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AS5046 (16%) (as5046-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: AS5046 (16%) (as5046-il)
Reynolds number: 200,000
Max Cl/Cd: 55.36 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-as5046-il-200000-n5.txt
Download as CSV file: xf-as5046-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.6429   0.09109   0.08709  -0.0395   1.0000   0.0134
 -13.000  -0.6680   0.08274   0.07859  -0.0447   1.0000   0.0132
 -12.750  -0.6912   0.07585   0.07155  -0.0484   1.0000   0.0131
 -12.500  -0.7124   0.06997   0.06550  -0.0509   1.0000   0.0130
 -12.250  -0.7317   0.06482   0.06016  -0.0525   1.0000   0.0129
 -12.000  -0.7489   0.06024   0.05539  -0.0533   1.0000   0.0129
 -11.750  -0.7639   0.05612   0.05107  -0.0534   1.0000   0.0128
 -11.500  -0.7763   0.05243   0.04716  -0.0531   1.0000   0.0127
 -11.250  -0.7858   0.04913   0.04365  -0.0522   1.0000   0.0127
 -11.000  -0.7722   0.04456   0.03854  -0.0568   0.8751   0.0127
 -10.750  -0.7662   0.04160   0.03511  -0.0570   0.8413   0.0127
 -10.500  -0.7594   0.03914   0.03228  -0.0562   0.8254   0.0127
 -10.250  -0.7491   0.03693   0.02974  -0.0553   0.8152   0.0128
 -10.000  -0.7360   0.03495   0.02747  -0.0544   0.8078   0.0129
  -9.750  -0.7191   0.03314   0.02539  -0.0537   0.8019   0.0131
  -9.500  -0.6995   0.03150   0.02350  -0.0531   0.7971   0.0133
  -9.250  -0.6783   0.03003   0.02182  -0.0525   0.7927   0.0135
  -9.000  -0.6562   0.02874   0.02035  -0.0519   0.7886   0.0138
  -8.750  -0.6344   0.02761   0.01906  -0.0513   0.7847   0.0141
  -8.500  -0.6140   0.02655   0.01795  -0.0506   0.7812   0.0144
  -8.250  -0.5945   0.02562   0.01699  -0.0500   0.7776   0.0148
  -8.000  -0.5747   0.02478   0.01611  -0.0494   0.7743   0.0154
  -7.750  -0.5546   0.02400   0.01525  -0.0489   0.7713   0.0163
  -7.500  -0.5343   0.02325   0.01438  -0.0482   0.7686   0.0171
  -7.250  -0.5160   0.02237   0.01348  -0.0476   0.7661   0.0179
  -7.000  -0.4969   0.02156   0.01265  -0.0470   0.7633   0.0186
  -6.750  -0.4772   0.02078   0.01184  -0.0465   0.7603   0.0194
  -6.500  -0.4567   0.02005   0.01103  -0.0460   0.7575   0.0203
  -6.250  -0.4357   0.01934   0.01026  -0.0456   0.7551   0.0215
  -6.000  -0.4134   0.01873   0.00959  -0.0454   0.7528   0.0231
  -5.750  -0.3900   0.01820   0.00898  -0.0452   0.7508   0.0258
  -5.500  -0.3660   0.01771   0.00843  -0.0451   0.7488   0.0301
  -5.250  -0.3422   0.01712   0.00786  -0.0449   0.7463   0.0372
  -5.000  -0.3199   0.01629   0.00722  -0.0448   0.7437   0.0690
  -4.750  -0.3068   0.01391   0.00607  -0.0450   0.7413   0.3052
  -4.500  -0.2876   0.01274   0.00604  -0.0445   0.7391   0.5182
  -4.250  -0.2599   0.01313   0.00654  -0.0440   0.7370   0.5801
  -4.000  -0.2313   0.01372   0.00709  -0.0436   0.7349   0.6133
  -3.750  -0.2029   0.01424   0.00753  -0.0432   0.7329   0.6295
  -3.500  -0.1737   0.01431   0.00748  -0.0436   0.7309   0.6374
