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S1016 (s1016-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S1016 (s1016-il)
Reynolds number: 1,000,000
Max Cl/Cd: 52.2 at α=9.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1016-il-1000000.txt
Download as CSV file: xf-s1016-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.500  -1.2497   0.06214   0.05732  -0.0657   0.8729   0.0226
 -19.250  -1.2571   0.05823   0.05333  -0.0668   0.8712   0.0231
 -19.000  -1.2589   0.05512   0.05015  -0.0676   0.8694   0.0236
 -18.750  -1.2605   0.05215   0.04709  -0.0682   0.8676   0.0241
 -18.500  -1.2586   0.04967   0.04452  -0.0685   0.8659   0.0248
 -18.250  -1.2544   0.04751   0.04227  -0.0686   0.8642   0.0254
 -18.000  -1.2495   0.04546   0.04013  -0.0686   0.8624   0.0258
 -17.750  -1.2517   0.04284   0.03743  -0.0684   0.8607   0.0267
 -17.500  -1.2488   0.04078   0.03532  -0.0680   0.8590   0.0276
 -17.250  -1.2429   0.03903   0.03353  -0.0676   0.8580   0.0284
 -17.000  -1.2343   0.03756   0.03200  -0.0672   0.8568   0.0295
 -16.750  -1.2247   0.03621   0.03059  -0.0667   0.8556   0.0302
 -16.500  -1.2206   0.03448   0.02881  -0.0658   0.8545   0.0313
 -16.250  -1.2131   0.03307   0.02738  -0.0650   0.8534   0.0325
 -16.000  -1.2030   0.03189   0.02616  -0.0643   0.8523   0.0338
 -15.750  -1.1903   0.03092   0.02513  -0.0636   0.8513   0.0349
 -15.500  -1.1813   0.02972   0.02389  -0.0626   0.8502   0.0362
 -15.250  -1.1714   0.02862   0.02278  -0.0616   0.8492   0.0378
 -15.000  -1.1596   0.02768   0.02180  -0.0606   0.8482   0.0392
 -14.750  -1.1453   0.02691   0.02097  -0.0598   0.8472   0.0404
 -14.500  -1.1336   0.02601   0.02003  -0.0588   0.8461   0.0421
 -14.250  -1.1215   0.02515   0.01917  -0.0577   0.8451   0.0440
 -14.000  -1.1069   0.02445   0.01844  -0.0567   0.8440   0.0456
 -13.750  -1.0908   0.02387   0.01781  -0.0559   0.8428   0.0470
 -13.500  -1.0782   0.02307   0.01700  -0.0547   0.8422   0.0494
 -13.250  -1.0633   0.02240   0.01634  -0.0537   0.8417   0.0515
 -13.000  -1.0466   0.02184   0.01576  -0.0528   0.8411   0.0535
 -12.750  -1.0304   0.02127   0.01516  -0.0519   0.8406   0.0553
 -12.500  -1.0158   0.02062   0.01452  -0.0507   0.8399   0.0581
 -12.250  -0.9987   0.02010   0.01400  -0.0498   0.8393   0.0607
 -12.000  -0.9802   0.01966   0.01353  -0.0490   0.8386   0.0623
 -11.750  -0.9649   0.01907   0.01295  -0.0478   0.8379   0.0660
 -11.500  -0.9478   0.01858   0.01247  -0.0468   0.8370   0.0690
 -11.250  -0.9285   0.01819   0.01206  -0.0460   0.8362   0.0714
 -11.000  -0.9115   0.01770   0.01158  -0.0449   0.8354   0.0755
 -10.750  -0.8936   0.01726   0.01116  -0.0440   0.8347   0.0793
 -10.500  -0.8739   0.01692   0.01079  -0.0432   0.8340   0.0821
 -10.250  -0.8568   0.01644   0.01036  -0.0420   0.8333   0.0876
 -10.000  -0.8373   0.01609   0.01001  -0.0412   0.8326   0.0918
  -9.750  -0.8184   0.01572   0.00964  -0.0402   0.8320   0.0967
  -9.500  -0.7998   0.01534   0.00929  -0.0392   0.8313   0.1021
  -9.250  -0.7794   0.01505   0.00899  -0.0384   0.8306   0.1062
  -9.000  -0.7609   0.01467   0.00865  -0.0373   0.8300   0.1128
  -8.750  -0.7405   0.01438   0.00837  -0.0365   0.8294   0.1180
  -8.500  -0.7215   0.01405   0.00806  -0.0354   0.8287   0.1246
  -8.250  -0.7017   0.01377   0.00780  -0.0345   0.8280   0.1310
  -8.000  -0.6820   0.01350   0.00756  -0.0335   0.8270   0.1382
  -7.750  -0.6624   0.01327   0.00736  -0.0325   0.8259   0.1456
