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UAG 88-143/20 (uag8814320-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: UAG 88-143/20 (uag8814320-il)
Reynolds number: 1,000,000
Max Cl/Cd: 169.26 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-uag8814320-il-1000000-n5.txt
Download as CSV file: xf-uag8814320-il-1000000-n5.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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500  -0.0092   0.04931   0.04655  -0.1708   0.7799   0.0034
  -9.250  -0.0515   0.04290   0.04011  -0.1709   0.7779   0.0034
  -9.000  -0.1308   0.02671   0.02338  -0.1674   0.7753   0.0034
  -8.750  -0.1320   0.02336   0.01969  -0.1648   0.7738   0.0034
  -8.500  -0.1261   0.02093   0.01692  -0.1624   0.7726   0.0033
  -8.250  -0.1141   0.01915   0.01485  -0.1605   0.7715   0.0032
  -8.000  -0.0990   0.01767   0.01307  -0.1587   0.7705   0.0030
  -7.750  -0.0799   0.01668   0.01188  -0.1576   0.7695   0.0030
  -7.500  -0.0591   0.01584   0.01086  -0.1566   0.7684   0.0029
  -7.250  -0.0375   0.01513   0.01001  -0.1558   0.7674   0.0029
  -7.000  -0.0151   0.01449   0.00924  -0.1550   0.7663   0.0028
  -6.750   0.0076   0.01390   0.00855  -0.1543   0.7652   0.0028
  -6.500   0.0307   0.01335   0.00791  -0.1536   0.7638   0.0028
  -6.250   0.0546   0.01287   0.00733  -0.1531   0.7625   0.0027
  -6.000   0.0786   0.01240   0.00679  -0.1525   0.7612   0.0027
  -5.750   0.1029   0.01195   0.00628  -0.1520   0.7600   0.0027
  -5.500   0.1276   0.01154   0.00580  -0.1516   0.7587   0.0027
  -5.250   0.1523   0.01114   0.00534  -0.1512   0.7575   0.0027
  -5.000   0.1775   0.01077   0.00491  -0.1508   0.7563   0.0026
  -4.750   0.2030   0.01045   0.00453  -0.1505   0.7551   0.0026
  -4.500   0.2282   0.01014   0.00418  -0.1501   0.7538   0.0026
  -4.250   0.2535   0.00988   0.00390  -0.1498   0.7523   0.0026
  -4.000   0.2787   0.00960   0.00359  -0.1494   0.7507   0.0026
  -3.750   0.3043   0.00937   0.00333  -0.1491   0.7490   0.0026
  -3.500   0.3301   0.00915   0.00307  -0.1488   0.7473   0.0026
  -3.250   0.3561   0.00897   0.00284  -0.1485   0.7457   0.0027
  -3.000   0.3823   0.00879   0.00263  -0.1483   0.7441   0.0027
  -2.750   0.4088   0.00865   0.00245  -0.1482   0.7426   0.0028
  -2.500   0.4352   0.00854   0.00230  -0.1481   0.7409   0.0029
  -2.250   0.4613   0.00844   0.00220  -0.1478   0.7390   0.0030
  -2.000   0.4875   0.00835   0.00211  -0.1477   0.7367   0.0032
  -1.750   0.5137   0.00825   0.00200  -0.1475   0.7343   0.0040
  -1.500   0.5396   0.00813   0.00189  -0.1473   0.7320   0.0135
  -1.250   0.5650   0.00796   0.00180  -0.1470   0.7299   0.0373
  -1.000   0.5903   0.00781   0.00176  -0.1467   0.7277   0.0655
  -0.750   0.6160   0.00774   0.00175  -0.1465   0.7250   0.0811
  -0.500   0.6410   0.00761   0.00173  -0.1461   0.7220   0.1148
  -0.250   0.6650   0.00742   0.00171  -0.1456   0.7190   0.1831
   0.000   0.6870   0.00710   0.00170  -0.1447   0.7161   0.3031
   0.250   0.7094   0.00687   0.00172  -0.1439   0.7129   0.4019
   0.500   0.7314   0.00665   0.00174  -0.1430   0.7092   0.4980
   0.750   0.7514   0.00639   0.00177  -0.1416   0.7055   0.6119
   1.000   0.7643   0.00600   0.00182  -0.1386   0.7016   0.7777
   1.250   0.8226   0.00580   0.00207  -0.1454   0.6980   0.9548
   1.500   0.8672   0.00589   0.00215  -0.1494   0.6937   0.9694
   1.750   0.9072   0.00600   0.00222  -0.1524   0.6894   0.9776
   2.000   0.9414   0.00610   0.00231  -0.1541   0.6848   0.9842
   2.250   0.9783   0.00618   0.00237  -0.1565   0.6795   0.9872
   2.500   1.0102   0.00628   0.00242  -0.1577   0.6737   0.9902
   2.750   1.0411   0.00637   0.00251  -0.1588   0.6668   0.9930
   3.000   1.0721   0.00649   0.00259  -0.1599   0.6597   0.9955
   3.250   1.1043   0.00658   0.00269  -0.1613   0.6519   0.9977
   3.500   1.1357   0.00671   0.00279  -0.1625   0.6441   0.9996
   3.750   1.1538   0.00686   0.00290  -0.1608   0.6345   1.0000
