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SM701 (sm701-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: SM701 (sm701-il)
Reynolds number: 200,000
Max Cl/Cd: 68.59 at α=5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-sm701-il-200000.txt
Download as CSV file: xf-sm701-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SM701                                           
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.3864   0.11578   0.11250  -0.0391   1.0000   0.0642
 -10.500  -0.3796   0.11185   0.10857  -0.0420   0.9981   0.0666
 -10.250  -0.4295   0.09486   0.09158  -0.0663   0.9907   0.0713
 -10.000  -0.4152   0.08935   0.08613  -0.0674   0.9881   0.0726
  -9.750  -0.3777   0.09076   0.08753  -0.0634   0.9864   0.0739
  -9.500  -0.3574   0.08790   0.08466  -0.0661   0.9839   0.0761
  -9.250  -0.2449   0.06960   0.06648  -0.0828   0.9621   0.0881
  -9.000  -0.2564   0.06139   0.05824  -0.0896   0.9590   0.0903
  -8.750  -0.2959   0.05365   0.05042  -0.0949   0.9490   0.0912
  -8.500  -0.3291   0.04848   0.04511  -0.0976   0.9391   0.0917
  -8.250  -0.3635   0.04466   0.04083  -0.0996   0.9274   0.0962
  -8.000  -0.4621   0.04163   0.03625  -0.0954   0.9239   0.0531
  -7.750  -0.4510   0.03531   0.02869  -0.0942   0.9180   0.0431
  -7.500  -0.4196   0.03294   0.02605  -0.0957   0.9159   0.0427
  -7.250  -0.3984   0.03095   0.02384  -0.0952   0.9110   0.0425
  -7.000  -0.3758   0.02953   0.02218  -0.0947   0.9055   0.0428
  -6.750  -0.3445   0.02728   0.01986  -0.0959   0.9032   0.0441
  -6.500  -0.3103   0.02597   0.01850  -0.0974   0.9014   0.0452
  -6.250  -0.2741   0.02471   0.01716  -0.0990   0.9001   0.0461
  -6.000  -0.2632   0.02419   0.01660  -0.0961   0.8920   0.0467
  -5.750  -0.2315   0.02324   0.01560  -0.0969   0.8892   0.0479
  -5.500  -0.1971   0.02232   0.01464  -0.0982   0.8872   0.0496
  -5.250  -0.1620   0.02128   0.01360  -0.0998   0.8857   0.0523
  -5.000  -0.1441   0.02081   0.01319  -0.0985   0.8799   0.0551
  -4.750  -0.1190   0.02028   0.01264  -0.0983   0.8751   0.0587
  -4.500  -0.0848   0.01932   0.01171  -0.1000   0.8729   0.0650
  -4.250  -0.0467   0.01826   0.01074  -0.1025   0.8713   0.0865
  -4.000  -0.0095   0.01534   0.00953  -0.1074   0.8700   0.4153
  -3.750   0.0297   0.01518   0.00968  -0.1092   0.8687   0.5466
  -3.500   0.0405   0.01566   0.01012  -0.1060   0.8596   0.5716
  -3.250   0.0762   0.01583   0.01024  -0.1069   0.8570   0.6033
  -3.000   0.1120   0.01606   0.01051  -0.1073   0.8550   0.6266
  -2.750   0.1496   0.01624   0.01068  -0.1082   0.8532   0.6457
  -2.500   0.1628   0.01669   0.01111  -0.1052   0.8448   0.6577
  -2.250   0.1969   0.01674   0.01110  -0.1057   0.8412   0.6706
  -2.000   0.2315   0.01690   0.01128  -0.1056   0.8386   0.6845
  -1.750   0.2683   0.01698   0.01136  -0.1059   0.8362   0.6971
  -1.500   0.2832   0.01712   0.01145  -0.1038   0.8268   0.7044
  -1.250   0.3223   0.01676   0.01101  -0.1056   0.8230   0.7083
  -1.000   0.3636   0.01644   0.01060  -0.1078   0.8199   0.7117
  -0.750   0.3795   0.01654   0.01069  -0.1057   0.8108   0.7159
  -0.500   0.4187   0.01621   0.01026  -0.1079   0.8063   0.7203
  -0.250   0.4507   0.01603   0.01002  -0.1088   0.8006   0.7240
   0.000   0.4756   0.01596   0.00994  -0.1081   0.7931   0.7269
   0.250   0.5130   0.01570   0.00960  -0.1097   0.7882   0.7300
   0.500   0.5363   0.01568   0.00958  -0.1089   0.7799   0.7340
   0.750   0.5716   0.01546   0.00927  -0.1104   0.7734   0.7386
   1.000   0.5992   0.01535   0.00915  -0.1103   0.7659   0.7416
   1.250   0.6275   0.01521   0.00900  -0.1102   0.7580   0.7446
   1.500   0.6566   0.01510   0.00886  -0.1103   0.7501   0.7484
   1.750   0.6856   0.01497   0.00870  -0.1105   0.7413   0.7530
   2.000   0.7141   0.01486   0.00856  -0.1106   0.7321   0.7573
   2.250   0.7428   0.01470   0.00838  -0.1105   0.7230   0.7604
   2.500   0.7660   0.01463   0.00834  -0.1095   0.7120   0.7644
   2.750   0.7959   0.01450   0.00817  -0.1098   0.7021   0.7691
   3.000   0.8225   0.01438   0.00803  -0.1095   0.6901   0.7741
   3.250   0.8438   0.01431   0.00800  -0.1080   0.6769   0.7782
