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UAG 88-143/20 (uag8814320-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: UAG 88-143/20 (uag8814320-il)
Reynolds number: 1,000,000
Max Cl/Cd: 185.15 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-uag8814320-il-1000000.txt
Download as CSV file: xf-uag8814320-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: UAG 88-143/20                                   
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.0719   0.05044   0.04781  -0.1729   0.8039   0.0047
 -10.250  -0.0944   0.04608   0.04349  -0.1750   0.8020   0.0046
 -10.000  -0.1371   0.04017   0.03750  -0.1730   0.8000   0.0046
  -9.750  -0.1814   0.02972   0.02669  -0.1708   0.7981   0.0045
  -9.500  -0.1838   0.02685   0.02356  -0.1685   0.7968   0.0045
  -9.250  -0.1793   0.02489   0.02137  -0.1662   0.7953   0.0044
  -9.000  -0.1722   0.02303   0.01929  -0.1639   0.7943   0.0044
  -8.750  -0.1621   0.02138   0.01743  -0.1618   0.7932   0.0044
  -8.500  -0.1501   0.01986   0.01568  -0.1599   0.7918   0.0043
  -8.250  -0.1400   0.01801   0.01352  -0.1575   0.7904   0.0043
  -8.000  -0.1244   0.01668   0.01195  -0.1557   0.7891   0.0043
  -7.750  -0.1052   0.01572   0.01082  -0.1545   0.7879   0.0043
  -7.500  -0.0847   0.01486   0.00979  -0.1534   0.7868   0.0043
  -7.250  -0.0643   0.01392   0.00866  -0.1522   0.7857   0.0044
  -7.000  -0.0419   0.01319   0.00777  -0.1514   0.7847   0.0045
  -6.750  -0.0185   0.01256   0.00699  -0.1507   0.7838   0.0046
  -6.500   0.0061   0.01211   0.00641  -0.1502   0.7828   0.0049
  -6.250   0.0300   0.01171   0.00593  -0.1496   0.7816   0.0058
  -6.000   0.0545   0.01138   0.00556  -0.1491   0.7805   0.0064
  -5.750   0.0792   0.01110   0.00525  -0.1486   0.7792   0.0070
  -5.500   0.1039   0.01081   0.00497  -0.1481   0.7778   0.0098
  -5.250   0.1292   0.01056   0.00472  -0.1478   0.7764   0.0136
  -5.000   0.1556   0.01039   0.00451  -0.1476   0.7751   0.0151
  -4.750   0.1819   0.01018   0.00429  -0.1475   0.7739   0.0187
  -4.500   0.2086   0.00999   0.00413  -0.1474   0.7728   0.0230
  -4.250   0.2359   0.00984   0.00400  -0.1475   0.7717   0.0284
  -4.000   0.2636   0.00970   0.00384  -0.1476   0.7706   0.0326
  -3.750   0.2913   0.00959   0.00375  -0.1478   0.7695   0.0379
  -3.500   0.3186   0.00956   0.00369  -0.1479   0.7682   0.0405
  -3.250   0.3436   0.00942   0.00356  -0.1475   0.7668   0.0448
  -3.000   0.3693   0.00931   0.00349  -0.1472   0.7651   0.0498
  -2.750   0.3959   0.00924   0.00342  -0.1471   0.7634   0.0530
  -2.500   0.4224   0.00908   0.00327  -0.1470   0.7618   0.0598
  -2.250   0.4497   0.00895   0.00315  -0.1471   0.7603   0.0656
  -2.000   0.4772   0.00880   0.00300  -0.1472   0.7590   0.0740
  -1.750   0.5048   0.00864   0.00286  -0.1473   0.7576   0.0874
  -1.500   0.5319   0.00846   0.00276  -0.1474   0.7562   0.1186
  -1.250   0.5555   0.00822   0.00273  -0.1468   0.7543   0.1888
  -1.000   0.5783   0.00796   0.00270  -0.1461   0.7522   0.2622
  -0.750   0.5998   0.00757   0.00266  -0.1451   0.7500   0.3912
  -0.500   0.6192   0.00706   0.00262  -0.1437   0.7479   0.5640
  -0.250   0.6364   0.00657   0.00257  -0.1416   0.7458   0.7276
   0.000   0.6558   0.00620   0.00258  -0.1396   0.7439   0.8606
   0.250   0.7003   0.00615   0.00264  -0.1434   0.7423   0.9328
   0.500   0.7453   0.00619   0.00271  -0.1474   0.7402   0.9557
   0.750   0.7817   0.00623   0.00274  -0.1494   0.7376   0.9669
   1.000   0.8335   0.00632   0.00280  -0.1549   0.7353   0.9766
   1.250   0.8786   0.00636   0.00282  -0.1588   0.7329   0.9836
   1.500   0.9269   0.00638   0.00279  -0.1636   0.7307   0.9873
   1.750   0.9703   0.00643   0.00282  -0.1673   0.7281   0.9917
   2.000   1.0083   0.00645   0.00285  -0.1699   0.7248   0.9947
   2.250   1.0462   0.00642   0.00283  -0.1725   0.7211   0.9970
   2.500   1.0827   0.00639   0.00277  -0.1748   0.7175   0.9990
   2.750   1.1122   0.00639   0.00278  -0.1756   0.7136   1.0000
   3.000   1.1314   0.00641   0.00282  -0.1741   0.7088   1.0000
   3.250   1.1520   0.00643   0.00281  -0.1728   0.7042   1.0000
