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OAF117 AIRFOIL (oaf117-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: OAF117 AIRFOIL (oaf117-il)
Reynolds number: 500,000
Max Cl/Cd: 78.47 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-oaf117-il-500000-n5.txt
Download as CSV file: xf-oaf117-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: OAF117 AIRFOIL                                  
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -1.1456   0.08435   0.08088   0.0055   1.0000   0.0171
 -15.000  -1.1751   0.07566   0.07207   0.0003   1.0000   0.0171
 -14.750  -1.2052   0.06694   0.06321  -0.0052   1.0000   0.0171
 -14.500  -1.2345   0.05833   0.05445  -0.0111   1.0000   0.0171
 -14.250  -1.2605   0.04994   0.04591  -0.0173   1.0000   0.0171
 -14.000  -1.2812   0.04171   0.03748  -0.0250   1.0000   0.0171
 -13.750  -1.2764   0.03516   0.03066  -0.0349   1.0000   0.0174
 -13.500  -1.2625   0.03259   0.02790  -0.0372   1.0000   0.0177
 -13.250  -1.2452   0.03063   0.02579  -0.0386   1.0000   0.0180
 -13.000  -1.2265   0.02882   0.02387  -0.0399   1.0000   0.0184
 -12.750  -1.2052   0.02743   0.02240  -0.0407   1.0000   0.0189
 -12.500  -1.1822   0.02627   0.02114  -0.0413   1.0000   0.0194
 -12.250  -1.1583   0.02523   0.02000  -0.0418   1.0000   0.0200
 -12.000  -1.1337   0.02426   0.01892  -0.0423   1.0000   0.0206
 -11.750  -1.1085   0.02337   0.01791  -0.0427   1.0000   0.0212
 -11.500  -1.0832   0.02236   0.01683  -0.0432   1.0000   0.0219
 -11.250  -1.0570   0.02153   0.01595  -0.0437   1.0000   0.0225
 -11.000  -1.0303   0.02080   0.01515  -0.0441   1.0000   0.0232
 -10.750  -1.0032   0.02012   0.01439  -0.0445   1.0000   0.0240
 -10.500  -0.9758   0.01949   0.01366  -0.0448   1.0000   0.0248
 -10.250  -0.9482   0.01877   0.01289  -0.0453   1.0000   0.0257
 -10.000  -0.9204   0.01814   0.01222  -0.0457   1.0000   0.0265
  -9.750  -0.8922   0.01758   0.01161  -0.0461   1.0000   0.0274
  -9.500  -0.8637   0.01706   0.01102  -0.0464   1.0000   0.0284
  -9.250  -0.8351   0.01659   0.01048  -0.0468   1.0000   0.0294
  -9.000  -0.8064   0.01599   0.00987  -0.0472   1.0000   0.0306
  -8.750  -0.7775   0.01552   0.00937  -0.0476   1.0000   0.0318
  -8.500  -0.7483   0.01509   0.00889  -0.0480   1.0000   0.0331
  -8.250  -0.7190   0.01470   0.00844  -0.0483   1.0000   0.0343
  -8.000  -0.6897   0.01420   0.00794  -0.0488   1.0000   0.0359
  -7.750  -0.6602   0.01381   0.00753  -0.0492   1.0000   0.0376
  -7.500  -0.6306   0.01346   0.00714  -0.0495   1.0000   0.0392
  -7.250  -0.6008   0.01306   0.00673  -0.0500   1.0000   0.0410
  -7.000  -0.5710   0.01270   0.00637  -0.0504   1.0000   0.0432
  -6.750  -0.5411   0.01239   0.00604  -0.0508   1.0000   0.0455
  -6.500  -0.5110   0.01205   0.00569  -0.0512   0.9939   0.0479
  -6.250  -0.4802   0.01188   0.00548  -0.0516   0.9333   0.0510
  -6.000  -0.4543   0.01176   0.00526  -0.0509   0.8997   0.0541
  -5.750  -0.4275   0.01158   0.00501  -0.0504   0.8724   0.0582
