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S8036 (16%) (s8036-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S8036 (16%) (s8036-il)
Reynolds number: 1,000,000
Max Cl/Cd: 82.14 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8036-il-1000000-n5.txt
Download as CSV file: xf-s8036-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8036 (16%)                                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.8925   0.10832   0.10539  -0.0426   1.0000   0.0059
 -18.500  -0.9260   0.09845   0.09537  -0.0477   1.0000   0.0059
 -18.250  -0.9552   0.08948   0.08625  -0.0523   1.0000   0.0060
 -18.000  -0.9777   0.08190   0.07853  -0.0562   1.0000   0.0059
 -17.750  -1.0091   0.07317   0.06963  -0.0608   1.0000   0.0060
 -17.500  -1.0211   0.06780   0.06414  -0.0634   1.0000   0.0060
 -17.250  -1.0399   0.06174   0.05796  -0.0663   1.0000   0.0058
 -17.000  -1.0454   0.05780   0.05391  -0.0679   1.0000   0.0060
 -16.750  -1.0598   0.05295   0.04893  -0.0697   1.0000   0.0059
 -16.500  -1.0656   0.04943   0.04531  -0.0707   1.0000   0.0059
 -16.250  -1.0696   0.04634   0.04212  -0.0712   1.0000   0.0060
 -16.000  -1.0766   0.04308   0.03876  -0.0716   1.0000   0.0059
 -15.750  -1.0763   0.04071   0.03631  -0.0715   1.0000   0.0060
 -15.500  -1.0776   0.03830   0.03380  -0.0713   1.0000   0.0061
 -15.250  -1.0770   0.03616   0.03157  -0.0708   1.0000   0.0061
 -15.000  -1.0720   0.03452   0.02986  -0.0701   1.0000   0.0061
 -14.750  -1.0733   0.03243   0.02768  -0.0692   1.0000   0.0061
 -14.500  -1.0697   0.03084   0.02602  -0.0680   1.0000   0.0061
 -14.250  -1.0652   0.02942   0.02453  -0.0668   1.0000   0.0062
 -14.000  -1.0646   0.02780   0.02283  -0.0650   1.0000   0.0061
 -13.750  -1.0644   0.02627   0.02122  -0.0630   1.0000   0.0063
 -13.500  -1.0591   0.02519   0.02007  -0.0610   1.0000   0.0063
 -13.250  -1.0576   0.02396   0.01878  -0.0584   1.0000   0.0065
 -13.000  -1.0503   0.02290   0.01766  -0.0565   0.9997   0.0066
 -12.750  -1.0266   0.02192   0.01661  -0.0576   0.9981   0.0066
 -12.500  -1.0023   0.02106   0.01572  -0.0585   0.9960   0.0069
 -12.250  -0.9789   0.02021   0.01481  -0.0591   0.9934   0.0068
 -12.000  -0.9593   0.01945   0.01401  -0.0587   0.9893   0.0070
 -11.750  -0.9376   0.01879   0.01330  -0.0585   0.9833   0.0071
 -11.500  -0.9336   0.01821   0.01267  -0.0546   0.9617   0.0072
 -11.250  -0.8951   0.01742   0.01184  -0.0577   0.9485   0.0074
 -11.000  -0.8422   0.01660   0.01095  -0.0638   0.9386   0.0076
 -10.750  -0.7776   0.01575   0.01003  -0.0725   0.9277   0.0079
 -10.500  -0.7179   0.01506   0.00920  -0.0801   0.8986   0.0082
 -10.250  -0.6963   0.01472   0.00867  -0.0794   0.8599   0.0084
 -10.000  -0.6833   0.01440   0.00823  -0.0768   0.8340   0.0088
  -9.750  -0.6696   0.01411   0.00784  -0.0743   0.8152   0.0088
  -9.500  -0.6553   0.01382   0.00747  -0.0719   0.7994   0.0091
  -9.250  -0.6405   0.01355   0.00712  -0.0695   0.7862   0.0096
  -9.000  -0.6251   0.01333   0.00683  -0.0672   0.7743   0.0099
  -8.750  -0.6090   0.01311   0.00655  -0.0650   0.7639   0.0103
  -8.500  -0.5920   0.01286   0.00624  -0.0630   0.7552   0.0108
  -8.250  -0.5731   0.01261   0.00596  -0.0614   0.7463   0.0113
  -8.000  -0.5537   0.01237   0.00568  -0.0599   0.7387   0.0122
  -7.500  -0.5133   0.01192   0.00516  -0.0570   0.7241   0.0146
