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AS5045 (15%) (as5045-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: AS5045 (15%) (as5045-il)
Reynolds number: 500,000
Max Cl/Cd: 70.33 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-as5045-il-500000-n5.txt
Download as CSV file: xf-as5045-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AS5045 (15%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.7120   0.08781   0.08447  -0.0251   0.7431   0.0068
 -13.000  -0.7501   0.07603   0.07247  -0.0328   0.7418   0.0067
 -12.750  -0.7807   0.06761   0.06382  -0.0374   0.7402   0.0066
 -12.500  -0.8072   0.06071   0.05669  -0.0402   0.7383   0.0066
 -12.250  -0.8295   0.05488   0.05060  -0.0419   0.7365   0.0066
 -12.000  -0.8472   0.04987   0.04534  -0.0427   0.7346   0.0066
 -11.750  -0.8597   0.04559   0.04079  -0.0430   0.7328   0.0067
 -11.500  -0.8672   0.04189   0.03682  -0.0428   0.7308   0.0067
 -11.250  -0.8697   0.03870   0.03337  -0.0425   0.7288   0.0068
 -11.000  -0.8676   0.03595   0.03036  -0.0419   0.7267   0.0069
 -10.750  -0.8613   0.03357   0.02775  -0.0414   0.7246   0.0070
 -10.500  -0.8519   0.03153   0.02547  -0.0407   0.7225   0.0071
 -10.250  -0.8410   0.02982   0.02355  -0.0398   0.7207   0.0072
 -10.000  -0.8257   0.02828   0.02180  -0.0393   0.7192   0.0073
  -9.750  -0.8080   0.02689   0.02025  -0.0389   0.7177   0.0074
  -9.500  -0.7890   0.02566   0.01886  -0.0385   0.7162   0.0075
  -9.250  -0.7690   0.02457   0.01764  -0.0381   0.7147   0.0076
  -9.000  -0.7482   0.02358   0.01653  -0.0377   0.7131   0.0076
  -8.750  -0.7268   0.02266   0.01552  -0.0374   0.7115   0.0077
  -8.500  -0.7059   0.02164   0.01441  -0.0370   0.7098   0.0078
  -8.250  -0.6853   0.02063   0.01334  -0.0367   0.7082   0.0081
  -8.000  -0.6627   0.01989   0.01256  -0.0366   0.7068   0.0083
  -7.750  -0.6394   0.01922   0.01185  -0.0365   0.7055   0.0085
  -7.500  -0.6156   0.01858   0.01115  -0.0365   0.7042   0.0088
  -7.250  -0.5917   0.01791   0.01042  -0.0365   0.7030   0.0090
  -7.000  -0.5673   0.01722   0.00969  -0.0366   0.7017   0.0092
  -6.750  -0.5423   0.01657   0.00900  -0.0367   0.7002   0.0094
  -6.500  -0.5167   0.01597   0.00835  -0.0369   0.6987   0.0096
  -6.250  -0.4905   0.01542   0.00776  -0.0372   0.6973   0.0099
  -6.000  -0.4638   0.01494   0.00722  -0.0375   0.6960   0.0102
  -5.750  -0.4369   0.01441   0.00667  -0.0379   0.6947   0.0105
  -5.500  -0.4094   0.01397   0.00620  -0.0383   0.6934   0.0111
  -5.250  -0.3815   0.01361   0.00581  -0.0387   0.6921   0.0117
  -5.000  -0.3532   0.01330   0.00545  -0.0391   0.6907   0.0125
  -4.750  -0.3248   0.01300   0.00511  -0.0395   0.6893   0.0135
  -4.500  -0.2962   0.01272   0.00481  -0.0399   0.6880   0.0155
  -4.250  -0.2673   0.01243   0.00453  -0.0405   0.6869   0.0202
  -4.000  -0.2384   0.01201   0.00421  -0.0411   0.6857   0.0412
