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AG04 (ag04-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: AG04 (ag04-il)
Reynolds number: 100,000
Max Cl/Cd: 45.33 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ag04-il-100000-n5.txt
Download as CSV file: xf-ag04-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AG04                                            
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.000  -0.5765   0.11133   0.10650   0.0166   1.0000   0.0427
  -8.750  -0.5735   0.10727   0.10247   0.0145   1.0000   0.0426
  -8.500  -0.5718   0.10299   0.09824   0.0115   1.0000   0.0422
  -8.250  -0.5659   0.09706   0.09228   0.0102   1.0000   0.0270
  -8.000  -0.5625   0.09299   0.08825   0.0085   1.0000   0.0259
  -7.750  -0.5601   0.08866   0.08397   0.0059   1.0000   0.0249
  -7.500  -0.5567   0.08388   0.07924   0.0020   1.0000   0.0240
  -7.250  -0.5499   0.07823   0.07362  -0.0037   1.0000   0.0230
  -7.000  -0.5403   0.07136   0.06674  -0.0111   1.0000   0.0219
  -6.500  -0.5066   0.05268   0.04759  -0.0280   1.0000   0.0194
  -6.250  -0.4911   0.04661   0.04123  -0.0315   1.0000   0.0192
  -6.000  -0.4728   0.04084   0.03501  -0.0342   1.0000   0.0191
  -5.750  -0.4521   0.03572   0.02934  -0.0359   1.0000   0.0191
  -5.500  -0.4293   0.03145   0.02444  -0.0368   1.0000   0.0192
  -5.250  -0.4054   0.02773   0.02013  -0.0371   1.0000   0.0196
  -5.000  -0.3817   0.02525   0.01732  -0.0373   1.0000   0.0216
  -4.750  -0.3562   0.02363   0.01540  -0.0371   1.0000   0.0246
  -4.500  -0.3298   0.02152   0.01288  -0.0367   1.0000   0.0266
  -4.250  -0.3035   0.01974   0.01076  -0.0360   1.0000   0.0285
  -4.000  -0.2782   0.01820   0.00915  -0.0356   1.0000   0.0330
  -3.750  -0.2520   0.01721   0.00800  -0.0351   1.0000   0.0406
  -3.500  -0.2264   0.01615   0.00688  -0.0346   1.0000   0.0524
  -3.250  -0.2007   0.01520   0.00597  -0.0343   1.0000   0.0725
  -3.000  -0.1750   0.01448   0.00531  -0.0339   1.0000   0.1049
  -2.750  -0.1494   0.01385   0.00484  -0.0336   1.0000   0.1463
  -2.500  -0.1240   0.01328   0.00446  -0.0332   1.0000   0.1972
  -2.250  -0.0987   0.01275   0.00412  -0.0329   1.0000   0.2622
  -2.000  -0.0737   0.01224   0.00390  -0.0325   1.0000   0.3451
  -1.750  -0.0490   0.01172   0.00373  -0.0320   1.0000   0.4488
  -1.500  -0.0254   0.01111   0.00361  -0.0311   1.0000   0.5843
  -1.250  -0.0026   0.01018   0.00353  -0.0287   1.0000   0.8640
  -1.000   0.0297   0.01010   0.00332  -0.0297   1.0000   1.0000
  -0.750   0.0542   0.01016   0.00325  -0.0293   1.0000   1.0000
  -0.500   0.0902   0.01024   0.00318  -0.0312   0.9899   1.0000
  -0.250   0.1333   0.01031   0.00311  -0.0344   0.9717   1.0000
   0.000   0.1741   0.01036   0.00306  -0.0370   0.9505   1.0000
   0.250   0.2132   0.01041   0.00302  -0.0391   0.9266   1.0000
   0.500   0.2484   0.01046   0.00299  -0.0403   0.8985   1.0000
   0.750   0.2799   0.01052   0.00296  -0.0405   0.8669   1.0000
