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NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0313 AIRFOIL (ms313-il)
Reynolds number: 500,000
Max Cl/Cd: 69.78 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ms313-il-500000-n5.txt
Download as CSV file: xf-ms313-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA/LANGLEY MS(1)-0313 AIRFOIL                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.9201   0.08413   0.08090  -0.0397   1.0000   0.0114
 -15.750  -0.9660   0.07029   0.06674  -0.0490   1.0000   0.0113
 -15.500  -0.9879   0.06242   0.05867  -0.0542   1.0000   0.0114
 -15.250  -1.0014   0.05663   0.05272  -0.0579   1.0000   0.0114
 -15.000  -1.0103   0.05199   0.04793  -0.0604   1.0000   0.0115
 -14.750  -1.0152   0.04816   0.04398  -0.0623   1.0000   0.0115
 -14.500  -1.0180   0.04483   0.04053  -0.0636   1.0000   0.0116
 -14.250  -1.0181   0.04197   0.03755  -0.0645   1.0000   0.0117
 -14.000  -1.0168   0.03940   0.03486  -0.0651   1.0000   0.0119
 -13.750  -1.0139   0.03710   0.03243  -0.0654   1.0000   0.0120
 -13.500  -1.0097   0.03499   0.03020  -0.0654   1.0000   0.0121
 -13.250  -1.0045   0.03308   0.02816  -0.0652   1.0000   0.0123
 -13.000  -0.9984   0.03135   0.02631  -0.0647   1.0000   0.0124
 -12.750  -0.9921   0.02980   0.02464  -0.0638   1.0000   0.0126
 -12.500  -0.9869   0.02843   0.02317  -0.0624   1.0000   0.0128
 -12.250  -0.9780   0.02717   0.02179  -0.0614   1.0000   0.0129
 -12.000  -0.9663   0.02604   0.02054  -0.0604   0.9991   0.0132
 -11.750  -0.9413   0.02481   0.01917  -0.0617   0.9928   0.0134
 -11.500  -0.9157   0.02373   0.01795  -0.0628   0.9861   0.0136
 -11.250  -0.8907   0.02253   0.01668  -0.0639   0.9795   0.0139
 -11.000  -0.8642   0.02162   0.01571  -0.0650   0.9726   0.0143
 -10.750  -0.8376   0.02085   0.01487  -0.0658   0.9657   0.0146
 -10.500  -0.8114   0.02013   0.01409  -0.0663   0.9583   0.0150
 -10.250  -0.7861   0.01946   0.01333  -0.0666   0.9514   0.0154
 -10.000  -0.7613   0.01880   0.01260  -0.0667   0.9439   0.0158
  -9.750  -0.7365   0.01820   0.01190  -0.0667   0.9372   0.0163
  -9.500  -0.7117   0.01767   0.01127  -0.0666   0.9298   0.0168
  -9.000  -0.6618   0.01654   0.01008  -0.0666   0.9171   0.0180
  -8.750  -0.6360   0.01609   0.00957  -0.0666   0.9113   0.0187
  -8.500  -0.6099   0.01563   0.00905  -0.0667   0.9063   0.0194
  -8.250  -0.5833   0.01518   0.00854  -0.0668   0.9008   0.0200
  -8.000  -0.5568   0.01470   0.00800  -0.0669   0.8953   0.0208
  -7.750  -0.5300   0.01429   0.00756  -0.0670   0.8906   0.0217
  -7.500  -0.5023   0.01394   0.00718  -0.0673   0.8858   0.0228
  -7.250  -0.4745   0.01361   0.00680  -0.0676   0.8812   0.0240
  -7.000  -0.4467   0.01322   0.00638  -0.0679   0.8768   0.0253
  -6.750  -0.4187   0.01289   0.00602  -0.0681   0.8729   0.0267
  -6.500  -0.3901   0.01258   0.00570  -0.0685   0.8683   0.0283
  -6.250  -0.3615   0.01227   0.00536  -0.0689   0.8638   0.0303
  -6.000  -0.3328   0.01199   0.00507  -0.0693   0.8599   0.0327
  -5.750  -0.3040   0.01175   0.00479  -0.0696   0.8565   0.0352
  -5.500  -0.2746   0.01147   0.00453  -0.0702   0.8525   0.0384
