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RG 14 10% AIRFOIL (rg1410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: RG 14 10% AIRFOIL (rg1410-il)
Reynolds number: 1,000,000
Max Cl/Cd: 85.54 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rg1410-il-1000000-n5.txt
Download as CSV file: xf-rg1410-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RG 14 10% 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  -1.0841   0.05849   0.05594  -0.0507   1.0000   0.0049
 -15.500  -1.1371   0.04357   0.04067  -0.0636   1.0000   0.0048
 -15.250  -1.1500   0.03885   0.03580  -0.0664   1.0000   0.0048
 -15.000  -1.1635   0.03511   0.03189  -0.0671   1.0000   0.0048
 -14.750  -1.1701   0.03263   0.02927  -0.0664   1.0000   0.0049
 -14.500  -1.1736   0.03072   0.02725  -0.0647   1.0000   0.0049
 -14.250  -1.1786   0.02905   0.02544  -0.0621   1.0000   0.0049
 -14.000  -1.1808   0.02785   0.02414  -0.0587   1.0000   0.0050
 -13.750  -1.1777   0.02677   0.02296  -0.0557   1.0000   0.0052
 -13.500  -1.1705   0.02567   0.02175  -0.0534   1.0000   0.0053
 -13.250  -1.1611   0.02465   0.02062  -0.0512   1.0000   0.0054
 -13.000  -1.1501   0.02369   0.01956  -0.0492   1.0000   0.0055
 -12.750  -1.1378   0.02279   0.01855  -0.0472   1.0000   0.0056
 -12.500  -1.1244   0.02193   0.01758  -0.0453   1.0000   0.0057
 -12.250  -1.1099   0.02114   0.01670  -0.0435   1.0000   0.0058
 -12.000  -1.0954   0.02030   0.01575  -0.0416   1.0000   0.0060
 -11.750  -1.0802   0.01949   0.01486  -0.0398   1.0000   0.0064
 -11.500  -1.0633   0.01884   0.01415  -0.0382   1.0000   0.0066
 -11.250  -1.0452   0.01830   0.01356  -0.0368   1.0000   0.0069
 -11.000  -1.0272   0.01772   0.01293  -0.0352   1.0000   0.0072
 -10.750  -1.0088   0.01721   0.01235  -0.0338   1.0000   0.0075
 -10.500  -0.9816   0.01667   0.01175  -0.0341   0.9992   0.0079
 -10.250  -0.9526   0.01610   0.01109  -0.0348   0.9980   0.0082
 -10.000  -0.9230   0.01559   0.01051  -0.0356   0.9966   0.0084
  -9.750  -0.8930   0.01505   0.00994  -0.0365   0.9953   0.0091
  -9.500  -0.8619   0.01465   0.00952  -0.0376   0.9942   0.0097
  -9.250  -0.8333   0.01425   0.00909  -0.0380   0.9925   0.0102
  -9.000  -0.8043   0.01385   0.00863  -0.0385   0.9904   0.0107
  -8.750  -0.7746   0.01346   0.00819  -0.0391   0.9885   0.0112
  -8.500  -0.7440   0.01311   0.00779  -0.0399   0.9867   0.0115
  -8.250  -0.7132   0.01264   0.00726  -0.0409   0.9851   0.0120
  -8.000  -0.6814   0.01219   0.00679  -0.0420   0.9837   0.0128
  -7.750  -0.6535   0.01188   0.00646  -0.0421   0.9805   0.0135
  -7.500  -0.6248   0.01155   0.00610  -0.0424   0.9768   0.0141
  -7.250  -0.5938   0.01122   0.00573  -0.0432   0.9738   0.0147
  -7.000  -0.5614   0.01090   0.00538  -0.0443   0.9715   0.0152
  -6.750  -0.5327   0.01065   0.00510  -0.0446   0.9668   0.0156
  -6.500  -0.5040   0.01024   0.00464  -0.0448   0.9614   0.0164
  -6.250  -0.4720   0.00987   0.00426  -0.0458   0.9574   0.0173
  -6.000  -0.4426   0.00958   0.00395  -0.0462   0.9509   0.0182
  -5.750  -0.4108   0.00931   0.00365  -0.0471   0.9445   0.0191
  -5.500  -0.3803   0.00906   0.00336  -0.0477   0.9361   0.0199