  -3.750  -0.2100   0.01059   0.00354  -0.0429   0.6842   0.2141
  -3.500  -0.1796   0.00930   0.00295  -0.0450   0.6826   0.3890
  -3.250  -0.1488   0.00850   0.00285  -0.0465   0.6811   0.5568
  -3.000  -0.1188   0.00865   0.00305  -0.0468   0.6795   0.5989
  -2.750  -0.0890   0.00874   0.00312  -0.0471   0.6779   0.6095
  -2.500  -0.0588   0.00877   0.00308  -0.0476   0.6762   0.6156
  -2.250  -0.0290   0.00882   0.00309  -0.0479   0.6745   0.6202
  -2.000   0.0007   0.00888   0.00310  -0.0483   0.6727   0.6242
  -1.750   0.0307   0.00890   0.00308  -0.0487   0.6706   0.6276
  -1.500   0.0609   0.00890   0.00305  -0.0492   0.6680   0.6309
  -1.250   0.0908   0.00889   0.00302  -0.0496   0.6652   0.6336
  -1.000   0.1205   0.00889   0.00301  -0.0500   0.6622   0.6357
  -0.750   0.1502   0.00889   0.00299  -0.0503   0.6594   0.6380
  -0.500   0.1799   0.00892   0.00298  -0.0507   0.6567   0.6407
  -0.250   0.2098   0.00892   0.00298  -0.0511   0.6534   0.6434
   0.000   0.2397   0.00890   0.00295  -0.0516   0.6494   0.6455
   0.250   0.2697   0.00888   0.00291  -0.0520   0.6456   0.6473
   0.500   0.2995   0.00886   0.00286  -0.0525   0.6420   0.6488
   0.750   0.3292   0.00883   0.00285  -0.0528   0.6380   0.6500
   1.000   0.3588   0.00880   0.00286  -0.0532   0.6326   0.6514
   1.250   0.3884   0.00877   0.00283  -0.0536   0.6271   0.6528
   1.500   0.4180   0.00875   0.00283  -0.0539   0.6208   0.6541
   1.750   0.4476   0.00872   0.00281  -0.0543   0.6131   0.6555
   2.000   0.4772   0.00870   0.00281  -0.0546   0.6048   0.6570
   2.250   0.5065   0.00869   0.00278  -0.0550   0.5946   0.6586
   2.500   0.5359   0.00870   0.00278  -0.0553   0.5812   0.6602
   2.750   0.5648   0.00874   0.00277  -0.0555   0.5642   0.6616
   3.000   0.5934   0.00882   0.00279  -0.0557   0.5402   0.6629
   3.250   0.6210   0.00902   0.00285  -0.0558   0.5077   0.6641
   3.500   0.6477   0.00930   0.00298  -0.0557   0.4704   0.6654
   3.750   0.6739   0.00966   0.00318  -0.0557   0.4300   0.6667
   4.000   0.6999   0.01006   0.00343  -0.0556   0.3917   0.6680
   4.250   0.7263   0.01041   0.00367  -0.0556   0.3602   0.6692
   4.500   0.7528   0.01075   0.00391  -0.0556   0.3316   0.6705
   4.750   0.7790   0.01111   0.00417  -0.0556   0.3031   0.6718
   5.000   0.8053   0.01145   0.00443  -0.0555   0.2791   0.6734
   5.250   0.8312   0.01183   0.00471  -0.0555   0.2537   0.6750
   5.500   0.8565   0.01226   0.00502  -0.0554   0.2254   0.6764
   5.750   0.8820   0.01267   0.00533  -0.0553   0.2026   0.6778
   6.000   0.9078   0.01303   0.00563  -0.0552   0.1853   0.6791
   6.500   0.9584   0.01377   0.00628  -0.0549   0.1537   0.6816
   6.750   0.9835   0.01414   0.00663  -0.0547   0.1408   0.6830
   7.000   1.0081   0.01454   0.00700  -0.0545   0.1280   0.6845
   7.250   1.0325   0.01496   0.00739  -0.0542   0.1163   0.6859
