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AVISTAR (avistar-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: AVISTAR (avistar-il)
Reynolds number: 200,000
Max Cl/Cd: 63.93 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-avistar-il-200000.txt
Download as CSV file: xf-avistar-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.750  -0.4926   0.08007   0.07626  -0.0614   1.0000   0.0716
  -9.500  -0.5332   0.07615   0.07228  -0.0616   1.0000   0.0717
  -9.250  -0.5686   0.07508   0.07125  -0.0554   1.0000   0.0717
  -9.000  -0.5993   0.07446   0.07065  -0.0488   1.0000   0.0716
  -8.750  -0.6434   0.07167   0.06732  -0.0475   0.9933   0.0721
  -8.500  -0.5994   0.06568   0.06180  -0.0501   0.9941   0.0737
  -8.250  -0.5728   0.06283   0.05898  -0.0525   0.9896   0.0754
  -8.000  -0.5542   0.05889   0.05487  -0.0561   0.9841   0.0788
  -7.750  -0.5569   0.05349   0.04893  -0.0581   0.9741   0.0843
  -7.500  -0.5229   0.05069   0.04620  -0.0612   0.9711   0.0870
  -7.250  -0.5176   0.04779   0.04274  -0.0611   0.9620   0.0957
  -7.000  -0.4831   0.04485   0.03997  -0.0640   0.9598   0.0987
  -6.750  -0.4714   0.04286   0.03759  -0.0634   0.9517   0.1091
  -6.500  -0.4404   0.04076   0.03562  -0.0651   0.9476   0.1145
  -6.250  -0.4161   0.03861   0.03334  -0.0662   0.9435   0.1266
  -6.000  -0.4022   0.03718   0.03176  -0.0649   0.9347   0.1398
  -5.750  -0.3797   0.03566   0.03016  -0.0650   0.9292   0.1552
  -5.500  -0.3561   0.02834   0.02067  -0.0588   0.9216   0.0728
  -5.250  -0.3278   0.02649   0.01877  -0.0588   0.9154   0.0707
  -5.000  -0.2981   0.02451   0.01664  -0.0589   0.9106   0.0685
  -4.750  -0.2722   0.02310   0.01500  -0.0581   0.9037   0.0662
  -4.500  -0.2458   0.02204   0.01371  -0.0573   0.8964   0.0651
  -4.250  -0.2165   0.02103   0.01259  -0.0571   0.8911   0.0650
  -4.000  -0.1921   0.02026   0.01182  -0.0564   0.8828   0.0661
  -3.750  -0.1657   0.01951   0.01105  -0.0558   0.8760   0.0673
  -3.500  -0.1389   0.01880   0.01030  -0.0553   0.8699   0.0680
  -3.250  -0.1150   0.01820   0.00970  -0.0543   0.8610   0.0687
  -3.000  -0.0894   0.01759   0.00905  -0.0534   0.8545   0.0697
  -2.750  -0.0664   0.01713   0.00860  -0.0522   0.8454   0.0709
  -2.500  -0.0429   0.01659   0.00803  -0.0510   0.8375   0.0728
  -2.250  -0.0217   0.01599   0.00748  -0.0496   0.8293   0.0752
  -2.000   0.0007   0.01556   0.00706  -0.0483   0.8204   0.0775
  -1.750   0.0248   0.01521   0.00665  -0.0472   0.8130   0.0804
  -1.500   0.0476   0.01490   0.00630  -0.0460   0.8028   0.0841
  -1.250   0.0726   0.01453   0.00588  -0.0450   0.7955   0.0921
  -1.000   0.0946   0.01413   0.00562  -0.0437   0.7841   0.1143
  -0.750   0.0985   0.01219   0.00530  -0.0392   0.7763   0.5138
  -0.500   0.1093   0.01152   0.00545  -0.0349   0.7648   0.7165
  -0.250   0.1381   0.01120   0.00546  -0.0339   0.7569   0.8197
   0.000   0.1774   0.01116   0.00553  -0.0355   0.7457   0.8834
   0.250   0.2257   0.01120   0.00552  -0.0391   0.7364   0.9222
   0.500   0.2882   0.01136   0.00561  -0.0458   0.7252   0.9415
   0.750   0.3427   0.01164   0.00580  -0.0507   0.7138   0.9559
   1.000   0.3942   0.01188   0.00590  -0.0551   0.7038   0.9703
   1.250   0.4402   0.01201   0.00596  -0.0588   0.6900   0.9806
