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S8036 (16%) (s8036-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: S8036 (16%) (s8036-il)
Reynolds number: 500,000
Max Cl/Cd: 73.25 at α=6.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s8036-il-500000-n5.txt
Download as CSV file: xf-s8036-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.7210   0.13252   0.12938  -0.0316   1.0000   0.0083
 -18.000  -0.7538   0.12114   0.11783  -0.0373   1.0000   0.0082
 -17.750  -0.7901   0.10972   0.10624  -0.0433   1.0000   0.0083
 -17.500  -0.8132   0.10109   0.09745  -0.0478   1.0000   0.0082
 -17.250  -0.8276   0.09472   0.09100  -0.0510   1.0000   0.0081
 -17.000  -0.8511   0.08647   0.08257  -0.0554   1.0000   0.0081
 -16.750  -0.8697   0.07956   0.07552  -0.0590   1.0000   0.0081
 -16.500  -0.8830   0.07376   0.06960  -0.0620   1.0000   0.0081
 -16.250  -0.8966   0.06813   0.06382  -0.0648   1.0000   0.0081
 -16.000  -0.9078   0.06320   0.05877  -0.0670   1.0000   0.0081
 -15.750  -0.9172   0.05874   0.05415  -0.0689   1.0000   0.0082
 -15.500  -0.9255   0.05473   0.05002  -0.0702   1.0000   0.0082
 -15.250  -0.9332   0.05106   0.04623  -0.0711   1.0000   0.0083
 -15.000  -0.9410   0.04760   0.04266  -0.0716   1.0000   0.0083
 -14.750  -0.9451   0.04468   0.03964  -0.0718   1.0000   0.0083
 -14.500  -0.9471   0.04213   0.03700  -0.0716   1.0000   0.0083
 -14.250  -0.9498   0.03964   0.03441  -0.0712   1.0000   0.0084
 -14.000  -0.9509   0.03741   0.03208  -0.0705   1.0000   0.0084
 -13.750  -0.9508   0.03542   0.03002  -0.0697   1.0000   0.0086
 -13.500  -0.9487   0.03369   0.02821  -0.0685   1.0000   0.0086
 -13.250  -0.9471   0.03203   0.02648  -0.0671   1.0000   0.0088
 -13.000  -0.9439   0.03058   0.02496  -0.0656   1.0000   0.0089
 -12.750  -0.9418   0.02917   0.02347  -0.0636   1.0000   0.0089
 -12.500  -0.9363   0.02809   0.02233  -0.0617   1.0000   0.0091
 -12.250  -0.9335   0.02692   0.02109  -0.0593   1.0000   0.0091
 -12.000  -0.9299   0.02591   0.02002  -0.0567   1.0000   0.0093
 -11.750  -0.9263   0.02504   0.01908  -0.0539   1.0000   0.0094
 -11.500  -0.9126   0.02399   0.01797  -0.0530   0.9987   0.0095
 -11.250  -0.8867   0.02298   0.01687  -0.0542   0.9950   0.0098
 -11.000  -0.8635   0.02205   0.01586  -0.0547   0.9899   0.0100
 -10.750  -0.8436   0.02120   0.01494  -0.0544   0.9808   0.0102
 -10.250  -0.8026   0.01958   0.01319  -0.0534   0.9472   0.0107
 -10.000  -0.7648   0.01867   0.01224  -0.0565   0.9359   0.0112
  -9.750  -0.7168   0.01779   0.01128  -0.0617   0.9264   0.0116
  -9.500  -0.6641   0.01692   0.01033  -0.0678   0.9135   0.0125
  -9.250  -0.6182   0.01617   0.00946  -0.0724   0.8922   0.0135
  -9.000  -0.5888   0.01568   0.00886  -0.0733   0.8677   0.0142
  -8.750  -0.5694   0.01532   0.00837  -0.0720   0.8463   0.0151
  -8.500  -0.5536   0.01501   0.00793  -0.0699   0.8283   0.0161
  -8.250  -0.5387   0.01472   0.00756  -0.0675   0.8129   0.0168
  -8.000  -0.5226   0.01444   0.00721  -0.0654   0.7995   0.0183
  -7.750  -0.5049   0.01415   0.00686  -0.0636   0.7888   0.0197
  -7.500  -0.4865   0.01388   0.00652  -0.0618   0.7786   0.0217
  -7.250  -0.4676   0.01360   0.00620  -0.0602   0.7695   0.0239
  -7.000  -0.4482   0.01336   0.00590  -0.0587   0.7605   0.0272
  -6.750  -0.4283   0.01309   0.00561  -0.0572   0.7528   0.0310
