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I.S.A. 962 (isa962-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: I.S.A. 962 (isa962-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.54 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-isa962-il-1000000-n5.txt
Download as CSV file: xf-isa962-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: I.S.A. 962                                      
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.3490   0.09149   0.08963  -0.0365   0.9343   0.0172
 -10.250  -0.3417   0.08907   0.08712  -0.0374   0.9153   0.0173
  -9.250  -0.4016   0.02823   0.02525  -0.0944   0.8720   0.0206
  -9.000  -0.3829   0.02428   0.02092  -0.0959   0.8670   0.0208
  -8.750  -0.3600   0.02228   0.01871  -0.0963   0.8621   0.0209
  -8.500  -0.3362   0.02071   0.01692  -0.0964   0.8569   0.0211
  -8.250  -0.3117   0.01943   0.01545  -0.0964   0.8516   0.0212
  -8.000  -0.2866   0.01819   0.01402  -0.0964   0.8450   0.0214
  -7.750  -0.2613   0.01711   0.01274  -0.0962   0.8375   0.0215
  -7.500  -0.2354   0.01614   0.01160  -0.0960   0.8297   0.0217
  -7.250  -0.2094   0.01524   0.01051  -0.0958   0.8201   0.0219
  -7.000  -0.1828   0.01446   0.00957  -0.0956   0.8088   0.0221
  -6.750  -0.1561   0.01376   0.00871  -0.0953   0.7986   0.0222
  -6.500  -0.1292   0.01314   0.00793  -0.0951   0.7872   0.0224
  -6.250  -0.1021   0.01258   0.00723  -0.0948   0.7739   0.0226
  -6.000  -0.0749   0.01209   0.00659  -0.0946   0.7590   0.0228
  -5.750  -0.0477   0.01167   0.00604  -0.0943   0.7436   0.0230
  -5.500  -0.0202   0.01129   0.00553  -0.0941   0.7300   0.0232
  -5.250   0.0075   0.01098   0.00511  -0.0939   0.7187   0.0234
  -5.000   0.0354   0.01074   0.00478  -0.0937   0.7072   0.0236
  -4.750   0.0634   0.01051   0.00447  -0.0935   0.6956   0.0238
  -4.500   0.0912   0.01028   0.00416  -0.0934   0.6827   0.0239
  -4.250   0.1191   0.01009   0.00388  -0.0932   0.6702   0.0240
  -4.000   0.1469   0.00966   0.00338  -0.0930   0.6597   0.0244
  -3.750   0.1748   0.00943   0.00310  -0.0929   0.6491   0.0248
  -3.500   0.2027   0.00929   0.00289  -0.0927   0.6338   0.0250
  -3.250   0.2306   0.00918   0.00272  -0.0926   0.6194   0.0253
  -3.000   0.2588   0.00906   0.00256  -0.0925   0.6072   0.0256
  -2.750   0.2868   0.00898   0.00241  -0.0923   0.5923   0.0259
  -2.500   0.3146   0.00893   0.00229  -0.0922   0.5745   0.0263
  -2.250   0.3425   0.00888   0.00217  -0.0920   0.5574   0.0266
  -2.000   0.3705   0.00883   0.00206  -0.0919   0.5423   0.0271
  -1.750   0.3985   0.00880   0.00197  -0.0918   0.5266   0.0275
  -1.500   0.4263   0.00880   0.00190  -0.0917   0.5079   0.0279
  -1.250   0.4539   0.00884   0.00186  -0.0915   0.4875   0.0283
  -1.000   0.4814   0.00888   0.00180  -0.0914   0.4629   0.0290
  -0.750   0.5081   0.00901   0.00179  -0.0911   0.4259   0.0300
  -0.500   0.5342   0.00925   0.00184  -0.0908   0.3798   0.0308
  -0.250   0.5611   0.00941   0.00188  -0.0905   0.3533   0.0317
   0.000   0.5884   0.00951   0.00192  -0.0904   0.3368   0.0327
   0.500   0.6438   0.00963   0.00198  -0.0902   0.3174   0.0366
   0.750   0.6715   0.00968   0.00202  -0.0901   0.3101   0.0423
   1.000   0.6991   0.00964   0.00210  -0.0901   0.3035   0.0969
   1.250   0.7267   0.00969   0.00217  -0.0900   0.2951   0.1126
   1.500   0.7541   0.00975   0.00225  -0.0899   0.2873   0.1362
   1.750   0.7815   0.00964   0.00237  -0.0900   0.2805   0.2398
   2.000   0.8085   0.00963   0.00250  -0.0899   0.2706   0.3291
   2.250   0.8349   0.00944   0.00266  -0.0899   0.2587   0.5008
   2.750   0.8883   0.00893   0.00300  -0.0897   0.2117   1.0000
   3.000   0.9126   0.00937   0.00325  -0.0892   0.1779   1.0000
   3.250   0.9385   0.00964   0.00344  -0.0889   0.1665   1.0000
   3.500   0.9648   0.00986   0.00360  -0.0887   0.1601   1.0000
   3.750   0.9909   0.01010   0.00379  -0.0884   0.1535   1.0000
   4.000   1.0175   0.01027   0.00395  -0.0882   0.1504   1.0000
