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S1016 (s1016-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S1016 (s1016-il)
Reynolds number: 1,000,000
Max Cl/Cd: 51.99 at α=9.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1016-il-1000000-n5.txt
Download as CSV file: xf-s1016-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1016                                           
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.2677   0.06371   0.05860  -0.0637   0.8374   0.0169
 -19.500  -1.2718   0.06015   0.05496  -0.0648   0.8363   0.0173
 -19.250  -1.2738   0.05695   0.05167  -0.0657   0.8352   0.0177
 -19.000  -1.2734   0.05414   0.04877  -0.0663   0.8340   0.0180
 -18.750  -1.2720   0.05154   0.04609  -0.0668   0.8329   0.0184
 -18.500  -1.2717   0.04891   0.04338  -0.0670   0.8317   0.0189
 -18.250  -1.2700   0.04652   0.04092  -0.0671   0.8306   0.0195
 -18.000  -1.2664   0.04439   0.03871  -0.0670   0.8295   0.0198
 -17.750  -1.2621   0.04239   0.03666  -0.0668   0.8284   0.0205
 -17.500  -1.2562   0.04062   0.03482  -0.0665   0.8273   0.0211
 -17.000  -1.2429   0.03734   0.03142  -0.0655   0.8253   0.0225
 -16.750  -1.2354   0.03583   0.02987  -0.0649   0.8247   0.0232
 -16.500  -1.2270   0.03443   0.02842  -0.0643   0.8239   0.0240
 -16.250  -1.2177   0.03316   0.02710  -0.0635   0.8231   0.0248
 -16.000  -1.2071   0.03201   0.02591  -0.0628   0.8222   0.0257
 -15.750  -1.1976   0.03081   0.02468  -0.0619   0.8213   0.0268
 -15.500  -1.1869   0.02972   0.02356  -0.0610   0.8204   0.0278
 -15.250  -1.1752   0.02873   0.02254  -0.0601   0.8196   0.0290
 -15.000  -1.1627   0.02782   0.02159  -0.0592   0.8188   0.0299
 -14.750  -1.1499   0.02695   0.02067  -0.0583   0.8180   0.0310
 -14.500  -1.1376   0.02605   0.01977  -0.0573   0.8172   0.0324
 -14.250  -1.1240   0.02526   0.01895  -0.0563   0.8164   0.0339
 -14.000  -1.1090   0.02457   0.01822  -0.0554   0.8156   0.0350
 -13.750  -1.0952   0.02382   0.01745  -0.0544   0.8149   0.0365
 -13.500  -1.0811   0.02311   0.01672  -0.0533   0.8141   0.0383
 -13.250  -1.0651   0.02250   0.01609  -0.0524   0.8134   0.0398
 -13.000  -1.0488   0.02192   0.01548  -0.0515   0.8127   0.0412
 -12.750  -1.0339   0.02129   0.01483  -0.0504   0.8119   0.0431
 -12.500  -1.0177   0.02072   0.01425  -0.0494   0.8111   0.0451
 -12.250  -1.0002   0.02023   0.01373  -0.0485   0.8104   0.0469
 -12.000  -0.9830   0.01973   0.01321  -0.0475   0.8096   0.0485
 -11.750  -0.9666   0.01919   0.01268  -0.0465   0.8087   0.0513
 -11.500  -0.9487   0.01872   0.01220  -0.0455   0.8083   0.0534
 -11.250  -0.9303   0.01828   0.01175  -0.0447   0.8079   0.0556
 -11.000  -0.9125   0.01780   0.01129  -0.0437   0.8074   0.0584
 -10.750  -0.8939   0.01738   0.01087  -0.0428   0.8070   0.0614
 -10.500  -0.8753   0.01696   0.01045  -0.0419   0.8064   0.0642
 -10.250  -0.8570   0.01653   0.01003  -0.0409   0.8059   0.0681
 -10.000  -0.8373   0.01617   0.00967  -0.0400   0.8053   0.0713
  -9.750  -0.8185   0.01576   0.00929  -0.0391   0.8046   0.0754
  -9.500  -0.7992   0.01539   0.00893  -0.0381   0.8038   0.0793
  -9.250  -0.7791   0.01506   0.00860  -0.0373   0.8032   0.0827
  -9.000  -0.7597   0.01469   0.00826  -0.0364   0.8026   0.0874
  -8.750  -0.7394   0.01438   0.00795  -0.0355   0.8020   0.0918
  -8.500  -0.7192   0.01406   0.00765  -0.0346   0.8013   0.0962
  -8.250  -0.6994   0.01373   0.00735  -0.0337   0.8007   0.1013
  -8.000  -0.6783   0.01346   0.00708  -0.0329   0.8001   0.1060
