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ONERA OA212 AIRFOIL (oa212-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: ONERA OA212 AIRFOIL (oa212-il)
Reynolds number: 1,000,000
Max Cl/Cd: 87.03 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-oa212-il-1000000-n5.txt
Download as CSV file: xf-oa212-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: ONERA OA212 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -1.4335   0.04891   0.04579  -0.0163   0.9062   0.0139
 -16.000  -1.4542   0.04409   0.04077  -0.0166   0.9034   0.0139
 -15.750  -1.4657   0.04089   0.03740  -0.0152   0.9007   0.0140
 -15.500  -1.4720   0.03838   0.03474  -0.0133   0.8981   0.0140
 -15.250  -1.4756   0.03634   0.03256  -0.0107   0.8950   0.0141
 -15.000  -1.4767   0.03470   0.03079  -0.0077   0.8918   0.0142
 -14.750  -1.4701   0.03321   0.02916  -0.0057   0.8890   0.0143
 -14.500  -1.4599   0.03183   0.02766  -0.0039   0.8865   0.0144
 -14.250  -1.4472   0.03055   0.02624  -0.0024   0.8843   0.0145
 -14.000  -1.4320   0.02936   0.02494  -0.0012   0.8817   0.0146
 -13.750  -1.4151   0.02828   0.02375  -0.0001   0.8788   0.0147
 -13.500  -1.3969   0.02730   0.02266   0.0009   0.8760   0.0148
 -13.250  -1.3777   0.02639   0.02164   0.0019   0.8734   0.0149
 -13.000  -1.3576   0.02556   0.02069   0.0028   0.8708   0.0150
 -12.750  -1.3393   0.02445   0.01947   0.0038   0.8682   0.0152
 -12.500  -1.3184   0.02350   0.01844   0.0045   0.8655   0.0154
 -12.250  -1.2962   0.02268   0.01755   0.0051   0.8624   0.0156
 -12.000  -1.2734   0.02195   0.01674   0.0057   0.8592   0.0158
 -11.750  -1.2501   0.02128   0.01600   0.0062   0.8561   0.0160
 -11.500  -1.2263   0.02065   0.01529   0.0067   0.8532   0.0162
 -11.250  -1.2019   0.02006   0.01463   0.0071   0.8504   0.0164
 -11.000  -1.1768   0.01947   0.01398   0.0074   0.8470   0.0166
 -10.750  -1.1515   0.01891   0.01336   0.0078   0.8434   0.0168
 -10.500  -1.1261   0.01838   0.01275   0.0081   0.8399   0.0171
 -10.250  -1.1005   0.01787   0.01216   0.0084   0.8364   0.0173
 -10.000  -1.0745   0.01739   0.01160   0.0086   0.8331   0.0175
  -9.750  -1.0479   0.01692   0.01108   0.0088   0.8295   0.0178
  -9.500  -1.0211   0.01649   0.01058   0.0089   0.8256   0.0179
  -9.250  -0.9949   0.01594   0.00998   0.0091   0.8215   0.0183
  -9.000  -0.9682   0.01549   0.00947   0.0093   0.8177   0.0187
  -8.750  -0.9408   0.01509   0.00904   0.0093   0.8142   0.0190
  -8.500  -0.9132   0.01471   0.00863   0.0094   0.8102   0.0194
  -8.250  -0.8855   0.01437   0.00825   0.0094   0.8058   0.0199
  -8.000  -0.8578   0.01405   0.00787   0.0094   0.8015   0.0204
  -7.750  -0.8298   0.01374   0.00751   0.0094   0.7977   0.0208
  -7.500  -0.8015   0.01343   0.00716   0.0094   0.7937   0.0211
  -7.250  -0.7734   0.01306   0.00676   0.0093   0.7891   0.0217
  -7.000  -0.7452   0.01274   0.00642   0.0093   0.7845   0.0223
  -6.750  -0.7167   0.01246   0.00611   0.0092   0.7806   0.0229
  -6.500  -0.6880   0.01219   0.00582   0.0090   0.7765   0.0235
  -6.250  -0.6592   0.01194   0.00554   0.0089   0.7718   0.0242
  -6.000  -0.6303   0.01171   0.00527   0.0088   0.7672   0.0247
  -5.750  -0.6016   0.01144   0.00498   0.0086   0.7631   0.0256