  -3.250  -0.1453   0.01447   0.00760  -0.0435   0.7285   0.6415
  -3.000  -0.1166   0.01455   0.00762  -0.0437   0.7259   0.6466
  -2.750  -0.0868   0.01451   0.00743  -0.0444   0.7233   0.6527
  -2.500  -0.0585   0.01458   0.00747  -0.0443   0.7209   0.6553
  -2.250  -0.0299   0.01464   0.00748  -0.0444   0.7185   0.6582
  -2.000  -0.0009   0.01468   0.00744  -0.0447   0.7163   0.6614
  -1.750   0.0283   0.01467   0.00737  -0.0452   0.7137   0.6651
  -1.500   0.0580   0.01461   0.00724  -0.0459   0.7106   0.6693
  -1.250   0.0862   0.01463   0.00726  -0.0460   0.7073   0.6713
  -1.000   0.1147   0.01465   0.00726  -0.0461   0.7042   0.6735
  -0.750   0.1436   0.01466   0.00723  -0.0463   0.7013   0.6759
  -0.500   0.1727   0.01466   0.00717  -0.0467   0.6983   0.6782
  -0.250   0.2013   0.01462   0.00715  -0.0470   0.6937   0.6808
   0.000   0.2305   0.01457   0.00706  -0.0475   0.6891   0.6835
   0.250   0.2604   0.01451   0.00692  -0.0481   0.6850   0.6860
   0.500   0.2890   0.01447   0.00687  -0.0483   0.6811   0.6874
   0.750   0.3168   0.01445   0.00691  -0.0484   0.6757   0.6890
   1.000   0.3453   0.01441   0.00689  -0.0485   0.6709   0.6907
   1.250   0.3744   0.01436   0.00682  -0.0488   0.6668   0.6924
   1.500   0.4028   0.01433   0.00683  -0.0490   0.6614   0.6942
   1.750   0.4313   0.01427   0.00680  -0.0492   0.6548   0.6964
   2.000   0.4606   0.01416   0.00664  -0.0495   0.6488   0.6986
   2.250   0.4887   0.01407   0.00661  -0.0497   0.6389   0.7006
   2.500   0.5179   0.01395   0.00646  -0.0501   0.6309   0.7025
   2.750   0.5456   0.01387   0.00646  -0.0501   0.6210   0.7038
   3.000   0.5734   0.01380   0.00646  -0.0501   0.6115   0.7054
   3.250   0.6013   0.01371   0.00639  -0.0501   0.6011   0.7071
   3.500   0.6291   0.01367   0.00640  -0.0501   0.5879   0.7088
   3.750   0.6568   0.01362   0.00639  -0.0501   0.5732   0.7105
   4.000   0.6843   0.01358   0.00633  -0.0500   0.5550   0.7122
   4.250   0.7111   0.01360   0.00629  -0.0499   0.5310   0.7141
   4.500   0.7371   0.01370   0.00628  -0.0496   0.5031   0.7163
   4.750   0.7619   0.01392   0.00635  -0.0491   0.4716   0.7184
   5.000   0.7852   0.01422   0.00652  -0.0485   0.4389   0.7200
   5.250   0.8077   0.01459   0.00678  -0.0477   0.4074   0.7214
   5.750   0.8517   0.01546   0.00743  -0.0462   0.3475   0.7246
   6.000   0.8735   0.01592   0.00781  -0.0454   0.3205   0.7265
   6.250   0.8951   0.01641   0.00821  -0.0447   0.2965   0.7287
   6.500   0.9171   0.01687   0.00862  -0.0440   0.2751   0.7310
   6.750   0.9389   0.01735   0.00905  -0.0434   0.2552   0.7331
   7.000   0.9603   0.01786   0.00950  -0.0427   0.2370   0.7351
   7.250   0.9806   0.01835   0.00998  -0.0419   0.2206   0.7367
   7.500   1.0005   0.01886   0.01048  -0.0409   0.2056   0.7385
   7.750   1.0203   0.01939   0.01101  -0.0400   0.1923   0.7404
   8.000   1.0395   0.01993   0.01155  -0.0390   0.1809   0.7425
