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S8035 for RC aerobatic 14% thick (s8035-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S8035 for RC aerobatic 14% thick (s8035-il)
Reynolds number: 200,000
Max Cl/Cd: 51.23 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8035-il-200000-n5.txt
Download as CSV file: xf-s8035-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S8035 for RC aerobatic  14% thick               
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.8917   0.14540   0.14110   0.0012   1.0000   0.0254
 -18.750  -0.9229   0.13417   0.12968  -0.0051   1.0000   0.0257
 -18.500  -0.9423   0.12600   0.12137  -0.0097   1.0000   0.0259
 -18.250  -0.9591   0.11860   0.11383  -0.0137   1.0000   0.0263
 -18.000  -0.9737   0.11180   0.10689  -0.0174   1.0000   0.0267
 -17.750  -0.9865   0.10555   0.10051  -0.0207   1.0000   0.0271
 -17.500  -0.9989   0.09952   0.09433  -0.0238   1.0000   0.0275
 -17.250  -1.0102   0.09380   0.08846  -0.0267   1.0000   0.0280
 -17.000  -1.0196   0.08856   0.08307  -0.0293   1.0000   0.0283
 -16.750  -1.0283   0.08370   0.07817  -0.0316   1.0000   0.0289
 -16.500  -1.0369   0.07891   0.07330  -0.0338   1.0000   0.0293
 -16.250  -1.0450   0.07426   0.06856  -0.0359   1.0000   0.0298
 -16.000  -1.0532   0.06972   0.06392  -0.0380   1.0000   0.0304
 -15.750  -1.0597   0.06554   0.05963  -0.0398   1.0000   0.0310
 -15.500  -1.0655   0.06159   0.05557  -0.0414   1.0000   0.0318
 -15.250  -1.0702   0.05793   0.05179  -0.0426   1.0000   0.0325
 -15.000  -1.0739   0.05451   0.04824  -0.0437   1.0000   0.0333
 -14.750  -1.0767   0.05132   0.04491  -0.0445   1.0000   0.0340
 -14.500  -1.0805   0.04813   0.04163  -0.0451   1.0000   0.0348
 -14.250  -1.0845   0.04505   0.03850  -0.0457   1.0000   0.0358
 -14.000  -1.0859   0.04237   0.03573  -0.0459   1.0000   0.0366
 -13.750  -1.0851   0.04002   0.03327  -0.0458   1.0000   0.0379
 -13.500  -1.0838   0.03784   0.03099  -0.0455   1.0000   0.0392
 -13.250  -1.0798   0.03599   0.02900  -0.0449   1.0000   0.0410
 -13.000  -1.0782   0.03406   0.02700  -0.0441   1.0000   0.0423
 -12.750  -1.0770   0.03225   0.02514  -0.0429   1.0000   0.0438
 -12.500  -1.0727   0.03076   0.02358  -0.0416   1.0000   0.0457
 -12.250  -1.0670   0.02945   0.02218  -0.0401   1.0000   0.0477
 -12.000  -1.0592   0.02835   0.02095  -0.0385   1.0000   0.0498
 -11.750  -1.0562   0.02707   0.01966  -0.0363   1.0000   0.0521
 -11.500  -1.0498   0.02607   0.01861  -0.0341   1.0000   0.0547
 -11.250  -1.0415   0.02523   0.01769  -0.0318   1.0000   0.0576
 -11.000  -1.0338   0.02442   0.01682  -0.0292   1.0000   0.0605
 -10.750  -1.0279   0.02364   0.01603  -0.0263   1.0000   0.0635
 -10.500  -1.0198   0.02300   0.01535  -0.0233   1.0000   0.0671
 -10.250  -1.0101   0.02242   0.01469  -0.0205   1.0000   0.0706
 -10.000  -1.0005   0.02173   0.01400  -0.0178   1.0000   0.0747
  -9.750  -0.9876   0.02117   0.01340  -0.0155   1.0000   0.0796
  -9.500  -0.9747   0.02059   0.01281  -0.0132   1.0000   0.0843
  -9.250  -0.9612   0.02004   0.01225  -0.0109   1.0000   0.0902
  -9.000  -0.9463   0.01954   0.01172  -0.0088   1.0000   0.0961
  -8.750  -0.9320   0.01901   0.01119  -0.0066   1.0000   0.1028
  -8.500  -0.9165   0.01855   0.01071  -0.0046   1.0000   0.1098
  -8.250  -0.9014   0.01807   0.01024  -0.0025   1.0000   0.1176
  -8.000  -0.8858   0.01762   0.00980  -0.0004   1.0000   0.1255
  -7.750  -0.8696   0.01722   0.00940   0.0016   1.0000   0.1342
