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GOE 502 AIRFOIL (goe502-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 502 AIRFOIL (goe502-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.2 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe502-il-1000000.txt
Download as CSV file: xf-goe502-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 502 AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.5864   0.08223   0.07970  -0.0980   0.9940   0.0325
 -15.250  -0.6242   0.07060   0.06786  -0.1085   0.9921   0.0327
 -15.000  -0.6385   0.06361   0.06076  -0.1151   0.9890   0.0328
 -14.750  -0.6414   0.05835   0.05541  -0.1210   0.9863   0.0330
 -14.500  -0.6479   0.05235   0.04928  -0.1283   0.9836   0.0330
 -14.250  -0.6423   0.04788   0.04473  -0.1346   0.9817   0.0332
 -14.000  -0.6438   0.04364   0.04040  -0.1392   0.9757   0.0333
 -13.750  -0.6361   0.03967   0.03635  -0.1449   0.9716   0.0335
 -13.500  -0.6236   0.03569   0.03226  -0.1516   0.9686   0.0337
 -13.250  -0.6140   0.03228   0.02876  -0.1566   0.9607   0.0339
 -13.000  -0.5898   0.02858   0.02492  -0.1650   0.9563   0.0341
 -12.750  -0.5604   0.02501   0.02119  -0.1750   0.9505   0.0344
 -12.500  -0.5353   0.02334   0.01940  -0.1786   0.9441   0.0347
 -12.250  -0.5060   0.02206   0.01799  -0.1818   0.9393   0.0350
 -12.000  -0.4888   0.02109   0.01693  -0.1819   0.9318   0.0353
 -11.750  -0.4656   0.02018   0.01591  -0.1828   0.9255   0.0355
 -11.500  -0.4442   0.01949   0.01512  -0.1828   0.9187   0.0358
 -11.250  -0.4243   0.01889   0.01442  -0.1823   0.9109   0.0360
 -11.000  -0.3992   0.01840   0.01382  -0.1826   0.9040   0.0362
 -10.750  -0.3870   0.01723   0.01260  -0.1810   0.8966   0.0368
 -10.500  -0.3653   0.01659   0.01190  -0.1806   0.8894   0.0371
 -10.250  -0.3435   0.01608   0.01135  -0.1800   0.8825   0.0374
 -10.000  -0.3214   0.01565   0.01087  -0.1793   0.8749   0.0377
  -9.750  -0.2968   0.01525   0.01040  -0.1790   0.8678   0.0381
  -9.500  -0.2744   0.01483   0.00995  -0.1782   0.8602   0.0385
  -9.250  -0.2505   0.01444   0.00949  -0.1777   0.8519   0.0389
  -9.000  -0.2265   0.01408   0.00906  -0.1772   0.8435   0.0394
  -8.750  -0.2025   0.01372   0.00863  -0.1766   0.8331   0.0398
  -8.500  -0.1783   0.01340   0.00824  -0.1760   0.8214   0.0402
  -8.250  -0.1541   0.01314   0.00788  -0.1753   0.8081   0.0405
  -7.750  -0.1084   0.01228   0.00685  -0.1737   0.7807   0.0415
  -7.500  -0.0843   0.01198   0.00649  -0.1731   0.7697   0.0421
  -7.250  -0.0595   0.01178   0.00621  -0.1725   0.7596   0.0427
  -7.000  -0.0339   0.01157   0.00596  -0.1720   0.7515   0.0434
  -6.750  -0.0082   0.01137   0.00569  -0.1716   0.7438   0.0440
  -6.500   0.0176   0.01120   0.00545  -0.1711   0.7370   0.0447
  -6.250   0.0445   0.01100   0.00522  -0.1708   0.7319   0.0453
  -6.000   0.0713   0.01087   0.00504  -0.1705   0.7262   0.0457
  -5.750   0.0960   0.01047   0.00458  -0.1700   0.7204   0.0467
  -5.500   0.1227   0.01024   0.00432  -0.1698   0.7156   0.0476
  -5.250   0.1498   0.01005   0.00411  -0.1695   0.7109   0.0485
