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


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il)
Reynolds number: 1,000,000
Max Cl/Cd: 80.43 at α=1.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ms317-il-1000000.txt
Download as CSV file: xf-ms317-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1510   0.09368   0.09004  -0.0430   1.0000   0.0186
 -19.500  -1.1630   0.08800   0.08426  -0.0459   1.0000   0.0187
 -19.250  -1.1736   0.08257   0.07873  -0.0487   1.0000   0.0189
 -19.000  -1.1825   0.07752   0.07357  -0.0512   1.0000   0.0190
 -18.750  -1.1898   0.07285   0.06880  -0.0534   1.0000   0.0191
 -18.500  -1.1954   0.06849   0.06435  -0.0554   1.0000   0.0192
 -18.250  -1.1993   0.06447   0.06023  -0.0572   1.0000   0.0194
 -18.000  -1.2013   0.06082   0.05649  -0.0586   1.0000   0.0195
 -17.750  -1.2018   0.05748   0.05305  -0.0599   1.0000   0.0197
 -17.500  -1.2007   0.05440   0.04989  -0.0609   1.0000   0.0198
 -17.250  -1.1979   0.05161   0.04700  -0.0618   1.0000   0.0200
 -17.000  -1.1935   0.04909   0.04441  -0.0625   1.0000   0.0201
 -16.750  -1.1902   0.04656   0.04180  -0.0630   1.0000   0.0202
 -16.500  -1.1944   0.04337   0.03853  -0.0634   1.0000   0.0205
 -16.250  -1.1931   0.04086   0.03596  -0.0636   1.0000   0.0208
 -16.000  -1.1886   0.03875   0.03380  -0.0637   1.0000   0.0210
 -15.750  -1.1818   0.03691   0.03192  -0.0636   1.0000   0.0212
 -15.500  -1.1730   0.03530   0.03026  -0.0635   1.0000   0.0215
 -15.250  -1.1635   0.03377   0.02868  -0.0633   1.0000   0.0218
 -15.000  -1.1528   0.03236   0.02724  -0.0631   1.0000   0.0221
 -14.750  -1.1415   0.03103   0.02585  -0.0628   1.0000   0.0224
 -14.500  -1.1294   0.02978   0.02456  -0.0624   1.0000   0.0227
 -14.250  -1.1163   0.02863   0.02336  -0.0621   1.0000   0.0230
 -14.000  -1.1018   0.02761   0.02229  -0.0617   1.0000   0.0233
 -13.750  -1.0876   0.02659   0.02121  -0.0613   1.0000   0.0235
 -13.500  -1.0811   0.02501   0.01961  -0.0605   1.0000   0.0241
 -13.250  -1.0689   0.02393   0.01851  -0.0597   1.0000   0.0246
 -13.000  -1.0551   0.02303   0.01759  -0.0590   1.0000   0.0250
 -12.750  -1.0418   0.02223   0.01678  -0.0580   1.0000   0.0254
 -12.500  -1.0300   0.02148   0.01601  -0.0567   0.9992   0.0259
 -12.250  -1.0009   0.02066   0.01515  -0.0585   0.9930   0.0264
 -12.000  -0.9727   0.01993   0.01438  -0.0600   0.9836   0.0269
 -11.750  -0.9502   0.01889   0.01329  -0.0608   0.9694   0.0276
 -11.500  -0.9335   0.01808   0.01243  -0.0602   0.9514   0.0283
 -11.250  -0.9145   0.01747   0.01177  -0.0596   0.9356   0.0290
 -11.000  -0.8930   0.01693   0.01118  -0.0594   0.9222   0.0298
 -10.750  -0.8700   0.01646   0.01063  -0.0594   0.9109   0.0305
 -10.500  -0.8470   0.01594   0.01003  -0.0594   0.8998   0.0314
 -10.250  -0.8237   0.01535   0.00942  -0.0594   0.8902   0.0325
 -10.000  -0.7990   0.01494   0.00897  -0.0594   0.8813   0.0336
  -9.750  -0.7730   0.01458   0.00856  -0.0596   0.8738   0.0347
  -9.500  -0.7472   0.01416   0.00810  -0.0598   0.8663   0.0359
  -9.250  -0.7213   0.01376   0.00767  -0.0599   0.8591   0.0375
  -9.000  -0.6939   0.01343   0.00732  -0.0603   0.8533   0.0392
  -8.750  -0.6667   0.01305   0.00694  -0.0606   0.8470   0.0414
  -8.500  -0.6392   0.01275   0.00661  -0.0609   0.8410   0.0440
  -8.250  -0.6111   0.01241   0.00627  -0.0614   0.8360   0.0472
  -8.000  -0.5826   0.01212   0.00598  -0.0618   0.8306   0.0508
  -7.750  -0.5542   0.01181   0.00568  -0.0623   0.8252   0.0559
