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AS5046 (16%) (as5046-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: AS5046 (16%) (as5046-il)
Reynolds number: 500,000
Max Cl/Cd: 69.67 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-as5046-il-500000-n5.txt
Download as CSV file: xf-as5046-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.7011   0.11763   0.11503  -0.0189   1.0000   0.0067
 -15.250  -0.7851   0.09188   0.08879  -0.0337   1.0000   0.0065
 -15.000  -0.8093   0.08288   0.07962  -0.0389   1.0000   0.0064
 -14.750  -0.8303   0.07531   0.07186  -0.0430   1.0000   0.0064
 -14.500  -0.8488   0.06881   0.06517  -0.0461   1.0000   0.0064
 -14.250  -0.8648   0.06329   0.05947  -0.0483   1.0000   0.0064
 -14.000  -0.8750   0.05808   0.05403  -0.0512   0.9331   0.0064
 -13.750  -0.8759   0.05322   0.04855  -0.0553   0.8206   0.0065
 -13.500  -0.8829   0.04992   0.04494  -0.0554   0.7966   0.0065
 -13.250  -0.8870   0.04690   0.04168  -0.0554   0.7841   0.0065
 -13.000  -0.8905   0.04391   0.03846  -0.0552   0.7758   0.0065
 -12.750  -0.8909   0.04126   0.03561  -0.0548   0.7688   0.0066
 -12.500  -0.8878   0.03902   0.03320  -0.0543   0.7634   0.0066
 -12.250  -0.8814   0.03713   0.03118  -0.0539   0.7586   0.0067
 -12.000  -0.8727   0.03552   0.02945  -0.0535   0.7540   0.0068
 -11.750  -0.8627   0.03403   0.02784  -0.0530   0.7499   0.0069
 -11.500  -0.8512   0.03266   0.02636  -0.0526   0.7464   0.0070
 -11.250  -0.8387   0.03134   0.02494  -0.0522   0.7430   0.0071
 -11.000  -0.8252   0.03008   0.02356  -0.0517   0.7399   0.0072
 -10.750  -0.8107   0.02886   0.02223  -0.0511   0.7372   0.0074
 -10.500  -0.7955   0.02769   0.02093  -0.0505   0.7346   0.0075
 -10.000  -0.7633   0.02544   0.01847  -0.0491   0.7303   0.0077
  -9.750  -0.7465   0.02439   0.01733  -0.0485   0.7281   0.0078
  -9.500  -0.7296   0.02338   0.01624  -0.0479   0.7257   0.0080
  -9.250  -0.7126   0.02242   0.01519  -0.0472   0.7233   0.0081
  -9.000  -0.6966   0.02152   0.01422  -0.0464   0.7212   0.0082
  -8.750  -0.6807   0.02071   0.01332  -0.0455   0.7193   0.0084
  -8.500  -0.6617   0.01994   0.01247  -0.0450   0.7175   0.0086
  -8.250  -0.6418   0.01926   0.01171  -0.0445   0.7158   0.0087
  -8.000  -0.6229   0.01841   0.01083  -0.0440   0.7143   0.0090
  -7.750  -0.6015   0.01776   0.01016  -0.0437   0.7125   0.0092
  -7.500  -0.5790   0.01720   0.00957  -0.0434   0.7106   0.0095
  -7.250  -0.5558   0.01666   0.00900  -0.0433   0.7087   0.0099
  -7.000  -0.5320   0.01616   0.00846  -0.0431   0.7070   0.0103
  -6.750  -0.5077   0.01568   0.00793  -0.0430   0.7055   0.0107
  -6.500  -0.4827   0.01526   0.00745  -0.0430   0.7039   0.0112
  -6.250  -0.4578   0.01479   0.00697  -0.0430   0.7024   0.0119
  -6.000  -0.4318   0.01445   0.00660  -0.0431   0.7009   0.0129
  -5.750  -0.4054   0.01414   0.00623  -0.0432   0.6993   0.0140
  -5.500  -0.3791   0.01375   0.00583  -0.0433   0.6978   0.0155
  -5.250  -0.3520   0.01343   0.00549  -0.0435   0.6963   0.0172
  -5.000  -0.3250   0.01310   0.00517  -0.0437   0.6948   0.0202
  -4.750  -0.2976   0.01280   0.00487  -0.0439   0.6933   0.0255
