867   0.8063   0.2616
  -2.750   0.0922   0.02453   0.01511  -0.0868   0.7989   0.3564
  -2.500   0.1125   0.02433   0.01515  -0.0853   0.7871   0.4334
  -2.250   0.1380   0.02410   0.01507  -0.0840   0.7782   0.5071
  -2.000   0.1607   0.02400   0.01506  -0.0823   0.7679   0.5689
  -1.750   0.1829   0.02393   0.01504  -0.0804   0.7581   0.6238
  -1.500   0.2061   0.02380   0.01496  -0.0783   0.7489   0.6752
  -1.250   0.2255   0.02378   0.01498  -0.0757   0.7384   0.7222
  -1.000   0.2497   0.02359   0.01476  -0.0736   0.7300   0.7713
  -0.750   0.2694   0.02359   0.01478  -0.0712   0.7190   0.8192
  -0.500   0.3042   0.02331   0.01439  -0.0710   0.7114   0.8743
  -0.250   0.3496   0.02327   0.01424  -0.0739   0.6997   0.9342
   0.000   0.4093   0.02301   0.01372  -0.0797   0.6906   1.0000
   0.250   0.4273   0.02321   0.01371  -0.0786   0.6794   1.0000
   0.500   0.4492   0.02343   0.01372  -0.0779   0.6688   1.0000
   0.750   0.4765   0.02349   0.01355  -0.0776   0.6597   1.0000
   1.000   0.4980   0.02383   0.01374  -0.0769   0.6482   1.0000
   1.250   0.5279   0.02383   0.01352  -0.0768   0.6401   1.0000
   1.750   0.5747   0.02447   0.01390  -0.0755   0.6182   1.0000
   2.000   0.6014   0.02464   0.01394  -0.0751   0.6085   1.0000
   2.250   0.6242   0.02503   0.01423  -0.0744   0.5974   1.0000
   2.500   0.6541   0.02506   0.01411  -0.0742   0.5892   1.0000
   2.750   0.6748   0.02558   0.01457  -0.0733   0.5774   1.0000
   3.000   0.7013   0.02581   0.01469  -0.0729   0.5680   1.0000
   3.250   0.7260   0.02613   0.01494  -0.0723   0.5577   1.0000
   3.500   0.7489   0.02656   0.01532  -0.0715   0.5472   1.0000
   3.750   0.7773   0.02670   0.01534  -0.0712   0.5384   1.0000
   4.000   0.7975   0.02730   0.01594  -0.0703   0.5271   1.0000
   4.250   0.8254   0.02747   0.01601  -0.0699   0.5185   1.0000
   4.500   0.8464   0.02803   0.01657  -0.0690   0.5075   1.0000
   4.750   0.8696   0.02848   0.01699  -0.0683   0.4978   1.0000
   5.000   0.8951   0.02879   0.01726  -0.0678   0.4884   1.0000
   5.250   0.9148   0.02946   0.01795  -0.0668   0.4779   1.0000
   5.500   0.9435   0.02961   0.01800  -0.0665   0.4697   1.0000
   5.750   0.9599   0.03045   0.01892  -0.0652   0.4586   1.0000
   6.000   0.9860   0.03078   0.01919  -0.0647   0.4503   1.0000
   6.250   1.0043   0.03151   0.01997  -0.0636   0.4400   1.0000
   6.500   1.0257   0.03210   0.02056  -0.0628   0.4309   1.0000
   6.750   1.0475   0.03266   0.02114  -0.0620   0.4218   1.0000
   7.000   1.0649   0.03348   0.02201  -0.0608   0.4123   1.0000
   7.250   1.0891   0.03389   0.02239  -0.0602   0.4038   1.0000
   7.500   1.1025   0.03496   0.02357  -0.0587   0.3944   1.0000
   7.750   1.1283   0.03527   0.02384  -0.0582   0.3864   1.0000
   8.000   1.1374   0.03657   0.02526  -0.0564   0.3770   1.0000
   8.250   1.1645   0.03684   0.02550  -0.0560   0.3695   1.0000
   8.500   1.1689   0.03838   0.02719  -0.0539   0.3602   1.0000
   8.750   1.1964   0.03860   0.02736  -0.0535   0.3529   1.0000
   9.000   1.1956   0.04043   0.02937  -0.0511   0.3442   1.0000
   9.250   1.2216   0.04073   0.02964  -0.0506   0.3369   1.0000
   9.500   1.2154   0.04276   0.03185  -0.0477   0.3290   1.0000
   9.750   1.2354   0.04338   0.03247  -0.0468   0.3218   1.0000
  10.000   1.2327   0.04544   0.03466  -0.0446   0.3146   1.0000
  10.250   1.2409   0.04684   0.03613  -0.0432   0.3073   1.0000
  10.500   1.2497   0.04828   0.03764  -0.0419   0.3006   1.0000
  10.750   1.2369   0.05145   0.04098  -0.0402   0.2934   1.0000
  11.000   1.2755   0.05062   0.04007  -0.0399   0.2874   1.0000
  11.250   1.2232   0.05761   0.04737  -0.0384   0.2801   1.0000
  11.500   1.2467   0.05780   0.04758  -0.0376   0.2740   1.0000
  11.750   1.2018   0.06549   0.05546  -0.0381   0.2668   1.0000
  12.000   1.1841   0.07072   0.06081  -0.0387   0.2598   1.0000
  12.250   1.2475   0.06584   0.05587  -0.0363   0.2558   1.0000
  12.500   1.1190   0.08701   0.07731  -0.0433   0.2433   1.0000
  12.750   1.1718   0.08214   0.07249  -0.0402   0.2412   1.0000
  13.000   1.0727   0.10259   0.09303  -0.0488   0.2272   1.0000
  13.250   1.1107   0.09941   0.08992  -0.0462   0.2254   1.0000
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