  -5.500  -0.5725   0.01120   0.00474   0.0084   0.7590   0.0267
  -5.250  -0.5433   0.01099   0.00452   0.0082   0.7542   0.0278
  -5.000  -0.5141   0.01081   0.00430   0.0080   0.7490   0.0287
  -4.750  -0.4848   0.01058   0.00406   0.0078   0.7428   0.0301
  -4.500  -0.4554   0.01038   0.00385   0.0076   0.7340   0.0315
  -4.250  -0.4258   0.01023   0.00366   0.0073   0.7256   0.0329
  -4.000  -0.3963   0.01004   0.00347   0.0070   0.7171   0.0348
  -3.750  -0.3666   0.00989   0.00329   0.0067   0.7088   0.0371
  -3.500  -0.3368   0.00973   0.00312   0.0064   0.6994   0.0395
  -3.250  -0.3069   0.00959   0.00297   0.0060   0.6906   0.0423
  -3.000  -0.2770   0.00945   0.00283   0.0057   0.6824   0.0453
  -2.750  -0.2470   0.00933   0.00270   0.0053   0.6755   0.0491
  -2.500  -0.2171   0.00919   0.00258   0.0049   0.6676   0.0535
  -2.250  -0.1869   0.00910   0.00247   0.0045   0.6590   0.0577
  -2.000  -0.1569   0.00898   0.00237   0.0041   0.6510   0.0630
  -1.750  -0.1266   0.00889   0.00228   0.0037   0.6420   0.0684
  -1.500  -0.0964   0.00880   0.00220   0.0032   0.6318   0.0739
  -1.250  -0.0660   0.00872   0.00212   0.0027   0.6212   0.0803
  -1.000  -0.0355   0.00866   0.00205   0.0022   0.6099   0.0866
  -0.750  -0.0051   0.00859   0.00199   0.0017   0.5983   0.0952
  -0.500   0.0255   0.00854   0.00193   0.0011   0.5838   0.1042
  -0.250   0.0563   0.00852   0.00189   0.0005   0.5668   0.1148
   0.000   0.0870   0.00849   0.00186  -0.0001   0.5493   0.1283
   0.250   0.1179   0.00846   0.00183  -0.0008   0.5276   0.1486
   0.500   0.1490   0.00846   0.00182  -0.0016   0.4997   0.1767
   0.750   0.1802   0.00843   0.00183  -0.0026   0.4679   0.2263
   1.000   0.2112   0.00830   0.00185  -0.0035   0.4409   0.3063
   1.250   0.2421   0.00808   0.00186  -0.0045   0.4165   0.4183
   1.500   0.2692   0.00680   0.00196  -0.0050   0.3972   0.8499
   1.750   0.2983   0.00694   0.00208  -0.0051   0.3819   0.8741
   2.000   0.3280   0.00707   0.00217  -0.0054   0.3696   0.8871
   2.250   0.3579   0.00722   0.00227  -0.0058   0.3582   0.8977
   2.500   0.3864   0.00737   0.00239  -0.0058   0.3476   0.9069
   2.750   0.4158   0.00751   0.00249  -0.0061   0.3397   0.9152
   3.000   0.4427   0.00765   0.00262  -0.0057   0.3308   0.9230
   3.250   0.4708   0.00780   0.00275  -0.0056   0.3236   0.9310
   3.500   0.5000   0.00790   0.00281  -0.0059   0.3160   0.9334
   3.750   0.5300   0.00800   0.00288  -0.0064   0.3090   0.9343
   4.000   0.5598   0.00810   0.00296  -0.0068   0.3027   0.9354
   4.250   0.5898   0.00823   0.00305  -0.0073   0.2953   0.9363
   4.500   0.6197   0.00833   0.00314  -0.0078   0.2896   0.9372
   4.750   0.6497   0.00845   0.00324  -0.0084   0.2826   0.9381
   5.000   0.6796   0.00859   0.00334  -0.0089   0.2758   0.9391
   5.250   0.7094   0.00871   0.00345  -0.0094   0.2686   0.9402
   5.500   0.7391   0.00888   0.00358  -0.0100   0.2594   0.9412
   5.750   0.7688   0.00910   0.00372  -0.0106   0.2438   0.9420
   6.000   0.7983   0.00937   0.00389  -0.0112   0.2234   0.9429
   6.250   0.8278   0.00961   0.00407  -0.0118   0.2088   0.9437
   6.500   0.8570   0.00988   0.00426  -0.0124   0.1943   0.9445