  -7.500  -0.6427   0.01299   0.00711  -0.0315   0.8254   0.1540
  -7.250  -0.6223   0.01272   0.00688  -0.0305   0.8250   0.1627
  -7.000  -0.6031   0.01240   0.00662  -0.0294   0.8246   0.1732
  -6.750  -0.5834   0.01212   0.00639  -0.0284   0.8240   0.1841
  -6.250  -0.5448   0.01155   0.00593  -0.0261   0.8225   0.2091
  -6.000  -0.5262   0.01125   0.00571  -0.0248   0.8216   0.2234
  -5.750  -0.5084   0.01096   0.00549  -0.0233   0.8208   0.2403
  -5.500  -0.4913   0.01066   0.00528  -0.0217   0.8198   0.2587
  -5.250  -0.4751   0.01036   0.00507  -0.0198   0.8186   0.2782
  -5.000  -0.4609   0.01011   0.00491  -0.0175   0.8175   0.2993
  -4.750  -0.4499   0.00987   0.00477  -0.0146   0.8162   0.3236
  -4.500  -0.4362   0.00965   0.00465  -0.0120   0.8150   0.3497
  -4.250  -0.4208   0.00937   0.00451  -0.0099   0.8138   0.3800
  -4.000  -0.4049   0.00908   0.00435  -0.0078   0.8126   0.4151
  -3.750  -0.3882   0.00878   0.00420  -0.0059   0.8114   0.4535
  -3.500  -0.3721   0.00848   0.00408  -0.0038   0.8100   0.4970
  -3.250  -0.3555   0.00824   0.00403  -0.0019   0.8084   0.5448
  -3.000  -0.3375   0.00784   0.00385  -0.0002   0.8072   0.5966
  -2.750  -0.3188   0.00743   0.00371   0.0014   0.8055   0.6533
  -2.500  -0.2954   0.00726   0.00374   0.0023   0.8034   0.7009
  -2.250  -0.2673   0.00724   0.00377   0.0024   0.8011   0.7246
  -2.000  -0.2383   0.00724   0.00377   0.0022   0.7989   0.7375
  -1.750  -0.2088   0.00720   0.00370   0.0020   0.7965   0.7455
  -1.500  -0.1789   0.00719   0.00366   0.0018   0.7942   0.7523
  -1.250  -0.1501   0.00728   0.00369   0.0016   0.7914   0.7581
  -1.000  -0.1200   0.00726   0.00370   0.0013   0.7891   0.7622
  -0.750  -0.0901   0.00727   0.00373   0.0010   0.7857   0.7664
  -0.500  -0.0602   0.00725   0.00370   0.0007   0.7824   0.7706
  -0.250  -0.0303   0.00723   0.00364   0.0004   0.7797   0.7742
   0.000   0.0000   0.00718   0.00358   0.0000   0.7771   0.7771
   0.250   0.0303   0.00724   0.00364  -0.0004   0.7742   0.7797
   0.500   0.0602   0.00725   0.00371  -0.0007   0.7706   0.7825
   0.750   0.0901   0.00727   0.00373  -0.0010   0.7664   0.7858
   1.000   0.1200   0.00726   0.00370  -0.0013   0.7621   0.7891
   1.250   0.1501   0.00728   0.00369  -0.0016   0.7580   0.7914
   1.500   0.1789   0.00719   0.00366  -0.0018   0.7523   0.7942
   1.750   0.2088   0.00720   0.00370  -0.0020   0.7455   0.7965
   2.000   0.2383   0.00724   0.00377  -0.0022   0.7375   0.7989
   2.250   0.2673   0.00724   0.00377  -0.0024   0.7250   0.8011
   2.500   0.2954   0.00726   0.00374  -0.0023   0.7009   0.8034
   2.750   0.3188   0.00743   0.00371  -0.0014   0.6532   0.8055
   3.000   0.3375   0.00783   0.00385   0.0002   0.5968   0.8072
   3.250   0.3558   0.00823   0.00403   0.0019   0.5457   0.8084
   3.500   0.3721   0.00848   0.00408   0.0038   0.4968   0.8100
   3.750   0.3882   0.00878   0.00420   0.0059   0.4532   0.8114
   4.000   0.4045   0.00909   0.00435   0.0079   0.4135   0.8126
   4.250   0.4207   0.00938   0.00451   0.0099   0.3792   0.8138
   4.500   0.4362   0.00965   0.00465   0.0120   0.3494   0.8150
   4.750   0.4494   0.00988   0.00478   0.0147   0.3220   0.8162
   5.000   0.4609   0.01011   0.00491   0.0175   0.2991   0.8175
   5.250   0.4752   0.01036   0.00507   0.0198   0.2781   0.8186
   5.500   0.4915   0.01065   0.00527   0.0216   0.2588   0.8198
   5.750   0.5086   0.01095   0.00549   0.0233   0.2405   0.8208
