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NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Xfoil prediction polar at RE=100,000 Ncrit=5


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il)
Reynolds number: 100,000
Max Cl/Cd: 35.55 at α=4.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-ms317-il-100000-n5.txt
Download as CSV file: xf-ms317-il-100000-n5.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 =     0.100 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.7144   0.09347   0.08709  -0.0554   1.0000   0.0443
 -14.750  -0.7696   0.08033   0.07361  -0.0638   1.0000   0.0439
 -14.500  -0.8047   0.07228   0.06526  -0.0681   1.0000   0.0439
 -14.250  -0.8309   0.06621   0.05890  -0.0705   1.0000   0.0442
 -14.000  -0.8520   0.06118   0.05357  -0.0718   1.0000   0.0445
 -13.750  -0.8694   0.05688   0.04894  -0.0723   1.0000   0.0450
 -13.500  -0.8654   0.05476   0.04680  -0.0721   1.0000   0.0455
 -13.250  -0.8627   0.05261   0.04459  -0.0718   1.0000   0.0461
 -13.000  -0.8610   0.05044   0.04232  -0.0713   1.0000   0.0468
 -12.750  -0.8593   0.04829   0.04004  -0.0706   1.0000   0.0475
 -12.500  -0.8571   0.04622   0.03781  -0.0696   1.0000   0.0483
 -12.250  -0.8553   0.04426   0.03566  -0.0683   1.0000   0.0493
 -12.000  -0.8547   0.04239   0.03353  -0.0665   1.0000   0.0505
 -11.750  -0.8480   0.04122   0.03241  -0.0648   1.0000   0.0514
 -11.500  -0.8455   0.04022   0.03142  -0.0624   1.0000   0.0523
 -11.250  -0.8479   0.03934   0.03052  -0.0591   1.0000   0.0533
 -11.000  -0.8537   0.03855   0.02967  -0.0550   1.0000   0.0542
 -10.750  -0.8578   0.03773   0.02877  -0.0511   1.0000   0.0552
 -10.500  -0.8473   0.03656   0.02740  -0.0496   0.9976   0.0567
 -10.250  -0.8186   0.03535   0.02625  -0.0515   0.9925   0.0586
 -10.000  -0.7911   0.03418   0.02500  -0.0529   0.9861   0.0612
  -9.750  -0.7608   0.03296   0.02365  -0.0546   0.9813   0.0642
  -9.500  -0.7338   0.03193   0.02265  -0.0558   0.9750   0.0669
  -9.250  -0.7043   0.03091   0.02150  -0.0572   0.9699   0.0707
  -9.000  -0.6736   0.02989   0.02053  -0.0591   0.9659   0.0745
  -8.750  -0.6473   0.02903   0.01957  -0.0598   0.9588   0.0792
  -8.500  -0.6181   0.02808   0.01868  -0.0612   0.9538   0.0839
  -8.250  -0.5897   0.02725   0.01780  -0.0623   0.9484   0.0901
  -8.000  -0.5650   0.02649   0.01706  -0.0627   0.9414   0.0964
  -7.750  -0.5359   0.02567   0.01627  -0.0639   0.9365   0.1041
  -7.500  -0.5102   0.02500   0.01560  -0.0644   0.9303   0.1128
  -7.250  -0.4853   0.02438   0.01498  -0.0646   0.9235   0.1231
  -7.000  -0.4570   0.02368   0.01435  -0.0655   0.9187   0.1356
  -6.750  -0.4317   0.02308   0.01381  -0.0659   0.9129   0.1503
  -6.500  -0.4080   0.02252   0.01334  -0.0659   0.9060   0.1681
  -6.250  -0.3810   0.02183   0.01279  -0.0665   0.9011   0.1919
  -6.000  -0.3532   0.02114   0.01226  -0.0674   0.8970   0.2236
  -5.750  -0.3326   0.02056   0.01189  -0.0670   0.8898   0.2615
