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AS5048 (18%) (as5048-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: AS5048 (18%) (as5048-il)
Reynolds number: 200,000
Max Cl/Cd: 56.31 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-as5048-il-200000-n5.txt
Download as CSV file: xf-as5048-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AS5048 (18%)                                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.6483   0.11030   0.10602  -0.0454   1.0000   0.0131
 -15.250  -0.6704   0.10145   0.09704  -0.0505   1.0000   0.0131
 -15.000  -0.6929   0.09339   0.08883  -0.0548   1.0000   0.0130
 -14.750  -0.7143   0.08633   0.08161  -0.0583   1.0000   0.0129
 -14.500  -0.7340   0.08023   0.07534  -0.0608   1.0000   0.0129
 -14.250  -0.7537   0.07470   0.06962  -0.0625   1.0000   0.0129
 -14.000  -0.7715   0.06983   0.06456  -0.0634   1.0000   0.0129
 -13.750  -0.7883   0.06534   0.05987  -0.0638   1.0000   0.0129
 -13.500  -0.8026   0.06133   0.05565  -0.0637   1.0000   0.0129
 -13.250  -0.8154   0.05762   0.05171  -0.0631   1.0000   0.0129
 -13.000  -0.8250   0.05433   0.04819  -0.0621   1.0000   0.0130
 -12.750  -0.8326   0.05130   0.04493  -0.0609   1.0000   0.0130
 -12.500  -0.8376   0.04854   0.04193  -0.0595   1.0000   0.0131
 -12.250  -0.8393   0.04611   0.03928  -0.0580   1.0000   0.0132
 -12.000  -0.8288   0.04389   0.03695  -0.0578   0.9981   0.0134
 -11.750  -0.8141   0.04173   0.03469  -0.0579   0.9337   0.0136
 -11.500  -0.7668   0.03901   0.03171  -0.0652   0.8992   0.0139
 -11.250  -0.7159   0.03658   0.02893  -0.0725   0.8663   0.0144
 -10.750  -0.6622   0.03373   0.02549  -0.0754   0.8241   0.0157
 -10.500  -0.6405   0.03258   0.02410  -0.0754   0.8135   0.0163
 -10.250  -0.6187   0.03154   0.02302  -0.0755   0.8054   0.0169
 -10.000  -0.5985   0.03058   0.02199  -0.0753   0.7990   0.0174
  -9.750  -0.5787   0.02965   0.02097  -0.0748   0.7935   0.0179
  -9.500  -0.5600   0.02873   0.01997  -0.0742   0.7890   0.0185
  -9.250  -0.5425   0.02783   0.01897  -0.0734   0.7851   0.0190
  -9.000  -0.5258   0.02693   0.01799  -0.0726   0.7813   0.0196
  -8.750  -0.5117   0.02590   0.01695  -0.0717   0.7777   0.0202
  -8.500  -0.4967   0.02497   0.01599  -0.0710   0.7743   0.0210
  -8.250  -0.4807   0.02414   0.01510  -0.0703   0.7711   0.0222
  -8.000  -0.4644   0.02334   0.01419  -0.0696   0.7682   0.0235
  -7.750  -0.4512   0.02235   0.01320  -0.0686   0.7650   0.0245
  -7.500  -0.4365   0.02153   0.01232  -0.0676   0.7621   0.0257
  -7.250  -0.4218   0.02082   0.01155  -0.0664   0.7595   0.0270
  -7.000  -0.4082   0.02023   0.01089  -0.0648   0.7570   0.0287
  -6.750  -0.3937   0.01969   0.01030  -0.0632   0.7548   0.0312
  -6.500  -0.3763   0.01917   0.00971  -0.0621   0.7527   0.0344
  -6.250  -0.3587   0.01865   0.00915  -0.0609   0.7504   0.0392
  -6.000  -0.3428   0.01800   0.00858  -0.0595   0.7478   0.0512
  -5.750  -0.3377   0.01667   0.00776  -0.0568   0.7453   0.1377
  -5.500  -0.3350   0.01512   0.00692  -0.0539   0.7430   0.2764
  -5.250  -0.3302   0.01371   0.00629  -0.0509   0.7409   0.4272
  -5.000  -0.3114   0.01357   0.00675  -0.0490   0.7390   0.5423
