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UAG 88-143/20 (uag8814320-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: UAG 88-143/20 (uag8814320-il)
Reynolds number: 200,000
Max Cl/Cd: 55.14 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-uag8814320-il-200000.txt
Download as CSV file: xf-uag8814320-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.500   0.1216   0.10146   0.09724  -0.1643   0.9065   0.0354
 -11.250   0.1252   0.09901   0.09479  -0.1652   0.9050   0.0375
 -11.000   0.1282   0.09672   0.09252  -0.1664   0.9033   0.0387
 -10.750   0.1269   0.09487   0.09070  -0.1666   0.9013   0.0393
 -10.500   0.1162   0.09377   0.08968  -0.1671   0.8986   0.0403
 -10.250   0.1146   0.09179   0.08774  -0.1672   0.8964   0.0404
 -10.000   0.1124   0.08967   0.08565  -0.1676   0.8940   0.0405
  -9.750   0.1108   0.08729   0.08330  -0.1683   0.8915   0.0407
  -9.500   0.1117   0.08484   0.08087  -0.1690   0.8895   0.0408
  -9.250   0.1037   0.08326   0.07936  -0.1673   0.8867   0.0408
  -9.000   0.1092   0.07971   0.07584  -0.1635   0.8851   0.0431
  -8.750   0.1112   0.07881   0.07496  -0.1610   0.8821   0.0458
  -8.500   0.1055   0.07718   0.07337  -0.1599   0.8792   0.0469
  -8.250   0.1018   0.07504   0.07125  -0.1599   0.8767   0.0478
  -8.000   0.0707   0.07582   0.07214  -0.1530   0.8708   0.0479
  -7.750   0.0438   0.07601   0.07242  -0.1474   0.8656   0.0475
  -7.500   0.0329   0.07385   0.07026  -0.1473   0.8625   0.0479
  -7.250  -0.0520   0.07988   0.07648  -0.1262   0.8510   0.0455
  -7.000  -0.0471   0.07599   0.07255  -0.1300   0.8491   0.0457
  -5.000  -0.1875   0.05493   0.05057  -0.0964   0.8050   0.0291
  -4.750  -0.1875   0.05103   0.04634  -0.0936   0.8010   0.0285
  -4.500  -0.1713   0.04544   0.04009  -0.0926   0.7987   0.0281
  -4.250  -0.1451   0.04091   0.03464  -0.0918   0.7972   0.0296
  -4.000  -0.1123   0.03891   0.03234  -0.0928   0.7959   0.0356
  -3.750  -0.1218   0.03888   0.03212  -0.0870   0.7879   0.0379
  -3.500  -0.0944   0.03772   0.03062  -0.0868   0.7853   0.0441
  -3.250  -0.0612   0.03754   0.03028  -0.0878   0.7836   0.0498
  -3.000  -0.0503   0.03761   0.03017  -0.0854   0.7784   0.0557
  -2.750  -0.0344   0.03751   0.03005  -0.0839   0.7736   0.0598
  -2.500  -0.0038   0.03716   0.02949  -0.0842   0.7714   0.0652
  -2.250   0.0300   0.03596   0.02803  -0.0848   0.7701   0.0689
  -2.000   0.0550   0.03556   0.02761  -0.0844   0.7672   0.0743
  -1.500   0.0898   0.03509   0.02695  -0.0812   0.7580   0.0836
  -1.250   0.1241   0.03479   0.02663  -0.0822   0.7566   0.0938
  -1.000   0.1242   0.03509   0.02696  -0.0783   0.7486   0.0995
  -0.750   0.1519   0.03494   0.02675  -0.0782   0.7459   0.1092
  -0.500   0.1833   0.03447   0.02634  -0.0787   0.7443   0.1211
  -0.250   0.2169   0.03401   0.02597  -0.0794   0.7431   0.1432
   0.000   0.3199   0.03214   0.02681  -0.0962   0.7436   1.0000
   0.250   0.3189   0.03292   0.02748  -0.0921   0.7351   1.0000
   0.500   0.3489   0.03294   0.02733  -0.0925   0.7325   1.0000
   0.750   0.3830   0.03285   0.02708  -0.0934   0.7309   1.0000
   1.000   0.4183   0.03275   0.02684  -0.0945   0.7298   1.0000
   1.250   0.4147   0.03368   0.02771  -0.0902   0.7200   1.0000
   1.500   0.4478   0.03357   0.02749  -0.0910   0.7182   1.0000
   1.750   0.4828   0.03339   0.02722  -0.0920   0.7170   1.0000
   2.000   0.5190   0.03317   0.02690  -0.0932   0.7161   1.0000
   2.250   0.5156   0.03414   0.02784  -0.0890   0.7054   1.0000
   2.500   0.5504   0.03388   0.02752  -0.0900   0.7041   1.0000
   2.750   0.5861   0.03357   0.02715  -0.0911   0.7031   1.0000
   3.000   0.5851   0.03461   0.02817  -0.0874   0.6925   1.0000
   3.250   0.6193   0.03428   0.02780  -0.0882   0.6910   1.0000
   3.500   0.6547   0.03391   0.02740  -0.0892   0.6900   1.0000
   3.750   0.6913   0.03344   0.02690  -0.0904   0.6892   1.0000
   4.000   0.6899   0.03453   0.02799  -0.0867   0.6780   1.0000