   4.250   1.0439   0.01045   0.00412  -0.0880   0.1470   1.0000
   4.500   1.0700   0.01067   0.00430  -0.0878   0.1429   1.0000
   4.750   1.0958   0.01090   0.00451  -0.0875   0.1387   1.0000
   5.000   1.1219   0.01109   0.00470  -0.0873   0.1359   1.0000
   5.250   1.1481   0.01128   0.00488  -0.0871   0.1333   1.0000
   5.500   1.1739   0.01149   0.00508  -0.0868   0.1304   1.0000
   5.750   1.1994   0.01172   0.00530  -0.0866   0.1272   1.0000
   6.000   1.2245   0.01198   0.00554  -0.0862   0.1232   1.0000
   6.250   1.2500   0.01219   0.00575  -0.0860   0.1198   1.0000
   6.500   1.2748   0.01246   0.00599  -0.0856   0.1141   1.0000
   6.750   1.2990   0.01277   0.00625  -0.0852   0.1084   1.0000
   7.000   1.3238   0.01301   0.00650  -0.0848   0.1048   1.0000
   7.250   1.3476   0.01333   0.00679  -0.0844   0.0996   1.0000
   7.500   1.3713   0.01365   0.00709  -0.0839   0.0946   1.0000
   7.750   1.3947   0.01397   0.00740  -0.0834   0.0900   1.0000
   8.000   1.4173   0.01435   0.00774  -0.0827   0.0850   1.0000
   8.250   1.4400   0.01469   0.00809  -0.0821   0.0805   1.0000
   8.500   1.4612   0.01514   0.00849  -0.0813   0.0747   1.0000
   8.750   1.4832   0.01551   0.00886  -0.0806   0.0710   1.0000
   9.000   1.5037   0.01596   0.00930  -0.0797   0.0664   1.0000
   9.250   1.5241   0.01640   0.00973  -0.0787   0.0624   1.0000
   9.500   1.5429   0.01692   0.01023  -0.0776   0.0571   1.0000
   9.750   1.5607   0.01746   0.01075  -0.0762   0.0516   1.0000
  10.000   1.5751   0.01813   0.01139  -0.0744   0.0446   1.0000
  10.250   1.5769   0.01945   0.01256  -0.0706   0.0245   1.0000
  10.500   1.5818   0.02067   0.01375  -0.0675   0.0156   1.0000
  10.750   1.5943   0.02145   0.01457  -0.0656   0.0139   1.0000
  11.000   1.6070   0.02223   0.01540  -0.0638   0.0130   1.0000
  11.250   1.6188   0.02311   0.01633  -0.0621   0.0122   1.0000
  11.500   1.6301   0.02406   0.01733  -0.0605   0.0115   1.0000
  11.750   1.6425   0.02496   0.01829  -0.0591   0.0112   1.0000
  12.000   1.6539   0.02595   0.01934  -0.0577   0.0107   1.0000
  12.250   1.6643   0.02706   0.02051  -0.0563   0.0103   1.0000
  12.500   1.6737   0.02828   0.02179  -0.0549   0.0099   1.0000
  12.750   1.6817   0.02965   0.02321  -0.0535   0.0095   1.0000
  13.000   1.6884   0.03117   0.02480  -0.0521   0.0091   1.0000
  13.250   1.6960   0.03265   0.02635  -0.0510   0.0089   1.0000
  13.500   1.7033   0.03420   0.02798  -0.0499   0.0087   1.0000
  13.750   1.7096   0.03590   0.02975  -0.0490   0.0085   1.0000
  14.000   1.7149   0.03776   0.03169  -0.0481   0.0084   1.0000
  14.250   1.7189   0.03978   0.03379  -0.0473   0.0082   1.0000
  14.500   1.7218   0.04199   0.03608  -0.0466   0.0080   1.0000
  14.750   1.7235   0.04440   0.03857  -0.0461   0.0078   1.0000
  15.000   1.7236   0.04703   0.04129  -0.0457   0.0076   1.0000
  15.250   1.7224   0.04992   0.04427  -0.0454   0.0075   1.0000
  15.500   1.7198   0.05309   0.04754  -0.0454   0.0074   1.0000
  15.750   1.7156   0.05657   0.05112  -0.0455   0.0072   1.0000
  16.000   1.7089   0.06048   0.05513  -0.0459   0.0071   1.0000
  16.250   1.7002   0.06478   0.05954  -0.0465   0.0070   1.0000
  16.500   1.6909   0.06932   0.06420  -0.0474   0.0069   1.0000
  16.750   1.6821   0.07388   0.06887  -0.0484   0.0068   1.0000
  17.000   1.6709   0.07889   0.07401  -0.0496   0.0068   1.0000
  17.250   1.6578   0.08436   0.07960  -0.0512   0.0067   1.0000
  17.500   1.6419   0.09041   0.08579  -0.0531   0.0067   1.0000
  17.750   1.6243   0.09684   0.09235  -0.0553   0.0066   1.0000
  18.000   1.6040   0.10389   0.09954  -0.0579   0.0066   1.0000
  18.250   1.5828   0.11125   0.10705  -0.0608   0.0066   1.0000
  18.500   1.5594   0.11904   0.11498  -0.0639   0.0066   1.0000
  18.750   1.5358   0.12700   0.12308  -0.0674   0.0066   1.0000
  19.000   1.5101   0.13554   0.13176  -0.0714   0.0066   1.0000
  19.250   1.4869   0.14379   0.14015  -0.0754   0.0066   1.0000
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