  -5.250  -0.3498   0.00885   0.00310  -0.0482   0.9264   0.0205
  -5.000  -0.3213   0.00862   0.00283  -0.0483   0.9139   0.0221
  -4.750  -0.2941   0.00843   0.00260  -0.0481   0.8999   0.0244
  -4.500  -0.2672   0.00828   0.00241  -0.0478   0.8858   0.0271
  -4.250  -0.2408   0.00810   0.00222  -0.0475   0.8717   0.0335
  -4.000  -0.2146   0.00793   0.00205  -0.0471   0.8578   0.0436
  -3.750  -0.1884   0.00779   0.00189  -0.0467   0.8436   0.0541
  -3.500  -0.1622   0.00766   0.00176  -0.0463   0.8287   0.0647
  -3.250  -0.1360   0.00755   0.00163  -0.0459   0.8128   0.0768
  -3.000  -0.1100   0.00744   0.00152  -0.0454   0.7962   0.0920
  -2.750  -0.0840   0.00731   0.00140  -0.0450   0.7791   0.1126
  -2.500  -0.0581   0.00718   0.00131  -0.0446   0.7615   0.1384
  -2.250  -0.0323   0.00703   0.00121  -0.0442   0.7439   0.1708
  -2.000  -0.0064   0.00691   0.00113  -0.0438   0.7259   0.2035
  -1.750   0.0193   0.00677   0.00107  -0.0434   0.7080   0.2433
  -1.500   0.0450   0.00665   0.00101  -0.0429   0.6883   0.2847
  -1.250   0.0702   0.00656   0.00096  -0.0424   0.6622   0.3305
  -1.000   0.0958   0.00648   0.00092  -0.0420   0.6380   0.3726
  -0.750   0.1212   0.00633   0.00089  -0.0415   0.6176   0.4343
  -0.500   0.1465   0.00617   0.00087  -0.0411   0.5982   0.4989
  -0.250   0.1717   0.00604   0.00086  -0.0406   0.5757   0.5627
   0.000   0.1967   0.00593   0.00086  -0.0400   0.5515   0.6275
   0.250   0.2216   0.00579   0.00088  -0.0394   0.5325   0.6956
   0.500   0.2468   0.00575   0.00095  -0.0388   0.5141   0.7525
   0.750   0.2729   0.00578   0.00101  -0.0383   0.4973   0.7847
   1.000   0.2995   0.00585   0.00106  -0.0380   0.4808   0.8047
   1.250   0.3260   0.00595   0.00111  -0.0376   0.4596   0.8180
   1.500   0.3523   0.00609   0.00118  -0.0372   0.4350   0.8290
   1.750   0.3786   0.00621   0.00125  -0.0368   0.4131   0.8406
   2.000   0.4050   0.00634   0.00133  -0.0365   0.3940   0.8515
   2.250   0.4309   0.00649   0.00141  -0.0360   0.3682   0.8602
   2.750   0.4818   0.00691   0.00163  -0.0351   0.3072   0.8771
   3.000   0.5074   0.00709   0.00174  -0.0346   0.2834   0.8868
   3.250   0.5326   0.00728   0.00186  -0.0340   0.2600   0.8968
   3.500   0.5571   0.00751   0.00201  -0.0333   0.2321   0.9067
   3.750   0.5815   0.00772   0.00215  -0.0326   0.2072   0.9175
   4.000   0.6057   0.00797   0.00231  -0.0319   0.1807   0.9279
   4.250   0.6301   0.00821   0.00249  -0.0312   0.1599   0.9363
   4.500   0.6554   0.00842   0.00265  -0.0307   0.1470   0.9443
   4.750   0.6816   0.00859   0.00281  -0.0303   0.1380   0.9529
   5.000   0.7092   0.00878   0.00298  -0.0303   0.1283   0.9613
   5.500   0.7682   0.00928   0.00338  -0.0313   0.1000   0.9775
   5.750   0.7986   0.00956   0.00360  -0.0321   0.0873   0.9846
   6.000   0.8299   0.00984   0.00384  -0.0331   0.0781   0.9910
   6.250   0.8606   0.01013   0.00409  -0.0339   0.0700   0.9986
   6.500   0.8858   0.01036   0.00432  -0.0335   0.0646   1.0000
   6.750   0.9091   0.01066   0.00458  -0.0327   0.0578   1.0000
   7.000   0.9332   0.01091   0.00482  -0.0321   0.0535   1.0000