   4.000   1.1678   0.00698   0.00302  -0.1581   0.6261   1.0000
   4.250   1.1779   0.00716   0.00316  -0.1546   0.6166   1.0000
   4.500   1.1850   0.00735   0.00332  -0.1504   0.6061   1.0000
   4.750   1.1849   0.00753   0.00348  -0.1447   0.5950   1.0000
   5.000   1.1855   0.00777   0.00368  -0.1391   0.5829   1.0000
   5.250   1.1885   0.00808   0.00396  -0.1343   0.5701   1.0000
   5.500   1.1915   0.00849   0.00433  -0.1296   0.5557   1.0000
   5.750   1.1966   0.00898   0.00478  -0.1256   0.5422   1.0000
   6.000   1.2003   0.00964   0.00539  -0.1216   0.5259   1.0000
   6.250   1.2049   0.01043   0.00613  -0.1180   0.5090   1.0000
   6.500   1.2130   0.01120   0.00685  -0.1152   0.4939   1.0000
   6.750   1.2202   0.01206   0.00765  -0.1123   0.4765   1.0000
   7.000   1.2146   0.01350   0.00892  -0.1075   0.4401   1.0000
   7.250   1.2111   0.01490   0.01014  -0.1032   0.4055   1.0000
   7.500   1.2214   0.01569   0.01087  -0.1010   0.3887   1.0000
   7.750   1.2127   0.01740   0.01231  -0.0961   0.3404   1.0000
   8.000   1.2184   0.01845   0.01323  -0.0933   0.3139   1.0000
   8.250   1.2173   0.01989   0.01446  -0.0897   0.2763   1.0000
   8.500   1.2162   0.02138   0.01572  -0.0862   0.2345   1.0000
   8.750   1.2141   0.02302   0.01711  -0.0827   0.1912   1.0000
   9.000   1.2197   0.02426   0.01821  -0.0803   0.1625   1.0000
   9.250   1.2156   0.02613   0.01981  -0.0768   0.1172   1.0000
   9.500   1.2158   0.02782   0.02128  -0.0739   0.0794   1.0000
   9.750   1.2147   0.02965   0.02291  -0.0710   0.0437   1.0000
  10.000   1.2109   0.03173   0.02479  -0.0678   0.0077   1.0000
  10.250   1.2205   0.03296   0.02602  -0.0662   0.0031   1.0000
  10.500   1.2344   0.03390   0.02700  -0.0652   0.0028   1.0000
  10.750   1.2465   0.03498   0.02812  -0.0640   0.0021   1.0000
  11.000   1.2578   0.03614   0.02935  -0.0627   0.0019   1.0000
  11.250   1.2704   0.03721   0.03046  -0.0617   0.0018   1.0000
  11.500   1.2821   0.03837   0.03167  -0.0605   0.0016   1.0000
  11.750   1.2926   0.03965   0.03299  -0.0594   0.0014   1.0000
  12.000   1.3038   0.04087   0.03427  -0.0583   0.0013   1.0000
  12.250   1.3140   0.04220   0.03564  -0.0572   0.0012   1.0000
  12.500   1.3215   0.04376   0.03727  -0.0558   0.0011   1.0000
  12.750   1.3222   0.04594   0.03954  -0.0539   0.0008   1.0000
  13.000   1.3315   0.04741   0.04108  -0.0529   0.0008   1.0000
  13.250   1.3466   0.04837   0.04205  -0.0525   0.0008   1.0000
  13.500   1.3502   0.05041   0.04418  -0.0511   0.0007   1.0000
  13.750   1.3609   0.05180   0.04560  -0.0503   0.0007   1.0000
  14.000   1.3654   0.05379   0.04768  -0.0491   0.0006   1.0000
  14.250   1.3704   0.05577   0.04972  -0.0481   0.0006   1.0000
  14.500   1.3757   0.05776   0.05178  -0.0471   0.0006   1.0000
  14.750   1.3798   0.05990   0.05400  -0.0461   0.0006   1.0000
  15.000   1.3818   0.06229   0.05647  -0.0452   0.0005   1.0000
  15.250   1.3908   0.06396   0.05818  -0.0447   0.0005   1.0000
  15.500   1.3885   0.06686   0.06119  -0.0436   0.0005   1.0000
  15.750   1.3873   0.06972   0.06417  -0.0427   0.0005   1.0000
  16.000   1.3902   0.07218   0.06670  -0.0422   0.0005   1.0000
  16.250   1.3903   0.07498   0.06958  -0.0416   0.0005   1.0000
  16.500   1.3937   0.07742   0.07210  -0.0412   0.0004   1.0000
  16.750   1.3914   0.08059   0.07536  -0.0407   0.0004   1.0000
  17.000   1.3930   0.08330   0.07815  -0.0405   0.0004   1.0000
  17.250   1.3898   0.08667   0.08161  -0.0402   0.0004   1.0000
  17.500   1.3864   0.09012   0.08516  -0.0401   0.0004   1.0000
  17.750   1.3803   0.09400   0.08916  -0.0400   0.0004   1.0000
  18.000   1.3815   0.09693   0.09215  -0.0402   0.0004   1.0000
  18.250   1.3833   0.09978   0.09507  -0.0405   0.0003   1.0000
  18.500   1.3796   0.10341   0.09879  -0.0408   0.0003   1.0000
  18.750   1.3675   0.10830   0.10382  -0.0413   0.0003   1.0000
  19.000   1.3692   0.11127   0.10685  -0.0419   0.0003   1.0000
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