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FX 79-W-151 A (fx79w151a-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: FX 79-W-151 A (fx79w151a-il)
Reynolds number: 500,000
Max Cl/Cd: 102.03 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-fx79w151a-il-500000-n5.txt
Download as CSV file: xf-fx79w151a-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: FX 79-W-151 A                                   
  
 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  -0.7312   0.08212   0.07911  -0.0548   1.0000   0.0090
 -15.000  -0.7830   0.07010   0.06696  -0.0620   1.0000   0.0089
 -14.750  -0.8321   0.05782   0.05449  -0.0699   1.0000   0.0087
 -14.500  -0.8702   0.04574   0.04215  -0.0800   1.0000   0.0087
 -14.250  -0.8943   0.03823   0.03440  -0.0865   1.0000   0.0086
 -14.000  -0.8927   0.03419   0.03018  -0.0909   0.9743   0.0087
 -13.750  -0.8740   0.03076   0.02649  -0.0970   0.9524   0.0089
 -13.500  -0.8521   0.02885   0.02440  -0.1002   0.9343   0.0092
 -13.250  -0.8423   0.02718   0.02252  -0.1004   0.9145   0.0093
 -13.000  -0.8390   0.02588   0.02104  -0.0984   0.8971   0.0095
 -12.750  -0.8351   0.02486   0.01986  -0.0957   0.8829   0.0095
 -12.500  -0.8288   0.02403   0.01888  -0.0929   0.8707   0.0099
 -12.250  -0.8228   0.02324   0.01795  -0.0898   0.8597   0.0102
 -12.000  -0.8147   0.02257   0.01713  -0.0870   0.8498   0.0103
 -11.750  -0.8069   0.02161   0.01603  -0.0843   0.8405   0.0108
 -11.500  -0.7941   0.02085   0.01516  -0.0822   0.8322   0.0112
 -11.250  -0.7788   0.02023   0.01442  -0.0805   0.8244   0.0115
 -11.000  -0.7624   0.01960   0.01370  -0.0788   0.8163   0.0122
 -10.750  -0.7451   0.01904   0.01301  -0.0773   0.8089   0.0129
 -10.500  -0.7266   0.01849   0.01236  -0.0759   0.8014   0.0133
 -10.250  -0.7086   0.01788   0.01164  -0.0744   0.7941   0.0142
 -10.000  -0.6893   0.01732   0.01102  -0.0732   0.7868   0.0152
  -9.750  -0.6690   0.01685   0.01045  -0.0720   0.7798   0.0162
  -9.500  -0.6477   0.01641   0.00990  -0.0710   0.7730   0.0175
  -9.250  -0.6269   0.01593   0.00934  -0.0699   0.7659   0.0190
  -9.000  -0.6051   0.01551   0.00886  -0.0689   0.7594   0.0207
  -8.750  -0.5823   0.01516   0.00842  -0.0681   0.7524   0.0225
  -8.500  -0.5601   0.01476   0.00795  -0.0672   0.7461   0.0244
  -8.250  -0.5370   0.01440   0.00754  -0.0664   0.7390   0.0268
  -8.000  -0.5135   0.01412   0.00717  -0.0656   0.7323   0.0290
  -7.750  -0.4903   0.01374   0.00677  -0.0649   0.7256   0.0321
  -7.500  -0.4665   0.01346   0.00642  -0.0642   0.7191   0.0353
  -7.250  -0.4425   0.01316   0.00608  -0.0635   0.7131   0.0387
  -7.000  -0.4185   0.01287   0.00576  -0.0629   0.7063   0.0429
  -6.750  -0.3943   0.01261   0.00545  -0.0622   0.7001   0.0479
  -6.500  -0.3697   0.01236   0.00519  -0.0617   0.6933   0.0541
  -6.250  -0.3452   0.01213   0.00493  -0.0611   0.6871   0.0606
  -6.000  -0.3199   0.01193   0.00471  -0.0606   0.6804   0.0666
  -5.750  -0.2950   0.01173   0.00449  -0.0601   0.6739   0.0733
