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AVISTAR (avistar-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: AVISTAR (avistar-il)
Reynolds number: 500,000
Max Cl/Cd: 71.98 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-avistar-il-500000-n5.txt
Download as CSV file: xf-avistar-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: AVISTAR                                         
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.7819   0.05460   0.05129  -0.0673   1.0000   0.0206
 -12.500  -0.8032   0.04934   0.04585  -0.0701   1.0000   0.0207
 -12.250  -0.8191   0.04554   0.04189  -0.0708   1.0000   0.0207
 -12.000  -0.8279   0.04299   0.03921  -0.0700   1.0000   0.0208
 -11.750  -0.8362   0.04082   0.03691  -0.0680   1.0000   0.0209
 -11.500  -0.8410   0.03930   0.03529  -0.0650   1.0000   0.0210
 -11.250  -0.8427   0.03789   0.03378  -0.0621   0.9965   0.0210
 -11.000  -0.8284   0.03614   0.03187  -0.0623   0.9805   0.0212
 -10.750  -0.8126   0.03442   0.02998  -0.0623   0.9629   0.0214
 -10.500  -0.7974   0.03270   0.02807  -0.0619   0.9456   0.0216
 -10.250  -0.7843   0.03113   0.02630  -0.0607   0.9292   0.0218
 -10.000  -0.7725   0.02950   0.02443  -0.0589   0.9147   0.0221
  -9.750  -0.7602   0.02776   0.02243  -0.0571   0.9029   0.0225
  -9.500  -0.7470   0.02588   0.02025  -0.0554   0.8928   0.0230
  -9.250  -0.7317   0.02409   0.01814  -0.0538   0.8840   0.0235
  -9.000  -0.7138   0.02277   0.01651  -0.0524   0.8746   0.0239
  -8.750  -0.6932   0.02196   0.01561  -0.0515   0.8657   0.0242
  -8.500  -0.6715   0.02141   0.01498  -0.0507   0.8565   0.0244
  -8.250  -0.6490   0.02092   0.01441  -0.0500   0.8484   0.0246
  -8.000  -0.6263   0.02035   0.01376  -0.0493   0.8400   0.0249
  -7.750  -0.6034   0.01977   0.01307  -0.0486   0.8328   0.0252
  -7.500  -0.5796   0.01916   0.01237  -0.0480   0.8266   0.0255
  -7.250  -0.5559   0.01853   0.01165  -0.0474   0.8208   0.0259
  -7.000  -0.5319   0.01791   0.01093  -0.0468   0.8158   0.0263
  -6.750  -0.5075   0.01729   0.01022  -0.0463   0.8111   0.0267
  -6.500  -0.4830   0.01673   0.00956  -0.0458   0.8057   0.0272
  -6.250  -0.4581   0.01628   0.00900  -0.0453   0.8002   0.0276
  -6.000  -0.4340   0.01573   0.00841  -0.0447   0.7951   0.0280
  -5.750  -0.4090   0.01530   0.00798  -0.0443   0.7896   0.0284
  -5.500  -0.3839   0.01493   0.00759  -0.0439   0.7841   0.0288
  -5.250  -0.3589   0.01457   0.00718  -0.0434   0.7789   0.0291
  -5.000  -0.3336   0.01421   0.00679  -0.0429   0.7738   0.0296
  -4.750  -0.3083   0.01385   0.00640  -0.0425   0.7679   0.0301
  -4.500  -0.2832   0.01351   0.00601  -0.0420   0.7617   0.0306
  -4.250  -0.2580   0.01319   0.00564  -0.0414   0.7556   0.0312
  -4.000  -0.2322   0.01292   0.00532  -0.0410   0.7486   0.0317
  -3.750  -0.2076   0.01257   0.00496  -0.0404   0.7418   0.0324
  -3.500  -0.1819   0.01231   0.00470  -0.0400   0.7352   0.0330