  -4.500  -0.2705   0.01239   0.00456  -0.0442   0.6917   0.0442
  -4.250  -0.2470   0.01116   0.00392  -0.0448   0.6900   0.1774
  -4.000  -0.2222   0.00972   0.00324  -0.0459   0.6882   0.3557
  -3.750  -0.1950   0.00866   0.00288  -0.0469   0.6867   0.5205
  -3.500  -0.1655   0.00864   0.00301  -0.0473   0.6851   0.5766
  -3.250  -0.1357   0.00876   0.00311  -0.0476   0.6835   0.5989
  -3.000  -0.1059   0.00885   0.00316  -0.0480   0.6817   0.6091
  -2.750  -0.0759   0.00890   0.00317  -0.0484   0.6798   0.6161
  -2.500  -0.0459   0.00891   0.00313  -0.0488   0.6776   0.6210
  -2.250  -0.0163   0.00894   0.00316  -0.0492   0.6754   0.6245
  -2.000   0.0135   0.00896   0.00315  -0.0496   0.6730   0.6280
  -1.750   0.0433   0.00898   0.00312  -0.0500   0.6706   0.6314
  -1.500   0.0733   0.00900   0.00307  -0.0505   0.6680   0.6345
  -1.250   0.1031   0.00902   0.00303  -0.0509   0.6652   0.6369
  -1.000   0.1325   0.00899   0.00303  -0.0512   0.6617   0.6390
  -0.750   0.1620   0.00899   0.00304  -0.0516   0.6576   0.6415
  -0.500   0.1916   0.00899   0.00302  -0.0519   0.6538   0.6438
  -0.250   0.2212   0.00899   0.00298  -0.0523   0.6506   0.6458
   0.000   0.2509   0.00899   0.00297  -0.0527   0.6474   0.6477
   0.250   0.2807   0.00897   0.00296  -0.0532   0.6434   0.6494
   0.500   0.3104   0.00896   0.00293  -0.0536   0.6390   0.6510
   0.750   0.3401   0.00895   0.00288  -0.0540   0.6344   0.6526
   1.000   0.3693   0.00890   0.00287  -0.0543   0.6274   0.6539
   1.250   0.3984   0.00886   0.00282  -0.0545   0.6186   0.6551
   1.500   0.4276   0.00884   0.00282  -0.0549   0.6099   0.6564
   1.750   0.4566   0.00884   0.00280  -0.0551   0.6012   0.6578
   2.000   0.4857   0.00884   0.00282  -0.0554   0.5902   0.6593
   2.250   0.5145   0.00886   0.00282  -0.0556   0.5777   0.6607
   2.500   0.5431   0.00890   0.00283  -0.0558   0.5635   0.6621
   2.750   0.5710   0.00899   0.00285  -0.0559   0.5430   0.6635
   3.000   0.5980   0.00915   0.00291  -0.0558   0.5150   0.6651
   3.250   0.6245   0.00937   0.00301  -0.0557   0.4862   0.6666
   3.500   0.6507   0.00965   0.00315  -0.0555   0.4567   0.6680
   3.750   0.6764   0.00997   0.00333  -0.0553   0.4251   0.6692
   4.000   0.7020   0.01027   0.00353  -0.0551   0.3955   0.6704
   4.250   0.7275   0.01057   0.00374  -0.0549   0.3682   0.6716
   4.500   0.7526   0.01091   0.00399  -0.0546   0.3405   0.6729
   4.750   0.7774   0.01128   0.00424  -0.0543   0.3126   0.6744
   5.000   0.8025   0.01161   0.00450  -0.0540   0.2880   0.6758
   5.250   0.8277   0.01193   0.00475  -0.0538   0.2678   0.6772
   5.500   0.8526   0.01228   0.00502  -0.0535   0.2480   0.6786
   5.750   0.8775   0.01262   0.00529  -0.0532   0.2297   0.6800
   6.000   0.9022   0.01295   0.00558  -0.0529   0.2134   0.6814
   6.250   0.9265   0.01332   0.00588  -0.0526   0.1967   0.6829
   6.500   0.9507   0.01369   0.00620  -0.0522   0.1823   0.6844
   6.750   0.9749   0.01405   0.00652  -0.0518   0.1708   0.6859
   7.000   0.9994   0.01435   0.00683  -0.0515   0.1612   0.6873
   7.250   1.0231   0.01469   0.00716  -0.0510   0.1520   0.6886