  -5.500  -0.2694   0.01159   0.00430  -0.0597   0.6680   0.0787
  -5.250  -0.2440   0.01141   0.00410  -0.0592   0.6615   0.0843
  -5.000  -0.2184   0.01129   0.00393  -0.0588   0.6552   0.0904
  -4.750  -0.1925   0.01116   0.00375  -0.0584   0.6489   0.0950
  -4.500  -0.1671   0.01102   0.00359  -0.0579   0.6427   0.1007
  -4.250  -0.1409   0.01092   0.00345  -0.0576   0.6366   0.1060
  -4.000  -0.1154   0.01079   0.00330  -0.0572   0.6300   0.1121
  -3.750  -0.0896   0.01069   0.00316  -0.0568   0.6244   0.1179
  -3.500  -0.0634   0.01059   0.00303  -0.0564   0.6184   0.1234
  -3.250  -0.0378   0.01048   0.00292  -0.0560   0.6126   0.1316
  -3.000  -0.0118   0.01039   0.00280  -0.0557   0.6071   0.1384
  -2.750   0.0141   0.01029   0.00269  -0.0553   0.6011   0.1462
  -2.250   0.0659   0.01012   0.00251  -0.0546   0.5900   0.1666
  -2.000   0.0916   0.01002   0.00243  -0.0542   0.5844   0.1813
  -1.500   0.1425   0.00980   0.00230  -0.0533   0.5737   0.2213
  -1.250   0.1676   0.00969   0.00225  -0.0528   0.5683   0.2496
  -1.000   0.1925   0.00957   0.00221  -0.0523   0.5636   0.2802
  -0.750   0.2175   0.00943   0.00217  -0.0519   0.5585   0.3174
  -0.500   0.2415   0.00928   0.00214  -0.0512   0.5528   0.3630
  -0.250   0.2646   0.00908   0.00212  -0.0503   0.5481   0.4256
   0.000   0.2872   0.00886   0.00212  -0.0494   0.5429   0.4945
   0.250   0.3091   0.00869   0.00212  -0.0482   0.5378   0.5579
   0.500   0.3304   0.00852   0.00214  -0.0469   0.5330   0.6195
   0.750   0.3513   0.00834   0.00217  -0.0454   0.5278   0.6841
   1.000   0.3717   0.00816   0.00222  -0.0438   0.5230   0.7562
   1.250   0.3978   0.00803   0.00229  -0.0433   0.5185   0.8226
   1.500   0.4476   0.00799   0.00242  -0.0481   0.5128   0.8866
   1.750   0.5220   0.00815   0.00258  -0.0583   0.5059   0.9267
   2.000   0.5678   0.00831   0.00272  -0.0622   0.5002   0.9433
   2.250   0.6030   0.00847   0.00286  -0.0638   0.4947   0.9563
   2.500   0.6377   0.00866   0.00301  -0.0652   0.4898   0.9686
   2.750   0.6707   0.00880   0.00314  -0.0664   0.4847   0.9770
   3.000   0.7073   0.00892   0.00323  -0.0685   0.4788   0.9798
   3.250   0.7413   0.00906   0.00333  -0.0700   0.4734   0.9836
   3.500   0.7743   0.00917   0.00344  -0.0713   0.4681   0.9873
   3.750   0.8104   0.00928   0.00354  -0.0733   0.4628   0.9896
   4.000   0.8456   0.00941   0.00365  -0.0751   0.4580   0.9925
   4.250   0.8806   0.00953   0.00378  -0.0769   0.4524   0.9955
   4.500   0.9159   0.00967   0.00390  -0.0788   0.4467   0.9984
   4.750   0.9489   0.00979   0.00402  -0.0802   0.4418   1.0000
   5.000   0.9710   0.00990   0.00415  -0.0793   0.4372   1.0000
   5.250   0.9925   0.01004   0.00429  -0.0782   0.4325   1.0000
   5.500   1.0137   0.01019   0.00445  -0.0771   0.4284   1.0000
   5.750   1.0356   0.01031   0.00460  -0.0761   0.4236   1.0000
   6.000   1.0567   0.01047   0.00477  -0.0750   0.4187   1.0000
   6.250   1.0770   0.01066   0.00496  -0.0737   0.4144   1.0000