   3.500   1.1711   0.00647   0.00287  -0.1712   0.6992   1.0000
   3.750   1.1900   0.00651   0.00292  -0.1696   0.6938   1.0000
   4.000   1.2092   0.00657   0.00296  -0.1680   0.6886   1.0000
   4.250   1.2267   0.00664   0.00306  -0.1661   0.6823   1.0000
   4.500   1.2442   0.00672   0.00312  -0.1642   0.6764   1.0000
   4.750   1.2607   0.00681   0.00323  -0.1621   0.6692   1.0000
   5.000   1.2753   0.00693   0.00333  -0.1595   0.6618   1.0000
   5.250   1.2900   0.00704   0.00347  -0.1570   0.6538   1.0000
   5.500   1.3021   0.00719   0.00361  -0.1539   0.6454   1.0000
   5.750   1.3104   0.00737   0.00376  -0.1499   0.6353   1.0000
   6.000   1.3034   0.00760   0.00394  -0.1427   0.6200   1.0000
   6.250   1.3030   0.00788   0.00418  -0.1370   0.6053   1.0000
   6.500   1.3067   0.00822   0.00450  -0.1323   0.5922   1.0000
   6.750   1.2979   0.00893   0.00511  -0.1255   0.5665   1.0000
   7.000   1.2945   0.00979   0.00589  -0.1202   0.5429   1.0000
   7.250   1.2911   0.01091   0.00692  -0.1154   0.5177   1.0000
   7.500   1.2794   0.01256   0.00837  -0.1096   0.4802   1.0000
   7.750   1.2749   0.01397   0.00962  -0.1050   0.4461   1.0000
   8.000   1.2663   0.01562   0.01105  -0.1000   0.4049   1.0000
   8.250   1.2603   0.01719   0.01240  -0.0955   0.3649   1.0000
   8.500   1.2673   0.01818   0.01330  -0.0929   0.3421   1.0000
   8.750   1.2514   0.02036   0.01509  -0.0873   0.2786   1.0000
   9.000   1.2491   0.02195   0.01645  -0.0837   0.2370   1.0000
   9.250   1.2312   0.02450   0.01852  -0.0783   0.1616   1.0000
   9.500   1.2200   0.02681   0.02045  -0.0739   0.0999   1.0000
   9.750   1.2083   0.02929   0.02258  -0.0697   0.0417   1.0000
  10.000   1.2025   0.03151   0.02459  -0.0662   0.0055   1.0000
  10.250   1.2139   0.03261   0.02574  -0.0648   0.0043   1.0000
  10.500   1.2237   0.03385   0.02707  -0.0632   0.0035   1.0000
  10.750   1.2349   0.03502   0.02830  -0.0618   0.0033   1.0000
  11.000   1.2459   0.03621   0.02954  -0.0605   0.0031   1.0000
  11.250   1.2564   0.03743   0.03082  -0.0592   0.0031   1.0000
  11.500   1.2648   0.03887   0.03233  -0.0577   0.0030   1.0000
  11.750   1.2728   0.04035   0.03388  -0.0562   0.0029   1.0000
  12.000   1.2796   0.04197   0.03557  -0.0547   0.0029   1.0000
  12.250   1.2860   0.04365   0.03733  -0.0532   0.0028   1.0000
  12.500   1.2908   0.04550   0.03925  -0.0517   0.0028   1.0000
  12.750   1.2961   0.04733   0.04117  -0.0503   0.0028   1.0000
  13.000   1.2986   0.04948   0.04340  -0.0487   0.0028   1.0000
  13.250   1.3026   0.05152   0.04552  -0.0474   0.0027   1.0000
  13.500   1.3095   0.05331   0.04736  -0.0464   0.0026   1.0000
  13.750   1.3102   0.05571   0.04985  -0.0450   0.0026   1.0000
  14.000   1.3122   0.05805   0.05226  -0.0438   0.0025   1.0000
  14.250   1.3139   0.06046   0.05474  -0.0427   0.0025   1.0000
  14.500   1.3146   0.06302   0.05737  -0.0416   0.0024   1.0000
  14.750   1.3142   0.06572   0.06017  -0.0405   0.0025   1.0000
  15.000   1.3128   0.06855   0.06308  -0.0394   0.0025   1.0000
  15.250   1.3135   0.07118   0.06578  -0.0386   0.0024   1.0000
  15.500   1.3146   0.07383   0.06850  -0.0380   0.0023   1.0000
  15.750   1.3139   0.07669   0.07144  -0.0371   0.0024   1.0000
  16.000   1.3134   0.07950   0.07436  -0.0363   0.0024   1.0000
  16.250   1.3132   0.08224   0.07720  -0.0354   0.0025   1.0000
  16.500   1.3145   0.08494   0.07997  -0.0350   0.0024   1.0000
  16.750   1.3142   0.08784   0.08291  -0.0348   0.0022   1.0000
  17.000   1.3159   0.09046   0.08567  -0.0341   0.0024   1.0000
  17.250   1.3163   0.09317   0.08848  -0.0334   0.0024   1.0000
  17.500   1.3166   0.09595   0.09136  -0.0329   0.0024   1.0000
  17.750   1.3150   0.09909   0.09452  -0.0331   0.0022   1.0000
  18.000   1.3144   0.10227   0.09784  -0.0331   0.0023   1.0000
  18.250   1.3129   0.10537   0.10109  -0.0327   0.0024   1.0000
  18.500   1.3105   0.10886   0.10468  -0.0331   0.0024   1.0000
  18.750   1.2919   0.11429   0.11054  -0.0318   0.0028   1.0000
  19.000   1.3021   0.11630   0.11235  -0.0340   0.0023   1.0000
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