  -5.500  -0.3997   0.01142   0.00477  -0.0502   0.8470   0.0627
  -5.250  -0.3714   0.01123   0.00451  -0.0501   0.8233   0.0694
  -5.000  -0.3425   0.01104   0.00427  -0.0501   0.8001   0.0780
  -4.750  -0.3134   0.01086   0.00406  -0.0502   0.7773   0.0895
  -4.500  -0.2841   0.01071   0.00386  -0.0503   0.7553   0.1033
  -4.250  -0.2546   0.01057   0.00368  -0.0505   0.7352   0.1161
  -4.000  -0.2250   0.01044   0.00352  -0.0507   0.7164   0.1279
  -3.750  -0.1953   0.01034   0.00336  -0.0509   0.6965   0.1384
  -3.500  -0.1655   0.01024   0.00322  -0.0511   0.6764   0.1499
  -3.250  -0.1357   0.01014   0.00310  -0.0513   0.6582   0.1646
  -3.000  -0.1059   0.01006   0.00299  -0.0516   0.6434   0.1787
  -2.750  -0.0760   0.00999   0.00289  -0.0518   0.6281   0.1923
  -2.500  -0.0461   0.00991   0.00279  -0.0520   0.6113   0.2069
  -2.250  -0.0162   0.00984   0.00272  -0.0523   0.5947   0.2246
  -2.000   0.0138   0.00973   0.00266  -0.0526   0.5811   0.2485
  -1.750   0.0438   0.00966   0.00261  -0.0529   0.5691   0.2699
  -1.500   0.0737   0.00962   0.00257  -0.0531   0.5576   0.2857
  -1.250   0.1037   0.00959   0.00254  -0.0533   0.5458   0.3022
  -1.000   0.1336   0.00956   0.00252  -0.0535   0.5348   0.3169
  -0.750   0.1634   0.00956   0.00250  -0.0537   0.5233   0.3307
  -0.500   0.1933   0.00955   0.00249  -0.0539   0.5112   0.3463
  -0.250   0.2232   0.00955   0.00250  -0.0541   0.5004   0.3616
   0.000   0.2530   0.00957   0.00250  -0.0543   0.4898   0.3758
   0.250   0.2828   0.00957   0.00252  -0.0545   0.4781   0.3915
   0.500   0.3127   0.00958   0.00255  -0.0547   0.4665   0.4088
   0.750   0.3424   0.00962   0.00259  -0.0549   0.4539   0.4253
   1.000   0.3722   0.00966   0.00262  -0.0551   0.4398   0.4409
   1.250   0.4019   0.00971   0.00267  -0.0553   0.4260   0.4559
   1.500   0.4316   0.00975   0.00273  -0.0555   0.4138   0.4750
   1.750   0.4613   0.00979   0.00280  -0.0557   0.4020   0.4955
   2.000   0.4910   0.00985   0.00287  -0.0559   0.3902   0.5155
   2.250   0.5206   0.00990   0.00295  -0.0561   0.3784   0.5362
   2.500   0.5502   0.00995   0.00305  -0.0563   0.3667   0.5598
   2.750   0.5797   0.00999   0.00316  -0.0565   0.3553   0.5911
   3.000   0.6092   0.01002   0.00328  -0.0567   0.3428   0.6323
   3.250   0.6385   0.01002   0.00342  -0.0569   0.3311   0.6830
   3.500   0.6672   0.01001   0.00357  -0.0569   0.3193   0.7439
   3.750   0.6940   0.00994   0.00371  -0.0564   0.3069   0.8253
   4.000   0.7156   0.00968   0.00364  -0.0545   0.2943   1.0000
   4.250   0.7450   0.00989   0.00380  -0.0548   0.2799   1.0000
   4.500   0.7742   0.01014   0.00397  -0.0550   0.2647   1.0000
   4.750   0.8034   0.01041   0.00415  -0.0552   0.2469   1.0000
   5.000   0.8324   0.01070   0.00436  -0.0554   0.2269   1.0000
   5.250   0.8612   0.01102   0.00457  -0.0556   0.2064   1.0000
   5.500   0.8899   0.01137   0.00482  -0.0558   0.1874   1.0000