  -7.750  -0.6582   0.01314   0.00680  -0.0319   0.7995   0.1116
  -7.500  -0.6375   0.01287   0.00654  -0.0311   0.7989   0.1173
  -7.250  -0.6171   0.01258   0.00628  -0.0301   0.7982   0.1235
  -7.000  -0.5963   0.01231   0.00603  -0.0293   0.7976   0.1295
  -6.750  -0.5755   0.01205   0.00579  -0.0284   0.7970   0.1362
  -6.500  -0.5551   0.01177   0.00555  -0.0273   0.7964   0.1440
  -6.250  -0.5341   0.01153   0.00533  -0.0264   0.7956   0.1509
  -6.000  -0.5139   0.01127   0.00511  -0.0254   0.7948   0.1598
  -5.750  -0.4939   0.01100   0.00489  -0.0243   0.7941   0.1699
  -5.500  -0.4736   0.01077   0.00468  -0.0232   0.7934   0.1803
  -5.250  -0.4541   0.01052   0.00449  -0.0220   0.7927   0.1917
  -5.000  -0.4348   0.01028   0.00430  -0.0206   0.7918   0.2037
  -4.750  -0.4160   0.01003   0.00412  -0.0192   0.7911   0.2171
  -4.500  -0.3970   0.00982   0.00396  -0.0178   0.7904   0.2295
  -4.000  -0.3640   0.00942   0.00371  -0.0138   0.7888   0.2625
  -3.750  -0.3455   0.00922   0.00359  -0.0122   0.7878   0.2812
  -3.500  -0.3262   0.00898   0.00347  -0.0108   0.7867   0.3040
  -3.250  -0.3056   0.00875   0.00334  -0.0096   0.7854   0.3272
  -3.000  -0.2845   0.00853   0.00321  -0.0085   0.7840   0.3514
  -2.750  -0.2641   0.00826   0.00308  -0.0072   0.7826   0.3824
  -2.500  -0.2428   0.00799   0.00293  -0.0062   0.7809   0.4115
  -2.250  -0.2218   0.00768   0.00274  -0.0050   0.7786   0.4471
  -2.000  -0.2006   0.00736   0.00255  -0.0039   0.7759   0.4848
  -1.750  -0.1790   0.00704   0.00239  -0.0028   0.7728   0.5245
  -1.500  -0.1581   0.00665   0.00221  -0.0016   0.7692   0.5714
  -1.250  -0.1361   0.00629   0.00203  -0.0006   0.7656   0.6185
  -1.000  -0.1136   0.00595   0.00191   0.0004   0.7621   0.6694
  -0.750  -0.0876   0.00583   0.00192   0.0008   0.7585   0.7108
  -0.500  -0.0587   0.00582   0.00197   0.0006   0.7537   0.7273
  -0.250  -0.0295   0.00582   0.00199   0.0003   0.7486   0.7370
   0.000   0.0000   0.00580   0.00194   0.0000   0.7435   0.7435
   0.250   0.0295   0.00582   0.00199  -0.0003   0.7370   0.7486
   0.500   0.0587   0.00582   0.00197  -0.0006   0.7273   0.7538
   0.750   0.0875   0.00583   0.00192  -0.0008   0.7105   0.7585
   1.000   0.1135   0.00595   0.00191  -0.0004   0.6693   0.7622
   1.250   0.1360   0.00629   0.00203   0.0006   0.6179   0.7656
   1.500   0.1581   0.00665   0.00221   0.0016   0.5711   0.7692
   1.750   0.1792   0.00703   0.00239   0.0028   0.5255   0.7728
   2.000   0.2006   0.00736   0.00255   0.0039   0.4848   0.7759
   2.250   0.2222   0.00766   0.00274   0.0049   0.4494   0.7786
   2.500   0.2429   0.00799   0.00293   0.0061   0.4122   0.7809
   2.750   0.2641   0.00826   0.00308   0.0072   0.3822   0.7826
   3.000   0.2846   0.00852   0.00321   0.0085   0.3518   0.7840
   3.250   0.3054   0.00876   0.00334   0.0096   0.3260   0.7854
   3.500   0.3262   0.00898   0.00347   0.0108   0.3039   0.7867
   3.750   0.3455   0.00922   0.00359   0.0122   0.2812   0.7878
   4.000   0.3638   0.00943   0.00371   0.0138   0.2616   0.7888
   4.250   0.3802   0.00961   0.00382   0.0159   0.2449   0.7897
   4.500   0.3971   0.00982   0.00396   0.0178   0.2295   0.7904
   4.750   0.4155   0.01005   0.00412   0.0193   0.2156   0.7911
   5.000   0.4346   0.01029   0.00430   0.0207   0.2029   0.7918
   5.250   0.4542   0.01051   0.00448   0.0219   0.1919   0.7927
   5.500   0.4737   0.01076   0.00468   0.0232   0.1804   0.7934
   5.750   0.4940   0.01100   0.00489   0.0242   0.1701   0.7941
