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AS5046 (16%) (as5046-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: AS5046 (16%) (as5046-il)
Reynolds number: 1,000,000
Max Cl/Cd: 83.55 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-as5046-il-1000000-n5.txt
Download as CSV file: xf-as5046-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AS5046 (16%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.8853   0.10705   0.10457  -0.0233   1.0000   0.0045
 -17.000  -0.9164   0.09642   0.09375  -0.0291   1.0000   0.0045
 -16.750  -0.9411   0.08753   0.08469  -0.0338   1.0000   0.0045
 -16.500  -0.9605   0.08011   0.07712  -0.0377   1.0000   0.0045
 -16.250  -0.9751   0.07385   0.07071  -0.0407   1.0000   0.0045
 -16.000  -0.9765   0.06733   0.06365  -0.0471   0.8436   0.0045
 -15.750  -0.9860   0.06292   0.05890  -0.0486   0.7890   0.0045
 -15.500  -0.9928   0.05879   0.05457  -0.0500   0.7734   0.0045
 -15.250  -0.9999   0.05483   0.05043  -0.0511   0.7635   0.0045
 -15.000  -1.0079   0.05096   0.04637  -0.0518   0.7565   0.0046
 -14.500  -1.0172   0.04461   0.03970  -0.0521   0.7456   0.0046
 -14.250  -1.0182   0.04196   0.03691  -0.0519   0.7411   0.0046
 -14.000  -1.0169   0.03962   0.03443  -0.0516   0.7369   0.0047
 -13.500  -1.0083   0.03557   0.03015  -0.0508   0.7300   0.0047
 -13.250  -1.0015   0.03380   0.02828  -0.0504   0.7271   0.0048
 -13.000  -0.9932   0.03219   0.02658  -0.0499   0.7242   0.0048
 -12.750  -0.9835   0.03071   0.02501  -0.0494   0.7214   0.0049
 -12.500  -0.9727   0.02934   0.02354  -0.0489   0.7185   0.0049
 -12.000  -0.9476   0.02688   0.02093  -0.0480   0.7137   0.0050
 -11.750  -0.9339   0.02573   0.01972  -0.0475   0.7117   0.0050
 -11.500  -0.9192   0.02466   0.01859  -0.0471   0.7097   0.0051
 -11.250  -0.9039   0.02364   0.01750  -0.0467   0.7077   0.0051
 -11.000  -0.8878   0.02267   0.01647  -0.0464   0.7058   0.0052
 -10.750  -0.8710   0.02176   0.01550  -0.0460   0.7040   0.0053
 -10.500  -0.8536   0.02090   0.01458  -0.0457   0.7021   0.0054
 -10.250  -0.8359   0.02008   0.01370  -0.0454   0.7001   0.0055
 -10.000  -0.8184   0.01931   0.01288  -0.0450   0.6983   0.0056
  -9.750  -0.8023   0.01861   0.01213  -0.0442   0.6969   0.0057
  -9.500  -0.7821   0.01796   0.01143  -0.0439   0.6956   0.0058
  -9.250  -0.7614   0.01733   0.01076  -0.0435   0.6942   0.0059
  -9.000  -0.7399   0.01674   0.01011  -0.0432   0.6928   0.0061
  -8.750  -0.7175   0.01619   0.00951  -0.0429   0.6914   0.0062
  -8.500  -0.6945   0.01568   0.00896  -0.0427   0.6898   0.0063
  -8.250  -0.6707   0.01521   0.00845  -0.0426   0.6882   0.0064
  -8.000  -0.6463   0.01479   0.00798  -0.0425   0.6867   0.0065
  -7.750  -0.6227   0.01423   0.00738  -0.0423   0.6852   0.0067
  -7.500  -0.5978   0.01381   0.00693  -0.0423   0.6838   0.0070
  -7.250  -0.5720   0.01346   0.00655  -0.0423   0.6823   0.0072
  -7.000  -0.5458   0.01312   0.00620  -0.0424   0.6814   0.0075
  -6.750  -0.5192   0.01280   0.00586  -0.0425   0.6804   0.0078
  -6.500  -0.4923   0.01249   0.00554  -0.0427   0.6792   0.0082
  -6.250  -0.4651   0.01221   0.00524  -0.0429   0.6779   0.0085
  -6.000  -0.4378   0.01192   0.00493  -0.0431   0.6765   0.0089