   7.250   0.9567   0.01122   0.00511  -0.0314   0.0477   1.0000
   7.500   0.9807   0.01150   0.00539  -0.0308   0.0431   1.0000
   7.750   1.0040   0.01185   0.00571  -0.0301   0.0375   1.0000
   8.000   1.0277   0.01217   0.00602  -0.0295   0.0335   1.0000
   8.250   1.0509   0.01252   0.00637  -0.0288   0.0297   1.0000
   8.500   1.0742   0.01287   0.00672  -0.0281   0.0270   1.0000
   8.750   1.0975   0.01321   0.00707  -0.0274   0.0248   1.0000
   9.000   1.1197   0.01363   0.00748  -0.0266   0.0216   1.0000
   9.250   1.1426   0.01398   0.00786  -0.0259   0.0201   1.0000
   9.500   1.1647   0.01439   0.00829  -0.0250   0.0180   1.0000
   9.750   1.1864   0.01483   0.00873  -0.0242   0.0161   1.0000
  10.000   1.2082   0.01524   0.00917  -0.0233   0.0144   1.0000
  10.250   1.2285   0.01575   0.00969  -0.0223   0.0124   1.0000
  10.500   1.2490   0.01623   0.01019  -0.0212   0.0106   1.0000
  10.750   1.2682   0.01679   0.01077  -0.0201   0.0088   1.0000
  11.000   1.2874   0.01732   0.01135  -0.0189   0.0080   1.0000
  11.250   1.3049   0.01795   0.01200  -0.0174   0.0068   1.0000
  11.500   1.3223   0.01855   0.01265  -0.0160   0.0062   1.0000
  11.750   1.3392   0.01913   0.01329  -0.0145   0.0059   1.0000
  12.000   1.3535   0.01972   0.01394  -0.0125   0.0056   1.0000
  12.250   1.3663   0.02035   0.01463  -0.0103   0.0054   1.0000
  12.500   1.3779   0.02104   0.01538  -0.0081   0.0051   1.0000
  12.750   1.3886   0.02181   0.01622  -0.0058   0.0048   1.0000
  13.000   1.3985   0.02263   0.01712  -0.0035   0.0047   1.0000
  13.250   1.4058   0.02364   0.01821  -0.0011   0.0044   1.0000
  13.500   1.4125   0.02472   0.01938   0.0011   0.0042   1.0000
  13.750   1.4209   0.02571   0.02045   0.0031   0.0041   1.0000
  14.000   1.4279   0.02683   0.02166   0.0049   0.0041   1.0000
  14.250   1.4335   0.02811   0.02303   0.0067   0.0040   1.0000
  14.500   1.4378   0.02956   0.02458   0.0083   0.0039   1.0000
  14.750   1.4423   0.03108   0.02619   0.0097   0.0038   1.0000
  15.000   1.4441   0.03292   0.02813   0.0109   0.0038   1.0000
  15.250   1.4452   0.03494   0.03027   0.0118   0.0037   1.0000
  15.500   1.4438   0.03736   0.03279   0.0125   0.0036   1.0000
  15.750   1.4440   0.03976   0.03529   0.0127   0.0036   1.0000
  16.000   1.4399   0.04281   0.03847   0.0126   0.0035   1.0000
  16.250   1.4347   0.04619   0.04197   0.0121   0.0034   1.0000
  16.500   1.4278   0.05003   0.04592   0.0111   0.0034   1.0000
  16.750   1.4198   0.05424   0.05025   0.0096   0.0033   1.0000
  17.000   1.4078   0.05927   0.05542   0.0075   0.0033   1.0000
  17.250   1.3937   0.06494   0.06124   0.0049   0.0033   1.0000
  17.500   1.3776   0.07123   0.06765   0.0017   0.0032   1.0000
  17.750   1.3581   0.07843   0.07501  -0.0021   0.0033   1.0000
  18.000   1.3293   0.08766   0.08441  -0.0073   0.0033   1.0000
  18.250   1.3001   0.09742   0.09434  -0.0128   0.0033   1.0000
  18.500   1.2661   0.10848   0.10557  -0.0191   0.0033   1.0000
  18.750   1.2276   0.12097   0.11824  -0.0263   0.0034   1.0000
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