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RG 14 10% AIRFOIL (rg1410-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: RG 14 10% AIRFOIL (rg1410-il)
Reynolds number: 1,000,000
Max Cl/Cd: 89.44 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-rg1410-il-1000000.txt
Download as CSV file: xf-rg1410-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.9183   0.05545   0.05316  -0.0505   1.0000   0.0082
 -13.500  -0.9504   0.04468   0.04215  -0.0604   1.0000   0.0081
 -13.250  -0.9622   0.04022   0.03754  -0.0631   1.0000   0.0082
 -13.000  -0.9790   0.03638   0.03350  -0.0634   1.0000   0.0082
 -12.750  -0.9894   0.03390   0.03088  -0.0619   1.0000   0.0083
 -12.500  -1.0020   0.03187   0.02869  -0.0584   1.0000   0.0083
 -12.250  -1.0041   0.03076   0.02746  -0.0548   1.0000   0.0084
 -12.000  -1.0010   0.02941   0.02597  -0.0522   1.0000   0.0085
 -11.750  -1.0177   0.02600   0.02222  -0.0475   1.0000   0.0088
 -11.500  -1.0130   0.02439   0.02044  -0.0447   1.0000   0.0089
 -11.250  -1.0012   0.02343   0.01940  -0.0426   1.0000   0.0092
 -11.000  -0.9870   0.02265   0.01855  -0.0407   1.0000   0.0094
 -10.750  -0.9709   0.02205   0.01790  -0.0390   1.0000   0.0096
 -10.500  -0.9542   0.02149   0.01728  -0.0374   1.0000   0.0099
 -10.250  -0.9385   0.02077   0.01646  -0.0356   1.0000   0.0102
 -10.000  -0.9221   0.02008   0.01568  -0.0338   1.0000   0.0106
  -9.750  -0.9053   0.01945   0.01495  -0.0321   1.0000   0.0109
  -9.500  -0.8864   0.01910   0.01453  -0.0306   1.0000   0.0112
  -9.250  -0.8675   0.01878   0.01414  -0.0291   1.0000   0.0114
  -9.000  -0.8591   0.01677   0.01193  -0.0263   1.0000   0.0121
  -8.750  -0.8326   0.01617   0.01129  -0.0265   0.9992   0.0126
  -8.500  -0.8002   0.01573   0.01080  -0.0278   0.9978   0.0131
  -8.250  -0.7677   0.01520   0.01022  -0.0291   0.9963   0.0138
  -8.000  -0.7344   0.01474   0.00969  -0.0305   0.9950   0.0145
  -7.750  -0.7004   0.01441   0.00929  -0.0320   0.9938   0.0150
  -7.500  -0.6727   0.01319   0.00796  -0.0325   0.9912   0.0159
  -7.250  -0.6405   0.01270   0.00745  -0.0337   0.9889   0.0169
  -7.000  -0.6070   0.01230   0.00703  -0.0351   0.9870   0.0177
  -6.750  -0.5730   0.01185   0.00653  -0.0366   0.9855   0.0186
  -6.500  -0.5382   0.01148   0.00612  -0.0382   0.9842   0.0193
  -6.250  -0.5071   0.01086   0.00544  -0.0390   0.9820   0.0204
  -6.000  -0.4782   0.01034   0.00489  -0.0394   0.9780   0.0219
  -5.750  -0.4452   0.00998   0.00451  -0.0406   0.9755   0.0230
  -5.500  -0.4107   0.00965   0.00415  -0.0420   0.9736   0.0243
  -5.250  -0.3752   0.00935   0.00382  -0.0437   0.9721   0.0256
  -5.000  -0.3426   0.00889   0.00336  -0.0447   0.9692   0.0289
  -4.750  -0.3141   0.00861   0.00307  -0.0448   0.9631   0.0316
  -4.500  -0.2818   0.00824   0.00274  -0.0457   0.9589   0.0400
  -4.250  -0.2524   0.00789   0.00248  -0.0461   0.9525   0.0590