  -6.500  -0.4082   0.01283   0.00533  -0.0558   0.7451   0.0356
  -6.250  -0.3877   0.01258   0.00507  -0.0545   0.7383   0.0416
  -6.000  -0.3668   0.01234   0.00482  -0.0532   0.7310   0.0487
  -5.500  -0.3251   0.01183   0.00435  -0.0506   0.7182   0.0700
  -5.250  -0.3042   0.01156   0.00413  -0.0493   0.7119   0.0852
  -5.000  -0.2834   0.01130   0.00391  -0.0480   0.7063   0.1049
  -4.750  -0.2621   0.01102   0.00371  -0.0468   0.7004   0.1269
  -4.500  -0.2415   0.01072   0.00350  -0.0455   0.6947   0.1551
  -4.000  -0.2015   0.01003   0.00309  -0.0426   0.6847   0.2373
  -3.750  -0.1824   0.00964   0.00289  -0.0410   0.6793   0.2923
  -3.500  -0.1645   0.00922   0.00270  -0.0392   0.6741   0.3592
  -3.250  -0.1454   0.00886   0.00255  -0.0375   0.6695   0.4175
  -3.000  -0.1248   0.00859   0.00245  -0.0360   0.6647   0.4665
  -2.750  -0.1029   0.00842   0.00238  -0.0348   0.6597   0.5043
  -2.500  -0.0800   0.00832   0.00233  -0.0337   0.6551   0.5358
  -2.250  -0.0559   0.00823   0.00231  -0.0329   0.6502   0.5637
  -2.000  -0.0315   0.00817   0.00228  -0.0320   0.6451   0.5852
  -1.750  -0.0064   0.00816   0.00225  -0.0314   0.6402   0.6007
  -1.500   0.0190   0.00814   0.00223  -0.0308   0.6353   0.6157
  -1.250   0.0443   0.00812   0.00223  -0.0302   0.6299   0.6312
  -1.000   0.0695   0.00810   0.00221  -0.0295   0.6246   0.6437
  -0.750   0.0954   0.00811   0.00220  -0.0290   0.6198   0.6527
  -0.500   0.1216   0.00810   0.00219  -0.0286   0.6144   0.6616
  -0.250   0.1477   0.00810   0.00218  -0.0282   0.6090   0.6687
   0.000   0.1737   0.00812   0.00218  -0.0278   0.6040   0.6755
   0.250   0.2003   0.00813   0.00218  -0.0275   0.5985   0.6823
   0.500   0.2263   0.00813   0.00219  -0.0270   0.5928   0.6885
   0.750   0.2520   0.00816   0.00219  -0.0265   0.5872   0.6955
   1.000   0.2783   0.00817   0.00221  -0.0262   0.5809   0.7024
   1.250   0.3037   0.00819   0.00223  -0.0256   0.5742   0.7093
   1.500   0.3294   0.00822   0.00225  -0.0251   0.5678   0.7164
   1.750   0.3551   0.00824   0.00228  -0.0246   0.5606   0.7226
   2.000   0.3801   0.00829   0.00232  -0.0240   0.5536   0.7296
   2.250   0.4056   0.00831   0.00236  -0.0235   0.5452   0.7367
   2.500   0.4299   0.00836   0.00240  -0.0228   0.5365   0.7440
   2.750   0.4545   0.00840   0.00245  -0.0221   0.5259   0.7520
   3.000   0.4784   0.00845   0.00250  -0.0212   0.5147   0.7599
   3.250   0.5017   0.00852   0.00256  -0.0203   0.5035   0.7690
   3.500   0.5254   0.00858   0.00264  -0.0194   0.4921   0.7779
   3.750   0.5486   0.00866   0.00272  -0.0185   0.4800   0.7882
   4.000   0.5713   0.00874   0.00281  -0.0174   0.4686   0.7985
   4.250   0.5930   0.00885   0.00291  -0.0162   0.4545   0.8100
   4.500   0.6144   0.00897   0.00303  -0.0149   0.4398   0.8233
   4.750   0.6352   0.00910   0.00317  -0.0135   0.4212   0.8372
   5.000   0.6554   0.00928   0.00333  -0.0121   0.3991   0.8531
   5.250   0.6761   0.00951   0.00353  -0.0108   0.3763   0.8725
   5.500   0.7020   0.00981   0.00380  -0.0107   0.3504   0.8943
   5.750   0.7383   0.01024   0.00415  -0.0130   0.3225   0.9134
   6.000   0.7805   0.01074   0.00456  -0.0166   0.2954   0.9274
   6.250   0.8248   0.01126   0.00498  -0.0208   0.2689   0.9368
   6.500   0.8632   0.01181   0.00543  -0.0237   0.2436   0.9471
