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RG 15A-1.8/11.0 AIRFOIL (rg15a111-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RG 15A-1.8/11.0 AIRFOIL (rg15a111-il)
Reynolds number: 1,000,000
Max Cl/Cd: 90.05 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rg15a111-il-1000000-n5.txt
Download as CSV file: xf-rg15a111-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RG 15A-1.8/11.0 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
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.8632   0.09280   0.09052  -0.0344   1.0000   0.0041
 -15.500  -0.9634   0.07032   0.06782  -0.0473   1.0000   0.0040
 -15.250  -1.0194   0.05497   0.05222  -0.0578   1.0000   0.0039
 -15.000  -1.0476   0.04595   0.04299  -0.0648   1.0000   0.0039
 -14.750  -1.0689   0.03978   0.03663  -0.0687   1.0000   0.0039
 -14.500  -1.0732   0.03662   0.03336  -0.0699   1.0000   0.0039
 -14.250  -1.0855   0.03311   0.02969  -0.0705   1.0000   0.0039
 -14.000  -1.0829   0.03142   0.02791  -0.0699   1.0000   0.0040
 -13.750  -1.0920   0.02922   0.02557  -0.0682   1.0000   0.0040
 -13.500  -1.0983   0.02784   0.02407  -0.0650   1.0000   0.0040
 -13.250  -1.1024   0.02671   0.02284  -0.0612   1.0000   0.0041
 -13.000  -1.0967   0.02565   0.02168  -0.0588   1.0000   0.0041
 -12.750  -1.0881   0.02470   0.02063  -0.0566   1.0000   0.0042
 -12.500  -1.0796   0.02365   0.01948  -0.0544   1.0000   0.0042
 -12.250  -1.0713   0.02249   0.01820  -0.0520   1.0000   0.0043
 -12.000  -1.0610   0.02140   0.01699  -0.0499   1.0000   0.0044
 -11.750  -1.0482   0.02047   0.01597  -0.0480   1.0000   0.0046
 -11.500  -1.0244   0.01957   0.01498  -0.0482   0.9992   0.0048
 -11.250  -0.9966   0.01880   0.01413  -0.0490   0.9979   0.0050
 -11.000  -0.9681   0.01810   0.01335  -0.0499   0.9965   0.0052
 -10.750  -0.9391   0.01741   0.01259  -0.0509   0.9952   0.0054
 -10.500  -0.9092   0.01678   0.01188  -0.0520   0.9941   0.0057
 -10.250  -0.8822   0.01615   0.01118  -0.0524   0.9923   0.0059
 -10.000  -0.8542   0.01559   0.01056  -0.0529   0.9902   0.0061
  -9.750  -0.8252   0.01505   0.00995  -0.0536   0.9883   0.0063
  -9.500  -0.7956   0.01443   0.00925  -0.0545   0.9864   0.0067
  -9.250  -0.7650   0.01392   0.00871  -0.0555   0.9849   0.0072
  -9.000  -0.7334   0.01350   0.00827  -0.0566   0.9837   0.0077
  -8.750  -0.7042   0.01315   0.00789  -0.0572   0.9816   0.0083
  -8.500  -0.6778   0.01277   0.00747  -0.0571   0.9777   0.0088
  -8.250  -0.6480   0.01243   0.00708  -0.0577   0.9749   0.0092
  -8.000  -0.6173   0.01194   0.00655  -0.0586   0.9725   0.0099
  -7.500  -0.5598   0.01122   0.00579  -0.0594   0.9650   0.0112
  -7.250  -0.5294   0.01091   0.00546  -0.0601   0.9608   0.0119
  -7.000  -0.4965   0.01060   0.00510  -0.0612   0.9575   0.0126
  -6.750  -0.4669   0.01034   0.00482  -0.0617   0.9513   0.0130
  -6.500  -0.4349   0.00991   0.00435  -0.0628   0.9453   0.0143
  -6.250  -0.4033   0.00960   0.00401  -0.0637   0.9376   0.0152
  -5.750  -0.3417   0.00911   0.00341  -0.0650   0.9161   0.0171
  -5.500  -0.3134   0.00890   0.00314  -0.0651   0.9028   0.0182
