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AS5045 (15%) (as5045-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AS5045 (15%) (as5045-il)
Reynolds number: 1,000,000
Max Cl/Cd: 81.91 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-as5045-il-1000000-n5.txt
Download as CSV file: xf-as5045-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.8608   0.09200   0.08901  -0.0184   0.7229   0.0046
 -15.000  -0.9040   0.07882   0.07558  -0.0264   0.7221   0.0045
 -14.500  -0.9535   0.06303   0.05937  -0.0347   0.7189   0.0045
 -14.250  -0.9700   0.05757   0.05373  -0.0368   0.7173   0.0046
 -14.000  -0.9826   0.05300   0.04898  -0.0382   0.7155   0.0046
 -13.750  -0.9921   0.04904   0.04485  -0.0390   0.7137   0.0046
 -13.500  -0.9980   0.04560   0.04124  -0.0394   0.7120   0.0047
 -13.250  -1.0013   0.04255   0.03803  -0.0396   0.7102   0.0047
 -13.000  -1.0018   0.03985   0.03517  -0.0395   0.7084   0.0048
 -12.750  -0.9994   0.03746   0.03263  -0.0394   0.7067   0.0048
 -12.500  -0.9950   0.03531   0.03033  -0.0391   0.7051   0.0049
 -12.250  -0.9884   0.03336   0.02823  -0.0388   0.7035   0.0049
 -12.000  -0.9799   0.03159   0.02633  -0.0385   0.7023   0.0050
 -11.750  -0.9696   0.02997   0.02460  -0.0381   0.7010   0.0051
 -11.500  -0.9576   0.02851   0.02303  -0.0378   0.6996   0.0051
 -11.250  -0.9445   0.02714   0.02155  -0.0374   0.6980   0.0052
 -11.000  -0.9299   0.02589   0.02020  -0.0371   0.6964   0.0052
 -10.750  -0.9144   0.02473   0.01894  -0.0368   0.6949   0.0053
 -10.500  -0.8995   0.02368   0.01779  -0.0363   0.6936   0.0053
 -10.250  -0.8823   0.02269   0.01670  -0.0361   0.6923   0.0054
 -10.000  -0.8623   0.02180   0.01572  -0.0361   0.6910   0.0054
  -9.750  -0.8416   0.02099   0.01483  -0.0360   0.6898   0.0055
  -9.500  -0.8201   0.02023   0.01399  -0.0358   0.6884   0.0055
  -9.250  -0.7979   0.01953   0.01322  -0.0358   0.6872   0.0055
  -9.000  -0.7778   0.01845   0.01206  -0.0355   0.6861   0.0056
  -8.750  -0.7560   0.01755   0.01111  -0.0354   0.6850   0.0057
  -8.500  -0.7328   0.01680   0.01030  -0.0354   0.6840   0.0058
  -8.250  -0.7085   0.01615   0.00961  -0.0355   0.6829   0.0059
  -8.000  -0.6835   0.01558   0.00899  -0.0357   0.6819   0.0060
  -7.750  -0.6579   0.01505   0.00843  -0.0359   0.6808   0.0061
  -7.500  -0.6317   0.01456   0.00791  -0.0361   0.6795   0.0062
  -7.250  -0.6052   0.01411   0.00742  -0.0364   0.6783   0.0064
  -7.000  -0.5782   0.01371   0.00700  -0.0367   0.6770   0.0066
  -6.750  -0.5509   0.01333   0.00658  -0.0370   0.6759   0.0068
  -6.500  -0.5234   0.01295   0.00617  -0.0374   0.6748   0.0070
  -6.250  -0.4956   0.01259   0.00577  -0.0377   0.6737   0.0072
  -6.000  -0.4676   0.01225   0.00540  -0.0381   0.6726   0.0074
  -5.750  -0.4393   0.01195   0.00507  -0.0385   0.6714   0.0076
  -5.500  -0.4107   0.01164   0.00473  -0.0390   0.6705   0.0078
  -5.250  -0.3820   0.01130   0.00438  -0.0394   0.6695   0.0083
  -5.000  -0.3531   0.01103   0.00411  -0.0399   0.6684   0.0088
