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RAE 101 AIRFOIL (rae101-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: RAE 101 AIRFOIL (rae101-il)
Reynolds number: 500,000
Max Cl/Cd: 56.36 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-rae101-il-500000-n5.txt
Download as CSV file: xf-rae101-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: RAE 101 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.9323   0.09329   0.09070  -0.0028   1.0000   0.0072
 -14.500  -0.9872   0.07672   0.07387  -0.0131   1.0000   0.0069
 -14.250  -1.0136   0.06752   0.06449  -0.0192   1.0000   0.0069
 -14.000  -1.0334   0.06017   0.05697  -0.0240   1.0000   0.0069
 -13.750  -1.0486   0.05418   0.05080  -0.0277   1.0000   0.0069
 -13.500  -1.0647   0.04858   0.04500  -0.0307   1.0000   0.0069
 -13.250  -1.0731   0.04456   0.04081  -0.0324   1.0000   0.0070
 -13.000  -1.0819   0.04090   0.03698  -0.0333   1.0000   0.0071
 -12.750  -1.0873   0.03802   0.03392  -0.0333   1.0000   0.0072
 -12.500  -1.0931   0.03538   0.03110  -0.0324   1.0000   0.0073
 -12.250  -1.0962   0.03325   0.02879  -0.0307   1.0000   0.0074
 -12.000  -1.0986   0.03133   0.02669  -0.0283   1.0000   0.0075
 -11.750  -1.0969   0.02985   0.02504  -0.0256   1.0000   0.0076
 -11.500  -1.0927   0.02839   0.02341  -0.0231   1.0000   0.0078
 -11.250  -1.0835   0.02699   0.02184  -0.0212   1.0000   0.0079
 -11.000  -1.0711   0.02579   0.02044  -0.0195   1.0000   0.0081
 -10.750  -1.0573   0.02465   0.01915  -0.0179   1.0000   0.0082
 -10.500  -1.0461   0.02314   0.01751  -0.0161   1.0000   0.0085
 -10.250  -1.0304   0.02209   0.01636  -0.0147   1.0000   0.0088
 -10.000  -1.0126   0.02124   0.01543  -0.0135   1.0000   0.0091
  -9.750  -0.9940   0.02043   0.01454  -0.0124   1.0000   0.0094
  -9.500  -0.9746   0.01970   0.01372  -0.0113   1.0000   0.0098
  -9.250  -0.9551   0.01893   0.01284  -0.0102   1.0000   0.0102
  -9.000  -0.9349   0.01825   0.01207  -0.0091   1.0000   0.0107
  -8.750  -0.9141   0.01762   0.01135  -0.0081   1.0000   0.0112
  -8.500  -0.8939   0.01692   0.01057  -0.0070   1.0000   0.0117
  -8.250  -0.8739   0.01620   0.00980  -0.0059   1.0000   0.0124
  -8.000  -0.8525   0.01565   0.00922  -0.0049   1.0000   0.0131
  -7.750  -0.8308   0.01514   0.00863  -0.0039   1.0000   0.0139
  -7.500  -0.8091   0.01464   0.00807  -0.0029   1.0000   0.0147
  -7.250  -0.7871   0.01418   0.00755  -0.0019   1.0000   0.0154
  -7.000  -0.7661   0.01361   0.00694  -0.0007   1.0000   0.0167
  -6.750  -0.7440   0.01320   0.00652   0.0002   1.0000   0.0183
  -6.500  -0.7216   0.01283   0.00611   0.0012   1.0000   0.0198
  -6.250  -0.6989   0.01249   0.00572   0.0021   1.0000   0.0211
  -6.000  -0.6773   0.01204   0.00526   0.0033   1.0000   0.0236
  -5.750  -0.6548   0.01171   0.00492   0.0042   1.0000   0.0263
  -5.500  -0.6324   0.01139   0.00458   0.0053   1.0000   0.0297
  -5.250  -0.6032   0.01104   0.00424   0.0047   0.9976   0.0349
  -5.000  -0.5701   0.01070   0.00392   0.0034   0.9921   0.0419
  -4.750  -0.5371   0.01036   0.00362   0.0021   0.9857   0.0529
  -4.500  -0.5043   0.01002   0.00332   0.0009   0.9785   0.0679
  -4.250  -0.4700   0.00963   0.00304  -0.0007   0.9710   0.0928
  -4.000  -0.4373   0.00921   0.00276  -0.0020   0.9604   0.1283
  -3.750  -0.4042   0.00870   0.00247  -0.0035   0.9480   0.1825
  -3.500  -0.3718   0.00813   0.00218  -0.0048   0.9317   0.2542
  -3.250  -0.3416   0.00764   0.00196  -0.0055   0.9115   0.3339
  -3.000  -0.3138   0.00740   0.00182  -0.0055   0.8871   0.3799
  -2.750  -0.2873   0.00725   0.00169  -0.0051   0.8626   0.4128
  -2.500  -0.2615   0.00715   0.00159  -0.0045   0.8385   0.4411
  -2.250  -0.2359   0.00706   0.00150  -0.0040   0.8155   0.4674
  -2.000  -0.2103   0.00699   0.00142  -0.0034   0.7935   0.4924
  -1.750  -0.1844   0.00693   0.00136  -0.0029   0.7732   0.5167
  -1.500  -0.1585   0.00688   0.00130  -0.0024   0.7534   0.5405
  -1.250  -0.1325   0.00684   0.00126  -0.0019   0.7346   0.5627
