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ONERA OA213 AIRFOIL (oa213-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: ONERA OA213 AIRFOIL (oa213-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.74 at α=9°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-oa213-il-1000000-n5.txt
Download as CSV file: xf-oa213-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: ONERA OA213 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.9864   0.03145   0.02791   0.0024   0.7902   0.0056
 -10.250  -0.9766   0.02784   0.02389   0.0035   0.7873   0.0056
 -10.000  -0.9595   0.02554   0.02133   0.0043   0.7841   0.0057
  -9.750  -0.9388   0.02395   0.01954   0.0049   0.7806   0.0058
  -9.500  -0.9163   0.02265   0.01807   0.0054   0.7772   0.0059
  -9.250  -0.8927   0.02157   0.01683   0.0058   0.7740   0.0059
  -9.000  -0.8681   0.02061   0.01575   0.0061   0.7708   0.0060
  -8.750  -0.8428   0.01975   0.01477   0.0064   0.7673   0.0061
  -8.500  -0.8172   0.01892   0.01383   0.0066   0.7635   0.0062
  -8.250  -0.7911   0.01819   0.01298   0.0069   0.7598   0.0063
  -8.000  -0.7646   0.01752   0.01220   0.0070   0.7564   0.0064
  -7.750  -0.7376   0.01691   0.01151   0.0071   0.7527   0.0066
  -7.500  -0.7104   0.01631   0.01082   0.0072   0.7487   0.0068
  -7.250  -0.6831   0.01573   0.01015   0.0073   0.7446   0.0069
  -7.000  -0.6556   0.01517   0.00947   0.0074   0.7407   0.0071
  -6.750  -0.6279   0.01460   0.00882   0.0075   0.7368   0.0073
  -6.500  -0.6000   0.01409   0.00823   0.0075   0.7322   0.0074
  -6.250  -0.5718   0.01364   0.00769   0.0075   0.7277   0.0075
  -6.000  -0.5436   0.01315   0.00713   0.0075   0.7235   0.0077
  -5.750  -0.5156   0.01260   0.00652   0.0075   0.7188   0.0080
  -5.500  -0.4870   0.01222   0.00610   0.0074   0.7136   0.0082
  -5.000  -0.4292   0.01159   0.00539   0.0071   0.7036   0.0088
  -4.750  -0.4002   0.01129   0.00505   0.0070   0.6977   0.0091
  -4.500  -0.3710   0.01101   0.00471   0.0068   0.6922   0.0094
  -4.250  -0.3417   0.01074   0.00441   0.0066   0.6862   0.0097
  -4.000  -0.3123   0.01051   0.00413   0.0064   0.6796   0.0100
  -3.750  -0.2829   0.01021   0.00380   0.0062   0.6723   0.0106
  -3.500  -0.2531   0.01002   0.00356   0.0059   0.6587   0.0112
  -3.250  -0.2231   0.00987   0.00334   0.0055   0.6408   0.0120
  -3.000  -0.1930   0.00972   0.00313   0.0051   0.6261   0.0129
  -2.500  -0.1327   0.00943   0.00275   0.0043   0.6012   0.0153
  -2.250  -0.1025   0.00929   0.00259   0.0038   0.5895   0.0168
  -2.000  -0.0722   0.00920   0.00245   0.0034   0.5770   0.0189
  -1.750  -0.0418   0.00910   0.00232   0.0029   0.5639   0.0218
  -1.500  -0.0113   0.00902   0.00221   0.0023   0.5500   0.0263
  -1.250   0.0192   0.00895   0.00211   0.0018   0.5351   0.0326
  -1.000   0.0497   0.00888   0.00203   0.0012   0.5206   0.0412
  -0.750   0.0803   0.00882   0.00197   0.0006   0.5039   0.0557
  -0.500   0.1110   0.00877   0.00192  -0.0001   0.4858   0.0744
  -0.250   0.1416   0.00870   0.00188  -0.0007   0.4674   0.1037
   0.000   0.1723   0.00862   0.00185  -0.0015   0.4432   0.1525
   0.250   0.2028   0.00838   0.00183  -0.0025   0.4160   0.2635
   0.500   0.2318   0.00745   0.00176  -0.0036   0.3906   0.5751
   0.750   0.2593   0.00691   0.00186  -0.0038   0.3648   0.8008
   1.000   0.2888   0.00705   0.00197  -0.0042   0.3380   0.8390
   1.250   0.3185   0.00720   0.00206  -0.0046   0.3162   0.8597
   1.500   0.3475   0.00733   0.00215  -0.0049   0.3000   0.8785
   1.750   0.3763   0.00746   0.00224  -0.0050   0.2864   0.8950
   2.000   0.4061   0.00761   0.00231  -0.0055   0.2734   0.8997
   2.250   0.4362   0.00777   0.00239  -0.0061   0.2605   0.9035
   2.500   0.4663   0.00793   0.00247  -0.0067   0.2487   0.9075
   2.750   0.4960   0.00805   0.00255  -0.0072   0.2404   0.9113
   3.000   0.5254   0.00821   0.00264  -0.0076   0.2318   0.9155
   3.250   0.5549   0.00833   0.00273  -0.0081   0.2243   0.9199
   3.500   0.5846   0.00851   0.00284  -0.0086   0.2160   0.9241