   7.500   1.0467   0.01504   0.00752  -0.0506   0.1431   0.6900
   7.750   1.0701   0.01539   0.00788  -0.0501   0.1347   0.6914
   8.250   1.1152   0.01617   0.00866  -0.0489   0.1178   0.6944
   8.500   1.1367   0.01661   0.00908  -0.0481   0.1093   0.6960
   8.750   1.1573   0.01708   0.00954  -0.0473   0.1004   0.6977
   9.000   1.1779   0.01754   0.01001  -0.0464   0.0926   0.6995
   9.250   1.1970   0.01807   0.01053  -0.0453   0.0854   0.7013
   9.500   1.2153   0.01861   0.01106  -0.0442   0.0785   0.7029
   9.750   1.2314   0.01914   0.01162  -0.0426   0.0731   0.7046
  10.000   1.2453   0.01970   0.01222  -0.0407   0.0681   0.7063
  10.250   1.2606   0.02035   0.01290  -0.0392   0.0637   0.7081
  10.500   1.2759   0.02103   0.01362  -0.0379   0.0593   0.7099
  10.750   1.2897   0.02184   0.01445  -0.0364   0.0554   0.7119
  11.000   1.3045   0.02262   0.01529  -0.0353   0.0522   0.7139
  11.250   1.3175   0.02358   0.01628  -0.0341   0.0490   0.7159
  11.500   1.3304   0.02460   0.01735  -0.0331   0.0464   0.7178
  11.750   1.3436   0.02567   0.01848  -0.0323   0.0439   0.7198
  12.000   1.3556   0.02689   0.01976  -0.0316   0.0417   0.7218
  12.250   1.3670   0.02819   0.02113  -0.0309   0.0397   0.7241
  12.500   1.3795   0.02943   0.02247  -0.0304   0.0380   0.7267
  12.750   1.3903   0.03082   0.02392  -0.0298   0.0363   0.7295
  13.000   1.3994   0.03236   0.02551  -0.0291   0.0346   0.7323
  13.250   1.4083   0.03394   0.02716  -0.0285   0.0334   0.7351
  13.500   1.4180   0.03544   0.02877  -0.0280   0.0322   0.7379
  13.750   1.4262   0.03706   0.03048  -0.0274   0.0308   0.7409
  14.000   1.4329   0.03885   0.03235  -0.0268   0.0296   0.7443
  14.250   1.4372   0.04087   0.03444  -0.0262   0.0286   0.7477
  14.500   1.4427   0.04279   0.03646  -0.0256   0.0277   0.7513
  14.750   1.4482   0.04474   0.03853  -0.0252   0.0269   0.7554
  15.000   1.4521   0.04688   0.04078  -0.0248   0.0260   0.7601
  15.250   1.4545   0.04918   0.04318  -0.0244   0.0252   0.7653
  15.500   1.4555   0.05171   0.04581  -0.0242   0.0244   0.7711
  15.750   1.4543   0.05461   0.04881  -0.0241   0.0236   0.7783
  16.000   1.4561   0.05726   0.05160  -0.0242   0.0231   0.7872
  16.250   1.4570   0.06010   0.05462  -0.0244   0.0225   0.7999
  16.500   1.4566   0.06316   0.05787  -0.0248   0.0219   0.8208
  16.750   1.4449   0.06562   0.06068  -0.0225   0.0215   1.0000
  17.000   1.4421   0.06924   0.06438  -0.0233   0.0209   1.0000
  17.250   1.4371   0.07323   0.06846  -0.0243   0.0204   1.0000
  17.500   1.4301   0.07763   0.07296  -0.0255   0.0199   1.0000
  17.750   1.4207   0.08249   0.07792  -0.0270   0.0196   1.0000
  18.000   1.4142   0.08699   0.08255  -0.0285   0.0192   1.0000
  18.250   1.4058   0.09183   0.08752  -0.0302   0.0189   1.0000
  18.500   1.3960   0.09699   0.09280  -0.0321   0.0186   1.0000
  18.750   1.3853   0.10238   0.09831  -0.0343   0.0183   1.0000
  19.000   1.3732   0.10807   0.10412  -0.0367   0.0180   1.0000
  19.250   1.3603   0.11394   0.11011  -0.0393   0.0177   1.0000
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