   6.000   0.5142   0.01126   0.00510   0.0253   0.1605   0.7948
   6.250   0.5344   0.01152   0.00533   0.0264   0.1513   0.7956
   6.500   0.5553   0.01177   0.00555   0.0273   0.1443   0.7964
   6.750   0.5752   0.01206   0.00580   0.0284   0.1351   0.7970
   7.000   0.5965   0.01231   0.00603   0.0292   0.1295   0.7976
   7.250   0.6172   0.01258   0.00628   0.0301   0.1234   0.7983
   7.500   0.6378   0.01286   0.00653   0.0310   0.1175   0.7989
   7.750   0.6587   0.01313   0.00679   0.0319   0.1122   0.7995
   8.000   0.6786   0.01345   0.00708   0.0329   0.1059   0.8001
   8.250   0.6998   0.01372   0.00734   0.0336   0.1021   0.8007
   8.500   0.7196   0.01405   0.00764   0.0346   0.0962   0.8014
   8.750   0.7397   0.01437   0.00795   0.0355   0.0919   0.8020
   9.000   0.7599   0.01469   0.00826   0.0363   0.0872   0.8026
   9.250   0.7794   0.01506   0.00859   0.0373   0.0827   0.8032
   9.500   0.7996   0.01538   0.00892   0.0381   0.0795   0.8039
   9.750   0.8189   0.01575   0.00928   0.0390   0.0755   0.8046
  10.000   0.8377   0.01616   0.00966   0.0400   0.0714   0.8053
  10.250   0.8575   0.01652   0.01003   0.0408   0.0682   0.8059
  10.500   0.8757   0.01696   0.01044   0.0418   0.0641   0.8065
  10.750   0.8944   0.01737   0.01085   0.0427   0.0615   0.8070
  11.000   0.9129   0.01780   0.01128   0.0436   0.0582   0.8074
  11.250   0.9307   0.01827   0.01174   0.0446   0.0554   0.8079
  11.500   0.9492   0.01871   0.01219   0.0455   0.0533   0.8083
  11.750   0.9671   0.01918   0.01267   0.0464   0.0513   0.8087
  12.000   0.9839   0.01969   0.01318   0.0474   0.0488   0.8096
  12.250   1.0007   0.02022   0.01372   0.0484   0.0467   0.8104
  12.500   1.0183   0.02071   0.01423   0.0493   0.0449   0.8111
  12.750   1.0344   0.02127   0.01481   0.0503   0.0430   0.8119
  13.000   1.0495   0.02191   0.01546   0.0514   0.0411   0.8127
  13.250   1.0658   0.02248   0.01606   0.0523   0.0399   0.8134
  13.500   1.0819   0.02308   0.01669   0.0532   0.0384   0.8141
  13.750   1.0959   0.02380   0.01742   0.0543   0.0364   0.8149
  14.000   1.1098   0.02454   0.01819   0.0553   0.0351   0.8157
  14.250   1.1248   0.02524   0.01892   0.0562   0.0337   0.8164
  14.500   1.1384   0.02602   0.01973   0.0572   0.0323   0.8172
  14.750   1.1508   0.02690   0.02063   0.0582   0.0311   0.8180
  15.000   1.1635   0.02779   0.02155   0.0592   0.0299   0.8188
  15.250   1.1762   0.02868   0.02249   0.0600   0.0289   0.8196
  15.500   1.1880   0.02967   0.02351   0.0609   0.0279   0.8204
  15.750   1.1990   0.03073   0.02460   0.0618   0.0268   0.8213
  16.000   1.2083   0.03195   0.02585   0.0627   0.0258   0.8222
  16.250   1.2190   0.03308   0.02703   0.0634   0.0247   0.8231
  16.500   1.2284   0.03436   0.02835   0.0641   0.0240   0.8240
  16.750   1.2368   0.03574   0.02978   0.0648   0.0232   0.8247
  17.000   1.2439   0.03729   0.03135   0.0654   0.0223   0.8253
  17.500   1.2577   0.04051   0.03471   0.0664   0.0212   0.8273
  17.750   1.2638   0.04227   0.03653   0.0667   0.0205   0.8285
  18.000   1.2685   0.04423   0.03856   0.0669   0.0200   0.8296
  18.250   1.2715   0.04641   0.04080   0.0670   0.0193   0.8307
  18.500   1.2733   0.04879   0.04325   0.0669   0.0188   0.8318
  18.750   1.2744   0.05132   0.04586   0.0667   0.0184   0.8329
  19.000   1.2758   0.05392   0.04855   0.0663   0.0181   0.8341
  19.250   1.2758   0.05677   0.05148   0.0657   0.0177   0.8353
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