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Cambered plate C=12% T=5% R=1.1 (cp-120-050-gn) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Cambered plate C=12% T=5% R=1.1 (cp-120-050-gn)
Reynolds number: 1,000,000
Max Cl/Cd: 53.7 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-cp-120-050-gn-1000000-n5.txt
Download as CSV file: xf-cp-120-050-gn-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Cambered plate C=12% T=5% R=1.1                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.500   0.1575   0.10676   0.10428  -0.1819   0.9317   0.0164
 -11.250   0.1659   0.10449   0.10200  -0.1828   0.9281   0.0165
 -11.000   0.1730   0.10042   0.09790  -0.1852   0.9246   0.0172
 -10.750   0.1902   0.09832   0.09578  -0.1880   0.9218   0.0173
 -10.500   0.2091   0.09633   0.09377  -0.1911   0.9195   0.0175
 -10.000   0.2368   0.09240   0.08980  -0.1947   0.9131   0.0180
  -9.750   0.2493   0.09049   0.08788  -0.1961   0.9091   0.0185
  -9.500   0.2625   0.08807   0.08543  -0.1982   0.9055   0.0186
  -9.250   0.2778   0.08568   0.08301  -0.2007   0.9022   0.0189
  -9.000   0.2820   0.08234   0.07965  -0.2019   0.8977   0.0198
  -8.750   0.2948   0.08095   0.07825  -0.2027   0.8936   0.0199
  -8.500   0.3092   0.07944   0.07672  -0.2040   0.8895   0.0201
  -8.250   0.3221   0.07711   0.07436  -0.2059   0.8856   0.0201
  -8.000   0.3338   0.07596   0.07321  -0.2061   0.8817   0.0205
  -7.750   0.3442   0.07435   0.07159  -0.2066   0.8772   0.0208
  -7.500   0.3559   0.07263   0.06985  -0.2075   0.8728   0.0211
  -7.250   0.3671   0.07071   0.06790  -0.2085   0.8687   0.0215
  -7.000   0.3741   0.06896   0.06615  -0.2084   0.8642   0.0218
  -6.750   0.3772   0.06647   0.06364  -0.2085   0.8585   0.0226
  -6.500   0.3875   0.06502   0.06217  -0.2087   0.8541   0.0227
  -6.250   0.3958   0.06379   0.06094  -0.2082   0.8500   0.0228
  -6.000   0.4047   0.06291   0.06008  -0.2074   0.8453   0.0231
  -5.750   0.4106   0.06175   0.05890  -0.2063   0.8403   0.0233
  -5.500   0.4201   0.06052   0.05765  -0.2062   0.8360   0.0238
  -5.250   0.4287   0.05902   0.05616  -0.2062   0.8318   0.0241
  -5.000   0.4378   0.05738   0.05452  -0.2064   0.8269   0.0243
  -4.750   0.4488   0.05570   0.05281  -0.2070   0.8223   0.0246
  -4.500   0.4578   0.05299   0.05007  -0.2087   0.8179   0.0255
  -4.250   0.4718   0.05184   0.04894  -0.2090   0.8139   0.0256
  -4.000   0.4865   0.05065   0.04774  -0.2094   0.8095   0.0258
  -3.750   0.5023   0.04949   0.04656  -0.2099   0.8054   0.0261
  -3.500   0.5187   0.04804   0.04510  -0.2109   0.8017   0.0264
  -3.250   0.5350   0.04652   0.04358  -0.2119   0.7978   0.0267
  -3.000   0.5524   0.04493   0.04198  -0.2131   0.7935   0.0270
  -2.500   0.5953   0.04033   0.03728  -0.2185   0.7853   0.0286
  -2.250   0.6122   0.03926   0.03622  -0.2185   0.7790   0.0287
  -2.000   0.6306   0.03815   0.03507  -0.2187   0.7736   0.0289
  -1.750   0.6410   0.03725   0.03414  -0.2169   0.7641   0.0292
  -1.500   0.6551   0.03612   0.03296  -0.2161   0.7551   0.0295
  -1.250   0.6754   0.03473   0.03154  -0.2167   0.7483   0.0298