   1.000   0.3086   0.01061   0.00295  -0.0401   0.8333   1.0000
   1.250   0.3354   0.01072   0.00295  -0.0392   0.7982   1.0000
   1.500   0.3612   0.01087   0.00297  -0.0382   0.7622   1.0000
   1.750   0.3867   0.01105   0.00304  -0.0372   0.7255   1.0000
   2.000   0.4122   0.01126   0.00311  -0.0362   0.6886   1.0000
   2.250   0.4379   0.01150   0.00321  -0.0354   0.6509   1.0000
   2.500   0.4635   0.01176   0.00334  -0.0346   0.6126   1.0000
   2.750   0.4890   0.01204   0.00353  -0.0338   0.5741   1.0000
   3.000   0.5145   0.01236   0.00371  -0.0331   0.5353   1.0000
   3.250   0.5400   0.01270   0.00392  -0.0325   0.4967   1.0000
   3.500   0.5656   0.01307   0.00418  -0.0319   0.4582   1.0000
   3.750   0.5911   0.01346   0.00450  -0.0314   0.4209   1.0000
   4.000   0.6166   0.01389   0.00482  -0.0309   0.3851   1.0000
   4.250   0.6421   0.01433   0.00519  -0.0304   0.3501   1.0000
   4.500   0.6674   0.01482   0.00559  -0.0300   0.3169   1.0000
   4.750   0.6929   0.01531   0.00604  -0.0296   0.2844   1.0000
   5.000   0.7181   0.01584   0.00657  -0.0292   0.2535   1.0000
   5.250   0.7432   0.01641   0.00711  -0.0288   0.2235   1.0000
   5.500   0.7681   0.01702   0.00769  -0.0285   0.1949   1.0000
   5.750   0.7929   0.01769   0.00834  -0.0281   0.1674   1.0000
   6.000   0.8173   0.01842   0.00905  -0.0277   0.1405   1.0000
   6.250   0.8416   0.01923   0.00992  -0.0273   0.1161   1.0000
   6.500   0.8653   0.02015   0.01085  -0.0268   0.0942   1.0000
   6.750   0.8884   0.02120   0.01191  -0.0263   0.0763   1.0000
   7.000   0.9107   0.02242   0.01314  -0.0257   0.0621   1.0000
   7.250   0.9328   0.02367   0.01452  -0.0251   0.0511   1.0000
   7.500   0.9544   0.02508   0.01609  -0.0243   0.0425   1.0000
   7.750   0.9739   0.02687   0.01802  -0.0234   0.0369   1.0000
   8.000   0.9951   0.02830   0.01971  -0.0226   0.0310   1.0000
   8.250   1.0127   0.03048   0.02200  -0.0217   0.0278   1.0000
   8.500   1.0313   0.03281   0.02470  -0.0206   0.0252   1.0000
   8.750   1.0492   0.03479   0.02701  -0.0197   0.0219   1.0000
   9.000   1.0647   0.03709   0.02955  -0.0188   0.0200   1.0000
   9.250   1.0758   0.04028   0.03301  -0.0178   0.0189   1.0000
   9.500   1.0819   0.04447   0.03762  -0.0166   0.0182   1.0000
   9.750   1.0853   0.04839   0.04206  -0.0156   0.0178   1.0000
  10.000   1.0827   0.05258   0.04673  -0.0147   0.0173   1.0000
  10.250   1.0732   0.05696   0.05151  -0.0143   0.0169   1.0000
  10.500   1.0573   0.06141   0.05624  -0.0145   0.0169   1.0000
  10.750   1.0393   0.06696   0.06202  -0.0174   0.0170   1.0000
  11.000   1.0209   0.07395   0.06919  -0.0228   0.0172   1.0000
  11.250   1.0024   0.08234   0.07771  -0.0297   0.0176   1.0000
  11.500   0.9839   0.09155   0.08699  -0.0366   0.0180   1.0000
  11.750   0.9656   0.10104   0.09652  -0.0429   0.0183   1.0000
  12.000   0.9460   0.11194   0.10748  -0.0495   0.0187   1.0000
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