  -5.750  -0.4103   0.01164   0.00466  -0.0433   0.6751   0.0096
  -5.500  -0.3824   0.01140   0.00441  -0.0436   0.6739   0.0105
  -5.250  -0.3544   0.01118   0.00418  -0.0439   0.6726   0.0116
  -5.000  -0.3263   0.01096   0.00396  -0.0442   0.6713   0.0135
  -4.750  -0.2980   0.01074   0.00375  -0.0445   0.6699   0.0160
  -4.500  -0.2697   0.01054   0.00355  -0.0448   0.6684   0.0199
  -4.250  -0.2413   0.01031   0.00335  -0.0452   0.6669   0.0284
  -4.000  -0.2131   0.00999   0.00313  -0.0456   0.6653   0.0539
  -3.750  -0.1865   0.00900   0.00265  -0.0464   0.6642   0.1817
  -3.500  -0.1586   0.00800   0.00221  -0.0475   0.6626   0.3200
  -3.250  -0.1294   0.00695   0.00178  -0.0489   0.6608   0.4791
  -3.000  -0.0992   0.00660   0.00174  -0.0497   0.6588   0.5656
  -2.750  -0.0691   0.00658   0.00173  -0.0502   0.6568   0.5828
  -2.500  -0.0390   0.00658   0.00171  -0.0507   0.6546   0.5918
  -2.250  -0.0091   0.00659   0.00170  -0.0511   0.6520   0.5992
  -2.000   0.0209   0.00662   0.00166  -0.0516   0.6491   0.6040
  -1.750   0.0510   0.00660   0.00166  -0.0520   0.6462   0.6078
  -1.500   0.0810   0.00658   0.00165  -0.0525   0.6424   0.6116
  -1.250   0.1110   0.00659   0.00163  -0.0529   0.6387   0.6149
  -1.000   0.1410   0.00660   0.00160  -0.0534   0.6356   0.6177
  -0.750   0.1709   0.00663   0.00158  -0.0538   0.6325   0.6198
  -0.500   0.2010   0.00661   0.00158  -0.0543   0.6292   0.6222
  -0.250   0.2309   0.00660   0.00159  -0.0547   0.6252   0.6249
   0.000   0.2607   0.00662   0.00159  -0.0552   0.6203   0.6273
   0.250   0.2904   0.00663   0.00158  -0.0556   0.6136   0.6293
   0.500   0.3200   0.00664   0.00156  -0.0559   0.6026   0.6309
   0.750   0.3495   0.00666   0.00155  -0.0563   0.5911   0.6323
   1.000   0.3789   0.00671   0.00155  -0.0566   0.5791   0.6338
   1.250   0.4080   0.00677   0.00156  -0.0569   0.5643   0.6351
   1.500   0.4369   0.00687   0.00159  -0.0572   0.5469   0.6361
   1.750   0.4653   0.00697   0.00163  -0.0574   0.5260   0.6374
   2.000   0.4930   0.00716   0.00171  -0.0575   0.4973   0.6388
   2.250   0.5203   0.00739   0.00183  -0.0575   0.4663   0.6402
   2.500   0.5477   0.00761   0.00195  -0.0576   0.4402   0.6415
   2.750   0.5752   0.00783   0.00208  -0.0577   0.4148   0.6428
   3.000   0.6023   0.00809   0.00223  -0.0577   0.3874   0.6440
   3.250   0.6293   0.00834   0.00238  -0.0577   0.3614   0.6452
   3.500   0.6565   0.00858   0.00253  -0.0577   0.3394   0.6466
   3.750   0.6833   0.00884   0.00270  -0.0577   0.3152   0.6480
   4.000   0.7098   0.00913   0.00288  -0.0577   0.2900   0.6493
   4.250   0.7360   0.00943   0.00306  -0.0576   0.2648   0.6504
   4.750   0.7893   0.00994   0.00343  -0.0575   0.2301   0.6523
   5.000   0.8156   0.01019   0.00362  -0.0574   0.2131   0.6537
   5.250   0.8420   0.01044   0.00383  -0.0573   0.1994   0.6552
   5.500   0.8679   0.01072   0.00405  -0.0572   0.1840   0.6565
   5.750   0.8936   0.01101   0.00429  -0.0570   0.1694   0.6577
   6.000   0.9201   0.01123   0.00450  -0.0569   0.1602   0.6589
   6.250   0.9461   0.01149   0.00473  -0.0568   0.1512   0.6602
   6.500   0.9719   0.01175   0.00497  -0.0566   0.1424   0.6614
