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NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il)
Reynolds number: 500,000
Max Cl/Cd: 69.9 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ms317-il-500000.txt
Download as CSV file: xf-ms317-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: NASA/LANGLEY MS(1)-0317 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -1.0041   0.09878   0.09489  -0.0460   1.0000   0.0248
 -18.500  -1.0236   0.09139   0.08732  -0.0504   1.0000   0.0249
 -18.250  -1.0387   0.08501   0.08079  -0.0540   1.0000   0.0250
 -18.000  -1.0509   0.07935   0.07498  -0.0571   1.0000   0.0252
 -17.750  -1.0601   0.07434   0.06983  -0.0597   1.0000   0.0253
 -17.500  -1.0672   0.06981   0.06517  -0.0618   1.0000   0.0255
 -17.250  -1.0728   0.06569   0.06091  -0.0636   1.0000   0.0257
 -17.000  -1.0769   0.06190   0.05699  -0.0651   1.0000   0.0259
 -16.750  -1.0797   0.05841   0.05336  -0.0664   1.0000   0.0262
 -16.500  -1.0813   0.05521   0.05003  -0.0673   1.0000   0.0264
 -16.250  -1.0817   0.05227   0.04695  -0.0681   1.0000   0.0267
 -16.000  -1.0810   0.04959   0.04413  -0.0686   1.0000   0.0269
 -15.750  -1.0796   0.04715   0.04154  -0.0689   1.0000   0.0271
 -15.500  -1.0742   0.04499   0.03936  -0.0684   1.0000   0.0275
 -15.250  -1.0668   0.04318   0.03752  -0.0682   1.0000   0.0279
 -15.000  -1.0586   0.04149   0.03581  -0.0681   1.0000   0.0283
 -14.750  -1.0502   0.03984   0.03412  -0.0680   1.0000   0.0287
 -14.500  -1.0412   0.03826   0.03248  -0.0678   1.0000   0.0291
 -14.250  -1.0320   0.03672   0.03087  -0.0675   1.0000   0.0296
 -14.000  -1.0219   0.03527   0.02933  -0.0671   1.0000   0.0301
 -13.750  -1.0111   0.03390   0.02786  -0.0666   1.0000   0.0305
 -13.500  -0.9996   0.03263   0.02650  -0.0662   1.0000   0.0309
 -13.250  -0.9889   0.03120   0.02505  -0.0653   1.0000   0.0315
 -13.000  -0.9771   0.02999   0.02385  -0.0645   1.0000   0.0320
 -12.750  -0.9646   0.02891   0.02276  -0.0638   1.0000   0.0326
 -12.500  -0.9519   0.02790   0.02173  -0.0630   1.0000   0.0332
 -12.250  -0.9398   0.02696   0.02076  -0.0620   1.0000   0.0338
 -12.000  -0.9298   0.02613   0.01988  -0.0605   1.0000   0.0345
 -11.750  -0.9297   0.02554   0.01925  -0.0571   1.0000   0.0350
 -11.500  -0.9116   0.02441   0.01811  -0.0574   0.9963   0.0359
 -11.250  -0.8820   0.02332   0.01704  -0.0597   0.9922   0.0370
 -11.000  -0.8529   0.02240   0.01610  -0.0616   0.9856   0.0381
 -10.750  -0.8216   0.02154   0.01517  -0.0637   0.9802   0.0393
 -10.500  -0.7974   0.02053   0.01413  -0.0646   0.9695   0.0405
 -10.250  -0.7749   0.01968   0.01329  -0.0650   0.9582   0.0418
 -10.000  -0.7516   0.01903   0.01259  -0.0652   0.9478   0.0434
  -9.750  -0.7295   0.01850   0.01198  -0.0649   0.9368   0.0449
  -9.500  -0.7105   0.01769   0.01118  -0.0646   0.9258   0.0467
  -9.250  -0.6880   0.01719   0.01062  -0.0643   0.9170   0.0487
  -9.000  -0.6646   0.01671   0.01009  -0.0641   0.9080   0.0509
  -8.750  -0.6421   0.01613   0.00950  -0.0639   0.9001   0.0536
  -8.500  -0.6165   0.01577   0.00909  -0.0639   0.8932   0.0568
  -8.250  -0.5921   0.01522   0.00858  -0.0640   0.8860   0.0610
  -8.000  -0.5666   0.01480   0.00813  -0.0640   0.8799   0.0659
  -7.750  -0.5397   0.01446   0.00777  -0.0643   0.8740   0.0715
  -7.500  -0.5130   0.01403   0.00738  -0.0646   0.8679   0.0783
  -7.250  -0.4860   0.01364   0.00701  -0.0649   0.8624   0.0858