  -7.250  -0.4917   0.01170   0.00492  -0.0559   0.7177   0.0160
  -7.000  -0.4708   0.01148   0.00468  -0.0546   0.7110   0.0183
  -6.750  -0.4493   0.01127   0.00445  -0.0534   0.7048   0.0207
  -6.500  -0.4268   0.01108   0.00424  -0.0523   0.6991   0.0231
  -6.250  -0.4048   0.01089   0.00403  -0.0512   0.6927   0.0263
  -6.000  -0.3824   0.01069   0.00384  -0.0502   0.6875   0.0299
  -5.750  -0.3596   0.01049   0.00365  -0.0492   0.6818   0.0348
  -5.500  -0.3369   0.01031   0.00346  -0.0482   0.6765   0.0411
  -5.250  -0.3142   0.01013   0.00329  -0.0472   0.6718   0.0487
  -4.750  -0.2682   0.00971   0.00296  -0.0453   0.6621   0.0709
  -4.500  -0.2460   0.00949   0.00280  -0.0443   0.6569   0.0887
  -4.250  -0.2233   0.00927   0.00264  -0.0433   0.6526   0.1076
  -4.000  -0.2007   0.00902   0.00249  -0.0423   0.6481   0.1338
  -3.250  -0.1350   0.00824   0.00206  -0.0389   0.6341   0.2403
  -3.000  -0.1144   0.00789   0.00191  -0.0375   0.6293   0.2958
  -2.750  -0.0938   0.00757   0.00178  -0.0361   0.6244   0.3528
  -2.500  -0.0718   0.00733   0.00168  -0.0350   0.6197   0.3988
  -2.250  -0.0486   0.00712   0.00159  -0.0340   0.6146   0.4392
  -2.000  -0.0254   0.00696   0.00153  -0.0331   0.6091   0.4770
  -1.750  -0.0025   0.00681   0.00148  -0.0320   0.6039   0.5150
  -1.500   0.0221   0.00670   0.00146  -0.0313   0.5992   0.5463
  -1.250   0.0474   0.00665   0.00144  -0.0307   0.5939   0.5661
  -1.000   0.0728   0.00663   0.00143  -0.0302   0.5885   0.5823
  -0.750   0.0989   0.00660   0.00143  -0.0297   0.5839   0.5989
  -0.500   0.1250   0.00658   0.00143  -0.0293   0.5785   0.6135
  -0.250   0.1506   0.00658   0.00143  -0.0288   0.5729   0.6237
   0.000   0.1774   0.00659   0.00143  -0.0285   0.5676   0.6318
   0.250   0.2035   0.00659   0.00144  -0.0281   0.5612   0.6398
   0.500   0.2296   0.00664   0.00145  -0.0277   0.5544   0.6464
   0.750   0.2563   0.00664   0.00146  -0.0274   0.5480   0.6522
   1.000   0.2823   0.00667   0.00148  -0.0270   0.5407   0.6585
   1.250   0.3088   0.00671   0.00150  -0.0267   0.5340   0.6644
   1.500   0.3345   0.00674   0.00152  -0.0262   0.5252   0.6704
   1.750   0.3601   0.00678   0.00155  -0.0257   0.5159   0.6776
   2.000   0.3852   0.00686   0.00159  -0.0252   0.5039   0.6838
   2.250   0.4099   0.00692   0.00163  -0.0245   0.4909   0.6901
   2.500   0.4349   0.00699   0.00168  -0.0239   0.4781   0.6966
   2.750   0.4598   0.00708   0.00174  -0.0233   0.4670   0.7022
   3.000   0.4837   0.00717   0.00181  -0.0225   0.4542   0.7089
   3.500   0.5313   0.00738   0.00197  -0.0209   0.4257   0.7227
   3.750   0.5547   0.00750   0.00206  -0.0200   0.4108   0.7305
   4.000   0.5760   0.00769   0.00218  -0.0188   0.3883   0.7385
   4.250   0.5966   0.00789   0.00231  -0.0174   0.3654   0.7474
   4.500   0.6158   0.00815   0.00248  -0.0158   0.3390   0.7563
   4.750   0.6352   0.00837   0.00264  -0.0141   0.3159   0.7666
   5.000   0.6545   0.00858   0.00281  -0.0125   0.2964   0.7770
   5.500   0.6920   0.00899   0.00316  -0.0090   0.2617   0.8019
   5.750   0.7089   0.00918   0.00333  -0.0069   0.2459   0.8161
   6.000   0.7237   0.00936   0.00351  -0.0044   0.2295   0.8338
   6.250   0.7388   0.00955   0.00371  -0.0019   0.2151   0.8556
   6.500   0.7555   0.00975   0.00396   0.0002   0.2000   0.8855