   1.500   0.4827   0.01205   0.00592  -0.0620   0.6764   0.9896
   1.750   0.5270   0.01206   0.00582  -0.0656   0.6639   0.9971
   2.000   0.5595   0.01201   0.00567  -0.0670   0.6521   1.0000
   2.250   0.5808   0.01197   0.00560  -0.0662   0.6408   1.0000
   2.500   0.6034   0.01198   0.00550  -0.0654   0.6322   1.0000
   2.750   0.6255   0.01201   0.00554  -0.0647   0.6219   1.0000
   3.000   0.6481   0.01207   0.00551  -0.0638   0.6118   1.0000
   3.250   0.6701   0.01212   0.00547  -0.0627   0.5991   1.0000
   3.500   0.6916   0.01217   0.00549  -0.0615   0.5844   1.0000
   3.750   0.7134   0.01226   0.00553  -0.0604   0.5700   1.0000
   4.000   0.7354   0.01238   0.00557  -0.0593   0.5556   1.0000
   4.250   0.7576   0.01252   0.00563  -0.0581   0.5414   1.0000
   4.500   0.7795   0.01267   0.00572  -0.0570   0.5257   1.0000
   4.750   0.8011   0.01283   0.00585  -0.0557   0.5092   1.0000
   5.000   0.8216   0.01300   0.00597  -0.0543   0.4876   1.0000
   5.250   0.8416   0.01319   0.00613  -0.0528   0.4625   1.0000
   5.500   0.8598   0.01345   0.00628  -0.0509   0.4262   1.0000
   5.750   0.8722   0.01402   0.00650  -0.0481   0.3496   1.0000
   6.000   0.8740   0.01545   0.00721  -0.0438   0.2464   1.0000
   6.250   0.8677   0.01755   0.00839  -0.0387   0.0974   1.0000
   6.500   0.8730   0.01888   0.00943  -0.0351   0.0632   1.0000
   6.750   0.8878   0.01954   0.01013  -0.0329   0.0585   1.0000
   7.000   0.9003   0.02032   0.01093  -0.0304   0.0555   1.0000
   7.250   0.9129   0.02105   0.01173  -0.0279   0.0537   1.0000
   7.500   0.9240   0.02179   0.01254  -0.0252   0.0523   1.0000
   7.750   0.9303   0.02258   0.01339  -0.0217   0.0511   1.0000
   8.000   0.9347   0.02349   0.01434  -0.0181   0.0500   1.0000
   8.250   0.9375   0.02461   0.01548  -0.0147   0.0490   1.0000
   8.500   0.9381   0.02602   0.01689  -0.0114   0.0481   1.0000
   8.750   0.9440   0.02730   0.01818  -0.0089   0.0472   1.0000
   9.000   0.9536   0.02842   0.01934  -0.0069   0.0465   1.0000
   9.250   0.9636   0.02961   0.02056  -0.0050   0.0460   1.0000
   9.500   0.9749   0.03081   0.02177  -0.0033   0.0455   1.0000
   9.750   0.9881   0.03197   0.02294  -0.0018   0.0450   1.0000
  10.000   1.0037   0.03308   0.02405  -0.0005   0.0446   1.0000
  10.250   1.0224   0.03413   0.02508   0.0006   0.0442   1.0000
  10.500   1.0444   0.03513   0.02607   0.0014   0.0439   1.0000
  10.750   1.0694   0.03614   0.02709   0.0019   0.0436   1.0000
  11.000   1.0971   0.03720   0.02815   0.0021   0.0432   1.0000
  11.250   1.1289   0.03841   0.02933   0.0017   0.0426   1.0000
  11.500   1.1708   0.03998   0.03087   0.0001   0.0420   1.0000
  11.750   1.2025   0.04152   0.03250  -0.0005   0.0422   1.0000
  12.000   1.2205   0.04304   0.03424   0.0006   0.0427   1.0000
  12.250   1.2333   0.04488   0.03639   0.0024   0.0436   1.0000
  12.500   1.2600   0.04740   0.03916   0.0024   0.0451   1.0000
  12.750   1.3461   0.05268   0.04441  -0.0063   0.0481   1.0000
  13.000   1.2832   0.04851   0.04114   0.0027   0.0550   1.0000
  13.250   1.2459   0.04950   0.04241   0.0106   0.0544   1.0000
  13.500   1.2088   0.04930   0.04256   0.0178   0.0564   1.0000
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