  -7.000  -0.4583   0.01330   0.00667  -0.0653   0.8571   0.0939
  -6.750  -0.4300   0.01295   0.00636  -0.0658   0.8515   0.1028
  -6.500  -0.4015   0.01262   0.00605  -0.0662   0.8463   0.1132
  -6.250  -0.3729   0.01228   0.00575  -0.0668   0.8417   0.1266
  -6.000  -0.3437   0.01192   0.00548  -0.0675   0.8369   0.1445
  -5.500  -0.2843   0.01113   0.00493  -0.0692   0.8272   0.2013
  -5.250  -0.2539   0.01066   0.00463  -0.0703   0.8230   0.2432
  -5.000  -0.2226   0.01014   0.00434  -0.0717   0.8187   0.3009
  -4.750  -0.1894   0.00934   0.00396  -0.0739   0.8143   0.3957
  -4.500  -0.1552   0.00862   0.00374  -0.0760   0.8099   0.5133
  -4.250  -0.1234   0.00848   0.00376  -0.0769   0.8059   0.5650
  -4.000  -0.0924   0.00852   0.00380  -0.0774   0.8021   0.5915
  -3.750  -0.0613   0.00859   0.00386  -0.0780   0.7983   0.6094
  -3.500  -0.0302   0.00865   0.00391  -0.0786   0.7942   0.6233
  -3.250   0.0002   0.00872   0.00399  -0.0789   0.7900   0.6331
  -3.000   0.0314   0.00881   0.00400  -0.0795   0.7860   0.6428
  -2.750   0.0614   0.00892   0.00409  -0.0797   0.7820   0.6495
  -2.500   0.0918   0.00902   0.00419  -0.0800   0.7780   0.6566
  -2.250   0.1229   0.00911   0.00424  -0.0806   0.7737   0.6642
  -2.000   0.1520   0.00925   0.00443  -0.0805   0.7695   0.6710
  -1.750   0.1822   0.00937   0.00451  -0.0808   0.7656   0.6772
  -1.500   0.2134   0.00952   0.00457  -0.0814   0.7613   0.6826
  -1.250   0.2420   0.00954   0.00467  -0.0813   0.7555   0.6874
  -1.000   0.2702   0.00961   0.00470  -0.0808   0.7450   0.6933
  -0.750   0.2998   0.00970   0.00474  -0.0809   0.7327   0.7004
  -0.500   0.3288   0.00969   0.00469  -0.0808   0.7241   0.7045
  -0.250   0.3582   0.00969   0.00471  -0.0810   0.7168   0.7070
   0.000   0.3878   0.00968   0.00469  -0.0812   0.7085   0.7094
   0.250   0.4176   0.00970   0.00467  -0.0815   0.7004   0.7121
   0.500   0.4479   0.00969   0.00465  -0.0819   0.6913   0.7149
   0.750   0.4783   0.00972   0.00461  -0.0823   0.6832   0.7176
   1.000   0.5092   0.00971   0.00461  -0.0830   0.6740   0.7201
   1.250   0.5392   0.00971   0.00455  -0.0834   0.6644   0.7225
   1.500   0.5685   0.00968   0.00454  -0.0835   0.6523   0.7245
   1.750   0.5976   0.00970   0.00455  -0.0837   0.6392   0.7264
   2.000   0.6264   0.00976   0.00457  -0.0838   0.6240   0.7285
   2.250   0.6551   0.00984   0.00461  -0.0839   0.6051   0.7308
   2.500   0.6834   0.00996   0.00465  -0.0840   0.5802   0.7332
   2.750   0.7109   0.01017   0.00471  -0.0839   0.5440   0.7355
   3.000   0.7354   0.01063   0.00485  -0.0835   0.4814   0.7378
   3.250   0.7570   0.01139   0.00519  -0.0826   0.4004   0.7400
   3.500   0.7788   0.01209   0.00553  -0.0819   0.3351   0.7422
   3.750   0.8012   0.01265   0.00586  -0.0812   0.2860   0.7442
   4.000   0.8242   0.01317   0.00619  -0.0805   0.2484   0.7463
   4.250   0.8478   0.01364   0.00651  -0.0799   0.2197   0.7484
   4.500   0.8719   0.01406   0.00681  -0.0794   0.1980   0.7506
   4.750   0.8964   0.01446   0.00712  -0.0790   0.1816   0.7527
   5.000   0.9210   0.01484   0.00742  -0.0786   0.1689   0.7549
   5.250   0.9448   0.01527   0.00776  -0.0782   0.1582   0.7570
   5.500   0.9702   0.01558   0.00804  -0.0779   0.1508   0.7593
   5.750   0.9929   0.01603   0.00842  -0.0772   0.1435   0.7614
   6.000   1.0173   0.01627   0.00870  -0.0767   0.1391   0.7635
   6.250   1.0400   0.01664   0.00906  -0.0760   0.1346   0.7654
