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TsAGI R-3a (12%) (tsagi-r-3a-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: TsAGI R-3a (12%) (tsagi-r-3a-il)
Reynolds number: 1,000,000
Max Cl/Cd: 108.91 at α=8.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-tsagi-r-3a-il-1000000-n5.txt
Download as CSV file: xf-tsagi-r-3a-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: TsAGI R-3a (12%)                                
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.9542   0.04099   0.03852  -0.0361   1.0045   0.0090
 -12.000  -0.9627   0.03592   0.03314  -0.0373   1.0045   0.0090
 -11.750  -0.9578   0.03265   0.02962  -0.0373   1.0045   0.0090
 -11.500  -0.9464   0.03019   0.02696  -0.0371   1.0045   0.0091
 -11.250  -0.9308   0.02829   0.02488  -0.0366   1.0045   0.0091
 -11.000  -0.9132   0.02661   0.02304  -0.0362   1.0045   0.0092
 -10.750  -0.8940   0.02513   0.02140  -0.0357   1.0045   0.0093
 -10.500  -0.8734   0.02381   0.01995  -0.0352   1.0045   0.0094
 -10.250  -0.8520   0.02258   0.01858  -0.0347   1.0045   0.0095
 -10.000  -0.8245   0.02130   0.01713  -0.0354   0.9607   0.0096
  -9.750  -0.8053   0.02042   0.01597  -0.0338   0.8909   0.0096
  -9.500  -0.7850   0.01968   0.01489  -0.0325   0.8235   0.0097
  -9.250  -0.7623   0.01898   0.01388  -0.0317   0.7603   0.0098
  -9.000  -0.7383   0.01834   0.01294  -0.0312   0.6998   0.0099
  -8.750  -0.7136   0.01775   0.01207  -0.0307   0.6433   0.0099
  -8.500  -0.6882   0.01721   0.01129  -0.0303   0.5951   0.0100
  -8.250  -0.6624   0.01670   0.01057  -0.0300   0.5564   0.0101
  -8.000  -0.6363   0.01622   0.00992  -0.0296   0.5270   0.0102
  -7.750  -0.6098   0.01577   0.00932  -0.0293   0.5040   0.0103
  -7.500  -0.5830   0.01535   0.00877  -0.0290   0.4840   0.0104
  -7.250  -0.5560   0.01498   0.00827  -0.0287   0.4642   0.0104
  -7.000  -0.5301   0.01430   0.00746  -0.0284   0.4485   0.0106
  -6.750  -0.5032   0.01385   0.00691  -0.0281   0.4369   0.0108
  -6.500  -0.4759   0.01347   0.00646  -0.0278   0.4299   0.0110
  -6.000  -0.4207   0.01282   0.00570  -0.0273   0.4181   0.0113
  -5.750  -0.3929   0.01253   0.00535  -0.0271   0.4130   0.0115
  -5.500  -0.3651   0.01225   0.00502  -0.0269   0.4089   0.0117
  -5.000  -0.3090   0.01173   0.00442  -0.0265   0.4019   0.0121
  -4.750  -0.2808   0.01149   0.00415  -0.0263   0.3991   0.0123
  -4.500  -0.2526   0.01127   0.00389  -0.0261   0.3962   0.0125
  -4.250  -0.2243   0.01107   0.00365  -0.0259   0.3929   0.0127
  -4.000  -0.1959   0.01090   0.00344  -0.0257   0.3895   0.0129
  -3.750  -0.1676   0.01068   0.00319  -0.0256   0.3864   0.0133
  -3.500  -0.1392   0.01047   0.00297  -0.0254   0.3842   0.0138
  -3.250  -0.1107   0.01030   0.00279  -0.0253   0.3810   0.0144
  -3.000  -0.0821   0.01015   0.00262  -0.0252   0.3778   0.0150
  -2.750  -0.0535   0.01003   0.00247  -0.0250   0.3743   0.0156
  -2.500  -0.0249   0.00991   0.00233  -0.0249   0.3703   0.0166
  -2.250   0.0038   0.00978   0.00220  -0.0248   0.3669   0.0181
  -2.000   0.0324   0.00964   0.00210  -0.0247   0.3624   0.0236
  -1.750   0.0611   0.00957   0.00202  -0.0246   0.3569   0.0304
  -1.500   0.0899   0.00951   0.00195  -0.0245   0.3519   0.0341
  -1.250   0.1186   0.00943   0.00187  -0.0245   0.3467   0.0378
  -1.000   0.1473   0.00937   0.00180  -0.0244   0.3395   0.0424
  -0.750   0.1760   0.00931   0.00174  -0.0244   0.3322   0.0497
  -0.500   0.2044   0.00919   0.00168  -0.0243   0.3202   0.0764
  -0.250   0.2327   0.00916   0.00165  -0.0243   0.3011   0.1013
   0.000   0.2609   0.00919   0.00165  -0.0242   0.2810   0.1236
   0.250   0.2890   0.00912   0.00166  -0.0242   0.2700   0.1658
   0.500   0.3167   0.00895   0.00168  -0.0241   0.2621   0.2452
   0.750   0.3443   0.00868   0.00170  -0.0241   0.2566   0.3551
   1.000   0.3718   0.00844   0.00173  -0.0241   0.2519   0.4593
   1.250   0.3992   0.00825   0.00178  -0.0239   0.2472   0.5541
   1.500   0.4259   0.00800   0.00185  -0.0236   0.2429   0.6701
