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Griffith 30% Suction Airfoil (griffith30symsuction-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: Griffith 30% Suction Airfoil (griffith30symsuction-il)
Reynolds number: 1,000,000
Max Cl/Cd: 15.27 at α=13.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-griffith30symsuction-il-1000000-n5.txt
Download as CSV file: xf-griffith30symsuction-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Griffith 30% Suction Airfoil                    
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.0209   0.08469   0.07888  -0.0588   0.7661   0.0171
 -19.500  -1.0134   0.08247   0.07661  -0.0599   0.7658   0.0178
 -19.250  -1.0032   0.08059   0.07470  -0.0610   0.7655   0.0187
 -19.000  -0.9943   0.07864   0.07272  -0.0618   0.7652   0.0198
 -18.750  -0.9865   0.07662   0.07066  -0.0625   0.7649   0.0211
 -18.500  -0.9754   0.07497   0.06898  -0.0633   0.7647   0.0224
 -18.250  -0.9655   0.07326   0.06725  -0.0639   0.7644   0.0243
 -18.000  -0.9560   0.07153   0.06550  -0.0644   0.7642   0.0261
 -17.750  -0.9468   0.06981   0.06377  -0.0648   0.7640   0.0289
 -17.500  -0.9363   0.06826   0.06221  -0.0652   0.7638   0.0324
 -17.250  -0.9272   0.06665   0.06060  -0.0654   0.7635   0.0369
 -17.000  -0.9202   0.06489   0.05886  -0.0653   0.7633   0.0427
 -16.750  -0.9100   0.06345   0.05745  -0.0653   0.7630   0.0495
 -16.500  -0.8984   0.06213   0.05615  -0.0655   0.7628   0.0560
 -16.250  -0.8862   0.06085   0.05489  -0.0657   0.7626   0.0619
 -16.000  -0.8743   0.05955   0.05360  -0.0659   0.7625   0.0674
 -15.750  -0.8609   0.05842   0.05248  -0.0660   0.7623   0.0727
 -15.500  -0.8455   0.05745   0.05151  -0.0663   0.7621   0.0777
 -15.250  -0.8318   0.05639   0.05048  -0.0664   0.7619   0.0835
 -15.000  -0.8181   0.05533   0.04944  -0.0665   0.7618   0.0895
 -14.750  -0.8051   0.05423   0.04835  -0.0665   0.7616   0.0965
 -14.500  -0.7925   0.05316   0.04733  -0.0663   0.7615   0.1069
 -14.000  -0.7699   0.05093   0.04529  -0.0656   0.7612   0.1369
 -13.750  -0.7589   0.04982   0.04426  -0.0652   0.7610   0.1526
 -13.500  -0.7436   0.04899   0.04347  -0.0652   0.7609   0.1633
 -13.250  -0.7275   0.04822   0.04275  -0.0652   0.7607   0.1722
 -13.000  -0.7093   0.04759   0.04214  -0.0654   0.7606   0.1807
 -12.750  -0.6936   0.04682   0.04142  -0.0653   0.7605   0.1905
 -12.500  -0.6755   0.04619   0.04081  -0.0654   0.7604   0.1984
 -12.250  -0.6578   0.04555   0.04016  -0.0655   0.7602   0.2041
 -12.000  -0.6403   0.04493   0.03956  -0.0655   0.7601   0.2096
 -11.750  -0.6207   0.04443   0.03907  -0.0658   0.7600   0.2136
 -11.500  -0.6003   0.04399   0.03861  -0.0660   0.7599   0.2167
 -11.250  -0.5795   0.04358   0.03818  -0.0664   0.7598   0.2194
 -11.000  -0.5425   0.04416   0.03880  -0.0722   0.7566   0.2252
 -10.750  -0.5231   0.04379   0.03847  -0.0729   0.7557   0.2320
 -10.500  -0.5039   0.04342   0.03810  -0.0733   0.7550   0.2371
 -10.250  -0.4836   0.04307   0.03775  -0.0737   0.7544   0.2413
 -10.000  -0.4650   0.04264   0.03734  -0.0737   0.7538   0.2482
  -9.750  -0.4484   0.04216   0.03689  -0.0734   0.7533   0.2569
  -9.500  -0.4304   0.04175   0.03650  -0.0732   0.7529   0.2649
  -9.250  -0.4162   0.04116   0.03597  -0.0725   0.7525   0.2773
  -9.000  -0.4018   0.04051   0.03536  -0.0717   0.7521   0.2896
  -8.750  -0.3908   0.03968   0.03462  -0.0703   0.7517   0.3099