  -7.500  -0.8543   0.01679   0.00900   0.0037   1.0000   0.1425
  -7.250  -0.8381   0.01644   0.00864   0.0057   1.0000   0.1517
  -7.000  -0.8228   0.01608   0.00830   0.0079   1.0000   0.1614
  -6.750  -0.8052   0.01572   0.00798   0.0095   0.9994   0.1716
  -6.500  -0.7696   0.01533   0.00760   0.0075   0.9943   0.1857
  -6.250  -0.7359   0.01494   0.00725   0.0060   0.9883   0.2010
  -6.000  -0.7010   0.01458   0.00693   0.0042   0.9824   0.2175
  -5.750  -0.6700   0.01422   0.00660   0.0033   0.9738   0.2343
  -5.500  -0.6379   0.01387   0.00630   0.0022   0.9655   0.2524
  -5.250  -0.6049   0.01353   0.00601   0.0010   0.9574   0.2716
  -5.000  -0.5737   0.01318   0.00573   0.0001   0.9481   0.2903
  -4.750  -0.5371   0.01286   0.00546  -0.0018   0.9413   0.3098
  -4.500  -0.5049   0.01258   0.00522  -0.0027   0.9308   0.3286
  -4.250  -0.4702   0.01230   0.00497  -0.0041   0.9219   0.3484
  -4.000  -0.4356   0.01203   0.00475  -0.0055   0.9120   0.3676
  -3.750  -0.4029   0.01178   0.00454  -0.0065   0.9005   0.3873
  -3.500  -0.3700   0.01155   0.00436  -0.0074   0.8887   0.4077
  -3.250  -0.3380   0.01135   0.00418  -0.0082   0.8759   0.4288
  -3.000  -0.3082   0.01116   0.00403  -0.0084   0.8618   0.4495
  -2.750  -0.2806   0.01101   0.00391  -0.0081   0.8463   0.4689
  -2.500  -0.2538   0.01089   0.00379  -0.0077   0.8305   0.4872
  -2.250  -0.2276   0.01079   0.00369  -0.0071   0.8150   0.5051
  -2.000  -0.2018   0.01070   0.00361  -0.0065   0.7997   0.5238
  -1.750  -0.1764   0.01061   0.00354  -0.0057   0.7843   0.5423
  -1.500  -0.1511   0.01053   0.00348  -0.0049   0.7689   0.5611
  -1.250  -0.1260   0.01046   0.00344  -0.0041   0.7528   0.5802
  -1.000  -0.1008   0.01042   0.00339  -0.0033   0.7361   0.5989
  -0.750  -0.0757   0.01038   0.00335  -0.0024   0.7189   0.6174
  -0.500  -0.0505   0.01036   0.00332  -0.0016   0.7019   0.6348
  -0.250  -0.0252   0.01035   0.00330  -0.0008   0.6852   0.6518
   0.000   0.0000   0.01034   0.00330   0.0000   0.6685   0.6684
   0.250   0.0253   0.01035   0.00330   0.0008   0.6519   0.6852
   0.500   0.0505   0.01036   0.00332   0.0016   0.6348   0.7019
   0.750   0.0757   0.01038   0.00335   0.0024   0.6173   0.7190
   1.000   0.1008   0.01042   0.00339   0.0033   0.5990   0.7361
   1.250   0.1259   0.01046   0.00344   0.0041   0.5800   0.7529
   1.500   0.1511   0.01053   0.00348   0.0049   0.5611   0.7689
   1.750   0.1764   0.01061   0.00354   0.0057   0.5424   0.7843
   2.000   0.2018   0.01070   0.00361   0.0065   0.5237   0.7998
   2.250   0.2276   0.01079   0.00369   0.0071   0.5053   0.8149
   2.500   0.2538   0.01089   0.00379   0.0077   0.4872   0.8305
   2.750   0.2806   0.01101   0.00391   0.0081   0.4690   0.8463
   3.000   0.3082   0.01116   0.00403   0.0084   0.4494   0.8618
   3.250   0.3379   0.01135   0.00418   0.0082   0.4288   0.8759
   3.500   0.3700   0.01155   0.00436   0.0074   0.4080   0.8886
   3.750   0.4029   0.01178   0.00454   0.0065   0.3872   0.9005
   4.000   0.4356   0.01203   0.00475   0.0055   0.3675   0.9120
   4.250   0.4701   0.01230   0.00497   0.0041   0.3484   0.9218
   4.500   0.5049   0.01258   0.00522   0.0027   0.3287   0.9308
   4.750   0.5372   0.01286   0.00546   0.0018   0.3100   0.9413
   5.000   0.5738   0.01318   0.00573  -0.0001   0.2904   0.9481
   5.250   0.6049   0.01353   0.00601  -0.0010   0.2716   0.9574
   5.500   0.6379   0.01387   0.00630  -0.0022   0.2525   0.9655