  -5.250  -0.2862   0.00869   0.00289  -0.0649   0.8889   0.0203
  -5.000  -0.2593   0.00852   0.00266  -0.0647   0.8751   0.0227
  -4.750  -0.2330   0.00830   0.00244  -0.0644   0.8608   0.0314
  -4.500  -0.2069   0.00810   0.00225  -0.0640   0.8464   0.0447
  -4.250  -0.1806   0.00796   0.00209  -0.0637   0.8319   0.0545
  -4.000  -0.1542   0.00784   0.00194  -0.0634   0.8171   0.0650
  -3.750  -0.1280   0.00768   0.00180  -0.0631   0.8021   0.0810
  -3.500  -0.1018   0.00754   0.00167  -0.0627   0.7872   0.1008
  -3.250  -0.0753   0.00742   0.00155  -0.0624   0.7724   0.1179
  -3.000  -0.0489   0.00729   0.00144  -0.0622   0.7579   0.1398
  -2.750  -0.0225   0.00715   0.00134  -0.0619   0.7433   0.1668
  -2.500   0.0041   0.00706   0.00126  -0.0616   0.7285   0.1896
  -2.250   0.0305   0.00692   0.00118  -0.0614   0.7133   0.2228
  -2.000   0.0566   0.00674   0.00110  -0.0611   0.6973   0.2713
  -1.750   0.0829   0.00659   0.00104  -0.0609   0.6816   0.3163
  -1.500   0.1091   0.00642   0.00098  -0.0606   0.6655   0.3706
  -1.000   0.1617   0.00614   0.00091  -0.0601   0.6334   0.4746
  -0.750   0.1882   0.00602   0.00089  -0.0599   0.6166   0.5266
  -0.500   0.2147   0.00594   0.00090  -0.0596   0.5999   0.5763
  -0.250   0.2414   0.00594   0.00092  -0.0594   0.5817   0.6114
   0.000   0.2683   0.00598   0.00095  -0.0591   0.5637   0.6352
   0.250   0.2953   0.00605   0.00098  -0.0589   0.5449   0.6527
   0.500   0.3223   0.00612   0.00102  -0.0587   0.5252   0.6671
   0.750   0.3492   0.00622   0.00107  -0.0585   0.5052   0.6795
   1.250   0.4030   0.00643   0.00118  -0.0580   0.4651   0.7018
   1.500   0.4299   0.00655   0.00124  -0.0578   0.4455   0.7117
   1.750   0.4567   0.00667   0.00132  -0.0576   0.4262   0.7221
   2.000   0.4834   0.00679   0.00140  -0.0573   0.4062   0.7324
   2.250   0.5101   0.00692   0.00148  -0.0571   0.3873   0.7419
   2.500   0.5367   0.00706   0.00158  -0.0568   0.3685   0.7520
   2.750   0.5632   0.00720   0.00168  -0.0566   0.3501   0.7621
   3.000   0.5893   0.00737   0.00180  -0.0563   0.3284   0.7722
   3.250   0.6152   0.00756   0.00193  -0.0559   0.3042   0.7829
   3.500   0.6410   0.00776   0.00206  -0.0555   0.2826   0.7931
   3.750   0.6670   0.00794   0.00220  -0.0552   0.2631   0.8015
   4.250   0.7190   0.00830   0.00250  -0.0545   0.2309   0.8191
   4.500   0.7447   0.00849   0.00266  -0.0541   0.2153   0.8287
   5.000   0.7948   0.00894   0.00304  -0.0532   0.1795   0.8510
   5.250   0.8186   0.00924   0.00328  -0.0525   0.1559   0.8638
   5.500   0.8424   0.00951   0.00350  -0.0517   0.1372   0.8791
   5.750   0.8661   0.00972   0.00372  -0.0509   0.1242   0.8971
   6.000   0.8885   0.00993   0.00394  -0.0498   0.1121   0.9200
   6.250   0.9119   0.01017   0.00419  -0.0490   0.0984   0.9544
   6.500   0.9446   0.01049   0.00447  -0.0503   0.0859   1.0000
   6.750   0.9691   0.01080   0.00474  -0.0498   0.0763   1.0000
   7.000   0.9935   0.01111   0.00502  -0.0493   0.0676   1.0000
   7.250   1.0178   0.01143   0.00532  -0.0488   0.0603   1.0000
   7.500   1.0414   0.01180   0.00564  -0.0481   0.0522   1.0000
