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RG 15A 2.5/13.0 AIRFOIL (rg15a213-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RG 15A 2.5/13.0 AIRFOIL (rg15a213-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.06 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rg15a213-il-1000000-n5.txt
Download as CSV file: xf-rg15a213-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RG 15A 2.5/13.0 AIRFOIL                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.9039   0.08749   0.08473  -0.0536   1.0000   0.0064
 -16.750  -0.9633   0.07389   0.07094  -0.0612   1.0000   0.0063
 -16.500  -1.0104   0.06228   0.05913  -0.0680   1.0000   0.0062
 -16.250  -1.0420   0.05330   0.04997  -0.0737   1.0000   0.0062
 -16.000  -1.0636   0.04659   0.04309  -0.0779   1.0000   0.0061
 -15.750  -1.0779   0.04171   0.03807  -0.0805   1.0000   0.0061
 -15.500  -1.0894   0.03783   0.03406  -0.0818   1.0000   0.0062
 -15.250  -1.0964   0.03486   0.03101  -0.0822   1.0000   0.0063
 -15.000  -1.1020   0.03237   0.02841  -0.0818   1.0000   0.0063
 -14.750  -1.1068   0.03024   0.02619  -0.0808   1.0000   0.0064
 -14.500  -1.1089   0.02861   0.02449  -0.0793   1.0000   0.0065
 -14.250  -1.1132   0.02718   0.02298  -0.0769   1.0000   0.0066
 -14.000  -1.1213   0.02604   0.02176  -0.0733   1.0000   0.0066
 -13.750  -1.1263   0.02519   0.02085  -0.0694   0.9997   0.0067
 -13.500  -1.1027   0.02417   0.01976  -0.0704   0.9982   0.0069
 -13.250  -1.0779   0.02317   0.01869  -0.0715   0.9964   0.0071
 -13.000  -1.0520   0.02225   0.01769  -0.0726   0.9949   0.0073
 -12.750  -1.0253   0.02143   0.01680  -0.0737   0.9936   0.0075
 -12.500  -1.0033   0.02062   0.01590  -0.0737   0.9913   0.0077
 -12.250  -0.9781   0.01992   0.01514  -0.0742   0.9892   0.0079
 -12.000  -0.9512   0.01924   0.01438  -0.0749   0.9873   0.0081
 -11.750  -0.9234   0.01852   0.01360  -0.0758   0.9856   0.0083
 -11.500  -0.8946   0.01779   0.01283  -0.0769   0.9843   0.0086
 -11.250  -0.8640   0.01724   0.01224  -0.0781   0.9833   0.0090
 -11.000  -0.8426   0.01671   0.01166  -0.0774   0.9792   0.0092
 -10.750  -0.8156   0.01623   0.01115  -0.0777   0.9763   0.0096
 -10.500  -0.7868   0.01571   0.01059  -0.0784   0.9741   0.0099
 -10.250  -0.7566   0.01522   0.01005  -0.0793   0.9724   0.0102
 -10.000  -0.7255   0.01475   0.00952  -0.0804   0.9711   0.0105
  -9.750  -0.7047   0.01435   0.00908  -0.0792   0.9650   0.0107
  -9.500  -0.6773   0.01380   0.00849  -0.0796   0.9615   0.0111
  -9.250  -0.6469   0.01330   0.00796  -0.0805   0.9591   0.0115
  -9.000  -0.6170   0.01291   0.00754  -0.0812   0.9556   0.0120
  -8.750  -0.5889   0.01255   0.00715  -0.0815   0.9503   0.0125
  -8.500  -0.5561   0.01217   0.00674  -0.0827   0.9465   0.0130
  -8.250  -0.5226   0.01179   0.00632  -0.0841   0.9427   0.0134
  -8.000  -0.4918   0.01147   0.00595  -0.0849   0.9357   0.0137
  -7.750  -0.4585   0.01103   0.00546  -0.0863   0.9295   0.0144
  -7.500  -0.4290   0.01067   0.00506  -0.0868   0.9201   0.0151
  -7.250  -0.3989   0.01038   0.00473  -0.0874   0.9107   0.0158
  -7.000  -0.3704   0.01013   0.00441  -0.0876   0.8995   0.0164
  -6.750  -0.3432   0.00991   0.00414  -0.0875   0.8878   0.0170
