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SOMERS S102 AIRFOIL (BLUNT) (s102b-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: SOMERS S102 AIRFOIL (BLUNT) (s102b-il)
Reynolds number: 1,000,000
Max Cl/Cd: 96.43 at α=3°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s102b-il-1000000.txt
Download as CSV file: xf-s102b-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: SOMERS S102 AIRFOIL (BLUNT)                     
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.4932   0.08084   0.07923  -0.0539   1.0000   0.0091
 -10.750  -0.5276   0.06943   0.06770  -0.0619   1.0000   0.0090
 -10.500  -0.5535   0.06249   0.06064  -0.0658   1.0000   0.0089
 -10.250  -0.5750   0.05739   0.05544  -0.0676   1.0000   0.0089
 -10.000  -0.5827   0.05185   0.04972  -0.0726   0.9826   0.0090
  -9.000  -0.6229   0.02676   0.02241  -0.0704   0.8800   0.0082
  -8.750  -0.6061   0.02401   0.01948  -0.0698   0.8627   0.0078
  -8.500  -0.5870   0.02190   0.01706  -0.0692   0.8465   0.0077
  -8.250  -0.5657   0.02019   0.01510  -0.0687   0.8321   0.0076
  -8.000  -0.5430   0.01878   0.01349  -0.0682   0.8195   0.0075
  -7.750  -0.5196   0.01763   0.01216  -0.0679   0.8082   0.0075
  -7.500  -0.4957   0.01663   0.01101  -0.0675   0.7975   0.0075
  -7.250  -0.4712   0.01577   0.01004  -0.0673   0.7883   0.0075
  -7.000  -0.4461   0.01511   0.00928  -0.0672   0.7799   0.0076
  -6.750  -0.4203   0.01451   0.00860  -0.0672   0.7723   0.0078
  -6.500  -0.3945   0.01393   0.00793  -0.0673   0.7651   0.0079
  -6.250  -0.3683   0.01331   0.00726  -0.0674   0.7588   0.0080
  -6.000  -0.3419   0.01270   0.00658  -0.0677   0.7526   0.0080
  -5.750  -0.3149   0.01217   0.00598  -0.0680   0.7472   0.0081
  -5.500  -0.2871   0.01166   0.00542  -0.0684   0.7421   0.0081
  -5.250  -0.2594   0.01102   0.00471  -0.0690   0.7371   0.0085
  -5.000  -0.2311   0.01063   0.00426  -0.0694   0.7322   0.0090
  -4.750  -0.2020   0.01032   0.00393  -0.0700   0.7282   0.0098
  -4.500  -0.1728   0.00999   0.00356  -0.0705   0.7240   0.0116
  -4.250  -0.1435   0.00963   0.00322  -0.0711   0.7202   0.0202
  -4.000  -0.1143   0.00929   0.00296  -0.0718   0.7164   0.0441
  -3.750  -0.0846   0.00886   0.00271  -0.0727   0.7134   0.0905
  -3.500  -0.0544   0.00803   0.00233  -0.0741   0.7103   0.2160
  -3.250  -0.0226   0.00638   0.00183  -0.0768   0.7072   0.5493
  -3.000   0.0074   0.00651   0.00193  -0.0772   0.7043   0.5714
  -2.750   0.0372   0.00671   0.00208  -0.0775   0.7013   0.5840
  -2.500   0.0668   0.00681   0.00218  -0.0778   0.6985   0.5922
  -2.250   0.0967   0.00706   0.00239  -0.0781   0.6959   0.6020
  -2.000   0.1258   0.00721   0.00260  -0.0782   0.6934   0.6110
  -1.750   0.1557   0.00721   0.00256  -0.0787   0.6910   0.6123
  -1.500   0.1856   0.00720   0.00251  -0.0792   0.6884   0.6130
  -1.250   0.2152   0.00723   0.00246  -0.0796   0.6846   0.6137
  -1.000   0.2450   0.00720   0.00241  -0.0801   0.6805   0.6143
  -0.750   0.2748   0.00717   0.00236  -0.0805   0.6759   0.6149
  -0.500   0.3042   0.00718   0.00231  -0.0809   0.6703   0.6155
  -0.250   0.3338   0.00718   0.00228  -0.0813   0.6649   0.6161
   0.000   0.3636   0.00717   0.00225  -0.0818   0.6600   0.6168
   0.250   0.3930   0.00719   0.00223  -0.0821   0.6548   0.6173
   0.500   0.4225   0.00717   0.00219  -0.0826   0.6493   0.6180
   0.750   0.4519   0.00711   0.00213  -0.0830   0.6427   0.6189
   1.000   0.4810   0.00713   0.00210  -0.0833   0.6358   0.6198
   1.250   0.5106   0.00709   0.00209  -0.0837   0.6297   0.6206
   1.500   0.5398   0.00710   0.00209  -0.0841   0.6234   0.6214
   1.750   0.5691   0.00712   0.00211  -0.0844   0.6176   0.6221
   2.000   0.5984   0.00712   0.00212  -0.0848   0.6099   0.6229
   2.250   0.6274   0.00716   0.00214  -0.0851   0.6007   0.6237
   2.500   0.6561   0.00721   0.00216  -0.0854   0.5888   0.6246
   2.750   0.6848   0.00726   0.00220  -0.0856   0.5733   0.6255
   3.000   0.7126   0.00739   0.00225  -0.0858   0.5442   0.6264
   3.250   0.7342   0.00811   0.00251  -0.0849   0.4400   0.6275
