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SG6050 (sg6050-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: SG6050 (sg6050-il)
Reynolds number: 100,000
Max Cl/Cd: 52.45 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-sg6050-il-100000-n5.txt
Download as CSV file: xf-sg6050-il-100000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SG6050                                          
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.6019   0.09185   0.08667  -0.0544   1.0000   0.0324
 -13.250  -0.6805   0.07319   0.06770  -0.0658   1.0000   0.0302
 -13.000  -0.7117   0.06440   0.05868  -0.0716   1.0000   0.0300
 -12.750  -0.7298   0.05815   0.05228  -0.0759   1.0000   0.0303
 -12.500  -0.7436   0.05306   0.04702  -0.0793   1.0000   0.0308
 -12.250  -0.7560   0.04885   0.04263  -0.0814   1.0000   0.0316
 -12.000  -0.7692   0.04544   0.03903  -0.0817   1.0000   0.0326
 -11.500  -0.8008   0.04156   0.03496  -0.0757   1.0000   0.0342
 -11.250  -0.8131   0.04061   0.03401  -0.0715   1.0000   0.0351
 -11.000  -0.8159   0.03948   0.03278  -0.0690   0.9974   0.0368
 -10.750  -0.7948   0.03739   0.03043  -0.0709   0.9894   0.0407
 -10.500  -0.7694   0.03586   0.02865  -0.0731   0.9825   0.0454
 -10.250  -0.7445   0.03470   0.02736  -0.0747   0.9742   0.0498
 -10.000  -0.7183   0.03341   0.02573  -0.0764   0.9671   0.0557
  -9.750  -0.6909   0.03269   0.02492  -0.0780   0.9598   0.0613
  -9.500  -0.6646   0.03168   0.02370  -0.0792   0.9528   0.0670
  -9.250  -0.6374   0.03084   0.02269  -0.0803   0.9458   0.0726
  -9.000  -0.6090   0.02971   0.02135  -0.0815   0.9402   0.0776
  -8.750  -0.5832   0.02889   0.02046  -0.0820   0.9325   0.0820
  -8.500  -0.5534   0.02795   0.01921  -0.0830   0.9272   0.0870
  -8.250  -0.5284   0.02701   0.01826  -0.0832   0.9198   0.0908
  -8.000  -0.5008   0.02621   0.01737  -0.0837   0.9136   0.0951
  -7.750  -0.4723   0.02545   0.01641  -0.0842   0.9081   0.0997
  -7.500  -0.4482   0.02467   0.01560  -0.0840   0.9005   0.1035
  -7.250  -0.4208   0.02395   0.01483  -0.0843   0.8950   0.1079
  -7.000  -0.3952   0.02338   0.01414  -0.0842   0.8885   0.1131
  -6.750  -0.3701   0.02273   0.01346  -0.0841   0.8819   0.1183
  -6.500  -0.3428   0.02211   0.01277  -0.0843   0.8770   0.1246
  -6.250  -0.3186   0.02161   0.01221  -0.0840   0.8697   0.1317
  -6.000  -0.2928   0.02105   0.01162  -0.0840   0.8638   0.1420
  -5.750  -0.2661   0.02044   0.01102  -0.0841   0.8589   0.1559
  -5.500  -0.2418   0.01993   0.01055  -0.0839   0.8518   0.1759
  -5.250  -0.2160   0.01929   0.01010  -0.0840   0.8464   0.2129
  -5.000  -0.1897   0.01885   0.00991  -0.0841   0.8413   0.2706
  -4.750  -0.1638   0.01877   0.00989  -0.0839   0.8346   0.3158
  -4.500  -0.1356   0.01874   0.00977  -0.0840   0.8294   0.3462
  -4.250  -0.1075   0.01873   0.00965  -0.0840   0.8244   0.3689
  -4.000  -0.0808   0.01874   0.00959  -0.0840   0.8179   0.3870
  -3.750  -0.0527   0.01868   0.00945  -0.0840   0.8128   0.4037
  -3.500  -0.0246   0.01862   0.00931  -0.0840   0.8079   0.4198
  -3.250   0.0018   0.01861   0.00928  -0.0839   0.8013   0.4365
  -3.000   0.0293   0.01852   0.00920  -0.0838   0.7962   0.4559
  -2.750   0.0569   0.01844   0.00911  -0.0837   0.7913   0.4745
  -2.500   0.0834   0.01840   0.00908  -0.0836   0.7845   0.4881
  -2.250   0.1119   0.01829   0.00889  -0.0837   0.7793   0.4982
  -2.000   0.1399   0.01818   0.00877  -0.0837   0.7741   0.5068
  -1.750   0.1669   0.01815   0.00872  -0.0837   0.7673   0.5167
  -1.500   0.1952   0.01802   0.00858  -0.0837   0.7622   0.5262
  -1.250   0.2229   0.01797   0.00853  -0.0837   0.7565   0.5374
  -1.000   0.2498   0.01793   0.00852  -0.0836   0.7500   0.5498
  -0.750   0.2782   0.01780   0.00842  -0.0836   0.7451   0.5641
  -0.500   0.3046   0.01778   0.00847  -0.0834   0.7387   0.5813
  -0.250   0.3314   0.01772   0.00848  -0.0832   0.7323   0.6030
   0.000   0.3593   0.01755   0.00840  -0.0829   0.7277   0.6315
   0.250   0.3834   0.01754   0.00857  -0.0822   0.7203   0.6704
   0.500   0.4078   0.01739   0.00862  -0.0811   0.7144   0.7240