   3.750   0.6136   0.00863   0.00294  -0.0090   0.2093   0.9283
   4.000   0.6425   0.00879   0.00306  -0.0094   0.2027   0.9333
   4.250   0.6715   0.00892   0.00318  -0.0097   0.1982   0.9386
   4.500   0.7002   0.00907   0.00330  -0.0101   0.1930   0.9435
   4.750   0.7286   0.00924   0.00343  -0.0104   0.1876   0.9491
   5.000   0.7572   0.00937   0.00356  -0.0107   0.1839   0.9550
   5.250   0.7857   0.00953   0.00370  -0.0110   0.1792   0.9612
   5.500   0.8144   0.00972   0.00386  -0.0115   0.1738   0.9686
   5.750   0.8445   0.00988   0.00401  -0.0122   0.1701   0.9753
   6.000   0.8753   0.01005   0.00418  -0.0131   0.1666   0.9827
   6.250   0.9073   0.01026   0.00436  -0.0143   0.1628   0.9896
   6.500   0.9390   0.01049   0.00456  -0.0155   0.1587   1.0000
   6.750   0.9678   0.01067   0.00476  -0.0161   0.1565   1.0000
   7.000   0.9964   0.01087   0.00496  -0.0166   0.1539   1.0000
   7.250   1.0248   0.01110   0.00518  -0.0171   0.1510   1.0000
   7.500   1.0530   0.01135   0.00541  -0.0176   0.1480   1.0000
   7.750   1.0809   0.01162   0.00567  -0.0181   0.1446   1.0000
   8.000   1.1089   0.01184   0.00591  -0.0186   0.1417   1.0000
   8.250   1.1363   0.01214   0.00617  -0.0190   0.1367   1.0000
   8.500   1.1634   0.01245   0.00647  -0.0194   0.1327   1.0000
   8.750   1.1907   0.01272   0.00675  -0.0198   0.1303   1.0000
   9.000   1.2177   0.01299   0.00704  -0.0202   0.1275   1.0000
   9.250   1.2441   0.01332   0.00736  -0.0206   0.1237   1.0000
   9.500   1.2700   0.01369   0.00771  -0.0209   0.1201   1.0000
   9.750   1.2961   0.01400   0.00805  -0.0212   0.1178   1.0000
  10.000   1.3218   0.01434   0.00840  -0.0214   0.1146   1.0000
  10.250   1.3464   0.01477   0.00882  -0.0216   0.1101   1.0000
  10.500   1.3707   0.01521   0.00926  -0.0218   0.1055   1.0000
  10.750   1.3943   0.01569   0.00974  -0.0220   0.1002   1.0000
  11.000   1.4167   0.01629   0.01031  -0.0221   0.0941   1.0000
  11.250   1.4362   0.01709   0.01106  -0.0221   0.0837   1.0000
  11.500   1.4298   0.01961   0.01327  -0.0197   0.0410   1.0000
  11.750   1.4322   0.02148   0.01508  -0.0181   0.0243   1.0000
  12.000   1.4449   0.02259   0.01621  -0.0173   0.0209   1.0000
  12.250   1.4590   0.02358   0.01725  -0.0167   0.0193   1.0000
  12.500   1.4723   0.02467   0.01838  -0.0161   0.0181   1.0000
  12.750   1.4843   0.02587   0.01963  -0.0155   0.0170   1.0000
  13.000   1.4963   0.02709   0.02090  -0.0149   0.0163   1.0000
  13.250   1.5085   0.02830   0.02217  -0.0144   0.0157   1.0000
  13.500   1.5194   0.02964   0.02357  -0.0139   0.0151   1.0000
  13.750   1.5288   0.03115   0.02514  -0.0135   0.0145   1.0000
  14.000   1.5367   0.03280   0.02685  -0.0131   0.0140   1.0000
  14.250   1.5433   0.03463   0.02874  -0.0127   0.0136   1.0000
  14.500   1.5479   0.03670   0.03089  -0.0123   0.0131   1.0000
  14.750   1.5542   0.03862   0.03289  -0.0122   0.0129   1.0000
  15.000   1.5594   0.04072   0.03506  -0.0121   0.0126   1.0000
  15.250   1.5631   0.04303   0.03746  -0.0121   0.0123   1.0000
  15.500   1.5656   0.04556   0.04008  -0.0122   0.0120   1.0000
  15.750   1.5666   0.04837   0.04297  -0.0126   0.0117   1.0000
  16.000   1.5659   0.05147   0.04616  -0.0131   0.0114   1.0000
  16.250   1.5630   0.05493   0.04970  -0.0137   0.0110   1.0000
  16.500   1.5576   0.05880   0.05366  -0.0146   0.0107   1.0000
  16.750   1.5485   0.06333   0.05830  -0.0159   0.0104   1.0000
  17.000   1.5399   0.06786   0.06294  -0.0172   0.0102   1.0000
  17.250   1.5301   0.07269   0.06789  -0.0187   0.0101   1.0000
  17.500   1.5174   0.07807   0.07340  -0.0205   0.0100   1.0000
  17.750   1.5008   0.08413   0.07959  -0.0226   0.0099   1.0000
  18.000   1.4804   0.09095   0.08656  -0.0252   0.0099   1.0000
  18.250   1.4559   0.09862   0.09437  -0.0281   0.0098   1.0000
  18.500   1.4273   0.10705   0.10297  -0.0315   0.0099   1.0000
  18.750   1.3968   0.11602   0.11209  -0.0352   0.0099   1.0000
  19.000   1.3662   0.12516   0.12138  -0.0392   0.0100   1.0000
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