   3.500   0.8674   0.01423   0.00793  -0.1071   0.6628   0.7830
   3.750   0.8924   0.01417   0.00783  -0.1065   0.6470   0.7887
   4.000   0.9137   0.01410   0.00778  -0.1051   0.6294   0.7931
   4.250   0.9345   0.01408   0.00772  -0.1035   0.6093   0.7984
   4.500   0.9555   0.01413   0.00770  -0.1022   0.5853   0.8053
   4.750   0.9729   0.01422   0.00769  -0.1000   0.5594   0.8107
   5.000   0.9898   0.01443   0.00779  -0.0979   0.5309   0.8173
   5.250   1.0066   0.01475   0.00795  -0.0960   0.5028   0.8242
   5.500   1.0204   0.01512   0.00818  -0.0933   0.4778   0.8310
   5.750   1.0356   0.01550   0.00847  -0.0912   0.4540   0.8393
   6.000   1.0468   0.01587   0.00876  -0.0881   0.4338   0.8473
   6.250   1.0604   0.01630   0.00910  -0.0858   0.4148   0.8570
   6.500   1.0731   0.01673   0.00946  -0.0831   0.3977   0.8675
   6.750   1.0855   0.01713   0.00984  -0.0805   0.3822   0.8785
   7.000   1.0980   0.01752   0.01022  -0.0779   0.3678   0.8915
   7.250   1.1093   0.01789   0.01058  -0.0751   0.3548   0.9073
   7.500   1.1179   0.01822   0.01090  -0.0717   0.3432   0.9301
   7.750   1.1319   0.01849   0.01115  -0.0697   0.3317   1.0000
   8.000   1.1575   0.01912   0.01177  -0.0704   0.3188   1.0000
   8.250   1.1811   0.01978   0.01238  -0.0707   0.3072   1.0000
   8.500   1.2035   0.02050   0.01299  -0.0707   0.2970   1.0000
   8.750   1.2238   0.02112   0.01363  -0.0703   0.2869   1.0000
   9.000   1.2445   0.02182   0.01429  -0.0698   0.2781   1.0000
   9.250   1.2630   0.02250   0.01494  -0.0690   0.2694   1.0000
   9.500   1.2821   0.02321   0.01566  -0.0683   0.2614   1.0000
   9.750   1.3000   0.02392   0.01635  -0.0674   0.2539   1.0000
  10.000   1.3190   0.02468   0.01711  -0.0667   0.2468   1.0000
  10.250   1.3350   0.02541   0.01788  -0.0656   0.2397   1.0000
  10.500   1.3546   0.02622   0.01864  -0.0650   0.2333   1.0000
  10.750   1.3695   0.02700   0.01952  -0.0638   0.2269   1.0000
  11.000   1.3871   0.02782   0.02030  -0.0630   0.2210   1.0000
  11.250   1.4030   0.02870   0.02126  -0.0619   0.2152   1.0000
  11.500   1.4167   0.02958   0.02220  -0.0607   0.2093   1.0000
  11.750   1.4376   0.03047   0.02300  -0.0604   0.2037   1.0000
  12.000   1.4472   0.03148   0.02419  -0.0588   0.1986   1.0000
  12.250   1.4601   0.03246   0.02522  -0.0576   0.1935   1.0000
  12.500   1.4793   0.03344   0.02612  -0.0571   0.1883   1.0000
  12.750   1.4871   0.03462   0.02751  -0.0555   0.1836   1.0000
  13.000   1.4978   0.03574   0.02871  -0.0543   0.1788   1.0000
  13.250   1.5167   0.03678   0.02964  -0.0539   0.1738   1.0000
  13.500   1.5211   0.03822   0.03131  -0.0523   0.1697   1.0000
  13.750   1.5292   0.03955   0.03274  -0.0511   0.1652   1.0000
  14.000   1.5423   0.04077   0.03392  -0.0503   0.1607   1.0000
  14.250   1.5493   0.04236   0.03567  -0.0492   0.1566   1.0000
  14.500   1.5537   0.04403   0.03749  -0.0480   0.1524   1.0000
  14.750   1.5605   0.04559   0.03909  -0.0470   0.1484   1.0000
  15.000   1.5711   0.04715   0.04066  -0.0464   0.1441   1.0000
  15.250   1.5709   0.04932   0.04304  -0.0453   0.1404   1.0000
  15.500   1.5737   0.05133   0.04515  -0.0445   0.1363   1.0000
  15.750   1.5833   0.05295   0.04671  -0.0441   0.1321   1.0000
  16.000   1.5799   0.05569   0.04968  -0.0434   0.1286   1.0000
  16.250   1.5781   0.05835   0.05250  -0.0430   0.1247   1.0000
  16.500   1.5791   0.06081   0.05499  -0.0427   0.1209   1.0000
  16.750   1.5797   0.06349   0.05773  -0.0426   0.1169   1.0000
  17.000   1.5739   0.06698   0.06143  -0.0428   0.1132   1.0000
  17.250   1.5709   0.07025   0.06480  -0.0431   0.1096   1.0000
  17.500   1.5730   0.07293   0.06740  -0.0434   0.1055   1.0000
  17.750   1.5635   0.07736   0.07211  -0.0443   0.1024   1.0000
  18.000   1.5568   0.08155   0.07645  -0.0455   0.0987   1.0000
  18.250   1.5524   0.08546   0.08040  -0.0466   0.0953   1.0000
  18.500   1.5465   0.08973   0.08477  -0.0479   0.0920   1.0000
  18.750   1.5367   0.09482   0.09008  -0.0499   0.0888   1.0000
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