   6.750   0.8860   0.01018   0.00448  -0.0130   0.1776   0.9454
   7.250   0.9420   0.01097   0.00505  -0.0139   0.1374   0.9474
   7.500   0.9689   0.01146   0.00541  -0.0142   0.1143   0.9484
   7.750   0.9954   0.01199   0.00581  -0.0145   0.0924   0.9494
   8.000   1.0216   0.01251   0.00622  -0.0148   0.0737   0.9504
   8.250   1.0475   0.01302   0.00665  -0.0149   0.0591   0.9515
   8.500   1.0734   0.01349   0.00706  -0.0151   0.0487   0.9526
   8.750   1.0992   0.01394   0.00746  -0.0152   0.0414   0.9537
   9.000   1.1248   0.01437   0.00787  -0.0153   0.0360   0.9550
   9.250   1.1503   0.01479   0.00828  -0.0154   0.0321   0.9564
   9.500   1.1754   0.01523   0.00870  -0.0154   0.0291   0.9579
   9.750   1.2004   0.01566   0.00913  -0.0154   0.0268   0.9591
  10.000   1.2247   0.01609   0.00958  -0.0153   0.0250   0.9604
  10.250   1.2481   0.01652   0.01002  -0.0151   0.0235   0.9619
  10.500   1.2706   0.01702   0.01053  -0.0148   0.0221   0.9637
  10.750   1.2931   0.01748   0.01102  -0.0144   0.0212   0.9656
  11.000   1.3148   0.01798   0.01155  -0.0141   0.0201   0.9677
  11.250   1.3355   0.01857   0.01216  -0.0137   0.0191   0.9701
  11.750   1.3722   0.01979   0.01346  -0.0123   0.0178   0.9773
  12.250   1.4043   0.02123   0.01498  -0.0106   0.0166   1.0000
  12.500   1.4201   0.02211   0.01589  -0.0099   0.0161   1.0000
  12.750   1.4347   0.02309   0.01691  -0.0092   0.0156   1.0000
  13.000   1.4499   0.02405   0.01791  -0.0086   0.0153   1.0000
  13.250   1.4644   0.02505   0.01897  -0.0080   0.0149   1.0000
  13.500   1.4781   0.02615   0.02013  -0.0074   0.0146   1.0000
  13.750   1.4907   0.02734   0.02137  -0.0068   0.0143   1.0000
  14.000   1.5022   0.02865   0.02273  -0.0063   0.0139   1.0000
  14.250   1.5126   0.03009   0.02421  -0.0057   0.0136   1.0000
  14.500   1.5214   0.03168   0.02586  -0.0052   0.0133   1.0000
  14.750   1.5285   0.03348   0.02772  -0.0047   0.0130   1.0000
  15.000   1.5346   0.03542   0.02973  -0.0044   0.0127   1.0000
  15.250   1.5413   0.03734   0.03173  -0.0041   0.0126   1.0000
  15.500   1.5466   0.03946   0.03392  -0.0039   0.0124   1.0000
  15.750   1.5507   0.04176   0.03630  -0.0039   0.0122   1.0000
  16.000   1.5532   0.04428   0.03891  -0.0039   0.0121   1.0000
  16.250   1.5546   0.04704   0.04176  -0.0041   0.0119   1.0000
  16.500   1.5546   0.05008   0.04488  -0.0046   0.0118   1.0000
  16.750   1.5533   0.05336   0.04825  -0.0052   0.0116   1.0000
  17.000   1.5505   0.05695   0.05194  -0.0060   0.0115   1.0000
  17.250   1.5458   0.06093   0.05601  -0.0071   0.0114   1.0000
  17.500   1.5396   0.06520   0.06039  -0.0084   0.0113   1.0000
  17.750   1.5311   0.06990   0.06519  -0.0099   0.0112   1.0000
  18.000   1.5214   0.07489   0.07029  -0.0116   0.0111   1.0000
  18.250   1.5096   0.08032   0.07582  -0.0136   0.0110   1.0000
  18.500   1.4964   0.08596   0.08157  -0.0157   0.0109   1.0000
  18.750   1.4818   0.09193   0.08766  -0.0181   0.0109   1.0000
  19.000   1.4671   0.09796   0.09380  -0.0205   0.0108   1.0000
  19.250   1.4509   0.10425   0.10019  -0.0230   0.0107   1.0000
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