  -7.500  -0.5255   0.01154   0.00541  -0.0628   0.8196   0.0618
  -7.250  -0.4961   0.01124   0.00516  -0.0634   0.8153   0.0682
  -7.000  -0.4666   0.01098   0.00493  -0.0640   0.8106   0.0746
  -6.750  -0.4370   0.01077   0.00471  -0.0645   0.8057   0.0810
  -6.500  -0.4074   0.01056   0.00450  -0.0651   0.8005   0.0884
  -6.250  -0.3772   0.01029   0.00429  -0.0659   0.7968   0.0971
  -6.000  -0.3469   0.01004   0.00409  -0.0666   0.7926   0.1070
  -5.750  -0.3165   0.00979   0.00389  -0.0674   0.7881   0.1198
  -5.500  -0.2860   0.00955   0.00369  -0.0682   0.7836   0.1371
  -5.250  -0.2551   0.00927   0.00351  -0.0691   0.7795   0.1598
  -5.000  -0.2238   0.00898   0.00333  -0.0701   0.7761   0.1866
  -4.750  -0.1922   0.00866   0.00315  -0.0712   0.7723   0.2192
  -4.500  -0.1602   0.00829   0.00296  -0.0725   0.7685   0.2632
  -4.250  -0.1276   0.00787   0.00275  -0.0740   0.7646   0.3219
  -4.000  -0.0927   0.00718   0.00247  -0.0763   0.7607   0.4327
  -3.750  -0.0585   0.00672   0.00232  -0.0781   0.7575   0.5164
  -3.500  -0.0260   0.00654   0.00228  -0.0791   0.7538   0.5574
  -3.250   0.0056   0.00648   0.00227  -0.0799   0.7498   0.5811
  -3.000   0.0369   0.00648   0.00227  -0.0805   0.7457   0.5977
  -2.750   0.0680   0.00653   0.00229  -0.0811   0.7414   0.6099
  -2.500   0.0992   0.00653   0.00230  -0.0817   0.7383   0.6194
  -2.250   0.1304   0.00654   0.00230  -0.0823   0.7344   0.6270
  -2.000   0.1612   0.00655   0.00231  -0.0828   0.7292   0.6336
  -1.750   0.1917   0.00661   0.00231  -0.0832   0.7198   0.6408
  -1.500   0.2221   0.00662   0.00229  -0.0835   0.7078   0.6484
  -1.250   0.2525   0.00666   0.00232  -0.0839   0.6985   0.6537
  -1.000   0.2831   0.00671   0.00234  -0.0844   0.6907   0.6584
  -0.750   0.3138   0.00680   0.00236  -0.0848   0.6827   0.6628
  -0.500   0.3440   0.00680   0.00240  -0.0852   0.6736   0.6688
  -0.250   0.3740   0.00691   0.00248  -0.0854   0.6650   0.6742
   0.000   0.4046   0.00698   0.00254  -0.0859   0.6575   0.6789
   0.250   0.4349   0.00707   0.00257  -0.0863   0.6479   0.6814
   0.500   0.4655   0.00708   0.00256  -0.0868   0.6369   0.6837
   0.750   0.4954   0.00712   0.00257  -0.0872   0.6249   0.6863
   1.000   0.5252   0.00720   0.00261  -0.0875   0.6105   0.6884
   1.250   0.5549   0.00729   0.00265  -0.0878   0.5936   0.6905
   1.500   0.5841   0.00744   0.00272  -0.0881   0.5728   0.6926
   1.750   0.6129   0.00762   0.00280  -0.0883   0.5412   0.6947
   2.000   0.6399   0.00801   0.00294  -0.0882   0.4868   0.6967
   2.250   0.6646   0.00865   0.00320  -0.0879   0.4099   0.6985
   2.500   0.6899   0.00922   0.00347  -0.0876   0.3491   0.7002
   2.750   0.7158   0.00971   0.00372  -0.0875   0.3007   0.7015
   3.000   0.7420   0.01008   0.00391  -0.0874   0.2626   0.7040
   3.250   0.7685   0.01041   0.00411  -0.0873   0.2326   0.7061
   3.750   0.8217   0.01107   0.00454  -0.0871   0.1891   0.7099
   4.000   0.8484   0.01136   0.00475  -0.0870   0.1734   0.7120
   4.250   0.8752   0.01164   0.00496  -0.0869   0.1611   0.7141
   4.500   0.9022   0.01189   0.00517  -0.0868   0.1511   0.7160
   4.750   0.9288   0.01217   0.00538  -0.0867   0.1420   0.7178
   5.000   0.9555   0.01243   0.00560  -0.0866   0.1348   0.7193
   5.250   0.9820   0.01270   0.00583  -0.0865   0.1285   0.7206
   5.500   1.0086   0.01293   0.00603  -0.0863   0.1238   0.7224
   5.750   1.0340   0.01321   0.00629  -0.0860   0.1183   0.7250
   6.000   1.0603   0.01343   0.00653  -0.0858   0.1155   0.7271
