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NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: NASA/LANGLEY MS(1)-0317 AIRFOIL (ms317-il)
Reynolds number: 200,000
Max Cl/Cd: 48.53 at α=4.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-ms317-il-200000.txt
Download as CSV file: xf-ms317-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.5797   0.08953   0.08539  -0.0633   1.0000   0.0516
 -14.500  -0.5697   0.08797   0.08386  -0.0634   1.0000   0.0523
 -14.250  -0.9042   0.05918   0.05355  -0.0733   1.0000   0.0459
 -14.000  -0.9118   0.05595   0.05018  -0.0734   1.0000   0.0462
 -13.750  -0.9170   0.05308   0.04717  -0.0731   1.0000   0.0465
 -13.500  -0.9206   0.05054   0.04451  -0.0726   1.0000   0.0470
 -13.250  -0.9253   0.04809   0.04191  -0.0717   1.0000   0.0475
 -13.000  -0.9312   0.04573   0.03937  -0.0703   1.0000   0.0481
 -12.750  -0.9387   0.04358   0.03702  -0.0681   1.0000   0.0487
 -12.500  -0.9491   0.04179   0.03505  -0.0648   1.0000   0.0492
 -12.250  -0.9589   0.04020   0.03326  -0.0611   1.0000   0.0497
 -12.000  -0.9697   0.03894   0.03180  -0.0566   1.0000   0.0501
 -11.750  -0.9827   0.03800   0.03066  -0.0515   1.0000   0.0505
 -11.500  -0.9827   0.03670   0.02932  -0.0480   1.0000   0.0510
 -11.250  -0.9789   0.03581   0.02845  -0.0449   1.0000   0.0517
 -11.000  -0.9586   0.03468   0.02728  -0.0450   0.9981   0.0528
 -10.750  -0.9262   0.03331   0.02580  -0.0472   0.9947   0.0544
 -10.500  -0.8948   0.03189   0.02408  -0.0493   0.9909   0.0564
 -10.250  -0.8621   0.03050   0.02273  -0.0511   0.9872   0.0583
 -10.000  -0.8275   0.02946   0.02168  -0.0533   0.9836   0.0605
  -9.750  -0.7916   0.02834   0.02039  -0.0556   0.9809   0.0630
  -9.500  -0.7606   0.02722   0.01932  -0.0568   0.9766   0.0654
  -9.250  -0.7272   0.02640   0.01849  -0.0587   0.9721   0.0686
  -9.000  -0.6912   0.02537   0.01739  -0.0609   0.9692   0.0722
  -8.750  -0.6536   0.02446   0.01657  -0.0635   0.9670   0.0763
  -8.500  -0.6246   0.02364   0.01571  -0.0643   0.9613   0.0809
  -8.250  -0.5909   0.02284   0.01498  -0.0663   0.9572   0.0867
  -8.000  -0.5562   0.02190   0.01411  -0.0684   0.9540   0.0935
  -7.750  -0.5205   0.02102   0.01326  -0.0707   0.9513   0.1024
  -7.500  -0.4967   0.02055   0.01276  -0.0706   0.9437   0.1111
  -7.250  -0.4667   0.01976   0.01208  -0.0719   0.9391   0.1223
  -7.000  -0.4345   0.01901   0.01141  -0.0735   0.9356   0.1358
  -6.750  -0.4105   0.01844   0.01093  -0.0736   0.9290   0.1502
  -6.500  -0.3835   0.01780   0.01040  -0.0742   0.9231   0.1693
  -6.250  -0.3539   0.01702   0.00980  -0.0755   0.9188   0.1976
  -6.000  -0.3268   0.01624   0.00928  -0.0764   0.9137   0.2401
  -5.750  -0.3017   0.01534   0.00877  -0.0773   0.9072   0.3100
  -5.500  -0.2721   0.01412   0.00828  -0.0792   0.9027   0.4384
  -5.250  -0.2427   0.01392   0.00856  -0.0792   0.8990   0.5428
  -5.000  -0.2156   0.01424   0.00895  -0.0787   0.8932   0.5869