  -5.250  -0.2453   0.01123   0.00428  -0.0706   0.8484   0.0424
  -5.000  -0.2160   0.01099   0.00406  -0.0711   0.8444   0.0479
  -4.750  -0.1866   0.01076   0.00383  -0.0715   0.8410   0.0551
  -4.500  -0.1568   0.01053   0.00364  -0.0721   0.8377   0.0650
  -4.250  -0.1269   0.01029   0.00346  -0.0727   0.8338   0.0799
  -4.000  -0.0969   0.01000   0.00327  -0.0734   0.8299   0.1039
  -3.750  -0.0667   0.00966   0.00307  -0.0742   0.8264   0.1429
  -3.250  -0.0047   0.00874   0.00269  -0.0765   0.8199   0.2865
  -3.000   0.0273   0.00816   0.00248  -0.0780   0.8162   0.3887
  -2.750   0.0597   0.00762   0.00237  -0.0795   0.8127   0.5085
  -2.500   0.0905   0.00744   0.00237  -0.0802   0.8095   0.5673
  -2.250   0.1207   0.00740   0.00239  -0.0806   0.8063   0.5994
  -2.000   0.1510   0.00739   0.00243  -0.0810   0.8024   0.6266
  -1.750   0.1809   0.00740   0.00251  -0.0813   0.7984   0.6500
  -1.500   0.2105   0.00743   0.00248  -0.0816   0.7922   0.6604
  -1.250   0.2393   0.00743   0.00244  -0.0815   0.7772   0.6679
  -1.000   0.2679   0.00746   0.00237  -0.0814   0.7559   0.6775
  -0.750   0.2966   0.00750   0.00238  -0.0814   0.7391   0.6859
  -0.500   0.3262   0.00756   0.00235  -0.0817   0.7261   0.6917
  -0.250   0.3554   0.00758   0.00235  -0.0819   0.7120   0.6949
   0.000   0.3844   0.00763   0.00235  -0.0820   0.6946   0.6982
   0.250   0.4133   0.00771   0.00235  -0.0821   0.6725   0.7016
   0.500   0.4418   0.00784   0.00236  -0.0822   0.6425   0.7051
   0.750   0.4694   0.00808   0.00238  -0.0821   0.5960   0.7086
   1.000   0.4944   0.00857   0.00252  -0.0817   0.5163   0.7114
   1.250   0.5188   0.00919   0.00276  -0.0812   0.4318   0.7142
   1.500   0.5440   0.00974   0.00300  -0.0810   0.3627   0.7174
   1.750   0.5702   0.01018   0.00319  -0.0809   0.3124   0.7208
   2.000   0.5969   0.01056   0.00338  -0.0808   0.2715   0.7240
   2.250   0.6237   0.01091   0.00356  -0.0808   0.2385   0.7269
   2.500   0.6504   0.01120   0.00375  -0.0807   0.2130   0.7298
   2.750   0.6772   0.01150   0.00395  -0.0806   0.1913   0.7327
   3.250   0.7313   0.01205   0.00433  -0.0806   0.1596   0.7392
   3.500   0.7587   0.01229   0.00452  -0.0806   0.1492   0.7424
   3.750   0.7855   0.01253   0.00473  -0.0805   0.1403   0.7451
   4.000   0.8124   0.01276   0.00495  -0.0804   0.1327   0.7480
   4.250   0.8391   0.01301   0.00518  -0.0802   0.1264   0.7512
   4.500   0.8660   0.01324   0.00541  -0.0802   0.1208   0.7546
   4.750   0.8924   0.01353   0.00565  -0.0800   0.1151   0.7578
   5.000   0.9190   0.01377   0.00590  -0.0799   0.1112   0.7608
   5.250   0.9452   0.01401   0.00616  -0.0797   0.1077   0.7638
   5.500   0.9711   0.01429   0.00644  -0.0794   0.1042   0.7670
   5.750   0.9965   0.01461   0.00676  -0.0791   0.1008   0.7703
   6.000   1.0227   0.01487   0.00705  -0.0789   0.0990   0.7738
   6.250   1.0484   0.01514   0.00735  -0.0786   0.0970   0.7771
   6.500   1.0735   0.01542   0.00768  -0.0782   0.0948   0.7802
   6.750   1.0983   0.01574   0.00801  -0.0778   0.0925   0.7835
   7.000   1.1226   0.01610   0.00837  -0.0773   0.0901   0.7870
   7.250   1.1463   0.01651   0.00880  -0.0768   0.0880   0.7909