   6.000   0.5265   0.01125   0.00571   0.0247   0.2240   0.8216
   6.250   0.5450   0.01154   0.00593   0.0260   0.2093   0.8225
   6.750   0.5832   0.01213   0.00639   0.0284   0.1832   0.8240
   7.000   0.6033   0.01240   0.00662   0.0294   0.1732   0.8246
   7.250   0.6225   0.01271   0.00687   0.0305   0.1627   0.8250
   7.500   0.6431   0.01298   0.00711   0.0314   0.1543   0.8254
   7.750   0.6627   0.01326   0.00735   0.0324   0.1459   0.8260
   8.000   0.6823   0.01349   0.00755   0.0334   0.1384   0.8270
   8.250   0.7020   0.01376   0.00780   0.0344   0.1313   0.8280
   8.500   0.7218   0.01405   0.00806   0.0354   0.1246   0.8287
   8.750   0.7409   0.01438   0.00836   0.0364   0.1180   0.8294
   9.000   0.7611   0.01467   0.00864   0.0373   0.1125   0.8300
   9.250   0.7797   0.01504   0.00898   0.0383   0.1062   0.8307
   9.500   0.8002   0.01533   0.00928   0.0391   0.1023   0.8313
   9.750   0.8188   0.01571   0.00963   0.0401   0.0968   0.8320
  10.000   0.8377   0.01608   0.01000   0.0411   0.0919   0.8326
  10.250   0.8572   0.01644   0.01035   0.0420   0.0876   0.8333
  10.500   0.8743   0.01691   0.01078   0.0431   0.0820   0.8340
  10.750   0.8941   0.01725   0.01114   0.0439   0.0793   0.8347
  11.000   0.9119   0.01769   0.01157   0.0449   0.0752   0.8354
  11.250   0.9291   0.01818   0.01204   0.0459   0.0713   0.8362
  11.500   0.9483   0.01857   0.01245   0.0467   0.0689   0.8370
  11.750   0.9652   0.01907   0.01295   0.0478   0.0658   0.8379
  12.000   0.9806   0.01966   0.01352   0.0490   0.0624   0.8387
  12.250   0.9992   0.02008   0.01398   0.0497   0.0605   0.8393
  12.500   1.0163   0.02061   0.01450   0.0507   0.0580   0.8399
  12.750   1.0310   0.02126   0.01514   0.0518   0.0552   0.8406
  13.000   1.0474   0.02181   0.01573   0.0527   0.0533   0.8412
  13.250   1.0639   0.02238   0.01632   0.0536   0.0515   0.8417
  13.500   1.0789   0.02304   0.01698   0.0546   0.0495   0.8422
  13.750   1.0916   0.02384   0.01777   0.0558   0.0470   0.8429
  14.000   1.1074   0.02443   0.01843   0.0567   0.0457   0.8440
  14.250   1.1223   0.02511   0.01913   0.0576   0.0439   0.8451
  14.500   1.1342   0.02599   0.02001   0.0587   0.0420   0.8461
  14.750   1.1459   0.02690   0.02096   0.0598   0.0405   0.8472
  15.000   1.1604   0.02765   0.02176   0.0606   0.0391   0.8482
  15.250   1.1724   0.02857   0.02272   0.0615   0.0378   0.8492
  15.500   1.1825   0.02966   0.02383   0.0625   0.0363   0.8502
  15.750   1.1914   0.03087   0.02508   0.0635   0.0349   0.8513
  16.000   1.2038   0.03185   0.02612   0.0642   0.0339   0.8524
  16.250   1.2143   0.03300   0.02730   0.0650   0.0325   0.8535
  16.500   1.2219   0.03440   0.02873   0.0658   0.0314   0.8546
  16.750   1.2260   0.03612   0.03049   0.0666   0.0301   0.8557
  17.000   1.2368   0.03737   0.03181   0.0671   0.0293   0.8569
  17.250   1.2444   0.03893   0.03342   0.0675   0.0284   0.8581
  17.500   1.2495   0.04074   0.03529   0.0680   0.0277   0.8591
  17.750   1.2537   0.04268   0.03728   0.0683   0.0267   0.8608
  18.000   1.2511   0.04535   0.04002   0.0685   0.0259   0.8626
  18.250   1.2572   0.04726   0.04202   0.0685   0.0253   0.8643
  18.500   1.2610   0.04946   0.04431   0.0684   0.0248   0.8660
  18.750   1.2628   0.05195   0.04688   0.0681   0.0242   0.8678
  19.000   1.2625   0.05476   0.04977   0.0676   0.0237   0.8696
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