  -1.000  -0.1063   0.00680   0.00122  -0.0015   0.7169   0.5840
  -0.500  -0.0533   0.00675   0.00118  -0.0007   0.6833   0.6200
  -0.250  -0.0267   0.00675   0.00116  -0.0003   0.6665   0.6358
   0.000   0.0000   0.00675   0.00116   0.0000   0.6507   0.6507
   0.250   0.0267   0.00675   0.00116   0.0003   0.6357   0.6663
   0.500   0.0533   0.00675   0.00118   0.0007   0.6200   0.6833
   1.000   0.1062   0.00680   0.00122   0.0015   0.5840   0.7169
   1.250   0.1325   0.00684   0.00126   0.0019   0.5628   0.7346
   1.500   0.1585   0.00688   0.00130   0.0024   0.5404   0.7535
   1.750   0.1843   0.00693   0.00136   0.0029   0.5166   0.7731
   2.000   0.2102   0.00699   0.00142   0.0034   0.4923   0.7935
   2.250   0.2358   0.00706   0.00150   0.0040   0.4676   0.8152
   2.500   0.2615   0.00715   0.00159   0.0046   0.4412   0.8384
   2.750   0.2872   0.00726   0.00169   0.0051   0.4120   0.8627
   3.000   0.3138   0.00740   0.00181   0.0055   0.3799   0.8871
   3.250   0.3416   0.00764   0.00196   0.0055   0.3336   0.9115
   3.750   0.4041   0.00870   0.00247   0.0035   0.1829   0.9479
   4.000   0.4374   0.00921   0.00276   0.0020   0.1283   0.9605
   4.250   0.4701   0.00963   0.00304   0.0007   0.0926   0.9711
   4.500   0.5044   0.01002   0.00332  -0.0009   0.0679   0.9787
   4.750   0.5372   0.01036   0.00362  -0.0021   0.0528   0.9858
   5.000   0.5701   0.01070   0.00392  -0.0034   0.0421   0.9921
   5.250   0.6033   0.01104   0.00424  -0.0048   0.0349   0.9977
   5.500   0.6322   0.01140   0.00458  -0.0052   0.0294   1.0000
   5.750   0.6547   0.01170   0.00492  -0.0042   0.0263   1.0000
   6.000   0.6771   0.01203   0.00526  -0.0032   0.0237   1.0000
   6.250   0.6988   0.01249   0.00571  -0.0021   0.0211   1.0000
   6.500   0.7214   0.01283   0.00611  -0.0012   0.0199   1.0000
   6.750   0.7439   0.01320   0.00653  -0.0002   0.0183   1.0000
   7.000   0.7660   0.01362   0.00695   0.0008   0.0168   1.0000
   7.250   0.7870   0.01419   0.00755   0.0019   0.0155   1.0000
   7.500   0.8091   0.01464   0.00807   0.0029   0.0147   1.0000
   7.750   0.8308   0.01514   0.00863   0.0039   0.0139   1.0000
   8.000   0.8524   0.01566   0.00922   0.0049   0.0132   1.0000
   8.250   0.8739   0.01621   0.00981   0.0059   0.0125   1.0000
   8.500   0.8940   0.01692   0.01057   0.0070   0.0118   1.0000
   8.750   0.9141   0.01764   0.01137   0.0081   0.0112   1.0000
   9.000   0.9351   0.01825   0.01206   0.0091   0.0107   1.0000
   9.250   0.9551   0.01896   0.01287   0.0102   0.0102   1.0000
   9.500   0.9747   0.01971   0.01373   0.0113   0.0098   1.0000
   9.750   0.9942   0.02045   0.01456   0.0123   0.0094   1.0000
  10.000   1.0130   0.02124   0.01542   0.0134   0.0091   1.0000
  10.250   1.0308   0.02210   0.01637   0.0146   0.0088   1.0000
  10.500   1.0464   0.02316   0.01753   0.0160   0.0085   1.0000
  10.750   1.0581   0.02462   0.01912   0.0178   0.0083   1.0000
  11.000   1.0720   0.02575   0.02040   0.0193   0.0081   1.0000
  11.250   1.0840   0.02700   0.02184   0.0210   0.0079   1.0000
  11.500   1.0931   0.02843   0.02344   0.0230   0.0078   1.0000
  11.750   1.0976   0.02987   0.02506   0.0255   0.0077   1.0000
  12.000   1.0990   0.03138   0.02674   0.0282   0.0075   1.0000
  12.250   1.0974   0.03323   0.02876   0.0305   0.0075   1.0000
  12.500   1.0948   0.03531   0.03102   0.0322   0.0073   1.0000
  12.750   1.0897   0.03787   0.03376   0.0331   0.0071   1.0000
  13.000   1.0868   0.04045   0.03650   0.0332   0.0071   1.0000
  13.250   1.0778   0.04409   0.04033   0.0324   0.0070   1.0000
  13.500   1.0654   0.04866   0.04509   0.0305   0.0069   1.0000
  13.750   1.0520   0.05384   0.05046   0.0277   0.0069   1.0000
  14.000   1.0349   0.06017   0.05697   0.0237   0.0069   1.0000
  14.250   1.0130   0.06789   0.06487   0.0187   0.0069   1.0000
  14.500   0.9894   0.07659   0.07374   0.0130   0.0069   1.0000
  14.750   0.9510   0.08934   0.08670   0.0049   0.0071   1.0000
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