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I.S.A. 960 (isa960-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: I.S.A. 960 (isa960-il)
Reynolds number: 1,000,000
Max Cl/Cd: 91.62 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-isa960-il-1000000-n5.txt
Download as CSV file: xf-isa960-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: I.S.A. 960                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -0.4192   0.15145   0.14710  -0.0130   0.2095   0.0040
 -14.000  -0.4151   0.14726   0.14289  -0.0146   0.2038   0.0041
 -12.000  -0.7052   0.02610   0.02299  -0.0981   0.9139   0.0049
 -11.750  -0.6875   0.02319   0.01976  -0.0987   0.8991   0.0050
 -11.500  -0.6664   0.02140   0.01775  -0.0989   0.8889   0.0051
 -11.250  -0.6436   0.02002   0.01619  -0.0989   0.8790   0.0053
 -11.000  -0.6200   0.01887   0.01485  -0.0987   0.8689   0.0054
 -10.750  -0.5958   0.01791   0.01371  -0.0986   0.8569   0.0056
 -10.500  -0.5713   0.01705   0.01268  -0.0983   0.8394   0.0057
 -10.250  -0.5477   0.01635   0.01169  -0.0977   0.7933   0.0059
 -10.000  -0.5244   0.01588   0.01084  -0.0970   0.7305   0.0061
  -9.750  -0.4994   0.01535   0.01006  -0.0967   0.6964   0.0063
  -9.500  -0.4736   0.01488   0.00937  -0.0964   0.6658   0.0065
  -9.250  -0.4546   0.01568   0.00893  -0.0952   0.3010   0.0066
  -9.000  -0.4294   0.01527   0.00818  -0.0950   0.2033   0.0069
  -8.750  -0.4026   0.01478   0.00755  -0.0949   0.1891   0.0073
  -8.500  -0.3759   0.01452   0.00707  -0.0947   0.1112   0.0078
  -8.250  -0.3485   0.01418   0.00665  -0.0946   0.1082   0.0082
  -8.000  -0.3210   0.01387   0.00625  -0.0945   0.1060   0.0088
  -7.750  -0.2934   0.01358   0.00587  -0.0944   0.1042   0.0092
  -7.500  -0.2658   0.01322   0.00542  -0.0942   0.1028   0.0098
  -7.250  -0.2381   0.01292   0.00507  -0.0942   0.1017   0.0107
  -7.000  -0.2103   0.01269   0.00477  -0.0941   0.1013   0.0116
  -6.750  -0.1823   0.01248   0.00450  -0.0940   0.1009   0.0125
  -6.500  -0.1544   0.01226   0.00423  -0.0939   0.1004   0.0139
  -6.250  -0.1265   0.01209   0.00405  -0.0938   0.0998   0.0158
  -6.000  -0.0985   0.01196   0.00388  -0.0938   0.0992   0.0174
  -5.750  -0.0705   0.01180   0.00367  -0.0937   0.0987   0.0191
  -5.500  -0.0425   0.01166   0.00351  -0.0937   0.0981   0.0211
  -5.250  -0.0144   0.01157   0.00338  -0.0936   0.0976   0.0231
  -5.000   0.0137   0.01151   0.00328  -0.0935   0.0971   0.0244
  -4.750   0.0418   0.01145   0.00316  -0.0935   0.0966   0.0252
  -4.500   0.0698   0.01132   0.00298  -0.0934   0.0962   0.0278
  -4.250   0.0978   0.01123   0.00286  -0.0934   0.0958   0.0299
  -4.000   0.1258   0.01117   0.00276  -0.0933   0.0955   0.0318
  -3.750   0.1538   0.01114   0.00269  -0.0933   0.0952   0.0334
  -3.500   0.1818   0.01110   0.00263  -0.0932   0.0949   0.0390
  -3.250   0.2096   0.01101   0.00263  -0.0932   0.0947   0.0616
  -3.000   0.2375   0.01104   0.00263  -0.0931   0.0945   0.0657
  -2.750   0.2654   0.01106   0.00265  -0.0931   0.0944   0.0706
  -2.500   0.2933   0.01111   0.00268  -0.0931   0.0942   0.0736
  -2.250   0.3211   0.01118   0.00271  -0.0930   0.0940   0.0753
  -2.000   0.3489   0.01125   0.00276  -0.0929   0.0938   0.0761
  -1.750   0.3765   0.01132   0.00280  -0.0929   0.0935   0.0775
  -1.500   0.4041   0.01140   0.00287  -0.0928   0.0932   0.0795
  -1.250   0.4316   0.01148   0.00294  -0.0927   0.0931   0.0818
  -1.000   0.4590   0.01157   0.00303  -0.0927   0.0930   0.0839
  -0.750   0.4864   0.01167   0.00312  -0.0926   0.0929   0.0860
  -0.500   0.5137   0.01178   0.00323  -0.0925   0.0929   0.0884
  -0.250   0.5408   0.01188   0.00336  -0.0924   0.0928   0.0990
   0.000   0.5679   0.01196   0.00352  -0.0923   0.0928   0.1287
   0.250   0.5949   0.01209   0.00368  -0.0922   0.0927   0.1385
   0.500   0.6218   0.01224   0.00383  -0.0921   0.0927   0.1438
   0.750   0.6486   0.01240   0.00399  -0.0920   0.0927   0.1497
   1.000   0.6753   0.01256   0.00417  -0.0919   0.0927   0.1557
   1.250   0.7019   0.01273   0.00435  -0.0917   0.0927   0.1626
   1.500   0.7284   0.01289   0.00454  -0.0916   0.0927   0.1700