  -5.000   0.1767   0.00990   0.00393  -0.1692   0.7061   0.0494
  -4.750   0.2035   0.00981   0.00378  -0.1689   0.7008   0.0504
  -4.500   0.2309   0.00971   0.00365  -0.1686   0.6962   0.0512
  -4.250   0.2577   0.00941   0.00333  -0.1684   0.6917   0.0528
  -4.000   0.2846   0.00925   0.00316  -0.1681   0.6867   0.0541
  -3.750   0.3113   0.00916   0.00301  -0.1677   0.6813   0.0555
  -3.500   0.3386   0.00906   0.00289  -0.1674   0.6764   0.0568
  -3.250   0.3658   0.00888   0.00270  -0.1671   0.6713   0.0590
  -3.000   0.3926   0.00875   0.00256  -0.1667   0.6656   0.0617
  -2.750   0.4188   0.00868   0.00244  -0.1662   0.6594   0.0655
  -2.500   0.4454   0.00835   0.00228  -0.1660   0.6541   0.0986
  -2.250   0.4717   0.00817   0.00220  -0.1656   0.6472   0.1300
  -2.000   0.4972   0.00811   0.00215  -0.1650   0.6400   0.1486
  -1.750   0.5244   0.00801   0.00212  -0.1647   0.6331   0.1652
  -1.500   0.5500   0.00798   0.00209  -0.1641   0.6243   0.1797
  -1.250   0.5762   0.00795   0.00208  -0.1636   0.6159   0.1933
  -1.000   0.6017   0.00795   0.00208  -0.1629   0.6059   0.2063
  -0.750   0.6273   0.00796   0.00209  -0.1623   0.5959   0.2185
  -0.250   0.6773   0.00804   0.00213  -0.1608   0.5748   0.2414
   0.000   0.7014   0.00811   0.00218  -0.1599   0.5649   0.2518
   0.250   0.7270   0.00817   0.00222  -0.1593   0.5560   0.2606
   0.500   0.7507   0.00826   0.00229  -0.1583   0.5470   0.2712
   0.750   0.7767   0.00831   0.00234  -0.1577   0.5400   0.2808
   1.000   0.8011   0.00839   0.00241  -0.1569   0.5329   0.2900
   1.250   0.8258   0.00848   0.00247  -0.1561   0.5265   0.2964
   1.500   0.8512   0.00852   0.00254  -0.1555   0.5207   0.3066
   1.750   0.8752   0.00862   0.00262  -0.1546   0.5144   0.3159
   2.000   0.8989   0.00870   0.00271  -0.1536   0.5089   0.3267
   2.250   0.9239   0.00874   0.00278  -0.1529   0.5045   0.3363
   2.500   0.9472   0.00880   0.00285  -0.1519   0.4993   0.3473
   2.750   0.9686   0.00892   0.00295  -0.1504   0.4932   0.3586
   3.000   0.9923   0.00896   0.00305  -0.1495   0.4879   0.3747
   3.250   1.0157   0.00901   0.00314  -0.1485   0.4822   0.3907
   3.500   1.0375   0.00913   0.00326  -0.1472   0.4766   0.4075
   3.750   1.0596   0.00924   0.00340  -0.1459   0.4716   0.4257
   4.000   1.0839   0.00929   0.00351  -0.1451   0.4673   0.4458
   4.250   1.1063   0.00939   0.00364  -0.1440   0.4618   0.4658
   4.500   1.1266   0.00955   0.00381  -0.1424   0.4555   0.4854
   4.750   1.1501   0.00961   0.00394  -0.1415   0.4514   0.5094
   5.000   1.1732   0.00966   0.00409  -0.1405   0.4470   0.5427
   5.250   1.1935   0.00967   0.00430  -0.1390   0.4419   0.6273
   5.500   1.2242   0.00932   0.00461  -0.1398   0.4355   1.0000
   5.750   1.2480   0.00944   0.00473  -0.1390   0.4305   1.0000
   6.000   1.2698   0.00961   0.00489  -0.1378   0.4247   1.0000
   6.250   1.2897   0.00985   0.00508  -0.1363   0.4189   1.0000
   6.500   1.3126   0.01000   0.00524  -0.1353   0.4141   1.0000
   6.750   1.3340   0.01020   0.00543  -0.1341   0.4078   1.0000
   7.000   1.3519   0.01050   0.00567  -0.1323   0.4000   1.0000