  -6.500  -0.3162   0.00973   0.00389  -0.0873   0.8760   0.0174
  -6.250  -0.2901   0.00949   0.00359  -0.0870   0.8637   0.0188
  -6.000  -0.2640   0.00931   0.00335  -0.0866   0.8510   0.0201
  -5.750  -0.2379   0.00915   0.00314  -0.0862   0.8380   0.0214
  -5.500  -0.2122   0.00895   0.00292  -0.0858   0.8251   0.0258
  -5.250  -0.1869   0.00871   0.00270  -0.0853   0.8122   0.0398
  -5.000  -0.1612   0.00853   0.00253  -0.0849   0.7992   0.0503
  -4.750  -0.1353   0.00839   0.00237  -0.0845   0.7860   0.0595
  -4.500  -0.1094   0.00826   0.00223  -0.0841   0.7727   0.0704
  -4.250  -0.0831   0.00815   0.00211  -0.0838   0.7592   0.0805
  -4.000  -0.0568   0.00804   0.00199  -0.0834   0.7462   0.0906
  -3.750  -0.0304   0.00795   0.00188  -0.0831   0.7330   0.1003
  -3.500  -0.0041   0.00785   0.00177  -0.0828   0.7199   0.1143
  -3.250   0.0220   0.00772   0.00168  -0.0825   0.7065   0.1367
  -3.000   0.0481   0.00760   0.00159  -0.0821   0.6930   0.1605
  -2.500   0.1011   0.00742   0.00145  -0.0816   0.6661   0.2034
  -2.250   0.1275   0.00730   0.00138  -0.0813   0.6526   0.2359
  -2.000   0.1538   0.00716   0.00133  -0.0811   0.6396   0.2748
  -1.750   0.1802   0.00705   0.00128  -0.0808   0.6261   0.3111
  -1.500   0.2065   0.00693   0.00124  -0.0806   0.6126   0.3558
  -1.250   0.2331   0.00686   0.00122  -0.0803   0.5988   0.3886
  -1.000   0.2596   0.00676   0.00119  -0.0801   0.5850   0.4315
  -0.750   0.2862   0.00666   0.00118  -0.0799   0.5710   0.4762
  -0.500   0.3127   0.00657   0.00118  -0.0797   0.5569   0.5231
  -0.250   0.3390   0.00650   0.00122  -0.0794   0.5424   0.5798
   0.000   0.3658   0.00652   0.00126  -0.0791   0.5281   0.6123
   0.250   0.3928   0.00658   0.00131  -0.0789   0.5137   0.6297
   0.500   0.4198   0.00667   0.00135  -0.0787   0.4991   0.6412
   0.750   0.4467   0.00676   0.00140  -0.0784   0.4845   0.6529
   1.000   0.4736   0.00685   0.00147  -0.0782   0.4702   0.6655
   1.250   0.5004   0.00696   0.00153  -0.0779   0.4551   0.6762
   1.500   0.5272   0.00706   0.00160  -0.0777   0.4408   0.6851
   1.750   0.5539   0.00719   0.00167  -0.0774   0.4258   0.6927
   2.000   0.5804   0.00731   0.00176  -0.0771   0.4113   0.7014
   2.500   0.6334   0.00757   0.00194  -0.0766   0.3819   0.7169
   2.750   0.6599   0.00771   0.00204  -0.0763   0.3675   0.7243
   3.000   0.6862   0.00784   0.00215  -0.0760   0.3541   0.7324
   3.250   0.7124   0.00799   0.00226  -0.0756   0.3400   0.7403
   3.500   0.7384   0.00814   0.00239  -0.0753   0.3269   0.7484
   4.000   0.7901   0.00847   0.00265  -0.0745   0.2996   0.7602
   4.250   0.8151   0.00870   0.00281  -0.0740   0.2809   0.7660
   4.500   0.8398   0.00895   0.00298  -0.0735   0.2611   0.7716
   4.750   0.8650   0.00914   0.00314  -0.0730   0.2480   0.7773
   5.000   0.8904   0.00933   0.00331  -0.0726   0.2369   0.7836
   5.250   0.9153   0.00953   0.00348  -0.0721   0.2256   0.7901
   5.750   0.9635   0.01003   0.00390  -0.0708   0.1960   0.8051
   6.000   0.9871   0.01029   0.00413  -0.0701   0.1815   0.8134
   6.250   1.0105   0.01056   0.00436  -0.0693   0.1681   0.8219
   6.500   1.0337   0.01083   0.00460  -0.0686   0.1560   0.8320
   6.750   1.0568   0.01106   0.00485  -0.0677   0.1460   0.8435