   6.750   0.7900   0.01006   0.00430  -0.0017   0.1842   0.9186
   7.000   0.8443   0.01053   0.00474  -0.0081   0.1675   0.9361
   7.250   0.8996   0.01105   0.00518  -0.0147   0.1505   0.9453
   7.500   0.9471   0.01153   0.00561  -0.0195   0.1387   0.9557
   7.750   0.9745   0.01191   0.00595  -0.0199   0.1299   0.9743
   8.000   0.9912   0.01221   0.00623  -0.0180   0.1236   0.9872
   8.250   1.0148   0.01258   0.00657  -0.0176   0.1165   0.9928
   8.500   1.0432   0.01293   0.00690  -0.0183   0.1103   0.9961
   8.750   1.0722   0.01335   0.00728  -0.0193   0.1029   0.9986
   9.000   1.0991   0.01372   0.00764  -0.0197   0.0969   1.0000
   9.250   1.1086   0.01407   0.00797  -0.0166   0.0922   1.0000
   9.500   1.1189   0.01443   0.00832  -0.0136   0.0881   1.0000
   9.750   1.1312   0.01477   0.00868  -0.0111   0.0855   1.0000
  10.000   1.1424   0.01518   0.00909  -0.0085   0.0820   1.0000
  10.250   1.1530   0.01566   0.00956  -0.0059   0.0784   1.0000
  10.500   1.1659   0.01610   0.01002  -0.0038   0.0764   1.0000
  10.750   1.1786   0.01657   0.01052  -0.0017   0.0743   1.0000
  11.000   1.1905   0.01712   0.01108   0.0003   0.0720   1.0000
  11.250   1.2018   0.01775   0.01171   0.0024   0.0697   1.0000
  11.500   1.2137   0.01839   0.01237   0.0042   0.0674   1.0000
  11.750   1.2265   0.01901   0.01303   0.0058   0.0656   1.0000
  12.000   1.2388   0.01971   0.01376   0.0074   0.0638   1.0000
  12.250   1.2499   0.02052   0.01458   0.0090   0.0617   1.0000
  12.500   1.2609   0.02137   0.01545   0.0105   0.0599   1.0000
  12.750   1.2723   0.02223   0.01634   0.0118   0.0583   1.0000
  13.000   1.2846   0.02308   0.01724   0.0130   0.0571   1.0000
  13.250   1.2956   0.02405   0.01823   0.0142   0.0547   1.0000
  13.500   1.3051   0.02513   0.01933   0.0154   0.0526   1.0000
  13.750   1.3145   0.02627   0.02049   0.0166   0.0509   1.0000
  14.000   1.3253   0.02733   0.02160   0.0176   0.0496   1.0000
  14.250   1.3355   0.02848   0.02279   0.0185   0.0485   1.0000
  14.500   1.3437   0.02978   0.02411   0.0195   0.0461   1.0000
  14.750   1.3507   0.03121   0.02556   0.0205   0.0442   1.0000
  15.000   1.3589   0.03257   0.02697   0.0213   0.0428   1.0000
  15.250   1.3671   0.03398   0.02842   0.0220   0.0414   1.0000
  15.500   1.3732   0.03557   0.03004   0.0228   0.0393   1.0000
  15.750   1.3776   0.03736   0.03185   0.0235   0.0374   1.0000
  16.000   1.3847   0.03897   0.03352   0.0240   0.0370   1.0000
  16.250   1.3905   0.04071   0.03530   0.0245   0.0352   1.0000
  16.500   1.3957   0.04255   0.03719   0.0250   0.0343   1.0000
  16.750   1.3984   0.04466   0.03934   0.0254   0.0328   1.0000
  17.000   1.4018   0.04677   0.04149   0.0257   0.0320   1.0000
  17.250   1.4063   0.04881   0.04359   0.0259   0.0310   1.0000
  17.500   1.4083   0.05114   0.04597   0.0260   0.0294   1.0000
  17.750   1.4109   0.05344   0.04834   0.0260   0.0290   1.0000
  18.000   1.4113   0.05602   0.05097   0.0260   0.0279   1.0000
  18.250   1.4111   0.05871   0.05371   0.0259   0.0268   1.0000
  18.500   1.4117   0.06139   0.05645   0.0256   0.0260   1.0000
  18.750   1.4120   0.06414   0.05928   0.0253   0.0256   1.0000
  19.000   1.4102   0.06715   0.06235   0.0249   0.0247   1.0000
  19.250   1.4063   0.07048   0.06575   0.0243   0.0239   1.0000
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