  -4.750  -0.1878   0.01463   0.00934  -0.0782   0.8876   0.6123
  -4.500  -0.1586   0.01500   0.00966  -0.0778   0.8832   0.6310
  -4.250  -0.1285   0.01534   0.00991  -0.0776   0.8796   0.6464
  -4.000  -0.1037   0.01590   0.01048  -0.0764   0.8737   0.6568
  -3.750  -0.0768   0.01630   0.01084  -0.0757   0.8683   0.6669
  -3.500  -0.0505   0.01676   0.01128  -0.0745   0.8641   0.6752
  -3.250  -0.0214   0.01702   0.01147  -0.0742   0.8607   0.6848
  -3.000   0.0012   0.01765   0.01213  -0.0722   0.8556   0.6910
  -2.750   0.0288   0.01797   0.01240  -0.0721   0.8497   0.7026
  -2.500   0.0506   0.01852   0.01298  -0.0694   0.8452   0.7074
  -2.250   0.0763   0.01885   0.01328  -0.0680   0.8415   0.7138
  -2.000   0.1056   0.01896   0.01334  -0.0685   0.8371   0.7229
  -1.750   0.1254   0.01946   0.01389  -0.0660   0.8310   0.7271
  -1.500   0.1493   0.01979   0.01422  -0.0643   0.8262   0.7339
  -1.250   0.1786   0.01984   0.01422  -0.0644   0.8226   0.7432
  -1.000   0.2002   0.02017   0.01456  -0.0620   0.8188   0.7474
  -0.750   0.2232   0.02036   0.01478  -0.0610   0.8114   0.7529
  -0.500   0.2601   0.02003   0.01436  -0.0638   0.8060   0.7603
  -0.250   0.2866   0.01980   0.01410  -0.0627   0.8015   0.7628
   0.000   0.3090   0.01970   0.01402  -0.0612   0.7913   0.7654
   0.250   0.3380   0.01916   0.01339  -0.0601   0.7822   0.7686
   0.500   0.3648   0.01886   0.01307  -0.0597   0.7699   0.7727
   0.750   0.3998   0.01844   0.01254  -0.0612   0.7626   0.7775
   1.000   0.4285   0.01823   0.01235  -0.0616   0.7531   0.7812
   1.250   0.4550   0.01795   0.01204  -0.0607   0.7450   0.7833
   1.500   0.4808   0.01779   0.01189  -0.0600   0.7358   0.7860
   1.750   0.5091   0.01755   0.01162  -0.0598   0.7263   0.7894
   2.000   0.5390   0.01733   0.01140  -0.0602   0.7161   0.7931
   2.250   0.5729   0.01702   0.01103  -0.0616   0.7054   0.7966
   2.500   0.6019   0.01681   0.01084  -0.0619   0.6928   0.7997
   2.750   0.6273   0.01659   0.01061  -0.0610   0.6811   0.8021
   3.000   0.6535   0.01639   0.01041  -0.0603   0.6670   0.8047
   3.250   0.6806   0.01623   0.01025  -0.0601   0.6496   0.8074
   3.500   0.7090   0.01607   0.01006  -0.0602   0.6288   0.8105
   3.750   0.7379   0.01599   0.00993  -0.0606   0.6004   0.8142
   4.000   0.7661   0.01598   0.00978  -0.0608   0.5600   0.8173
   4.250   0.7847   0.01617   0.00968  -0.0589   0.4975   0.8195
   4.500   0.7960   0.01689   0.00989  -0.0559   0.4117   0.8223
   4.750   0.8066   0.01783   0.01039  -0.0533   0.3383   0.8255
   5.000   0.8209   0.01872   0.01092  -0.0516   0.2852   0.8287
   5.250   0.8393   0.01950   0.01146  -0.0508   0.2505   0.8317
   5.500   0.8604   0.02026   0.01200  -0.0505   0.2271   0.8346
   5.750   0.8761   0.02076   0.01243  -0.0486   0.2122   0.8370
   6.000   0.8927   0.02131   0.01293  -0.0469   0.2009   0.8399
   6.250   0.9097   0.02195   0.01346  -0.0455   0.1917   0.8429