   4.250   0.7256   0.03402   0.02747  -0.0877   0.6769   1.0000
   4.500   0.7629   0.03340   0.02685  -0.0888   0.6761   1.0000
   4.750   0.7638   0.03446   0.02792  -0.0855   0.6650   1.0000
   5.000   0.8000   0.03379   0.02727  -0.0865   0.6639   1.0000
   5.250   0.8371   0.03302   0.02651  -0.0875   0.6630   1.0000
   5.500   0.8741   0.03222   0.02575  -0.0885   0.6622   1.0000
   5.750   0.8764   0.03327   0.02683  -0.0854   0.6510   1.0000
   6.000   0.9129   0.03240   0.02600  -0.0863   0.6500   1.0000
   6.250   0.9510   0.03135   0.02502  -0.0874   0.6494   1.0000
   6.500   0.9893   0.03025   0.02397  -0.0884   0.6489   1.0000
   6.750   1.0295   0.02904   0.02283  -0.0897   0.6484   1.0000
   7.000   1.0320   0.03000   0.02383  -0.0865   0.6369   1.0000
   7.250   1.0726   0.02873   0.02266  -0.0878   0.6362   1.0000
   7.500   1.1157   0.02734   0.02136  -0.0896   0.6355   1.0000
   7.750   1.1618   0.02584   0.01996  -0.0917   0.6345   1.0000
   8.250   1.1849   0.02660   0.02089  -0.0872   0.6142   1.0000
   8.500   1.2272   0.02530   0.01968  -0.0888   0.6100   1.0000
   8.750   1.2491   0.02515   0.01963  -0.0878   0.6006   1.0000
   9.000   1.2953   0.02373   0.01830  -0.0900   0.5941   1.0000
   9.250   1.3069   0.02386   0.01845  -0.0874   0.5758   1.0000
   9.500   1.3173   0.02389   0.01839  -0.0845   0.5477   1.0000
   9.750   1.3212   0.02446   0.01884  -0.0809   0.5138   1.0000
  10.000   1.3219   0.02539   0.01955  -0.0772   0.4767   1.0000
  10.250   1.3227   0.02654   0.02057  -0.0737   0.4451   1.0000
  10.500   1.3207   0.02796   0.02183  -0.0702   0.4128   1.0000
  10.750   1.3108   0.02995   0.02357  -0.0659   0.3716   1.0000
  11.000   1.3020   0.03208   0.02548  -0.0620   0.3328   1.0000
  11.250   1.2884   0.03470   0.02782  -0.0580   0.2874   1.0000
  11.500   1.2695   0.03792   0.03066  -0.0538   0.2322   1.0000
  11.750   1.2480   0.04158   0.03384  -0.0497   0.1681   1.0000
  12.000   1.2277   0.04535   0.03712  -0.0462   0.1024   1.0000
  12.250   1.2077   0.04931   0.04060  -0.0429   0.0440   1.0000
  12.500   1.1972   0.05264   0.04372  -0.0404   0.0209   1.0000
  12.750   1.1992   0.05491   0.04608  -0.0389   0.0171   1.0000
  13.000   1.2000   0.05736   0.04863  -0.0375   0.0150   1.0000
  13.250   1.1982   0.06018   0.05161  -0.0360   0.0138   1.0000
  13.500   1.1980   0.06286   0.05443  -0.0348   0.0135   1.0000
  13.750   1.1979   0.06560   0.05736  -0.0337   0.0130   1.0000
  14.000   1.1967   0.06853   0.06044  -0.0327   0.0126   1.0000
  14.250   1.1953   0.07153   0.06357  -0.0318   0.0124   1.0000
  14.500   1.1927   0.07471   0.06688  -0.0309   0.0122   1.0000
  14.750   1.1919   0.07768   0.06996  -0.0302   0.0120   1.0000
  15.000   1.1908   0.08070   0.07309  -0.0295   0.0118   1.0000
  15.250   1.1917   0.08345   0.07594  -0.0287   0.0116   1.0000
  15.500   1.1950   0.08588   0.07846  -0.0280   0.0116   1.0000
  15.750   1.2003   0.08799   0.08067  -0.0270   0.0116   1.0000
  16.000   1.2083   0.08971   0.08248  -0.0260   0.0115   1.0000
  16.250   1.2183   0.09122   0.08411  -0.0249   0.0116   1.0000
  16.500   1.2297   0.09266   0.08569  -0.0237   0.0117   1.0000
  16.750   1.2405   0.09436   0.08756  -0.0226   0.0120   1.0000
  17.000   1.2477   0.09668   0.09011  -0.0218   0.0122   1.0000
  17.250   1.2512   0.09964   0.09331  -0.0212   0.0124   1.0000
  17.500   1.2505   0.10326   0.09717  -0.0209   0.0127   1.0000
  17.750   1.2464   0.10751   0.10166  -0.0209   0.0131   1.0000
  18.000   1.2487   0.11147   0.10583  -0.0206   0.0136   1.0000
  18.250   1.2448   0.11501   0.10952  -0.0214   0.0138   1.0000
  18.500   1.2381   0.11909   0.11379  -0.0227   0.0141   1.0000
  18.750   1.2249   0.12456   0.11954  -0.0245   0.0145   1.0000
  19.000   1.2011   0.13245   0.12782  -0.0275   0.0154   1.0000
  19.250   1.1757   0.14096   0.13664  -0.0315   0.0159   1.0000
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