   1.750   0.7547   0.01307   0.00475  -0.0914   0.0927   0.1818
   2.000   0.7810   0.01316   0.00498  -0.0913   0.0927   0.2422
   2.250   0.8071   0.01326   0.00522  -0.0912   0.0927   0.3038
   2.750   0.8549   0.01225   0.00580  -0.0902   0.0928   1.0000
   3.000   0.8803   0.01254   0.00607  -0.0899   0.0927   1.0000
   3.250   0.9047   0.01293   0.00646  -0.0895   0.0923   1.0000
   3.500   0.9319   0.01301   0.00653  -0.0895   0.0921   1.0000
   3.750   0.9577   0.01323   0.00674  -0.0893   0.0920   1.0000
   4.000   0.9830   0.01351   0.00702  -0.0890   0.0919   1.0000
   4.250   1.0080   0.01379   0.00730  -0.0887   0.0919   1.0000
   4.500   1.0339   0.01398   0.00749  -0.0885   0.0917   1.0000
   4.750   1.0602   0.01411   0.00763  -0.0884   0.0913   1.0000
   5.000   1.0877   0.01411   0.00765  -0.0885   0.0904   1.0000
   5.250   1.1166   0.01399   0.00753  -0.0889   0.0885   1.0000
   5.500   1.1443   0.01398   0.00751  -0.0891   0.0870   1.0000
   5.750   1.1728   0.01390   0.00741  -0.0894   0.0854   1.0000
   6.000   1.1999   0.01395   0.00744  -0.0894   0.0839   1.0000
   6.250   1.2267   0.01400   0.00751  -0.0895   0.0823   1.0000
   6.500   1.2570   0.01372   0.00702  -0.0902   0.0574   1.0000
   6.750   1.2774   0.01436   0.00759  -0.0892   0.0411   1.0000
   7.000   1.2941   0.01530   0.00838  -0.0877   0.0161   1.0000
   7.250   1.3160   0.01575   0.00884  -0.0870   0.0122   1.0000
   7.500   1.3376   0.01619   0.00931  -0.0862   0.0106   1.0000
   7.750   1.3582   0.01670   0.00984  -0.0853   0.0091   1.0000
   8.000   1.3792   0.01715   0.01032  -0.0844   0.0084   1.0000
   8.250   1.3995   0.01762   0.01083  -0.0835   0.0076   1.0000
   8.500   1.4187   0.01814   0.01138  -0.0824   0.0069   1.0000
   8.750   1.4361   0.01876   0.01202  -0.0810   0.0062   1.0000
   9.000   1.4537   0.01928   0.01259  -0.0797   0.0059   1.0000
   9.250   1.4690   0.01983   0.01318  -0.0779   0.0056   1.0000
   9.500   1.4836   0.02042   0.01382  -0.0761   0.0053   1.0000
   9.750   1.4977   0.02107   0.01452  -0.0743   0.0050   1.0000
  10.000   1.5111   0.02179   0.01528  -0.0725   0.0048   1.0000
  10.250   1.5234   0.02261   0.01616  -0.0706   0.0045   1.0000
  10.500   1.5334   0.02362   0.01723  -0.0686   0.0042   1.0000
  10.750   1.5456   0.02450   0.01817  -0.0670   0.0041   1.0000
  11.000   1.5571   0.02545   0.01919  -0.0654   0.0039   1.0000
  11.250   1.5681   0.02648   0.02029  -0.0639   0.0038   1.0000
  11.500   1.5783   0.02759   0.02146  -0.0624   0.0036   1.0000
  11.750   1.5874   0.02883   0.02277  -0.0609   0.0035   1.0000
  12.000   1.5959   0.03016   0.02417  -0.0595   0.0034   1.0000
  12.250   1.6034   0.03161   0.02569  -0.0582   0.0032   1.0000
  12.500   1.6098   0.03320   0.02738  -0.0569   0.0032   1.0000
  12.750   1.6153   0.03496   0.02921  -0.0557   0.0031   1.0000
  13.000   1.6189   0.03694   0.03127  -0.0546   0.0030   1.0000
  13.250   1.6202   0.03924   0.03367  -0.0536   0.0029   1.0000
  13.500   1.6186   0.04197   0.03650  -0.0527   0.0028   1.0000
  13.750   1.6166   0.04480   0.03945  -0.0521   0.0027   1.0000
  14.000   1.6161   0.04755   0.04230  -0.0516   0.0027   1.0000
  14.250   1.6146   0.05051   0.04536  -0.0513   0.0026   1.0000
  14.500   1.6109   0.05383   0.04879  -0.0512   0.0026   1.0000
  14.750   1.6063   0.05739   0.05247  -0.0513   0.0026   1.0000
  15.000   1.6004   0.06130   0.05649  -0.0517   0.0025   1.0000
  15.250   1.5928   0.06560   0.06091  -0.0524   0.0025   1.0000
  15.500   1.5836   0.07025   0.06569  -0.0533   0.0025   1.0000
  15.750   1.5724   0.07538   0.07094  -0.0545   0.0025   1.0000
  16.000   1.5608   0.08071   0.07639  -0.0559   0.0024   1.0000
  16.250   1.5465   0.08659   0.08242  -0.0577   0.0024   1.0000
  16.500   1.5305   0.09285   0.08881  -0.0597   0.0024   1.0000
  16.750   1.5138   0.09939   0.09547  -0.0619   0.0024   1.0000
  17.000   1.4955   0.10636   0.10257  -0.0645   0.0024   1.0000
  17.250   1.4766   0.11355   0.10990  -0.0672   0.0024   1.0000
  17.500   1.4582   0.12083   0.11731  -0.0702   0.0024   1.0000
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