   6.500   0.9305   0.02246   0.01398  -0.0447   0.1840   0.8459
   6.750   0.9509   0.02304   0.01450  -0.0441   0.1774   0.8489
   7.000   0.9738   0.02376   0.01515  -0.0440   0.1716   0.8517
   7.250   0.9917   0.02416   0.01560  -0.0426   0.1668   0.8542
   7.500   1.0102   0.02469   0.01612  -0.0413   0.1627   0.8572
   7.750   1.0340   0.02556   0.01685  -0.0411   0.1584   0.8605
   8.000   1.0568   0.02606   0.01745  -0.0407   0.1556   0.8639
   8.250   1.0820   0.02666   0.01810  -0.0408   0.1524   0.8670
   8.500   1.1054   0.02725   0.01871  -0.0406   0.1493   0.8698
   8.750   1.1270   0.02785   0.01929  -0.0399   0.1466   0.8729
   9.000   1.1578   0.02881   0.02016  -0.0407   0.1435   0.8761
   9.250   1.1795   0.02941   0.02089  -0.0402   0.1417   0.8801
   9.500   1.2041   0.03013   0.02170  -0.0402   0.1396   0.8837
   9.750   1.2257   0.03078   0.02243  -0.0396   0.1374   0.8869
  10.000   1.2465   0.03143   0.02313  -0.0389   0.1352   0.8905
  10.250   1.2705   0.03216   0.02386  -0.0388   0.1332   0.8944
  10.500   1.3035   0.03324   0.02489  -0.0402   0.1310   0.8983
  10.750   1.3291   0.03438   0.02613  -0.0404   0.1291   0.9024
  11.000   1.3424   0.03509   0.02700  -0.0386   0.1277   0.9075
  11.250   1.3599   0.03597   0.02803  -0.0376   0.1259   0.9126
  11.500   1.3765   0.03685   0.02904  -0.0365   0.1241   0.9176
  11.750   1.3918   0.03766   0.02994  -0.0352   0.1223   0.9234
  12.000   1.4112   0.03853   0.03083  -0.0347   0.1204   0.9295
  12.250   1.4341   0.03945   0.03172  -0.0345   0.1186   0.9359
  12.500   1.4545   0.04105   0.03342  -0.0342   0.1167   0.9435
  12.750   1.4558   0.04196   0.03456  -0.0311   0.1155   0.9557
  13.000   1.4589   0.04301   0.03582  -0.0286   0.1141   0.9796
  13.250   1.4705   0.04441   0.03739  -0.0280   0.1123   1.0000
  13.500   1.4837   0.04586   0.03895  -0.0278   0.1106   1.0000
  13.750   1.4981   0.04723   0.04040  -0.0276   0.1089   1.0000
  14.000   1.5208   0.04844   0.04155  -0.0283   0.1072   1.0000
  14.250   1.5417   0.05073   0.04389  -0.0289   0.1054   1.0000
  14.500   1.5340   0.05302   0.04647  -0.0270   0.1044   1.0000
  14.750   1.5262   0.05564   0.04936  -0.0255   0.1032   1.0000
  15.000   1.5198   0.05838   0.05232  -0.0243   0.1018   1.0000
  15.250   1.5169   0.06097   0.05508  -0.0236   0.1004   1.0000
  15.500   1.5188   0.06321   0.05742  -0.0231   0.0990   1.0000
  15.750   1.5223   0.06531   0.05958  -0.0228   0.0977   1.0000
  16.000   1.5357   0.06678   0.06102  -0.0228   0.0964   1.0000
  16.250   1.5442   0.06957   0.06383  -0.0227   0.0949   1.0000
  16.500   1.5114   0.07475   0.06935  -0.0221   0.0943   1.0000
  16.750   1.4734   0.08112   0.07605  -0.0226   0.0938   1.0000
  17.000   1.4267   0.08938   0.08467  -0.0246   0.0933   1.0000
  17.250   1.3572   0.10216   0.09787  -0.0299   0.0930   1.0000
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