   7.500   1.0568   0.01537   0.00778  -0.0539   0.1056   0.6874
   7.750   1.0808   0.01578   0.00819  -0.0536   0.0960   0.6888
   8.000   1.1043   0.01623   0.00863  -0.0532   0.0874   0.6903
   8.500   1.1503   0.01717   0.00955  -0.0523   0.0726   0.6933
   8.750   1.1723   0.01769   0.01007  -0.0518   0.0666   0.6948
   9.000   1.1945   0.01817   0.01058  -0.0512   0.0612   0.6964
   9.250   1.2152   0.01872   0.01115  -0.0505   0.0562   0.6981
   9.500   1.2361   0.01923   0.01170  -0.0498   0.0523   0.6998
   9.750   1.2553   0.01984   0.01234  -0.0489   0.0484   0.7014
  10.000   1.2746   0.02041   0.01297  -0.0480   0.0457   0.7031
  10.250   1.2925   0.02104   0.01364  -0.0470   0.0428   0.7049
  10.500   1.3062   0.02177   0.01439  -0.0453   0.0403   0.7067
  10.750   1.3197   0.02248   0.01517  -0.0437   0.0386   0.7086
  11.000   1.3345   0.02326   0.01603  -0.0424   0.0370   0.7104
  11.500   1.3602   0.02529   0.01817  -0.0403   0.0334   0.7140
  11.750   1.3725   0.02647   0.01944  -0.0396   0.0321   0.7160
  12.000   1.3859   0.02763   0.02070  -0.0391   0.0309   0.7181
  12.250   1.3984   0.02890   0.02206  -0.0386   0.0295   0.7204
  12.500   1.4095   0.03031   0.02353  -0.0381   0.0281   0.7229
  12.750   1.4183   0.03194   0.02520  -0.0375   0.0267   0.7255
  13.250   1.4399   0.03480   0.02827  -0.0365   0.0245   0.7306
  13.500   1.4484   0.03644   0.02999  -0.0360   0.0234   0.7333
  13.750   1.4551   0.03826   0.03187  -0.0354   0.0225   0.7362
  14.000   1.4603   0.04023   0.03392  -0.0348   0.0217   0.7392
  14.250   1.4669   0.04208   0.03589  -0.0343   0.0210   0.7423
  14.500   1.4724   0.04404   0.03797  -0.0339   0.0202   0.7456
  14.750   1.4765   0.04617   0.04020  -0.0335   0.0195   0.7493
  15.000   1.4791   0.04850   0.04263  -0.0331   0.0188   0.7534
  15.250   1.4799   0.05103   0.04526  -0.0328   0.0183   0.7578
  15.500   1.4783   0.05390   0.04823  -0.0327   0.0177   0.7624
  15.750   1.4794   0.05660   0.05107  -0.0327   0.0173   0.7682
  16.000   1.4797   0.05951   0.05412  -0.0329   0.0168   0.7748
  16.250   1.4791   0.06265   0.05741  -0.0333   0.0163   0.7828
  16.500   1.4773   0.06605   0.06096  -0.0338   0.0158   0.7932
  17.000   1.4692   0.07374   0.06899  -0.0356   0.0150   0.8328
  17.250   1.4566   0.07740   0.07297  -0.0351   0.0147   1.0000
  17.500   1.4473   0.08237   0.07805  -0.0367   0.0143   1.0000
  17.750   1.4385   0.08738   0.08318  -0.0385   0.0140   1.0000
  18.000   1.4290   0.09254   0.08847  -0.0404   0.0138   1.0000
  18.250   1.4182   0.09802   0.09409  -0.0425   0.0135   1.0000
  18.500   1.4062   0.10384   0.10004  -0.0450   0.0132   1.0000
  18.750   1.3929   0.10994   0.10627  -0.0476   0.0130   1.0000
  19.000   1.3782   0.11637   0.11282  -0.0506   0.0127   1.0000
  19.250   1.3631   0.12301   0.11959  -0.0538   0.0125   1.0000
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