   7.250   1.3743   0.01068   0.00586  -0.1313   0.3934   1.0000
   7.500   1.3928   0.01097   0.00612  -0.1297   0.3855   1.0000
   7.750   1.4127   0.01123   0.00636  -0.1283   0.3789   1.0000
   8.000   1.4318   0.01153   0.00663  -0.1268   0.3707   1.0000
   8.250   1.4496   0.01187   0.00695  -0.1251   0.3632   1.0000
   8.500   1.4689   0.01217   0.00725  -0.1237   0.3556   1.0000
   8.750   1.4851   0.01260   0.00763  -0.1219   0.3472   1.0000
   9.000   1.5026   0.01298   0.00800  -0.1203   0.3368   1.0000
   9.250   1.5180   0.01347   0.00844  -0.1184   0.3264   1.0000
   9.500   1.5319   0.01403   0.00895  -0.1163   0.3150   1.0000
   9.750   1.5467   0.01457   0.00946  -0.1144   0.3026   1.0000
  10.000   1.5600   0.01520   0.01004  -0.1124   0.2899   1.0000
  10.250   1.5701   0.01600   0.01077  -0.1100   0.2739   1.0000
  10.500   1.5780   0.01695   0.01162  -0.1073   0.2547   1.0000
  10.750   1.5831   0.01808   0.01264  -0.1045   0.2344   1.0000
  11.000   1.5865   0.01936   0.01381  -0.1016   0.2131   1.0000
  11.250   1.5879   0.02082   0.01515  -0.0986   0.1919   1.0000
  11.500   1.5941   0.02207   0.01634  -0.0963   0.1796   1.0000
  11.750   1.6002   0.02337   0.01761  -0.0941   0.1700   1.0000
  12.000   1.6084   0.02459   0.01881  -0.0922   0.1627   1.0000
  12.250   1.6168   0.02586   0.02008  -0.0905   0.1566   1.0000
  12.500   1.6268   0.02705   0.02129  -0.0890   0.1519   1.0000
  12.750   1.6335   0.02852   0.02275  -0.0874   0.1463   1.0000
  13.000   1.6435   0.02980   0.02406  -0.0861   0.1426   1.0000
  13.250   1.6533   0.03113   0.02541  -0.0848   0.1387   1.0000
  13.500   1.6604   0.03271   0.02700  -0.0835   0.1343   1.0000
  13.750   1.6674   0.03432   0.02864  -0.0822   0.1301   1.0000
  14.000   1.6766   0.03578   0.03013  -0.0811   0.1263   1.0000
  14.250   1.6820   0.03759   0.03194  -0.0799   0.1219   1.0000
  14.500   1.6872   0.03946   0.03383  -0.0788   0.1173   1.0000
  14.750   1.6938   0.04120   0.03560  -0.0777   0.1130   1.0000
  15.000   1.6943   0.04353   0.03793  -0.0764   0.1074   1.0000
  15.250   1.6981   0.04559   0.04001  -0.0754   0.1018   1.0000
  15.500   1.6977   0.04808   0.04249  -0.0743   0.0956   1.0000
  15.750   1.6937   0.05099   0.04538  -0.0731   0.0879   1.0000
  16.000   1.6907   0.05384   0.04824  -0.0721   0.0811   1.0000
  16.250   1.6853   0.05701   0.05141  -0.0712   0.0744   1.0000
  16.500   1.6805   0.06019   0.05460  -0.0704   0.0696   1.0000
  16.750   1.6755   0.06345   0.05788  -0.0697   0.0655   1.0000
  17.000   1.6712   0.06670   0.06117  -0.0692   0.0627   1.0000
  17.250   1.6679   0.06991   0.06442  -0.0688   0.0601   1.0000
  17.500   1.6637   0.07326   0.06780  -0.0684   0.0581   1.0000
  17.750   1.6599   0.07665   0.07125  -0.0683   0.0564   1.0000
  18.000   1.6586   0.07974   0.07440  -0.0682   0.0549   1.0000
  18.250   1.6571   0.08289   0.07761  -0.0681   0.0538   1.0000
  18.500   1.6522   0.08656   0.08133  -0.0683   0.0524   1.0000
  18.750   1.6474   0.09024   0.08506  -0.0685   0.0511   1.0000
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