  -5.500  -0.3074   0.01979   0.01142  -0.0675   0.8845   0.3171
  -5.250  -0.2806   0.01897   0.01109  -0.0682   0.8804   0.3993
  -5.000  -0.2575   0.01889   0.01149  -0.0669   0.8750   0.4846
  -4.750  -0.2340   0.01928   0.01206  -0.0652   0.8689   0.5380
  -4.500  -0.2056   0.01957   0.01235  -0.0648   0.8644   0.5734
  -4.250  -0.1754   0.01986   0.01257  -0.0647   0.8607   0.5981
  -4.000  -0.1480   0.02014   0.01277  -0.0644   0.8554   0.6181
  -3.750  -0.1222   0.02051   0.01308  -0.0637   0.8495   0.6342
  -3.500  -0.0940   0.02085   0.01335  -0.0633   0.8451   0.6493
  -3.250  -0.0637   0.02107   0.01347  -0.0634   0.8415   0.6641
  -3.000  -0.0398   0.02160   0.01398  -0.0616   0.8366   0.6720
  -2.750  -0.0139   0.02178   0.01409  -0.0615   0.8306   0.6837
  -2.500   0.0101   0.02224   0.01454  -0.0597   0.8262   0.6905
  -2.250   0.0401   0.02233   0.01455  -0.0601   0.8226   0.7027
  -2.000   0.0642   0.02275   0.01497  -0.0581   0.8188   0.7089
  -1.750   0.0868   0.02299   0.01519  -0.0574   0.8119   0.7183
  -1.500   0.1134   0.02305   0.01521  -0.0571   0.8071   0.7241
  -1.250   0.1412   0.02306   0.01519  -0.0567   0.8032   0.7277
  -1.000   0.1708   0.02299   0.01507  -0.0569   0.7998   0.7320
  -0.750   0.1949   0.02308   0.01515  -0.0571   0.7927   0.7376
  -0.500   0.2247   0.02298   0.01502  -0.0579   0.7877   0.7422
  -0.250   0.2527   0.02294   0.01497  -0.0576   0.7838   0.7449
   0.000   0.2807   0.02290   0.01491  -0.0575   0.7792   0.7481
   0.250   0.3040   0.02298   0.01502  -0.0570   0.7708   0.7519
   0.500   0.3358   0.02278   0.01478  -0.0578   0.7651   0.7561
   0.750   0.3689   0.02251   0.01447  -0.0591   0.7576   0.7607
   1.000   0.3948   0.02222   0.01418  -0.0581   0.7460   0.7628
   1.250   0.4203   0.02190   0.01385  -0.0569   0.7324   0.7655
   1.500   0.4502   0.02146   0.01335  -0.0565   0.7203   0.7686
   1.750   0.4769   0.02125   0.01316  -0.0562   0.7071   0.7720
   2.000   0.5051   0.02109   0.01299  -0.0564   0.6945   0.7755
   2.250   0.5379   0.02080   0.01267  -0.0573   0.6822   0.7795
   2.500   0.5623   0.02066   0.01255  -0.0564   0.6676   0.7819
   2.750   0.5865   0.02056   0.01249  -0.0555   0.6512   0.7844
   3.000   0.6118   0.02044   0.01238  -0.0548   0.6329   0.7873
   3.250   0.6380   0.02032   0.01224  -0.0543   0.6118   0.7907
   3.500   0.6645   0.02026   0.01214  -0.0541   0.5851   0.7942
   3.750   0.6922   0.02022   0.01200  -0.0542   0.5489   0.7975
   4.000   0.7156   0.02028   0.01183  -0.0531   0.4985   0.7999
   4.250   0.7333   0.02063   0.01181  -0.0511   0.4362   0.8024
   4.500   0.7479   0.02127   0.01209  -0.0490   0.3786   0.8055
   4.750   0.7629   0.02200   0.01251  -0.0472   0.3319   0.8089
   5.000   0.7801   0.02272   0.01299  -0.0460   0.2948   0.8122
   5.250   0.7995   0.02340   0.01349  -0.0453   0.2655   0.8154
   5.500   0.8167   0.02405   0.01401  -0.0441   0.2437   0.8181