  -4.750  -0.3240   0.01081   0.00388  -0.0404   0.6674   0.0093
  -4.500  -0.2947   0.01060   0.00366  -0.0409   0.6663   0.0099
  -4.250  -0.2654   0.01039   0.00345  -0.0414   0.6651   0.0109
  -4.000  -0.2359   0.01019   0.00325  -0.0419   0.6637   0.0130
  -3.750  -0.2064   0.00995   0.00306  -0.0424   0.6624   0.0213
  -3.500  -0.1768   0.00957   0.00282  -0.0432   0.6612   0.0567
  -3.250  -0.1463   0.00836   0.00228  -0.0451   0.6599   0.2333
  -3.000  -0.1148   0.00735   0.00186  -0.0470   0.6584   0.3902
  -2.750  -0.0828   0.00654   0.00163  -0.0487   0.6566   0.5500
  -2.500  -0.0525   0.00650   0.00164  -0.0492   0.6547   0.5755
  -2.250  -0.0223   0.00649   0.00165  -0.0497   0.6526   0.5906
  -2.000   0.0079   0.00649   0.00164  -0.0501   0.6501   0.5985
  -1.750   0.0380   0.00648   0.00161  -0.0506   0.6475   0.6034
  -1.500   0.0681   0.00648   0.00160  -0.0510   0.6448   0.6080
  -1.250   0.0980   0.00649   0.00157  -0.0514   0.6420   0.6116
  -1.000   0.1281   0.00650   0.00155  -0.0519   0.6391   0.6142
  -0.750   0.1583   0.00650   0.00153  -0.0523   0.6358   0.6167
  -0.500   0.1883   0.00648   0.00152  -0.0528   0.6323   0.6192
  -0.250   0.2183   0.00648   0.00152  -0.0532   0.6283   0.6216
   0.000   0.2481   0.00649   0.00151  -0.0536   0.6245   0.6242
   0.250   0.2782   0.00649   0.00152  -0.0541   0.6199   0.6268
   0.500   0.3081   0.00650   0.00152  -0.0545   0.6138   0.6289
   0.750   0.3380   0.00651   0.00150  -0.0549   0.6070   0.6304
   1.000   0.3678   0.00652   0.00149  -0.0553   0.5978   0.6316
   1.250   0.3975   0.00655   0.00149  -0.0557   0.5874   0.6328
   1.500   0.4270   0.00658   0.00149  -0.0561   0.5735   0.6342
   1.750   0.4561   0.00665   0.00151  -0.0564   0.5547   0.6356
   2.000   0.4849   0.00679   0.00156  -0.0566   0.5302   0.6367
   2.250   0.5131   0.00700   0.00166  -0.0568   0.4972   0.6380
   2.500   0.5410   0.00726   0.00178  -0.0570   0.4626   0.6393
   2.750   0.5689   0.00753   0.00193  -0.0572   0.4310   0.6407
   3.000   0.5965   0.00783   0.00209  -0.0573   0.3964   0.6420
   3.250   0.6238   0.00816   0.00227  -0.0575   0.3602   0.6432
   3.750   0.6791   0.00870   0.00260  -0.0578   0.3071   0.6456
   4.000   0.7065   0.00899   0.00279  -0.0579   0.2820   0.6468
   4.250   0.7340   0.00926   0.00296  -0.0580   0.2600   0.6479
   4.500   0.7616   0.00950   0.00314  -0.0582   0.2413   0.6491
   4.750   0.7883   0.00982   0.00337  -0.0582   0.2162   0.6503
   5.000   0.8146   0.01018   0.00361  -0.0582   0.1907   0.6515
   5.500   0.8685   0.01074   0.00407  -0.0583   0.1601   0.6541
   6.000   0.9220   0.01129   0.00454  -0.0583   0.1349   0.6567
   6.250   0.9484   0.01159   0.00480  -0.0583   0.1229   0.6579
   6.500   0.9747   0.01190   0.00507  -0.0583   0.1121   0.6591
   6.750   1.0007   0.01222   0.00535  -0.0582   0.1021   0.6603
   7.000   1.0263   0.01257   0.00565  -0.0581   0.0917   0.6616
   7.250   1.0522   0.01289   0.00595  -0.0580   0.0838   0.6629
   7.500   1.0775   0.01324   0.00627  -0.0578   0.0760   0.6639