  -3.250  -0.1562   0.01207   0.00444  -0.0396   0.7274   0.0337
  -3.000  -0.1305   0.01185   0.00418  -0.0391   0.7201   0.0344
  -2.750  -0.1045   0.01162   0.00394  -0.0387   0.7114   0.0351
  -2.500  -0.0787   0.01144   0.00370  -0.0383   0.7025   0.0359
  -2.250  -0.0525   0.01126   0.00349  -0.0379   0.6918   0.0366
  -2.000  -0.0271   0.01105   0.00325  -0.0374   0.6809   0.0377
  -1.750  -0.0011   0.01092   0.00309  -0.0370   0.6689   0.0390
  -1.500   0.0252   0.01080   0.00293  -0.0366   0.6568   0.0403
  -1.250   0.0514   0.01070   0.00278  -0.0363   0.6446   0.0415
  -1.000   0.0772   0.01059   0.00263  -0.0358   0.6319   0.0430
  -0.750   0.1034   0.01051   0.00251  -0.0354   0.6189   0.0449
  -0.500   0.1297   0.01046   0.00242  -0.0351   0.6065   0.0472
  -0.250   0.1557   0.01041   0.00233  -0.0347   0.5942   0.0506
   0.250   0.2075   0.01030   0.00219  -0.0338   0.5690   0.0691
   0.500   0.2199   0.00906   0.00201  -0.0313   0.5580   0.4048
   0.750   0.2403   0.00870   0.00199  -0.0298   0.5459   0.5178
   1.000   0.2592   0.00835   0.00205  -0.0279   0.5359   0.6404
   1.250   0.2823   0.00829   0.00210  -0.0268   0.5266   0.6920
   1.500   0.3069   0.00822   0.00215  -0.0260   0.5185   0.7309
   1.750   0.3311   0.00817   0.00220  -0.0252   0.5104   0.7699
   2.000   0.3567   0.00810   0.00227  -0.0246   0.5028   0.8094
   2.250   0.3865   0.00804   0.00237  -0.0249   0.4950   0.8663
   2.500   0.4246   0.00808   0.00246  -0.0271   0.4883   0.9084
   2.750   0.4780   0.00820   0.00257  -0.0330   0.4742   0.9292
   3.000   0.5263   0.00838   0.00269  -0.0378   0.4567   0.9374
   3.250   0.5736   0.00857   0.00282  -0.0423   0.4394   0.9434
   3.500   0.6166   0.00882   0.00298  -0.0458   0.4183   0.9498
   3.750   0.6579   0.00914   0.00316  -0.0490   0.3843   0.9568
   4.000   0.6932   0.00984   0.00349  -0.0512   0.3095   0.9667
   4.500   0.7456   0.01154   0.00450  -0.0518   0.1883   0.9981
   4.750   0.7609   0.01329   0.00552  -0.0506   0.0385   1.0000
   5.000   0.7817   0.01359   0.00580  -0.0494   0.0332   1.0000
   5.250   0.8027   0.01390   0.00608  -0.0482   0.0305   1.0000
   5.500   0.8241   0.01418   0.00637  -0.0470   0.0288   1.0000
   5.750   0.8449   0.01450   0.00668  -0.0458   0.0273   1.0000
   6.000   0.8650   0.01487   0.00705  -0.0445   0.0262   1.0000
   6.250   0.8857   0.01521   0.00740  -0.0432   0.0254   1.0000
   6.500   0.9058   0.01557   0.00776  -0.0419   0.0245   1.0000
   6.750   0.9254   0.01595   0.00815  -0.0405   0.0237   1.0000
   7.000   0.9442   0.01638   0.00859  -0.0390   0.0230   1.0000
   7.250   0.9614   0.01689   0.00910  -0.0373   0.0223   1.0000
   7.500   0.9796   0.01733   0.00955  -0.0357   0.0219   1.0000
   7.750   0.9968   0.01781   0.01006  -0.0340   0.0215   1.0000
   8.000   1.0130   0.01832   0.01060  -0.0321   0.0210   1.0000
   8.250   1.0269   0.01885   0.01116  -0.0298   0.0206   1.0000