   0.750   0.4313   0.01724   0.00868  -0.0793   0.7093   0.7937
   1.000   0.4553   0.01732   0.00890  -0.0781   0.7014   0.8700
   1.250   0.4881   0.01727   0.00884  -0.0787   0.6959   0.9232
   1.500   0.5259   0.01735   0.00893  -0.0808   0.6884   0.9625
   1.750   0.5673   0.01737   0.00890  -0.0837   0.6816   0.9939
   2.000   0.5958   0.01740   0.00888  -0.0840   0.6750   1.0000
   2.250   0.6193   0.01755   0.00899  -0.0834   0.6672   1.0000
   2.500   0.6465   0.01755   0.00890  -0.0833   0.6615   1.0000
   2.750   0.6692   0.01778   0.00915  -0.0826   0.6527   1.0000
   3.000   0.6969   0.01779   0.00909  -0.0826   0.6466   1.0000
   3.250   0.7202   0.01803   0.00936  -0.0820   0.6376   1.0000
   3.500   0.7479   0.01806   0.00933  -0.0819   0.6310   1.0000
   3.750   0.7716   0.01829   0.00959  -0.0814   0.6218   1.0000
   4.000   0.7995   0.01832   0.00959  -0.0813   0.6148   1.0000
   4.250   0.8231   0.01858   0.00989  -0.0808   0.6051   1.0000
   4.500   0.8513   0.01862   0.00989  -0.0808   0.5980   1.0000
   4.750   0.8742   0.01891   0.01025  -0.0801   0.5878   1.0000
   5.000   0.9008   0.01904   0.01037  -0.0799   0.5795   1.0000
   5.250   0.9252   0.01927   0.01065  -0.0794   0.5698   1.0000
   5.500   0.9500   0.01949   0.01090  -0.0790   0.5604   1.0000
   5.750   0.9761   0.01965   0.01106  -0.0787   0.5513   1.0000
   6.000   0.9991   0.01995   0.01143  -0.0780   0.5405   1.0000
   6.250   1.0239   0.02017   0.01166  -0.0776   0.5304   1.0000
   6.500   1.0483   0.02039   0.01190  -0.0770   0.5196   1.0000
   6.750   1.0701   0.02073   0.01231  -0.0761   0.5074   1.0000
   7.000   1.0928   0.02104   0.01265  -0.0754   0.4957   1.0000
   7.250   1.1158   0.02133   0.01295  -0.0746   0.4842   1.0000
   7.500   1.1371   0.02168   0.01335  -0.0736   0.4718   1.0000
   7.750   1.1567   0.02210   0.01383  -0.0724   0.4586   1.0000
   8.000   1.1759   0.02253   0.01430  -0.0711   0.4453   1.0000
   8.250   1.1944   0.02298   0.01479  -0.0698   0.4319   1.0000
   8.500   1.2119   0.02347   0.01531  -0.0682   0.4184   1.0000
   8.750   1.2279   0.02400   0.01587  -0.0665   0.4046   1.0000
   9.000   1.2421   0.02459   0.01648  -0.0645   0.3904   1.0000
   9.250   1.2526   0.02525   0.01717  -0.0620   0.3760   1.0000
   9.500   1.2610   0.02601   0.01798  -0.0593   0.3612   1.0000
   9.750   1.2691   0.02687   0.01887  -0.0567   0.3462   1.0000
  10.000   1.2767   0.02784   0.01987  -0.0543   0.3308   1.0000
  10.250   1.2834   0.02893   0.02099  -0.0519   0.3152   1.0000
  10.500   1.2892   0.03016   0.02224  -0.0497   0.2993   1.0000
  10.750   1.2941   0.03152   0.02363  -0.0475   0.2832   1.0000
  11.000   1.2978   0.03305   0.02515  -0.0455   0.2669   1.0000
  11.250   1.3005   0.03474   0.02685  -0.0435   0.2505   1.0000
  11.500   1.3024   0.03659   0.02871  -0.0417   0.2338   1.0000
  11.750   1.3033   0.03860   0.03072  -0.0401   0.2172   1.0000
  12.000   1.3031   0.04078   0.03291  -0.0385   0.2012   1.0000
  12.250   1.3021   0.04313   0.03525  -0.0371   0.1862   1.0000
  12.500   1.3005   0.04562   0.03775  -0.0358   0.1723   1.0000
  12.750   1.2981   0.04826   0.04039  -0.0346   0.1597   1.0000
  13.250   1.2928   0.05388   0.04607  -0.0328   0.1367   1.0000
  13.500   1.2902   0.05684   0.04908  -0.0322   0.1265   1.0000
  13.750   1.2864   0.06006   0.05233  -0.0317   0.1174   1.0000
  14.000   1.2816   0.06349   0.05578  -0.0314   0.1087   1.0000
  14.250   1.2784   0.06686   0.05923  -0.0312   0.1002   1.0000
  14.500   1.2726   0.07063   0.06301  -0.0312   0.0930   1.0000
  14.750   1.2677   0.07441   0.06689  -0.0314   0.0855   1.0000
  15.000   1.2625   0.07833   0.07086  -0.0318   0.0790   1.0000
  15.250   1.2557   0.08254   0.07512  -0.0324   0.0732   1.0000
  15.500   1.2509   0.08659   0.07926  -0.0330   0.0676   1.0000
  15.750   1.2438   0.09105   0.08377  -0.0339   0.0630   1.0000
  16.000   1.2385   0.09531   0.08812  -0.0349   0.0587   1.0000
  16.250   1.2326   0.09974   0.09264  -0.0360   0.0548   1.0000
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