   6.750   0.8948   0.01233   0.00585  -0.0251   0.2214   0.9595
   7.250   0.9390   0.01322   0.00662  -0.0237   0.1906   0.9876
   7.500   0.9649   0.01371   0.00703  -0.0239   0.1753   0.9944
   7.750   0.9957   0.01416   0.00743  -0.0252   0.1624   0.9987
   8.000   1.0115   0.01454   0.00777  -0.0234   0.1534   1.0000
   8.250   1.0188   0.01485   0.00807  -0.0197   0.1464   1.0000
   8.500   1.0259   0.01523   0.00842  -0.0161   0.1399   1.0000
   8.750   1.0354   0.01560   0.00878  -0.0130   0.1331   1.0000
   9.000   1.0436   0.01607   0.00923  -0.0098   0.1267   1.0000
   9.250   1.0550   0.01647   0.00965  -0.0072   0.1217   1.0000
   9.500   1.0643   0.01700   0.01016  -0.0045   0.1159   1.0000
   9.750   1.0750   0.01752   0.01069  -0.0020   0.1112   1.0000
  10.000   1.0859   0.01808   0.01126   0.0002   0.1063   1.0000
  10.250   1.0953   0.01876   0.01193   0.0026   0.1016   1.0000
  10.500   1.1068   0.01940   0.01259   0.0045   0.0974   1.0000
  10.750   1.1176   0.02011   0.01331   0.0064   0.0935   1.0000
  11.000   1.1275   0.02092   0.01413   0.0083   0.0901   1.0000
  11.250   1.1388   0.02171   0.01495   0.0100   0.0871   1.0000
  11.500   1.1500   0.02253   0.01581   0.0115   0.0840   1.0000
  11.750   1.1603   0.02346   0.01676   0.0129   0.0813   1.0000
  12.000   1.1693   0.02452   0.01783   0.0144   0.0784   1.0000
  12.250   1.1806   0.02547   0.01884   0.0157   0.0763   1.0000
  12.500   1.1914   0.02648   0.01989   0.0168   0.0743   1.0000
  12.750   1.2012   0.02759   0.02104   0.0180   0.0720   1.0000
  13.000   1.2098   0.02882   0.02230   0.0191   0.0698   1.0000
  13.250   1.2172   0.03018   0.02368   0.0202   0.0676   1.0000
  13.500   1.2275   0.03134   0.02491   0.0211   0.0660   1.0000
  13.750   1.2368   0.03261   0.02624   0.0219   0.0643   1.0000
  14.000   1.2448   0.03400   0.02769   0.0228   0.0625   1.0000
  14.250   1.2515   0.03554   0.02926   0.0236   0.0607   1.0000
  14.500   1.2566   0.03724   0.03099   0.0244   0.0590   1.0000
  14.750   1.2650   0.03870   0.03253   0.0250   0.0577   1.0000
  15.000   1.2724   0.04029   0.03418   0.0255   0.0559   1.0000
  15.250   1.2786   0.04202   0.03597   0.0260   0.0543   1.0000
  15.500   1.2838   0.04387   0.03788   0.0265   0.0528   1.0000
  15.750   1.2871   0.04596   0.04000   0.0269   0.0513   1.0000
  16.000   1.2915   0.04799   0.04210   0.0271   0.0500   1.0000
  16.250   1.2975   0.04990   0.04409   0.0273   0.0485   1.0000
  16.500   1.3016   0.05204   0.04629   0.0275   0.0469   1.0000
  16.750   1.3039   0.05440   0.04871   0.0275   0.0457   1.0000
  17.000   1.3049   0.05697   0.05132   0.0274   0.0444   1.0000
  17.250   1.3069   0.05946   0.05388   0.0273   0.0428   1.0000
  17.500   1.3092   0.06197   0.05648   0.0271   0.0415   1.0000
  17.750   1.3102   0.06467   0.05925   0.0268   0.0405   1.0000
  18.000   1.3096   0.06760   0.06224   0.0263   0.0390   1.0000
  18.250   1.3071   0.07082   0.06553   0.0257   0.0381   1.0000
  18.500   1.3035   0.07426   0.06904   0.0250   0.0374   1.0000
  18.750   1.3029   0.07734   0.07222   0.0243   0.0365   1.0000
  19.000   1.3013   0.08059   0.07556   0.0235   0.0353   1.0000
  19.250   1.2975   0.08418   0.07923   0.0226   0.0343   1.0000
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