  -4.750  -0.2845   0.01387   0.00705  -0.0486   0.7370   0.5840
  -4.500  -0.2565   0.01433   0.00745  -0.0483   0.7352   0.6091
  -4.250  -0.2287   0.01479   0.00787  -0.0479   0.7332   0.6254
  -4.000  -0.2018   0.01502   0.00801  -0.0478   0.7313   0.6371
  -3.750  -0.1732   0.01526   0.00822  -0.0477   0.7292   0.6417
  -3.500  -0.1454   0.01534   0.00824  -0.0477   0.7269   0.6467
  -3.250  -0.1182   0.01529   0.00804  -0.0480   0.7247   0.6528
  -3.000  -0.0896   0.01537   0.00808  -0.0481   0.7227   0.6555
  -2.750  -0.0610   0.01544   0.00811  -0.0483   0.7208   0.6583
  -2.500  -0.0324   0.01549   0.00808  -0.0485   0.7189   0.6615
  -2.250  -0.0041   0.01550   0.00801  -0.0488   0.7170   0.6651
  -2.000   0.0228   0.01544   0.00789  -0.0490   0.7145   0.6694
  -1.750   0.0502   0.01545   0.00788  -0.0491   0.7119   0.6717
  -1.500   0.0779   0.01548   0.00791  -0.0492   0.7093   0.6738
  -1.250   0.1060   0.01549   0.00790  -0.0493   0.7067   0.6761
  -1.000   0.1344   0.01549   0.00786  -0.0496   0.7043   0.6784
  -0.750   0.1632   0.01549   0.00780  -0.0500   0.7021   0.6809
  -0.500   0.1919   0.01549   0.00774  -0.0505   0.6997   0.6835
  -0.250   0.2185   0.01545   0.00770  -0.0506   0.6962   0.6860
   0.000   0.2457   0.01542   0.00767  -0.0507   0.6924   0.6880
   0.250   0.2735   0.01540   0.00765  -0.0508   0.6887   0.6895
   0.500   0.3024   0.01536   0.00758  -0.0511   0.6852   0.6910
   0.750   0.3302   0.01535   0.00757  -0.0512   0.6814   0.6926
   1.000   0.3562   0.01534   0.00761  -0.0510   0.6765   0.6946
   1.250   0.3838   0.01531   0.00759  -0.0511   0.6722   0.6967
   1.500   0.4126   0.01526   0.00752  -0.0514   0.6685   0.6986
   1.750   0.4412   0.01522   0.00747  -0.0518   0.6648   0.7005
   2.000   0.4670   0.01520   0.00750  -0.0516   0.6590   0.7027
   2.250   0.4947   0.01514   0.00745  -0.0518   0.6539   0.7046
   2.500   0.5236   0.01503   0.00733  -0.0519   0.6492   0.7060
   2.750   0.5476   0.01495   0.00735  -0.0513   0.6403   0.7074
   3.000   0.5753   0.01478   0.00717  -0.0512   0.6328   0.7089
   3.250   0.6000   0.01472   0.00721  -0.0507   0.6230   0.7105
   3.500   0.6272   0.01461   0.00710  -0.0506   0.6156   0.7124
   3.750   0.6526   0.01458   0.00716  -0.0503   0.6052   0.7145
   4.000   0.6789   0.01453   0.00715  -0.0501   0.5954   0.7166
   4.250   0.7052   0.01446   0.00708  -0.0499   0.5843   0.7185
   4.500   0.7308   0.01442   0.00706  -0.0495   0.5695   0.7203
   4.750   0.7556   0.01438   0.00701  -0.0490   0.5524   0.7218
   5.000   0.7795   0.01438   0.00701  -0.0482   0.5323   0.7232
   5.250   0.8017   0.01446   0.00702  -0.0472   0.5077   0.7250
   5.500   0.8222   0.01465   0.00711  -0.0458   0.4801   0.7270
   5.750   0.8412   0.01494   0.00728  -0.0443   0.4524   0.7290
   6.000   0.8593   0.01530   0.00754  -0.0427   0.4244   0.7311
   6.250   0.8765   0.01572   0.00784  -0.0410   0.3971   0.7331
   6.500   0.8920   0.01620   0.00820  -0.0390   0.3709   0.7351
   6.750   0.9077   0.01669   0.00860  -0.0372   0.3454   0.7371
   7.000   0.9215   0.01720   0.00903  -0.0350   0.3226   0.7388