   5.750   0.8327   0.02463   0.01451  -0.0424   0.2267   0.8209
   6.000   0.8498   0.02521   0.01503  -0.0410   0.2130   0.8242
   6.250   0.8672   0.02582   0.01559  -0.0398   0.2024   0.8277
   6.500   0.8853   0.02645   0.01617  -0.0388   0.1932   0.8312
   6.750   0.9054   0.02710   0.01679  -0.0383   0.1854   0.8345
   7.000   0.9213   0.02769   0.01738  -0.0367   0.1786   0.8373
   7.250   0.9376   0.02841   0.01805  -0.0354   0.1730   0.8407
   7.500   0.9578   0.02903   0.01873  -0.0347   0.1672   0.8444
   7.750   0.9779   0.02976   0.01945  -0.0341   0.1623   0.8482
   8.000   0.9986   0.03062   0.02022  -0.0339   0.1584   0.8517
   8.250   1.0185   0.03125   0.02094  -0.0330   0.1547   0.8546
   8.500   1.0382   0.03194   0.02168  -0.0323   0.1511   0.8580
   8.750   1.0580   0.03269   0.02246  -0.0316   0.1477   0.8620
   9.000   1.0787   0.03353   0.02325  -0.0313   0.1448   0.8663
   9.250   1.0997   0.03433   0.02409  -0.0308   0.1420   0.8703
   9.500   1.1191   0.03507   0.02496  -0.0300   0.1393   0.8743
   9.750   1.1397   0.03589   0.02585  -0.0295   0.1368   0.8785
  10.000   1.1610   0.03676   0.02676  -0.0293   0.1344   0.8829
  10.250   1.1806   0.03761   0.02764  -0.0287   0.1323   0.8871
  10.500   1.2013   0.03848   0.02847  -0.0281   0.1303   0.8917
  10.750   1.2198   0.03947   0.02961  -0.0275   0.1283   0.8973
  11.000   1.2366   0.04048   0.03078  -0.0266   0.1263   0.9031
  11.250   1.2528   0.04149   0.03195  -0.0257   0.1244   0.9097
  11.500   1.2691   0.04255   0.03312  -0.0249   0.1226   0.9166
  11.750   1.2838   0.04355   0.03420  -0.0238   0.1208   0.9243
  12.000   1.3000   0.04454   0.03524  -0.0230   0.1192   0.9330
  12.500   1.3278   0.04686   0.03775  -0.0210   0.1162   0.9647
  12.750   1.3360   0.04853   0.03968  -0.0203   0.1146   1.0000
  13.000   1.3460   0.05043   0.04180  -0.0200   0.1128   1.0000
  13.250   1.3554   0.05233   0.04386  -0.0197   0.1111   1.0000
  13.500   1.3655   0.05417   0.04582  -0.0195   0.1095   1.0000
  13.750   1.3772   0.05590   0.04761  -0.0194   0.1081   1.0000
  14.000   1.3927   0.05740   0.04911  -0.0195   0.1066   1.0000
  14.250   1.4023   0.05943   0.05121  -0.0193   0.1052   1.0000
  14.500   1.3925   0.06279   0.05492  -0.0186   0.1040   1.0000
  14.750   1.3819   0.06642   0.05884  -0.0182   0.1027   1.0000
  15.000   1.3708   0.07024   0.06292  -0.0181   0.1014   1.0000
  15.250   1.3596   0.07420   0.06711  -0.0183   0.1001   1.0000
  15.500   1.3494   0.07820   0.07130  -0.0189   0.0989   1.0000
  15.750   1.3413   0.08208   0.07532  -0.0196   0.0978   1.0000
  16.000   1.3378   0.08555   0.07889  -0.0205   0.0967   1.0000
  16.250   1.3462   0.08767   0.08102  -0.0209   0.0956   1.0000
  16.500   1.3266   0.09352   0.08706  -0.0229   0.0947   1.0000
  16.750   1.2404   0.11040   0.10452  -0.0317   0.0942   1.0000
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