   6.500   1.0987   0.01080   0.00515  -0.0727   0.4100   1.0000
   6.750   1.1193   0.01097   0.00535  -0.0715   0.4053   1.0000
   7.000   1.1388   0.01119   0.00557  -0.0700   0.4005   1.0000
   7.250   1.1592   0.01137   0.00579  -0.0688   0.3951   1.0000
   7.500   1.1767   0.01162   0.00603  -0.0670   0.3862   1.0000
   7.750   1.1926   0.01191   0.00630  -0.0650   0.3730   1.0000
   8.000   1.2054   0.01229   0.00662  -0.0625   0.3564   1.0000
   8.250   1.2166   0.01271   0.00698  -0.0597   0.3380   1.0000
   8.500   1.2232   0.01324   0.00741  -0.0561   0.3142   1.0000
   8.750   1.2263   0.01376   0.00785  -0.0518   0.2955   1.0000
   9.000   1.2281   0.01449   0.00846  -0.0478   0.2688   1.0000
   9.250   1.2242   0.01567   0.00944  -0.0434   0.2302   1.0000
   9.500   1.2215   0.01706   0.01065  -0.0396   0.1958   1.0000
   9.750   1.2129   0.01899   0.01234  -0.0357   0.1541   1.0000
  10.000   1.2095   0.02082   0.01401  -0.0328   0.1222   1.0000
  10.250   1.2064   0.02279   0.01584  -0.0303   0.0936   1.0000
  10.500   1.2058   0.02473   0.01768  -0.0283   0.0721   1.0000
  10.750   1.2035   0.02689   0.01975  -0.0264   0.0518   1.0000
  11.000   1.2008   0.02922   0.02200  -0.0248   0.0342   1.0000
  11.250   1.2042   0.03112   0.02389  -0.0236   0.0261   1.0000
  11.500   1.2065   0.03320   0.02598  -0.0226   0.0196   1.0000
  11.750   1.2104   0.03519   0.02800  -0.0217   0.0163   1.0000
  12.000   1.2159   0.03708   0.02994  -0.0209   0.0145   1.0000
  12.250   1.2201   0.03916   0.03207  -0.0203   0.0129   1.0000
  12.500   1.2244   0.04128   0.03424  -0.0197   0.0121   1.0000
  12.750   1.2291   0.04341   0.03645  -0.0192   0.0110   1.0000
  13.000   1.2337   0.04561   0.03872  -0.0188   0.0107   1.0000
  13.250   1.2371   0.04798   0.04114  -0.0185   0.0100   1.0000
  13.500   1.2405   0.05038   0.04362  -0.0182   0.0097   1.0000
  13.750   1.2402   0.05323   0.04652  -0.0180   0.0090   1.0000
  14.000   1.2424   0.05587   0.04926  -0.0178   0.0085   1.0000
  14.250   1.2459   0.05840   0.05187  -0.0178   0.0084   1.0000
  14.500   1.2474   0.06117   0.05471  -0.0178   0.0080   1.0000
  14.750   1.2501   0.06386   0.05747  -0.0178   0.0075   1.0000
  15.000   1.2493   0.06702   0.06072  -0.0179   0.0075   1.0000
  15.250   1.2508   0.06992   0.06367  -0.0181   0.0071   1.0000
  15.500   1.2503   0.07310   0.06692  -0.0184   0.0068   1.0000
  15.750   1.2481   0.07655   0.07045  -0.0187   0.0068   1.0000
  16.000   1.2434   0.08039   0.07437  -0.0192   0.0066   1.0000
  16.250   1.2434   0.08365   0.07772  -0.0197   0.0067   1.0000
  16.500   1.2446   0.08678   0.08094  -0.0202   0.0064   1.0000
  16.750   1.2409   0.09061   0.08486  -0.0208   0.0063   1.0000
  17.000   1.2417   0.09381   0.08814  -0.0214   0.0060   1.0000
  17.250   1.2398   0.09746   0.09187  -0.0221   0.0058   1.0000
  17.500   1.2386   0.10104   0.09553  -0.0229   0.0060   1.0000
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