   3.500   0.7543   0.00903   0.00296  -0.0839   0.3384   0.6285
   3.750   0.7769   0.00969   0.00329  -0.0834   0.2709   0.6295
   4.000   0.8008   0.01019   0.00357  -0.0830   0.2257   0.6304
   4.250   0.8259   0.01057   0.00382  -0.0827   0.1968   0.6313
   4.500   0.8516   0.01088   0.00403  -0.0826   0.1783   0.6321
   4.750   0.8777   0.01114   0.00424  -0.0825   0.1656   0.6328
   5.000   0.9036   0.01142   0.00447  -0.0824   0.1556   0.6335
   5.250   0.9300   0.01160   0.00465  -0.0823   0.1496   0.6349
   5.500   0.9555   0.01186   0.00489  -0.0821   0.1424   0.6362
   5.750   0.9820   0.01203   0.00509  -0.0821   0.1388   0.6375
   6.000   1.0080   0.01225   0.00531  -0.0820   0.1348   0.6388
   6.250   1.0332   0.01252   0.00557  -0.0817   0.1306   0.6400
   6.500   1.0580   0.01281   0.00588  -0.0814   0.1266   0.6413
   6.750   1.0841   0.01299   0.00610  -0.0813   0.1246   0.6426
   7.000   1.1095   0.01321   0.00635  -0.0811   0.1220   0.6440
   7.250   1.1342   0.01348   0.00662  -0.0808   0.1189   0.6454
   7.500   1.1576   0.01383   0.00697  -0.0802   0.1153   0.6468
   7.750   1.1809   0.01416   0.00733  -0.0797   0.1126   0.6482
   8.000   1.2059   0.01437   0.00759  -0.0794   0.1110   0.6495
   8.250   1.2303   0.01458   0.00785  -0.0791   0.1089   0.6516
   8.500   1.2539   0.01484   0.00814  -0.0786   0.1062   0.6536
   8.750   1.2761   0.01518   0.00850  -0.0779   0.1032   0.6555
   9.000   1.2955   0.01568   0.00902  -0.0768   0.0997   0.6574
   9.250   1.3195   0.01587   0.00928  -0.0764   0.0984   0.6594
   9.500   1.3423   0.01611   0.00957  -0.0758   0.0962   0.6615
   9.750   1.3617   0.01641   0.00989  -0.0745   0.0936   0.6635
  10.000   1.3791   0.01681   0.01029  -0.0730   0.0904   0.6654
  10.250   1.3971   0.01726   0.01079  -0.0718   0.0869   0.6681
  10.500   1.4185   0.01754   0.01114  -0.0711   0.0843   0.6709
  10.750   1.4377   0.01796   0.01158  -0.0701   0.0810   0.6738
  11.000   1.4543   0.01854   0.01216  -0.0687   0.0768   0.6769
  11.250   1.4730   0.01900   0.01268  -0.0677   0.0740   0.6800
  11.500   1.4903   0.01955   0.01326  -0.0666   0.0699   0.6833
  11.750   1.5055   0.02025   0.01397  -0.0653   0.0651   0.6873
  12.000   1.5213   0.02093   0.01469  -0.0641   0.0602   0.6917
  12.250   1.5345   0.02181   0.01555  -0.0627   0.0543   0.6964
  12.500   1.5461   0.02282   0.01656  -0.0612   0.0482   0.7016
  12.750   1.5583   0.02382   0.01759  -0.0599   0.0432   0.7079
  13.000   1.5690   0.02496   0.01875  -0.0584   0.0385   0.7144
  13.250   1.5792   0.02617   0.01999  -0.0571   0.0343   0.7223
  13.500   1.5900   0.02736   0.02123  -0.0558   0.0309   0.7314
  14.000   1.6082   0.03008   0.02408  -0.0534   0.0244   0.7568
  14.250   1.6160   0.03158   0.02567  -0.0521   0.0217   0.7752
  14.500   1.6244   0.03304   0.02725  -0.0511   0.0195   0.8025
  15.000   1.6334   0.03588   0.03052  -0.0477   0.0160   1.0000
  15.250   1.6378   0.03779   0.03247  -0.0466   0.0144   1.0000
  15.500   1.6440   0.03958   0.03432  -0.0457   0.0133   1.0000
  15.750   1.6476   0.04164   0.03644  -0.0448   0.0122   1.0000
  16.000   1.6505   0.04380   0.03866  -0.0439   0.0112   1.0000
  16.250   1.6542   0.04594   0.04088  -0.0432   0.0104   1.0000
  16.500   1.6555   0.04839   0.04340  -0.0426   0.0096   1.0000
  16.750   1.6545   0.05114   0.04623  -0.0420   0.0089   1.0000
  17.000   1.6562   0.05366   0.04884  -0.0417   0.0085   1.0000
  17.250   1.6557   0.05649   0.05176  -0.0414   0.0080   1.0000
  17.500   1.6530   0.05967   0.05502  -0.0413   0.0076   1.0000
  17.750   1.6479   0.06322   0.05867  -0.0413   0.0071   1.0000
  18.000   1.6416   0.06702   0.06256  -0.0415   0.0068   1.0000
  18.250   1.6369   0.07071   0.06637  -0.0419   0.0066   1.0000
  18.500   1.6299   0.07485   0.07062  -0.0426   0.0063   1.0000
  18.750   1.6203   0.07948   0.07537  -0.0436   0.0061   1.0000
  19.000   1.6077   0.08470   0.08071  -0.0449   0.0058   1.0000
  19.250   1.5915   0.09065   0.08679  -0.0468   0.0057   1.0000
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