   5.750   0.6700   0.01422   0.00660  -0.0033   0.2343   0.9738
   6.000   0.7011   0.01458   0.00693  -0.0042   0.2174   0.9824
   6.250   0.7360   0.01494   0.00725  -0.0060   0.2009   0.9883
   6.500   0.7697   0.01533   0.00760  -0.0076   0.1857   0.9943
   6.750   0.8053   0.01572   0.00797  -0.0096   0.1718   0.9994
   7.000   0.8228   0.01608   0.00830  -0.0079   0.1614   1.0000
   7.250   0.8381   0.01644   0.00863  -0.0057   0.1517   1.0000
   7.500   0.8543   0.01679   0.00899  -0.0037   0.1426   1.0000
   7.750   0.8696   0.01722   0.00940  -0.0016   0.1342   1.0000
   8.000   0.8858   0.01762   0.00980   0.0004   0.1255   1.0000
   8.250   0.9014   0.01807   0.01024   0.0025   0.1176   1.0000
   8.500   0.9165   0.01855   0.01070   0.0046   0.1098   1.0000
   8.750   0.9321   0.01901   0.01119   0.0066   0.1028   1.0000
   9.000   0.9463   0.01955   0.01171   0.0088   0.0960   1.0000
   9.250   0.9612   0.02004   0.01225   0.0109   0.0901   1.0000
   9.500   0.9748   0.02059   0.01281   0.0132   0.0844   1.0000
   9.750   0.9877   0.02117   0.01340   0.0155   0.0795   1.0000
  10.000   1.0006   0.02172   0.01400   0.0178   0.0747   1.0000
  10.250   1.0102   0.02242   0.01469   0.0205   0.0707   1.0000
  10.500   1.0199   0.02300   0.01535   0.0233   0.0671   1.0000
  10.750   1.0281   0.02364   0.01603   0.0262   0.0636   1.0000
  11.000   1.0341   0.02442   0.01682   0.0292   0.0605   1.0000
  11.250   1.0418   0.02523   0.01768   0.0318   0.0577   1.0000
  11.500   1.0502   0.02606   0.01861   0.0340   0.0547   1.0000
  11.750   1.0566   0.02706   0.01966   0.0362   0.0520   1.0000
  12.000   1.0598   0.02833   0.02093   0.0384   0.0498   1.0000
  12.250   1.0675   0.02944   0.02217   0.0400   0.0477   1.0000
  12.500   1.0733   0.03074   0.02357   0.0416   0.0457   1.0000
  12.750   1.0776   0.03222   0.02512   0.0429   0.0439   1.0000
  13.000   1.0791   0.03402   0.02696   0.0440   0.0423   1.0000
  13.250   1.0812   0.03591   0.02893   0.0448   0.0407   1.0000
  13.500   1.0843   0.03783   0.03097   0.0454   0.0394   1.0000
  13.750   1.0863   0.03995   0.03321   0.0458   0.0379   1.0000
  14.000   1.0868   0.04234   0.03569   0.0458   0.0366   1.0000
  14.250   1.0854   0.04503   0.03846   0.0456   0.0356   1.0000
  14.500   1.0818   0.04807   0.04157   0.0450   0.0348   1.0000
  14.750   1.0782   0.05123   0.04482   0.0443   0.0340   1.0000
  15.000   1.0756   0.05442   0.04815   0.0435   0.0332   1.0000
  15.250   1.0719   0.05784   0.05170   0.0425   0.0324   1.0000
  15.500   1.0671   0.06152   0.05550   0.0412   0.0316   1.0000
  15.750   1.0614   0.06542   0.05952   0.0397   0.0310   1.0000
  16.000   1.0544   0.06969   0.06389   0.0378   0.0303   1.0000
  16.250   1.0470   0.07414   0.06843   0.0358   0.0298   1.0000
  16.500   1.0385   0.07881   0.07319   0.0337   0.0293   1.0000
  16.750   1.0303   0.08358   0.07804   0.0314   0.0288   1.0000
  17.000   1.0216   0.08844   0.08295   0.0291   0.0283   1.0000
  17.250   1.0111   0.09390   0.08856   0.0264   0.0278   1.0000
  17.500   1.0007   0.09944   0.09425   0.0237   0.0275   1.0000
  17.750   0.9883   0.10549   0.10045   0.0205   0.0270   1.0000
  18.000   0.9753   0.11180   0.10690   0.0172   0.0266   1.0000
  18.250   0.9606   0.11860   0.11383   0.0135   0.0262   1.0000
  18.500   0.9439   0.12602   0.12138   0.0094   0.0258   1.0000
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