  -1.000   0.6963   0.03326   0.03002  -0.2175   0.7407   0.0302
  -0.750   0.7313   0.03024   0.02689  -0.2224   0.7341   0.0317
  -0.500   0.7489   0.02944   0.02606  -0.2215   0.7237   0.0319
  -0.250   0.7663   0.02868   0.02525  -0.2206   0.7129   0.0321
   0.000   0.7825   0.02783   0.02432  -0.2194   0.6998   0.0323
   0.250   0.7992   0.02701   0.02340  -0.2183   0.6843   0.0325
   0.500   0.8146   0.02620   0.02249  -0.2168   0.6636   0.0329
   0.750   0.8284   0.02545   0.02159  -0.2150   0.6376   0.0332
   1.000   0.8414   0.02476   0.02072  -0.2130   0.6073   0.0336
   1.250   0.8628   0.02295   0.01852  -0.2132   0.5599   0.0351
   1.500   0.8521   0.02376   0.01887  -0.2062   0.4729   0.0351
   1.750   0.8205   0.02615   0.02043  -0.1955   0.2953   0.0351
   2.000   0.7977   0.02840   0.02187  -0.1869   0.0482   0.0352
   2.250   0.8206   0.02805   0.02143  -0.1867   0.0318   0.0353
   2.500   0.8451   0.02763   0.02095  -0.1867   0.0284   0.0356
   2.750   0.8715   0.02702   0.02027  -0.1871   0.0267   0.0359
   3.000   0.8983   0.02635   0.01952  -0.1875   0.0258   0.0363
   3.500   0.9671   0.02276   0.01545  -0.1908   0.0241   0.0388
   3.750   0.9886   0.02248   0.01509  -0.1898   0.0235   0.0390
   4.000   1.0098   0.02226   0.01479  -0.1887   0.0232   0.0394
   4.250   1.0326   0.02171   0.01410  -0.1878   0.0231   0.0401
   4.500   1.0584   0.02018   0.01204  -0.1873   0.0229   0.0418
   4.750   1.0772   0.02031   0.01206  -0.1857   0.0228   0.0421
   5.000   1.0955   0.02043   0.01211  -0.1840   0.0224   0.0425
   5.250   1.1133   0.02073   0.01239  -0.1822   0.0222   0.0428
   5.500   1.1311   0.02110   0.01275  -0.1805   0.0220   0.0430
   5.750   1.1485   0.02150   0.01315  -0.1787   0.0218   0.0434
   6.000   1.1650   0.02196   0.01361  -0.1767   0.0218   0.0438
   6.250   1.1815   0.02242   0.01405  -0.1748   0.0215   0.0441
   6.500   1.1980   0.02289   0.01451  -0.1730   0.0215   0.0444
   6.750   1.2145   0.02338   0.01500  -0.1711   0.0213   0.0448
   7.000   1.2299   0.02394   0.01557  -0.1691   0.0211   0.0450
   7.250   1.2454   0.02452   0.01615  -0.1671   0.0210   0.0452
   7.500   1.2602   0.02517   0.01682  -0.1650   0.0209   0.0455
   7.750   1.2753   0.02582   0.01748  -0.1631   0.0208   0.0457
   8.000   1.2895   0.02653   0.01820  -0.1610   0.0207   0.0458
   8.250   1.3037   0.02727   0.01897  -0.1590   0.0205   0.0460
   8.500   1.3179   0.02804   0.01976  -0.1570   0.0204   0.0463
   8.750   1.3307   0.02891   0.02065  -0.1548   0.0203   0.0466
   9.000   1.3436   0.02979   0.02157  -0.1527   0.0201   0.0468
   9.250   1.3562   0.03072   0.02253  -0.1506   0.0200   0.0471
   9.500   1.3670   0.03182   0.02366  -0.1484   0.0198   0.0474
   9.750   1.3763   0.03306   0.02495  -0.1460   0.0195   0.0478
  10.000   1.3853   0.03438   0.02632  -0.1436   0.0193   0.0483
  10.250   1.3966   0.03553   0.02751  -0.1416   0.0192   0.0487
  10.500   1.4100   0.03652   0.02853  -0.1398   0.0192   0.0493
  10.750   1.4215   0.03770   0.02975  -0.1379   0.0191   0.0500
  11.000   1.4340   0.03879   0.03088  -0.1361   0.0190   0.0509
  11.250   1.4455   0.04001   0.03214  -0.1343   0.0189   0.0522