   8.500   1.0372   0.01940   0.01173  -0.0269   0.0203   1.0000
   8.750   1.0473   0.01999   0.01235  -0.0241   0.0200   1.0000
   9.000   1.0577   0.02066   0.01305  -0.0216   0.0197   1.0000
   9.250   1.0679   0.02141   0.01384  -0.0192   0.0195   1.0000
   9.500   1.0772   0.02230   0.01475  -0.0169   0.0192   1.0000
   9.750   1.0849   0.02335   0.01584  -0.0146   0.0190   1.0000
  10.000   1.0932   0.02445   0.01699  -0.0125   0.0188   1.0000
  10.250   1.1034   0.02550   0.01809  -0.0108   0.0187   1.0000
  10.500   1.1128   0.02666   0.01930  -0.0092   0.0185   1.0000
  10.750   1.1218   0.02790   0.02060  -0.0077   0.0183   1.0000
  11.000   1.1306   0.02920   0.02197  -0.0062   0.0181   1.0000
  11.250   1.1392   0.03058   0.02340  -0.0049   0.0179   1.0000
  11.500   1.1476   0.03201   0.02489  -0.0037   0.0176   1.0000
  11.750   1.1559   0.03350   0.02643  -0.0026   0.0174   1.0000
  12.000   1.1638   0.03507   0.02806  -0.0016   0.0172   1.0000
  12.250   1.1708   0.03674   0.02979  -0.0007   0.0170   1.0000
  12.500   1.1777   0.03848   0.03158   0.0002   0.0169   1.0000
  12.750   1.1841   0.04030   0.03346   0.0010   0.0167   1.0000
  13.000   1.1901   0.04218   0.03539   0.0017   0.0166   1.0000
  13.250   1.1961   0.04411   0.03738   0.0023   0.0164   1.0000
  13.500   1.2017   0.04611   0.03943   0.0029   0.0163   1.0000
  13.750   1.2072   0.04817   0.04154   0.0034   0.0162   1.0000
  14.000   1.2123   0.05030   0.04372   0.0038   0.0161   1.0000
  14.250   1.2171   0.05249   0.04596   0.0042   0.0160   1.0000
  14.500   1.2219   0.05469   0.04821   0.0046   0.0159   1.0000
  14.750   1.2263   0.05693   0.05049   0.0051   0.0157   1.0000
  15.000   1.2318   0.05915   0.05280   0.0053   0.0157   1.0000
  15.250   1.2369   0.06145   0.05519   0.0055   0.0156   1.0000
  15.500   1.2418   0.06381   0.05764   0.0056   0.0155   1.0000
  15.750   1.2463   0.06623   0.06015   0.0057   0.0154   1.0000
  16.000   1.2503   0.06875   0.06276   0.0057   0.0153   1.0000
  16.250   1.2537   0.07134   0.06545   0.0056   0.0152   1.0000
  16.500   1.2565   0.07405   0.06827   0.0055   0.0151   1.0000
  16.750   1.2588   0.07688   0.07121   0.0053   0.0150   1.0000
  17.000   1.2600   0.07990   0.07434   0.0049   0.0149   1.0000
  17.250   1.2606   0.08305   0.07761   0.0044   0.0148   1.0000
  17.500   1.2600   0.08642   0.08108   0.0037   0.0146   1.0000
  17.750   1.2587   0.08994   0.08472   0.0029   0.0145   1.0000
  18.000   1.2569   0.09361   0.08850   0.0019   0.0144   1.0000
  18.250   1.2540   0.09749   0.09250   0.0007   0.0143   1.0000
  18.500   1.2504   0.10152   0.09665  -0.0006   0.0142   1.0000
  18.750   1.2457   0.10578   0.10103  -0.0021   0.0141   1.0000
  19.000   1.2399   0.11030   0.10569  -0.0038   0.0140   1.0000
  19.250   1.2331   0.11511   0.11062  -0.0058   0.0139   1.0000
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