  -4.000  -0.2220   0.00762   0.00227  -0.0466   0.9455   0.0763
  -3.750  -0.1925   0.00735   0.00207  -0.0469   0.9372   0.0961
  -3.500  -0.1626   0.00711   0.00189  -0.0473   0.9283   0.1192
  -3.250  -0.1354   0.00689   0.00174  -0.0471   0.9165   0.1469
  -3.000  -0.1087   0.00663   0.00160  -0.0469   0.9039   0.1839
  -2.750  -0.0824   0.00640   0.00147  -0.0465   0.8907   0.2260
  -2.500  -0.0566   0.00616   0.00136  -0.0461   0.8769   0.2773
  -2.250  -0.0315   0.00586   0.00126  -0.0456   0.8628   0.3472
  -2.000  -0.0065   0.00558   0.00117  -0.0450   0.8484   0.4206
  -1.750   0.0186   0.00534   0.00110  -0.0445   0.8331   0.4880
  -1.500   0.0432   0.00509   0.00103  -0.0438   0.8175   0.5641
  -1.250   0.0678   0.00486   0.00098  -0.0430   0.8007   0.6351
  -1.000   0.0913   0.00465   0.00098  -0.0420   0.7820   0.7199
  -0.750   0.1159   0.00460   0.00101  -0.0411   0.7619   0.7752
  -0.500   0.1416   0.00464   0.00103  -0.0404   0.7407   0.8025
  -0.250   0.1676   0.00470   0.00104  -0.0398   0.7207   0.8210
   0.000   0.1939   0.00476   0.00106  -0.0393   0.7022   0.8351
   0.250   0.2202   0.00483   0.00108  -0.0388   0.6828   0.8468
   0.500   0.2462   0.00491   0.00111  -0.0382   0.6616   0.8577
   0.750   0.2723   0.00501   0.00114  -0.0377   0.6393   0.8686
   1.000   0.2980   0.00510   0.00118  -0.0371   0.6170   0.8781
   1.250   0.3241   0.00520   0.00122  -0.0366   0.5977   0.8863
   1.500   0.3501   0.00530   0.00127  -0.0360   0.5769   0.8948
   1.750   0.3754   0.00542   0.00132  -0.0354   0.5540   0.9031
   2.000   0.4011   0.00554   0.00138  -0.0348   0.5315   0.9120
   2.250   0.4260   0.00566   0.00144  -0.0340   0.5069   0.9196
   2.500   0.4509   0.00583   0.00151  -0.0334   0.4778   0.9277
   2.750   0.4750   0.00599   0.00160  -0.0325   0.4505   0.9359
   3.000   0.4993   0.00614   0.00168  -0.0316   0.4249   0.9453
   3.250   0.5233   0.00631   0.00178  -0.0307   0.4009   0.9554
   3.500   0.5494   0.00649   0.00189  -0.0302   0.3761   0.9642
   3.750   0.5771   0.00672   0.00201  -0.0302   0.3463   0.9731
   4.000   0.6084   0.00696   0.00215  -0.0311   0.3181   0.9795
   4.250   0.6398   0.00724   0.00230  -0.0320   0.2871   0.9845
   4.500   0.6730   0.00757   0.00248  -0.0334   0.2503   0.9873
   4.750   0.7053   0.00795   0.00269  -0.0347   0.2119   0.9904
   5.000   0.7364   0.00837   0.00293  -0.0357   0.1737   0.9941
   5.250   0.7698   0.00870   0.00316  -0.0372   0.1530   0.9968
   5.500   0.8032   0.00898   0.00338  -0.0386   0.1389   0.9995
   5.750   0.8232   0.00921   0.00357  -0.0372   0.1276   1.0000
   6.000   0.8430   0.00945   0.00376  -0.0357   0.1159   1.0000
   6.250   0.8644   0.00972   0.00398  -0.0345   0.1026   1.0000
   6.500   0.8865   0.01004   0.00422  -0.0335   0.0893   1.0000
   6.750   0.9095   0.01033   0.00448  -0.0326   0.0801   1.0000
   7.000   0.9331   0.01062   0.00476  -0.0319   0.0723   1.0000