  11.500   1.4578   0.04117   0.03335  -0.1325   0.0188   0.0537
  11.750   1.4692   0.04244   0.03466  -0.1308   0.0187   0.0556
  12.000   1.4803   0.04374   0.03602  -0.1290   0.0186   0.0605
  12.250   1.4921   0.04500   0.03737  -0.1273   0.0185   0.0963
  12.500   1.5040   0.04619   0.03883  -0.1257   0.0183   0.3116
  13.000   1.5484   0.04895   0.04250  -0.1274   0.0180   1.0000
  13.250   1.5590   0.05030   0.04388  -0.1257   0.0179   1.0000
  13.500   1.5703   0.05159   0.04521  -0.1240   0.0178   1.0000
  13.750   1.5811   0.05297   0.04662  -0.1223   0.0177   1.0000
  14.000   1.5918   0.05436   0.04805  -0.1207   0.0176   1.0000
  14.250   1.6028   0.05571   0.04944  -0.1192   0.0175   1.0000
  14.500   1.6140   0.05705   0.05082  -0.1176   0.0173   1.0000
  14.750   1.6250   0.05845   0.05225  -0.1162   0.0172   1.0000
  15.000   1.6355   0.05990   0.05375  -0.1148   0.0171   1.0000
  15.250   1.6459   0.06140   0.05528  -0.1134   0.0169   1.0000
  15.500   1.6564   0.06287   0.05680  -0.1121   0.0168   1.0000
  15.750   1.6665   0.06442   0.05838  -0.1108   0.0167   1.0000
  16.000   1.6760   0.06603   0.06005  -0.1095   0.0166   1.0000
  16.250   1.6855   0.06766   0.06171  -0.1082   0.0165   1.0000
  16.500   1.6949   0.06930   0.06340  -0.1070   0.0164   1.0000
  16.750   1.7039   0.07101   0.06517  -0.1058   0.0164   1.0000
  17.000   1.7121   0.07285   0.06705  -0.1046   0.0163   1.0000
  17.250   1.7205   0.07466   0.06891  -0.1035   0.0162   1.0000
  17.500   1.7288   0.07648   0.07079  -0.1024   0.0161   1.0000
  17.750   1.7364   0.07842   0.07280  -0.1013   0.0160   1.0000
  18.000   1.7444   0.08039   0.07488  -0.1001   0.0158   1.0000
  18.250   1.7503   0.08257   0.07715  -0.0992   0.0157   1.0000
  18.500   1.7561   0.08477   0.07944  -0.0983   0.0157   1.0000
  18.750   1.7609   0.08712   0.08189  -0.0975   0.0156   1.0000
  19.000   1.7651   0.08956   0.08444  -0.0967   0.0156   1.0000
  19.250   1.7690   0.09205   0.08703  -0.0960   0.0155   1.0000
  19.500   1.7714   0.09476   0.08985  -0.0954   0.0154   1.0000
  19.750   1.7734   0.09753   0.09274  -0.0949   0.0154   1.0000
  20.000   1.7738   0.10056   0.09590  -0.0945   0.0153   1.0000
  20.250   1.7735   0.10369   0.09918  -0.0942   0.0152   1.0000
  20.500   1.7714   0.10715   0.10279  -0.0941   0.0151   1.0000
  20.750   1.7685   0.11071   0.10650  -0.0942   0.0150   1.0000
  21.000   1.7636   0.11462   0.11057  -0.0945   0.0148   1.0000
  21.250   1.7580   0.11866   0.11475  -0.0950   0.0147   1.0000
  21.500   1.7512   0.12292   0.11918  -0.0958   0.0145   1.0000
  21.750   1.7419   0.12766   0.12408  -0.0970   0.0144   1.0000
  22.000   1.7306   0.13279   0.12938  -0.0985   0.0143   1.0000
  22.250   1.7167   0.13851   0.13529  -0.1006   0.0142   1.0000
  22.500   1.6999   0.14489   0.14187  -0.1034   0.0140   1.0000
  22.750   1.6802   0.15203   0.14921  -0.1069   0.0139   1.0000
  23.000   1.6586   0.15982   0.15718  -0.1113   0.0138   1.0000
  23.250   1.6267   0.17023   0.16784  -0.1180   0.0137   1.0000
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