   6.500   1.0597   0.01718   0.00956  -0.0747   0.1300   0.7675
   6.750   1.0832   0.01746   0.00989  -0.0741   0.1276   0.7696
   7.000   1.1056   0.01781   0.01027  -0.0733   0.1249   0.7719
   7.250   1.1265   0.01822   0.01068  -0.0723   0.1223   0.7743
   7.500   1.1449   0.01873   0.01117  -0.0709   0.1197   0.7769
   7.750   1.1567   0.01939   0.01182  -0.0684   0.1172   0.7793
   8.000   1.1759   0.01973   0.01223  -0.0671   0.1159   0.7818
   8.250   1.1950   0.02019   0.01274  -0.0659   0.1144   0.7841
   8.500   1.2138   0.02070   0.01330  -0.0647   0.1128   0.7865
   8.750   1.2321   0.02125   0.01390  -0.0635   0.1113   0.7891
   9.000   1.2500   0.02187   0.01453  -0.0623   0.1098   0.7920
   9.250   1.2667   0.02259   0.01526  -0.0611   0.1082   0.7950
   9.500   1.2811   0.02354   0.01620  -0.0596   0.1064   0.7976
   9.750   1.2977   0.02431   0.01702  -0.0584   0.1053   0.8002
  10.000   1.3160   0.02491   0.01770  -0.0574   0.1044   0.8028
  10.250   1.3338   0.02556   0.01842  -0.0565   0.1033   0.8056
  10.500   1.3512   0.02627   0.01919  -0.0555   0.1021   0.8086
  10.750   1.3683   0.02701   0.01998  -0.0545   0.1008   0.8118
  11.000   1.3852   0.02780   0.02080  -0.0537   0.0995   0.8153
  11.250   1.4012   0.02861   0.02164  -0.0527   0.0982   0.8185
  11.500   1.4152   0.02958   0.02263  -0.0515   0.0967   0.8216
  11.750   1.4283   0.03077   0.02383  -0.0501   0.0950   0.8248
  12.000   1.4444   0.03158   0.02473  -0.0493   0.0943   0.8285
  12.250   1.4600   0.03247   0.02571  -0.0485   0.0934   0.8323
  12.500   1.4751   0.03340   0.02673  -0.0477   0.0923   0.8360
  12.750   1.4891   0.03438   0.02779  -0.0467   0.0913   0.8397
  13.000   1.5029   0.03541   0.02889  -0.0458   0.0902   0.8438
  13.250   1.5162   0.03651   0.03004  -0.0450   0.0891   0.8483
  13.500   1.5290   0.03765   0.03122  -0.0442   0.0881   0.8528
  13.750   1.5400   0.03888   0.03249  -0.0431   0.0870   0.8575
  14.000   1.5517   0.04022   0.03384  -0.0418   0.0854   0.8625
  14.250   1.5631   0.04150   0.03523  -0.0411   0.0848   0.8681
  14.500   1.5730   0.04283   0.03670  -0.0402   0.0840   0.8734
  14.750   1.5827   0.04423   0.03822  -0.0394   0.0830   0.8795
  15.000   1.5921   0.04570   0.03979  -0.0387   0.0820   0.8860
  15.250   1.6006   0.04720   0.04139  -0.0379   0.0809   0.8929
  15.500   1.6093   0.04878   0.04304  -0.0373   0.0799   0.9010
  15.750   1.6164   0.05042   0.04475  -0.0366   0.0789   0.9102
  16.000   1.6229   0.05209   0.04647  -0.0357   0.0778   0.9218
  16.250   1.6277   0.05369   0.04813  -0.0342   0.0765   0.9404
  16.500   1.6293   0.05564   0.05024  -0.0334   0.0759   1.0000
  16.750   1.6354   0.05796   0.05269  -0.0336   0.0749   1.0000
  17.000   1.6412   0.06031   0.05513  -0.0338   0.0738   1.0000
  17.250   1.6466   0.06270   0.05761  -0.0341   0.0728   1.0000
  17.500   1.6513   0.06520   0.06017  -0.0344   0.0717   1.0000
  17.750   1.6555   0.06776   0.06278  -0.0347   0.0708   1.0000
  18.000   1.6588   0.07041   0.06546  -0.0350   0.0698   1.0000
  18.250   1.6602   0.07314   0.06820  -0.0350   0.0685   1.0000
  18.500   1.6593   0.07662   0.07185  -0.0359   0.0677   1.0000
  18.750   1.6582   0.08012   0.07549  -0.0368   0.0667   1.0000
  19.000   1.6570   0.08365   0.07912  -0.0378   0.0656   1.0000
  19.250   1.6557   0.08724   0.08280  -0.0389   0.0646   1.0000
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