   1.750   0.4519   0.00776   0.00192  -0.0231   0.2401   0.7734
   2.000   0.4766   0.00759   0.00200  -0.0221   0.2367   0.8593
   2.250   0.5011   0.00753   0.00209  -0.0209   0.2330   0.9327
   2.500   0.5468   0.00764   0.00219  -0.0244   0.2276   0.9880
   2.750   0.5848   0.00773   0.00225  -0.0264   0.2251   0.9955
   3.000   0.6116   0.00783   0.00232  -0.0261   0.2224   0.9955
   3.250   0.6385   0.00794   0.00239  -0.0258   0.2197   0.9955
   3.500   0.6655   0.00807   0.00248  -0.0255   0.2166   0.9955
   3.750   0.6926   0.00821   0.00258  -0.0252   0.2134   0.9955
   4.000   0.7200   0.00832   0.00267  -0.0250   0.2116   0.9955
   4.250   0.7475   0.00842   0.00277  -0.0248   0.2100   0.9955
   4.500   0.7750   0.00853   0.00287  -0.0246   0.2083   0.9955
   4.750   0.8026   0.00865   0.00297  -0.0245   0.2065   0.9955
   5.000   0.8301   0.00878   0.00309  -0.0243   0.2046   0.9955
   5.250   0.8576   0.00892   0.00321  -0.0242   0.2026   0.9955
   5.500   0.8849   0.00908   0.00335  -0.0241   0.2003   0.9955
   5.750   0.9122   0.00925   0.00350  -0.0239   0.1977   0.9955
   6.000   0.9399   0.00936   0.00363  -0.0238   0.1963   0.9955
   6.250   0.9674   0.00948   0.00376  -0.0237   0.1944   0.9955
   6.500   0.9949   0.00962   0.00390  -0.0236   0.1923   0.9955
   6.750   1.0222   0.00977   0.00405  -0.0235   0.1898   0.9955
   7.000   1.0493   0.00994   0.00421  -0.0234   0.1870   0.9955
   7.250   1.0763   0.01014   0.00439  -0.0233   0.1840   0.9955
   7.500   1.1036   0.01028   0.00456  -0.0232   0.1820   0.9955
   7.750   1.1307   0.01044   0.00473  -0.0231   0.1789   0.9955
   8.000   1.1574   0.01065   0.00491  -0.0230   0.1729   0.9955
   8.250   1.1839   0.01087   0.00512  -0.0228   0.1672   0.9955
   8.500   1.2100   0.01113   0.00534  -0.0227   0.1590   0.9955
   8.750   1.2359   0.01142   0.00560  -0.0225   0.1511   0.9955
   9.000   1.2611   0.01177   0.00590  -0.0222   0.1427   0.9955
   9.500   1.3110   0.01250   0.00658  -0.0217   0.1289   0.9955
   9.750   1.3356   0.01287   0.00693  -0.0214   0.1241   0.9955
  10.000   1.3604   0.01321   0.00728  -0.0211   0.1202   0.9955
  10.250   1.3851   0.01354   0.00762  -0.0208   0.1162   0.9955
  10.500   1.4088   0.01397   0.00803  -0.0204   0.1116   0.9955
  10.750   1.4332   0.01430   0.00839  -0.0201   0.1086   0.9955
  11.000   1.4573   0.01464   0.00875  -0.0197   0.1058   0.9955
  11.250   1.4802   0.01509   0.00919  -0.0193   0.1016   0.9955
  11.500   1.5032   0.01551   0.00962  -0.0188   0.0978   0.9955
  11.750   1.5260   0.01592   0.01005  -0.0184   0.0943   0.9955
  12.000   1.5473   0.01645   0.01058  -0.0177   0.0900   0.9955
  12.250   1.5692   0.01689   0.01104  -0.0172   0.0862   0.9955
  12.500   1.5886   0.01754   0.01167  -0.0164   0.0802   0.9955
  12.750   1.6058   0.01831   0.01241  -0.0154   0.0715   0.9955
  13.000   1.6123   0.01987   0.01383  -0.0133   0.0516   0.9955
  13.250   1.6138   0.02162   0.01552  -0.0108   0.0379   0.9955
  13.500   1.6161   0.02289   0.01681  -0.0081   0.0327   0.9955
  13.750   1.6183   0.02429   0.01825  -0.0060   0.0288   0.9955
  14.000   1.6160   0.02628   0.02029  -0.0044   0.0231   0.9955
  14.250   1.5987   0.03029   0.02434  -0.0042   0.0136   0.9955
  14.500   1.5916   0.03416   0.02832  -0.0056   0.0116   0.9955
  14.750   1.5855   0.03841   0.03269  -0.0076   0.0110   0.9955
  15.000   1.5760   0.04323   0.03764  -0.0099   0.0105   0.9955
  15.250   1.5625   0.04850   0.04304  -0.0120   0.0103   0.9955
  15.500   1.5444   0.05420   0.04887  -0.0141   0.0101   0.9955
  15.750   1.5236   0.06014   0.05494  -0.0161   0.0100   0.9955
  16.000   1.5016   0.06612   0.06103  -0.0180   0.0100   0.9955
  16.250   1.4768   0.07248   0.06752  -0.0201   0.0099   0.9955
  16.500   1.4541   0.07880   0.07397  -0.0223   0.0099   0.9955
  16.750   1.4335   0.08507   0.08034  -0.0245   0.0098   0.9955
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