   7.250   0.9560   0.01099   0.00507  -0.0311   0.0632   1.0000
   7.500   0.9798   0.01127   0.00535  -0.0304   0.0574   1.0000
   7.750   1.0032   0.01162   0.00567  -0.0297   0.0511   1.0000
   8.000   1.0267   0.01195   0.00600  -0.0290   0.0459   1.0000
   8.250   1.0498   0.01231   0.00636  -0.0283   0.0408   1.0000
   8.500   1.0729   0.01268   0.00671  -0.0276   0.0367   1.0000
   8.750   1.0954   0.01310   0.00712  -0.0268   0.0326   1.0000
   9.000   1.1184   0.01345   0.00749  -0.0261   0.0297   1.0000
   9.250   1.1396   0.01397   0.00800  -0.0251   0.0258   1.0000
   9.500   1.1626   0.01430   0.00837  -0.0244   0.0239   1.0000
   9.750   1.1834   0.01482   0.00887  -0.0234   0.0210   1.0000
  10.000   1.2047   0.01527   0.00937  -0.0224   0.0190   1.0000
  10.250   1.2251   0.01579   0.00988  -0.0214   0.0167   1.0000
  10.500   1.2443   0.01640   0.01054  -0.0201   0.0147   1.0000
  10.750   1.2641   0.01691   0.01109  -0.0190   0.0134   1.0000
  11.000   1.2796   0.01775   0.01196  -0.0172   0.0117   1.0000
  11.250   1.2985   0.01826   0.01253  -0.0160   0.0110   1.0000
  11.500   1.3163   0.01882   0.01314  -0.0146   0.0103   1.0000
  11.750   1.3315   0.01948   0.01384  -0.0128   0.0096   1.0000
  12.000   1.3407   0.02035   0.01478  -0.0101   0.0090   1.0000
  12.250   1.3485   0.02126   0.01579  -0.0072   0.0085   1.0000
  12.500   1.3601   0.02197   0.01657  -0.0050   0.0083   1.0000
  12.750   1.3701   0.02278   0.01746  -0.0027   0.0080   1.0000
  13.000   1.3785   0.02370   0.01847  -0.0004   0.0078   1.0000
  13.250   1.3859   0.02471   0.01956   0.0018   0.0075   1.0000
  13.500   1.3930   0.02578   0.02070   0.0039   0.0072   1.0000
  13.750   1.3967   0.02713   0.02214   0.0061   0.0070   1.0000
  14.000   1.3990   0.02866   0.02376   0.0081   0.0068   1.0000
  14.250   1.3918   0.03102   0.02625   0.0103   0.0065   1.0000
  14.500   1.3910   0.03308   0.02842   0.0116   0.0065   1.0000
  14.750   1.3795   0.03629   0.03178   0.0128   0.0063   1.0000
  15.000   1.3729   0.03937   0.03500   0.0132   0.0062   1.0000
  15.250   1.3709   0.04219   0.03794   0.0132   0.0062   1.0000
  15.500   1.3640   0.04581   0.04169   0.0126   0.0062   1.0000
  15.750   1.3616   0.04909   0.04509   0.0117   0.0061   1.0000
  16.000   1.3465   0.05432   0.05046   0.0098   0.0061   1.0000
  16.250   1.3374   0.05903   0.05530   0.0079   0.0060   1.0000
  16.500   1.3251   0.06449   0.06090   0.0053   0.0060   1.0000
  16.750   1.3153   0.06981   0.06634   0.0026   0.0059   1.0000
  17.000   1.2929   0.07748   0.07416  -0.0014   0.0060   1.0000
  17.250   1.2760   0.08455   0.08137  -0.0053   0.0059   1.0000
  17.500   1.2541   0.09277   0.08973  -0.0098   0.0059   1.0000
  17.750   1.2327   0.10118   0.09827  -0.0145   0.0060   1.0000
  18.000   1.2106   0.10998   0.10720  -0.0195   0.0060   1.0000
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