   7.750   1.1026   0.01359   0.00661  -0.0576   0.0693   0.6652
   8.000   1.1279   0.01391   0.00694  -0.0574   0.0638   0.6665
   8.250   1.1521   0.01432   0.00732  -0.0571   0.0572   0.6678
   8.500   1.1769   0.01466   0.00767  -0.0568   0.0530   0.6690
   8.750   1.2006   0.01508   0.00809  -0.0565   0.0482   0.6703
   9.000   1.2247   0.01545   0.00848  -0.0561   0.0450   0.6717
   9.250   1.2477   0.01589   0.00892  -0.0557   0.0414   0.6731
   9.500   1.2708   0.01631   0.00937  -0.0552   0.0387   0.6746
   9.750   1.2936   0.01673   0.00981  -0.0547   0.0367   0.6761
  10.000   1.3154   0.01721   0.01030  -0.0541   0.0345   0.6776
  10.250   1.3365   0.01771   0.01082  -0.0533   0.0324   0.6789
  10.500   1.3579   0.01816   0.01131  -0.0527   0.0310   0.6800
  10.750   1.3780   0.01866   0.01185  -0.0518   0.0294   0.6814
  11.000   1.3963   0.01927   0.01248  -0.0508   0.0274   0.6830
  11.250   1.4145   0.01982   0.01308  -0.0497   0.0259   0.6845
  11.500   1.4277   0.02040   0.01369  -0.0478   0.0243   0.6861
  11.750   1.4413   0.02112   0.01445  -0.0462   0.0228   0.6877
  12.000   1.4551   0.02192   0.01529  -0.0449   0.0217   0.6894
  12.250   1.4695   0.02273   0.01617  -0.0437   0.0209   0.6911
  12.500   1.4829   0.02368   0.01718  -0.0428   0.0200   0.6928
  12.750   1.4956   0.02479   0.01834  -0.0421   0.0191   0.6943
  13.000   1.5076   0.02604   0.01963  -0.0414   0.0182   0.6958
  13.250   1.5198   0.02733   0.02099  -0.0409   0.0175   0.6977
  13.500   1.5321   0.02861   0.02234  -0.0405   0.0169   0.6998
  13.750   1.5434   0.02998   0.02379  -0.0400   0.0163   0.7021
  14.000   1.5534   0.03147   0.02534  -0.0394   0.0155   0.7044
  14.250   1.5618   0.03308   0.02700  -0.0388   0.0148   0.7066
  14.500   1.5695   0.03478   0.02876  -0.0382   0.0141   0.7087
  14.750   1.5775   0.03642   0.03048  -0.0377   0.0137   0.7108
  15.250   1.5899   0.04009   0.03430  -0.0365   0.0126   0.7154
  15.500   1.5939   0.04213   0.03642  -0.0359   0.0121   0.7181
  15.750   1.5962   0.04437   0.03873  -0.0354   0.0116   0.7208
  16.000   1.5983   0.04666   0.04111  -0.0349   0.0111   0.7237
  16.250   1.6006   0.04896   0.04351  -0.0345   0.0108   0.7265
  16.500   1.6014   0.05147   0.04611  -0.0343   0.0104   0.7296
  16.750   1.6015   0.05422   0.04896  -0.0342   0.0100   0.7333
  17.000   1.6006   0.05721   0.05204  -0.0343   0.0096   0.7373
  17.250   1.5983   0.06045   0.05537  -0.0346   0.0092   0.7414
  17.500   1.5945   0.06399   0.05902  -0.0350   0.0089   0.7458
  17.750   1.5911   0.06762   0.06276  -0.0357   0.0086   0.7513
  18.000   1.5867   0.07147   0.06673  -0.0366   0.0084   0.7575
  18.250   1.5806   0.07567   0.07106  -0.0376   0.0081   0.7651
  18.500   1.5724   0.08026   0.07578  -0.0390   0.0078   0.7743
  18.750   1.5630   0.08516   0.08083  -0.0406   0.0076   0.7866
  19.000   1.5508   0.09058   0.08641  -0.0425   0.0074   0.8034
  19.250   1.5375   0.09627   0.09233  -0.0447   0.0072   0.8427
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