   6.250   1.0861   0.01367   0.00677  -0.0856   0.1128   0.7291
   6.500   1.1112   0.01396   0.00705  -0.0852   0.1099   0.7309
   6.750   1.1350   0.01433   0.00740  -0.0846   0.1064   0.7328
   7.000   1.1601   0.01459   0.00767  -0.0842   0.1048   0.7348
   7.250   1.1850   0.01484   0.00794  -0.0838   0.1033   0.7367
   7.500   1.2093   0.01512   0.00824  -0.0833   0.1018   0.7385
   7.750   1.2327   0.01544   0.00855  -0.0826   0.1002   0.7401
   8.000   1.2552   0.01578   0.00890  -0.0818   0.0986   0.7422
   8.250   1.2757   0.01618   0.00932  -0.0807   0.0968   0.7451
   8.500   1.2941   0.01667   0.00984  -0.0792   0.0950   0.7475
   8.750   1.3154   0.01696   0.01017  -0.0782   0.0943   0.7498
   9.000   1.3322   0.01729   0.01054  -0.0764   0.0936   0.7522
   9.250   1.3504   0.01768   0.01097  -0.0748   0.0928   0.7548
   9.500   1.3695   0.01811   0.01143  -0.0736   0.0918   0.7572
   9.750   1.3885   0.01857   0.01191  -0.0724   0.0907   0.7593
  10.000   1.4072   0.01905   0.01241  -0.0712   0.0895   0.7615
  10.250   1.4247   0.01961   0.01299  -0.0699   0.0880   0.7646
  10.500   1.4387   0.02039   0.01380  -0.0683   0.0862   0.7674
  10.750   1.4538   0.02114   0.01460  -0.0668   0.0852   0.7701
  11.000   1.4727   0.02167   0.01518  -0.0658   0.0847   0.7729
  11.250   1.4908   0.02227   0.01583  -0.0649   0.0841   0.7759
  11.500   1.5085   0.02291   0.01650  -0.0639   0.0833   0.7787
  11.750   1.5257   0.02358   0.01723  -0.0629   0.0825   0.7819
  12.000   1.5427   0.02427   0.01797  -0.0619   0.0816   0.7853
  12.250   1.5591   0.02502   0.01877  -0.0609   0.0807   0.7886
  12.500   1.5745   0.02587   0.01965  -0.0599   0.0798   0.7920
  12.750   1.5883   0.02683   0.02065  -0.0587   0.0789   0.7954
  13.000   1.5992   0.02803   0.02187  -0.0574   0.0777   0.7984
  13.250   1.6074   0.02945   0.02336  -0.0559   0.0766   0.8026
  13.500   1.6240   0.03025   0.02424  -0.0552   0.0762   0.8066
  13.750   1.6400   0.03110   0.02515  -0.0544   0.0755   0.8108
  14.000   1.6551   0.03204   0.02615  -0.0536   0.0748   0.8149
  14.250   1.6696   0.03302   0.02720  -0.0529   0.0739   0.8193
  14.500   1.6830   0.03411   0.02835  -0.0520   0.0730   0.8243
  14.750   1.6962   0.03522   0.02952  -0.0512   0.0721   0.8295
  15.000   1.7074   0.03651   0.03084  -0.0504   0.0712   0.8344
  15.250   1.7166   0.03796   0.03235  -0.0494   0.0702   0.8397
  15.500   1.7204   0.03991   0.03436  -0.0482   0.0690   0.8452
  15.750   1.7310   0.04133   0.03585  -0.0475   0.0683   0.8509
  16.000   1.7438   0.04256   0.03718  -0.0470   0.0677   0.8570
  16.250   1.7559   0.04387   0.03857  -0.0464   0.0668   0.8638
  16.500   1.7665   0.04533   0.04010  -0.0459   0.0658   0.8705
  16.750   1.7770   0.04680   0.04165  -0.0453   0.0648   0.8784
  17.000   1.7852   0.04856   0.04346  -0.0448   0.0638   0.8868
  17.250   1.7904   0.05058   0.04555  -0.0442   0.0626   0.8969
  17.500   1.7914   0.05306   0.04811  -0.0435   0.0614   0.9091
  17.750   1.8000   0.05462   0.04981  -0.0429   0.0607   0.9307
  18.000   1.8045   0.05631   0.05162  -0.0420   0.0598   1.0000
  18.250   1.8116   0.05839   0.05376  -0.0419   0.0587   1.0000
  18.500   1.8170   0.06068   0.05609  -0.0418   0.0575   1.0000
  18.750   1.8189   0.06342   0.05887  -0.0419   0.0564   1.0000
  19.000   1.8151   0.06688   0.06238  -0.0420   0.0551   1.0000
  19.250   1.8203   0.06924   0.06482  -0.0421   0.0542   1.0000
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