   7.250   0.9346   0.01767   0.00947  -0.0327   0.3026   0.7407
   7.500   0.9465   0.01816   0.00994  -0.0302   0.2841   0.7429
   7.750   0.9588   0.01871   0.01046  -0.0279   0.2669   0.7453
   8.000   0.9722   0.01932   0.01105  -0.0259   0.2507   0.7479
   8.250   0.9857   0.01999   0.01169  -0.0241   0.2359   0.7504
   8.500   0.9986   0.02071   0.01239  -0.0224   0.2222   0.7529
   8.750   1.0116   0.02145   0.01312  -0.0207   0.2095   0.7552
   9.000   1.0247   0.02217   0.01387  -0.0191   0.1983   0.7574
   9.250   1.0368   0.02299   0.01471  -0.0175   0.1888   0.7599
   9.500   1.0493   0.02384   0.01560  -0.0162   0.1793   0.7626
   9.750   1.0626   0.02471   0.01652  -0.0150   0.1712   0.7655
  10.000   1.0745   0.02573   0.01755  -0.0139   0.1630   0.7687
  10.250   1.0881   0.02667   0.01855  -0.0130   0.1552   0.7720
  10.500   1.0991   0.02776   0.01969  -0.0119   0.1478   0.7753
  10.750   1.1122   0.02876   0.02079  -0.0111   0.1407   0.7792
  11.000   1.1229   0.02996   0.02202  -0.0102   0.1334   0.7833
  11.250   1.1356   0.03106   0.02319  -0.0094   0.1266   0.7876
  11.500   1.1456   0.03231   0.02450  -0.0085   0.1197   0.7919
  11.750   1.1565   0.03350   0.02579  -0.0076   0.1133   0.7971
  12.000   1.1657   0.03484   0.02719  -0.0067   0.1070   0.8031
  12.250   1.1748   0.03617   0.02860  -0.0058   0.1013   0.8100
  12.500   1.1827   0.03756   0.03008  -0.0048   0.0955   0.8190
  12.750   1.1884   0.03906   0.03167  -0.0036   0.0907   0.8310
  13.000   1.1933   0.04036   0.03314  -0.0019   0.0861   0.8525
  13.250   1.1819   0.04124   0.03422   0.0030   0.0833   1.0000
  13.500   1.1883   0.04307   0.03608   0.0034   0.0793   1.0000
  13.750   1.1961   0.04479   0.03788   0.0038   0.0753   1.0000
  14.000   1.2007   0.04683   0.03995   0.0042   0.0718   1.0000
  14.250   1.2051   0.04893   0.04209   0.0046   0.0688   1.0000
  14.500   1.2115   0.05091   0.04417   0.0048   0.0657   1.0000
  14.750   1.2152   0.05316   0.04648   0.0050   0.0628   1.0000
  15.000   1.2162   0.05577   0.04913   0.0051   0.0605   1.0000
  15.250   1.2206   0.05809   0.05155   0.0051   0.0582   1.0000
  15.500   1.2243   0.06054   0.05411   0.0050   0.0559   1.0000
  15.750   1.2256   0.06331   0.05695   0.0048   0.0539   1.0000
  16.000   1.2244   0.06644   0.06012   0.0044   0.0522   1.0000
  16.250   1.2245   0.06947   0.06324   0.0040   0.0505   1.0000
  16.500   1.2259   0.07240   0.06631   0.0035   0.0489   1.0000
  16.750   1.2257   0.07563   0.06964   0.0028   0.0473   1.0000
  17.000   1.2237   0.07914   0.07324   0.0020   0.0459   1.0000
  17.250   1.2195   0.08298   0.07716   0.0009   0.0447   1.0000
  17.500   1.2152   0.08687   0.08111  -0.0002   0.0436   1.0000
  17.750   1.2136   0.09051   0.08490  -0.0013   0.0424   1.0000
  18.000   1.2105   0.09440   0.08892  -0.0026   0.0412   1.0000
  18.250   1.2064   0.09848   0.09312  -0.0040   0.0402   1.0000
  18.500   1.2013   0.10277   0.09751  -0.0057   0.0392   1.0000
  18.750   1.1956   0.10720   0.10203  -0.0076   0.0383   1.0000
  19.000   1.1897   0.11167   0.10655  -0.0095   0.0375   1.0000
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