   7.000   1.0789   0.01134   0.00512  -0.0668   0.1343   0.8568
   7.250   1.1003   0.01162   0.00540  -0.0656   0.1235   0.8723
   7.500   1.1204   0.01192   0.00569  -0.0642   0.1125   0.8921
   7.750   1.1382   0.01216   0.00598  -0.0623   0.1026   0.9243
   8.000   1.1639   0.01245   0.00629  -0.0622   0.0926   1.0000
   8.250   1.1854   0.01280   0.00661  -0.0612   0.0854   1.0000
   8.500   1.2062   0.01317   0.00695  -0.0601   0.0782   1.0000
   8.750   1.2267   0.01351   0.00728  -0.0589   0.0726   1.0000
   9.000   1.2452   0.01389   0.00763  -0.0574   0.0669   1.0000
   9.250   1.2639   0.01425   0.00798  -0.0559   0.0624   1.0000
   9.500   1.2817   0.01464   0.00837  -0.0543   0.0578   1.0000
   9.750   1.2988   0.01507   0.00879  -0.0526   0.0529   1.0000
  10.000   1.3150   0.01554   0.00924  -0.0508   0.0470   1.0000
  10.250   1.3309   0.01603   0.00972  -0.0490   0.0417   1.0000
  10.500   1.3447   0.01663   0.01028  -0.0469   0.0353   1.0000
  11.000   1.3728   0.01780   0.01145  -0.0430   0.0280   1.0000
  11.250   1.3866   0.01841   0.01206  -0.0411   0.0260   1.0000
  11.500   1.4004   0.01903   0.01271  -0.0393   0.0245   1.0000
  11.750   1.4148   0.01961   0.01333  -0.0376   0.0238   1.0000
  12.000   1.4284   0.02025   0.01402  -0.0359   0.0230   1.0000
  12.250   1.4410   0.02097   0.01477  -0.0341   0.0221   1.0000
  12.500   1.4519   0.02179   0.01563  -0.0322   0.0210   1.0000
  12.750   1.4625   0.02267   0.01654  -0.0304   0.0202   1.0000
  13.000   1.4737   0.02354   0.01746  -0.0288   0.0193   1.0000
  13.250   1.4850   0.02442   0.01840  -0.0273   0.0189   1.0000
  13.500   1.4955   0.02539   0.01943  -0.0258   0.0184   1.0000
  13.750   1.5050   0.02647   0.02056  -0.0243   0.0178   1.0000
  14.000   1.5134   0.02766   0.02180  -0.0229   0.0172   1.0000
  14.250   1.5206   0.02900   0.02318  -0.0215   0.0165   1.0000
  14.500   1.5266   0.03048   0.02472  -0.0202   0.0158   1.0000
  14.750   1.5338   0.03194   0.02624  -0.0191   0.0154   1.0000
  15.000   1.5407   0.03346   0.02784  -0.0182   0.0151   1.0000
  15.250   1.5466   0.03513   0.02958  -0.0173   0.0146   1.0000
  15.500   1.5515   0.03698   0.03149  -0.0166   0.0139   1.0000
  15.750   1.5553   0.03899   0.03357  -0.0160   0.0135   1.0000
  16.000   1.5572   0.04127   0.03591  -0.0155   0.0129   1.0000
  16.250   1.5586   0.04371   0.03842  -0.0152   0.0124   1.0000
  16.500   1.5607   0.04617   0.04096  -0.0151   0.0117   1.0000
  16.750   1.5607   0.04895   0.04382  -0.0152   0.0109   1.0000
  17.000   1.5601   0.05190   0.04685  -0.0155   0.0106   1.0000
  17.250   1.5563   0.05537   0.05039  -0.0160   0.0096   1.0000
  17.500   1.5529   0.05892   0.05403  -0.0167   0.0089   1.0000
  17.750   1.5469   0.06292   0.05810  -0.0177   0.0079   1.0000
  18.000   1.5387   0.06739   0.06265  -0.0191   0.0072   1.0000
  18.250   1.5293   0.07217   0.06753  -0.0207   0.0064   1.0000
  18.500   1.5177   0.07746   0.07293  -0.0227   0.0058   1.0000
  18.750   1.5056   0.08297   0.07854  -0.0250   0.0053   1.0000
  19.000   1.4918   0.08895   0.08463  -0.0276   0.0049   1.0000
  19.250   1.4793   0.09485   0.09065  -0.0303   0.0047   1.0000
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