   7.750   1.0653   0.01214   0.00596  -0.0476   0.0451   1.0000
   8.000   1.0883   0.01254   0.00633  -0.0469   0.0378   1.0000
   8.250   1.1109   0.01297   0.00671  -0.0461   0.0311   1.0000
   8.500   1.1338   0.01336   0.00710  -0.0454   0.0274   1.0000
   8.750   1.1563   0.01377   0.00750  -0.0446   0.0239   1.0000
   9.000   1.1791   0.01413   0.00788  -0.0439   0.0219   1.0000
   9.250   1.2009   0.01456   0.00831  -0.0430   0.0196   1.0000
   9.500   1.2226   0.01498   0.00875  -0.0422   0.0177   1.0000
   9.750   1.2445   0.01537   0.00917  -0.0413   0.0165   1.0000
  10.000   1.2653   0.01581   0.00963  -0.0403   0.0148   1.0000
  10.250   1.2852   0.01630   0.01013  -0.0392   0.0131   1.0000
  10.500   1.3052   0.01676   0.01062  -0.0381   0.0116   1.0000
  10.750   1.3233   0.01732   0.01119  -0.0367   0.0099   1.0000
  11.000   1.3412   0.01785   0.01175  -0.0353   0.0084   1.0000
  11.250   1.3558   0.01845   0.01237  -0.0333   0.0068   1.0000
  11.500   1.3694   0.01905   0.01301  -0.0312   0.0058   1.0000
  11.750   1.3814   0.01973   0.01373  -0.0289   0.0049   1.0000
  12.000   1.3943   0.02037   0.01443  -0.0268   0.0045   1.0000
  12.250   1.4061   0.02109   0.01520  -0.0246   0.0041   1.0000
  12.500   1.4167   0.02188   0.01604  -0.0225   0.0037   1.0000
  12.750   1.4265   0.02274   0.01697  -0.0203   0.0035   1.0000
  13.000   1.4351   0.02370   0.01800  -0.0181   0.0033   1.0000
  13.250   1.4428   0.02474   0.01912  -0.0160   0.0031   1.0000
  13.500   1.4513   0.02577   0.02024  -0.0141   0.0030   1.0000
  13.750   1.4584   0.02694   0.02149  -0.0123   0.0030   1.0000
  14.000   1.4642   0.02827   0.02290  -0.0106   0.0029   1.0000
  14.250   1.4700   0.02965   0.02438  -0.0091   0.0028   1.0000
  14.500   1.4735   0.03131   0.02612  -0.0076   0.0027   1.0000
  14.750   1.4764   0.03311   0.02802  -0.0064   0.0026   1.0000
  15.000   1.4785   0.03508   0.03009  -0.0054   0.0026   1.0000
  15.250   1.4791   0.03732   0.03243  -0.0047   0.0025   1.0000
  15.500   1.4787   0.03980   0.03501  -0.0042   0.0025   1.0000
  15.750   1.4772   0.04253   0.03785  -0.0041   0.0024   1.0000
  16.000   1.4734   0.04568   0.04111  -0.0042   0.0023   1.0000
  16.250   1.4693   0.04905   0.04459  -0.0047   0.0024   1.0000
  16.500   1.4623   0.05299   0.04865  -0.0057   0.0023   1.0000
  16.750   1.4550   0.05720   0.05298  -0.0070   0.0023   1.0000
  17.000   1.4443   0.06212   0.05804  -0.0089   0.0022   1.0000
  17.250   1.4309   0.06774   0.06380  -0.0113   0.0022   1.0000
  17.500   1.4157   0.07392   0.07012  -0.0142   0.0022   1.0000
  17.750   1.3995   0.08056   0.07690  -0.0175   0.0022   1.0000
  18.000   1.3827   0.08755   0.08402  -0.0211   0.0022   1.0000
  18.250   1.3605   0.09581   0.09243  -0.0255   0.0022   1.0000
  18.500   1.3374   0.10450   0.10128  -0.0303   0.0022   1.0000
  18.750   1.3135   0.11364   0.11057  -0.0355   0.0022   1.0000
  19.000   1.2890   0.12313   0.12019  -0.0410   0.0022   1.0000
  19.250   1.2629   0.13320   0.13041  -0.0469   0.0022   1.0000
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