  -8.500  -0.3820   0.03874   0.03380  -0.0686   0.7513   0.3369
  -8.250  -0.3732   0.03780   0.03296  -0.0667   0.7509   0.3626
  -8.000  -0.3646   0.03688   0.03212  -0.0649   0.7506   0.3831
  -7.750  -0.3523   0.03621   0.03151  -0.0636   0.7503   0.3985
  -7.500  -0.3362   0.03570   0.03103  -0.0627   0.7501   0.4120
  -7.250  -0.3258   0.03495   0.03035  -0.0610   0.7498   0.4286
  -7.000  -0.3235   0.03570   0.03118  -0.0595   0.7445   0.4439
  -6.750  -0.3237   0.03500   0.03057  -0.0561   0.7431   0.4657
  -6.500  -0.3390   0.03373   0.02950  -0.0501   0.7419   0.5060
  -6.250  -0.3671   0.03204   0.02809  -0.0417   0.7408   0.5624
  -6.000  -0.3604   0.03148   0.02762  -0.0389   0.7403   0.5872
  -5.750  -0.3450   0.03115   0.02733  -0.0375   0.7398   0.6006
  -5.500  -0.3289   0.03079   0.02700  -0.0363   0.7395   0.6126
  -5.250  -0.3596   0.03155   0.02778  -0.0266   0.7328   0.6189
  -5.000  -0.3537   0.03156   0.02782  -0.0231   0.7310   0.6268
  -4.750  -0.3484   0.03113   0.02739  -0.0197   0.7299   0.6337
  -4.500  -0.3313   0.03098   0.02724  -0.0184   0.7292   0.6384
  -4.250  -0.3046   0.03110   0.02739  -0.0189   0.7287   0.6429
  -4.000  -0.2848   0.03095   0.02724  -0.0181   0.7283   0.6481
  -3.750  -0.3199   0.03108   0.02738  -0.0073   0.7220   0.6544
  -3.500  -0.2967   0.03150   0.02781  -0.0071   0.7199   0.6572
  -3.250  -0.2692   0.03175   0.02808  -0.0077   0.7189   0.6599
  -3.000  -0.2438   0.03186   0.02820  -0.0080   0.7180   0.6638
  -2.750  -0.2288   0.03155   0.02790  -0.0064   0.7171   0.6693
  -2.500  -0.2059   0.03149   0.02783  -0.0062   0.7165   0.6725
  -2.250  -0.1730   0.03174   0.02810  -0.0077   0.7161   0.6743
  -2.000  -0.1423   0.03190   0.02827  -0.0089   0.7157   0.6762
  -1.750  -0.1143   0.03194   0.02831  -0.0096   0.7152   0.6780
  -0.250  -0.0003   0.03294   0.02935  -0.0042   0.7023   0.6922
   0.750   0.0611   0.03278   0.02918   0.0020   0.6896   0.7038
   1.000   0.0904   0.03260   0.02900   0.0010   0.6884   0.7046
   1.250   0.1200   0.03237   0.02876   0.0000   0.6873   0.7055
   1.750   0.1323   0.03243   0.02881   0.0064   0.6785   0.7119
   2.000   0.1423   0.03190   0.02827   0.0089   0.6762   0.7157
   2.250   0.1729   0.03174   0.02810   0.0078   0.6743   0.7161
   2.500   0.2058   0.03149   0.02783   0.0062   0.6725   0.7165
   2.750   0.2289   0.03155   0.02789   0.0064   0.6693   0.7172
   3.000   0.2438   0.03185   0.02820   0.0080   0.6638   0.7180
   3.250   0.2692   0.03174   0.02807   0.0077   0.6599   0.7189
   3.500   0.2965   0.03149   0.02781   0.0072   0.6572   0.7200
   3.750   0.3189   0.03106   0.02735   0.0075   0.6545   0.7221
   4.000   0.2849   0.03094   0.02723   0.0181   0.6481   0.7283
   4.250   0.3046   0.03109   0.02738   0.0189   0.6429   0.7287
   4.500   0.3313   0.03097   0.02723   0.0185   0.6384   0.7292
   4.750   0.3484   0.03112   0.02738   0.0197   0.6337   0.7299
   5.000   0.3535   0.03154   0.02781   0.0232   0.6270   0.7310
   5.250   0.3581   0.03153   0.02777   0.0269   0.6191   0.7329
   5.500   0.3293   0.03078   0.02698   0.0362   0.6127   0.7395
   5.750   0.3453   0.03114   0.02731   0.0375   0.6006   0.7399
   6.000   0.3607   0.03147   0.02761   0.0388   0.5872   0.7403
   6.250   0.3673   0.03203   0.02807   0.0416   0.5623   0.7408
   6.500   0.3389   0.03373   0.02950   0.0501   0.5053   0.7419