   5.750   0.9185   0.01172   0.00510  -0.0560   0.1714   1.0000
   6.000   0.9470   0.01207   0.00538  -0.0561   0.1570   1.0000
   6.250   0.9754   0.01243   0.00567  -0.0563   0.1433   1.0000
   6.500   1.0036   0.01280   0.00599  -0.0564   0.1301   1.0000
   6.750   1.0316   0.01319   0.00632  -0.0565   0.1169   1.0000
   7.000   1.0594   0.01361   0.00667  -0.0566   0.1040   1.0000
   7.250   1.0869   0.01406   0.00706  -0.0566   0.0912   1.0000
   7.500   1.1142   0.01455   0.00748  -0.0567   0.0789   1.0000
   7.750   1.1413   0.01504   0.00791  -0.0567   0.0690   1.0000
   8.000   1.1682   0.01552   0.00837  -0.0567   0.0610   1.0000
   8.250   1.1949   0.01601   0.00884  -0.0566   0.0546   1.0000
   8.500   1.2213   0.01652   0.00933  -0.0566   0.0494   1.0000
   8.750   1.2476   0.01703   0.00985  -0.0565   0.0453   1.0000
   9.000   1.2736   0.01754   0.01037  -0.0563   0.0421   1.0000
   9.250   1.2992   0.01808   0.01092  -0.0561   0.0391   1.0000
   9.500   1.3245   0.01864   0.01150  -0.0559   0.0368   1.0000
   9.750   1.3497   0.01918   0.01208  -0.0557   0.0347   1.0000
  10.000   1.3740   0.01980   0.01272  -0.0554   0.0329   1.0000
  10.250   1.3981   0.02044   0.01340  -0.0550   0.0315   1.0000
  10.500   1.4219   0.02104   0.01405  -0.0546   0.0302   1.0000
  10.750   1.4450   0.02170   0.01476  -0.0542   0.0289   1.0000
  11.000   1.4668   0.02249   0.01557  -0.0537   0.0277   1.0000
  11.250   1.4885   0.02322   0.01637  -0.0531   0.0268   1.0000
  11.500   1.5098   0.02395   0.01717  -0.0524   0.0259   1.0000
  11.750   1.5298   0.02475   0.01803  -0.0517   0.0250   1.0000
  12.000   1.5483   0.02564   0.01898  -0.0508   0.0243   1.0000
  12.250   1.5648   0.02667   0.02006  -0.0498   0.0236   1.0000
  12.500   1.5790   0.02780   0.02126  -0.0485   0.0231   1.0000
  12.750   1.5925   0.02885   0.02241  -0.0471   0.0226   1.0000
  13.000   1.6027   0.03004   0.02370  -0.0455   0.0221   1.0000
  13.250   1.6067   0.03146   0.02522  -0.0433   0.0217   1.0000
  13.500   1.6096   0.03328   0.02715  -0.0419   0.0214   1.0000
  13.750   1.6127   0.03545   0.02942  -0.0413   0.0210   1.0000
  14.000   1.6149   0.03800   0.03208  -0.0412   0.0206   1.0000
  14.250   1.6156   0.04099   0.03517  -0.0417   0.0203   1.0000
  14.500   1.6138   0.04449   0.03877  -0.0426   0.0200   1.0000
  14.750   1.6088   0.04857   0.04297  -0.0438   0.0197   1.0000
  15.000   1.6008   0.05314   0.04766  -0.0454   0.0195   1.0000
  15.250   1.5948   0.05750   0.05215  -0.0468   0.0193   1.0000
  15.500   1.5861   0.06226   0.05704  -0.0483   0.0192   1.0000
  15.750   1.5758   0.06727   0.06219  -0.0500   0.0190   1.0000
  16.000   1.5635   0.07263   0.06767  -0.0519   0.0189   1.0000
  16.250   1.5500   0.07820   0.07337  -0.0538   0.0188   1.0000
  16.500   1.5359   0.08396   0.07927  -0.0560   0.0187   1.0000
  16.750   1.5222   0.08984   0.08526  -0.0582   0.0185   1.0000
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