   6.750   0.9979   0.01199   0.00521  -0.0565   0.1353   0.6628
   7.000   1.0229   0.01230   0.00548  -0.0562   0.1260   0.6643
   7.250   1.0485   0.01255   0.00573  -0.0560   0.1193   0.6657
   7.500   1.0730   0.01288   0.00602  -0.0557   0.1106   0.6669
   7.750   1.0972   0.01323   0.00633  -0.0553   0.1015   0.6680
   8.000   1.1212   0.01356   0.00665  -0.0549   0.0933   0.6690
   8.250   1.1445   0.01394   0.00699  -0.0544   0.0852   0.6702
   8.500   1.1672   0.01434   0.00737  -0.0538   0.0776   0.6716
   8.750   1.1903   0.01469   0.00773  -0.0532   0.0717   0.6730
   9.000   1.2121   0.01512   0.00815  -0.0525   0.0659   0.6744
   9.250   1.2345   0.01549   0.00853  -0.0518   0.0613   0.6758
   9.500   1.2550   0.01597   0.00899  -0.0509   0.0558   0.6773
   9.750   1.2763   0.01637   0.00941  -0.0501   0.0523   0.6790
  10.000   1.2955   0.01687   0.00991  -0.0490   0.0481   0.6806
  10.250   1.3151   0.01732   0.01038  -0.0480   0.0451   0.6822
  10.500   1.3312   0.01782   0.01089  -0.0464   0.0422   0.6836
  10.750   1.3454   0.01834   0.01143  -0.0444   0.0398   0.6849
  11.000   1.3621   0.01887   0.01200  -0.0430   0.0379   0.6860
  11.250   1.3775   0.01950   0.01266  -0.0415   0.0357   0.6878
  11.500   1.3919   0.02021   0.01340  -0.0401   0.0338   0.6894
  11.750   1.4075   0.02087   0.01412  -0.0389   0.0326   0.6911
  12.000   1.4219   0.02165   0.01495  -0.0377   0.0311   0.6929
  12.250   1.4348   0.02259   0.01593  -0.0365   0.0294   0.6947
  12.500   1.4477   0.02361   0.01699  -0.0356   0.0280   0.6965
  12.750   1.4616   0.02463   0.01807  -0.0349   0.0270   0.6983
  13.000   1.4744   0.02577   0.01926  -0.0342   0.0258   0.7001
  13.250   1.4860   0.02705   0.02058  -0.0336   0.0246   0.7017
  13.500   1.4972   0.02840   0.02198  -0.0330   0.0235   0.7036
  13.750   1.5091   0.02968   0.02333  -0.0324   0.0227   0.7059
  14.000   1.5198   0.03107   0.02479  -0.0319   0.0218   0.7084
  14.250   1.5290   0.03258   0.02636  -0.0312   0.0208   0.7109
  14.500   1.5367   0.03423   0.02806  -0.0306   0.0200   0.7133
  14.750   1.5445   0.03587   0.02976  -0.0299   0.0193   0.7157
  15.000   1.5522   0.03752   0.03149  -0.0293   0.0187   0.7179
  15.250   1.5585   0.03932   0.03336  -0.0287   0.0181   0.7203
  15.500   1.5637   0.04121   0.03533  -0.0282   0.0175   0.7232
  15.750   1.5676   0.04326   0.03745  -0.0276   0.0170   0.7262
  16.000   1.5695   0.04553   0.03979  -0.0271   0.0163   0.7294
  16.250   1.5718   0.04780   0.04215  -0.0266   0.0159   0.7326
  16.750   1.5768   0.05258   0.04712  -0.0262   0.0151   0.7400
  17.000   1.5777   0.05529   0.04992  -0.0262   0.0147   0.7445
  17.250   1.5773   0.05820   0.05293  -0.0264   0.0143   0.7493
  17.500   1.5760   0.06134   0.05617  -0.0267   0.0139   0.7548
  17.750   1.5731   0.06478   0.05971  -0.0272   0.0135   0.7620
  18.000   1.5683   0.06855   0.06360  -0.0279   0.0132   0.7706
  18.250   1.5640   0.07235   0.06753  -0.0287   0.0130   0.7829
  18.500   1.5598   0.07625   0.07160  -0.0297   0.0127   0.8016
  18.750   1.5545   0.08043   0.07604  -0.0311   0.0125   0.8565
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