   8.250   1.0577   0.02051   0.01213  -0.0379   0.1701   0.7448
   8.500   1.0769   0.02104   0.01271  -0.0370   0.1603   0.7475
   8.750   1.0943   0.02165   0.01334  -0.0358   0.1514   0.7502
   9.000   1.1094   0.02225   0.01397  -0.0343   0.1424   0.7525
   9.250   1.1235   0.02284   0.01463  -0.0326   0.1345   0.7548
   9.500   1.1370   0.02361   0.01543  -0.0310   0.1263   0.7572
   9.750   1.1530   0.02432   0.01622  -0.0299   0.1181   0.7599
  10.000   1.1664   0.02522   0.01715  -0.0287   0.1107   0.7628
  10.250   1.1806   0.02613   0.01810  -0.0277   0.1030   0.7658
  10.500   1.1933   0.02718   0.01921  -0.0267   0.0963   0.7687
  10.750   1.2053   0.02829   0.02039  -0.0257   0.0899   0.7716
  11.000   1.2168   0.02951   0.02168  -0.0249   0.0844   0.7751
  11.250   1.2280   0.03080   0.02304  -0.0242   0.0790   0.7791
  11.500   1.2377   0.03227   0.02455  -0.0235   0.0746   0.7834
  11.750   1.2484   0.03361   0.02603  -0.0228   0.0703   0.7876
  12.000   1.2561   0.03523   0.02771  -0.0220   0.0666   0.7923
  12.250   1.2645   0.03682   0.02940  -0.0213   0.0634   0.7975
  12.500   1.2730   0.03839   0.03109  -0.0206   0.0603   0.8031
  12.750   1.2787   0.04020   0.03299  -0.0199   0.0576   0.8097
  13.250   1.2892   0.04389   0.03696  -0.0184   0.0530   0.8279
  13.500   1.2931   0.04578   0.03901  -0.0175   0.0508   0.8423
  13.750   1.2927   0.04776   0.04115  -0.0161   0.0492   0.8702
  14.000   1.2843   0.04968   0.04322  -0.0137   0.0480   1.0000
  14.250   1.2877   0.05206   0.04570  -0.0136   0.0464   1.0000
  14.500   1.2911   0.05448   0.04823  -0.0135   0.0447   1.0000
  14.750   1.2929   0.05711   0.05097  -0.0136   0.0432   1.0000
  15.000   1.2929   0.06005   0.05399  -0.0139   0.0419   1.0000
  15.250   1.2909   0.06333   0.05733  -0.0144   0.0408   1.0000
  15.500   1.2895   0.06662   0.06071  -0.0149   0.0397   1.0000
  15.750   1.2897   0.06983   0.06408  -0.0155   0.0385   1.0000
  16.000   1.2884   0.07332   0.06769  -0.0163   0.0374   1.0000
  16.250   1.2860   0.07705   0.07155  -0.0174   0.0364   1.0000
  16.500   1.2825   0.08103   0.07563  -0.0187   0.0355   1.0000
  16.750   1.2775   0.08527   0.07995  -0.0201   0.0347   1.0000
  17.000   1.2714   0.08969   0.08444  -0.0216   0.0340   1.0000
  17.250   1.2664   0.09411   0.08899  -0.0232   0.0333   1.0000
  17.500   1.2610   0.09868   0.09372  -0.0250   0.0326   1.0000
  17.750   1.2546   0.10349   0.09868  -0.0271   0.0318   1.0000
  18.000   1.2476   0.10845   0.10378  -0.0293   0.0311   1.0000
  18.250   1.2404   0.11356   0.10900  -0.0317   0.0305   1.0000
  18.500   1.2330   0.11877   0.11433  -0.0344   0.0299   1.0000
  18.750   1.2257   0.12403   0.11968  -0.0371   0.0293   1.0000
  19.000   1.2191   0.12913   0.12487  -0.0398   0.0288   1.0000
  19.250   1.2139   0.13393   0.12970  -0.0424   0.0283   1.0000
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