   7.500   1.1708   0.01681   0.00917  -0.0763   0.0869   0.7944
   7.750   1.1947   0.01713   0.00956  -0.0757   0.0857   0.7979
   8.000   1.2183   0.01747   0.00996  -0.0751   0.0843   0.8017
   8.250   1.2417   0.01783   0.01036  -0.0745   0.0826   0.8057
   8.500   1.2646   0.01820   0.01075  -0.0738   0.0805   0.8096
   8.750   1.2862   0.01863   0.01120  -0.0729   0.0783   0.8136
   9.000   1.3066   0.01914   0.01175  -0.0719   0.0764   0.8182
   9.250   1.3289   0.01949   0.01218  -0.0711   0.0754   0.8228
   9.500   1.3502   0.01988   0.01264  -0.0702   0.0741   0.8270
   9.750   1.3706   0.02027   0.01312  -0.0691   0.0726   0.8316
  10.000   1.3901   0.02069   0.01360  -0.0679   0.0710   0.8368
  10.250   1.4068   0.02114   0.01409  -0.0662   0.0695   0.8424
  10.500   1.4231   0.02165   0.01466  -0.0645   0.0679   0.8485
  10.750   1.4385   0.02232   0.01537  -0.0628   0.0661   0.8551
  11.000   1.4568   0.02278   0.01595  -0.0615   0.0651   0.8615
  11.250   1.4744   0.02330   0.01656  -0.0602   0.0637   0.8690
  11.500   1.4914   0.02384   0.01720  -0.0588   0.0620   0.8770
  11.750   1.5076   0.02444   0.01787  -0.0574   0.0603   0.8872
  12.000   1.5222   0.02508   0.01859  -0.0558   0.0587   0.9002
  12.250   1.5339   0.02582   0.01940  -0.0538   0.0569   0.9203
  12.500   1.5444   0.02634   0.02007  -0.0514   0.0557   1.0000
  12.750   1.5607   0.02712   0.02092  -0.0504   0.0538   1.0000
  13.000   1.5759   0.02797   0.02182  -0.0493   0.0518   1.0000
  13.250   1.5899   0.02893   0.02280  -0.0481   0.0499   1.0000
  13.500   1.6033   0.02994   0.02389  -0.0470   0.0480   1.0000
  13.750   1.6166   0.03097   0.02498  -0.0459   0.0458   1.0000
  14.000   1.6285   0.03212   0.02617  -0.0447   0.0432   1.0000
  14.250   1.6389   0.03341   0.02751  -0.0436   0.0410   1.0000
  14.500   1.6491   0.03475   0.02891  -0.0424   0.0386   1.0000
  14.750   1.6568   0.03630   0.03050  -0.0412   0.0361   1.0000
  15.000   1.6640   0.03794   0.03221  -0.0401   0.0342   1.0000
  15.250   1.6701   0.03971   0.03406  -0.0389   0.0325   1.0000
  15.500   1.6742   0.04170   0.03612  -0.0379   0.0310   1.0000
  15.750   1.6769   0.04387   0.03836  -0.0369   0.0298   1.0000
  16.000   1.6801   0.04603   0.04064  -0.0360   0.0288   1.0000
  16.250   1.6813   0.04847   0.04317  -0.0353   0.0278   1.0000
  16.500   1.6802   0.05123   0.04603  -0.0347   0.0267   1.0000
  16.750   1.6771   0.05434   0.04924  -0.0344   0.0259   1.0000
  17.000   1.6724   0.05779   0.05281  -0.0343   0.0252   1.0000
  17.250   1.6693   0.06120   0.05636  -0.0345   0.0245   1.0000
  17.500   1.6635   0.06509   0.06038  -0.0351   0.0238   1.0000
  17.750   1.6550   0.06953   0.06496  -0.0360   0.0233   1.0000
  18.000   1.6435   0.07465   0.07022  -0.0375   0.0227   1.0000
  18.250   1.6284   0.08057   0.07629  -0.0396   0.0223   1.0000
  18.500   1.6089   0.08746   0.08335  -0.0424   0.0220   1.0000
  18.750   1.5848   0.09544   0.09151  -0.0461   0.0218   1.0000
  19.000   1.5556   0.10463   0.10089  -0.0506   0.0216   1.0000
  19.250   1.5210   0.11499   0.11146  -0.0560   0.0217   1.0000
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