   6.750   0.3238   0.03500   0.03056   0.0561   0.4653   0.7431
   7.000   0.3237   0.03569   0.03117   0.0594   0.4435   0.7446
   7.250   0.3265   0.03495   0.03034   0.0608   0.4282   0.7498
   7.500   0.3371   0.03569   0.03101   0.0625   0.4119   0.7501
   7.750   0.3533   0.03620   0.03149   0.0634   0.3983   0.7503
   8.000   0.3657   0.03686   0.03210   0.0647   0.3829   0.7506
   8.250   0.3743   0.03778   0.03294   0.0665   0.3624   0.7509
   8.500   0.3832   0.03872   0.03377   0.0683   0.3366   0.7513
   8.750   0.3920   0.03966   0.03459   0.0701   0.3097   0.7517
   9.000   0.4032   0.04048   0.03533   0.0714   0.2894   0.7521
   9.250   0.4178   0.04112   0.03593   0.0722   0.2775   0.7525
   9.500   0.4321   0.04171   0.03646   0.0729   0.2651   0.7529
   9.750   0.4500   0.04213   0.03686   0.0731   0.2569   0.7533
  10.000   0.4667   0.04262   0.03731   0.0733   0.2480   0.7538
  10.250   0.4854   0.04304   0.03772   0.0733   0.2412   0.7544
  10.500   0.5059   0.04338   0.03806   0.0729   0.2370   0.7550
  10.750   0.5251   0.04376   0.03843   0.0725   0.2317   0.7557
  11.000   0.5445   0.04413   0.03877   0.0718   0.2249   0.7566
  11.250   0.5817   0.04355   0.03815   0.0660   0.2194   0.7598
  11.500   0.6026   0.04397   0.03858   0.0656   0.2167   0.7599
  11.750   0.6230   0.04441   0.03904   0.0653   0.2134   0.7600
  12.000   0.6426   0.04491   0.03954   0.0651   0.2094   0.7601
  12.250   0.6601   0.04553   0.04014   0.0651   0.2034   0.7602
  12.500   0.6782   0.04615   0.04077   0.0650   0.1978   0.7604
  12.750   0.6961   0.04679   0.04139   0.0648   0.1902   0.7605
  13.000   0.7120   0.04756   0.04210   0.0649   0.1804   0.7606
  13.250   0.7304   0.04819   0.04272   0.0647   0.1724   0.7607
  13.500   0.7463   0.04897   0.04344   0.0647   0.1627   0.7609
  13.750   0.7611   0.04983   0.04425   0.0647   0.1512   0.7610
  14.000   0.7724   0.05093   0.04527   0.0651   0.1358   0.7612
  14.250   0.7833   0.05206   0.04630   0.0655   0.1197   0.7613
  14.500   0.7953   0.05315   0.04731   0.0658   0.1061   0.7615
  14.750   0.8083   0.05420   0.04831   0.0659   0.0961   0.7616
  15.000   0.8213   0.05531   0.04940   0.0659   0.0890   0.7618
  15.250   0.8350   0.05636   0.05044   0.0658   0.0830   0.7619
  15.500   0.8487   0.05743   0.05149   0.0657   0.0772   0.7621
  15.750   0.8642   0.05840   0.05245   0.0654   0.0722   0.7623
  16.000   0.8780   0.05951   0.05354   0.0652   0.0671   0.7625
  16.250   0.8896   0.06083   0.05486   0.0651   0.0614   0.7627
  16.500   0.9019   0.06211   0.05613   0.0649   0.0554   0.7628
  16.750   0.9134   0.06344   0.05743   0.0647   0.0488   0.7630
  17.000   0.9235   0.06490   0.05885   0.0646   0.0420   0.7633
  17.250   0.9308   0.06663   0.06058   0.0647   0.0364   0.7635
  17.500   0.9399   0.06826   0.06220   0.0645   0.0319   0.7638
  17.750   0.9508   0.06979   0.06373   0.0641   0.0286   0.7640
  18.000   0.9605   0.07147   0.06542   0.0637   0.0259   0.7642
  18.250   0.9698   0.07323   0.06722   0.0631   0.0240   0.7644
  18.500   0.9795   0.07496   0.06896   0.0625   0.0222   0.7647
  18.750   0.9910   0.07658   0.07061   0.0618   0.0209   0.7649
  19.000   0.9989   0.07860   0.07267   0.0610   0.0197   0.7652
  19.250   1.0076   0.08057   0.07467   0.0602   0.0185   0.7655
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