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St. CYR 24 (Bartel 35-IIIC) (stcyr24-il) Xfoil prediction polar at RE=100,000 Ncrit=9


Details Polar file
Airfoil: St. CYR 24 (Bartel 35-IIIC) (stcyr24-il)
Reynolds number: 100,000
Max Cl/Cd: 56.84 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-stcyr24-il-100000.txt
Download as CSV file: xf-stcyr24-il-100000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: St. CYR 24 (Bartel 35-IIIC)                     
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.100 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -8.750  -0.3038   0.11015   0.10563  -0.0298   0.9803   0.1026
  -8.500  -0.3221   0.10939   0.10491  -0.0318   0.9739   0.1047
  -8.250  -0.3468   0.10832   0.10381  -0.0440   0.9652   0.1058
  -8.000  -0.3200   0.10331   0.09887  -0.0359   0.9630   0.1073
  -7.750  -0.2986   0.10022   0.09579  -0.0355   0.9587   0.1098
  -7.500  -0.2847   0.09748   0.09304  -0.0381   0.9536   0.1130
  -7.250  -0.2864   0.09517   0.09074  -0.0400   0.9463   0.1161
  -7.000  -0.2698   0.09023   0.08570  -0.0533   0.9397   0.1204
  -6.750  -0.2695   0.08810   0.08363  -0.0488   0.9329   0.1216
  -6.500  -0.2513   0.08551   0.08105  -0.0489   0.9273   0.1243
  -6.250  -0.2283   0.08247   0.07794  -0.0537   0.9213   0.1301
  -6.000  -0.2184   0.07855   0.07389  -0.0604   0.9123   0.1355
  -5.750  -0.1927   0.07594   0.07132  -0.0602   0.9076   0.1388
  -5.500  -0.1741   0.07306   0.06820  -0.0674   0.8982   0.1503
  -5.250  -0.1553   0.07049   0.06573  -0.0656   0.8923   0.1532
  -5.000  -0.1176   0.06750   0.06250  -0.0730   0.8859   0.1669
  -4.750  -0.1099   0.06552   0.06061  -0.0702   0.8772   0.1693
  -4.500  -0.0671   0.06262   0.05750  -0.0766   0.8718   0.1843
  -4.250  -0.0578   0.06098   0.05593  -0.0742   0.8626   0.1881
  -4.000  -0.0232   0.05852   0.05331  -0.0780   0.8558   0.2032
  -3.750   0.0211   0.05600   0.05069  -0.0822   0.8519   0.2215
  -3.500   0.0296   0.05505   0.04964  -0.0809   0.8397   0.2373
  -3.250   0.0673   0.05264   0.04722  -0.0832   0.8350   0.2573
  -3.000   0.1591   0.04165   0.03380  -0.0961   0.8339   0.1183
  -2.750   0.1718   0.04089   0.03277  -0.0938   0.8221   0.1188
  -2.500   0.2152   0.03917   0.03067  -0.0959   0.8173   0.1189
  -2.250   0.2377   0.03833   0.02959  -0.0950   0.8077   0.1197
  -2.000   0.2723   0.03722   0.02848  -0.0960   0.8008   0.1245
  -1.750   0.3204   0.03609   0.02714  -0.0985   0.7972   0.1314
  -1.500   0.3332   0.03598   0.02689  -0.0960   0.7843   0.1347
  -1.250   0.3777   0.03500   0.02597  -0.0981   0.7801   0.1461
  -1.000   0.3940   0.03493   0.02593  -0.0962   0.7683   0.1532
  -0.750   0.4356   0.03414   0.02521  -0.0976   0.7632   0.1700
  -0.500   0.4584   0.03404   0.02519  -0.0966   0.7530   0.1868
  -0.250   0.4955   0.03332   0.02459  -0.0974   0.7466   0.2191
   0.000   0.5455   0.03153   0.02343  -0.1000   0.7438   0.3485
   0.250   0.6232   0.02878   0.02190  -0.1069   0.7426   1.0000
   0.500   0.6353   0.02908   0.02208  -0.1040   0.7281   1.0000
   0.750   0.7005   0.02709   0.01988  -0.1079   0.7259   1.0000
   1.000   0.7204   0.02678   0.01947  -0.1057   0.7124   1.0000
   1.250   0.7846   0.02481   0.01736  -0.1097   0.7092   1.0000
   1.500   0.8016   0.02472   0.01721  -0.1072   0.6963   1.0000
   1.750   0.8549   0.02344   0.01583  -0.1101   0.6921   1.0000
   2.000   0.8735   0.02337   0.01572  -0.1080   0.6793   1.0000
   2.250   0.9275   0.02206   0.01432  -0.1112   0.6740   1.0000
   2.500   0.9466   0.02197   0.01421  -0.1091   0.6602   1.0000
   2.750   0.9742   0.02164   0.01384  -0.1084   0.6478   1.0000
   3.000   1.0141   0.02095   0.01306  -0.1096   0.6366   1.0000
   3.250   1.0483   0.02048   0.01251  -0.1100   0.6228   1.0000
   3.500   1.0744   0.02031   0.01226  -0.1091   0.6063   1.0000
   3.750   1.1026   0.02015   0.01200  -0.1086   0.5886   1.0000
   4.000   1.1258   0.02019   0.01194  -0.1074   0.5688   1.0000
   4.250   1.1465   0.02037   0.01201  -0.1058   0.5476   1.0000
   4.500   1.1677   0.02062   0.01213  -0.1044   0.5254   1.0000
   4.750   1.1902   0.02094   0.01225  -0.1032   0.5026   1.0000
   5.000   1.2065   0.02144   0.01260  -0.1011   0.4787   1.0000
   5.250   1.2196   0.02202   0.01306  -0.0985   0.4545   1.0000
   5.500   1.2352   0.02264   0.01345  -0.0964   0.4310   1.0000
   5.750   1.2478   0.02335   0.01399  -0.0938   0.4090   1.0000
   6.000   1.2610   0.02411   0.01462  -0.0915   0.3893   1.0000
   6.250   1.2779   0.02491   0.01527  -0.0899   0.3724   1.0000
   6.500   1.2989   0.02571   0.01589  -0.0891   0.3581   1.0000
   6.750   1.3155   0.02650   0.01664  -0.0875   0.3458   1.0000
   7.000   1.3366   0.02735   0.01747  -0.0868   0.3356   1.0000
   7.250   1.3640   0.02817   0.01818  -0.0871   0.3270   1.0000
   7.500   1.3857   0.02911   0.01915  -0.0866   0.3197   1.0000
   7.750   1.4103   0.02998   0.02003  -0.0866   0.3131   1.0000
   8.000   1.4466   0.03102   0.02097  -0.0886   0.3073   1.0000
   8.250   1.4592   0.03196   0.02210  -0.0866   0.3022   1.0000
   8.500   1.4803   0.03285   0.02303  -0.0860   0.2966   1.0000
   8.750   1.5175   0.03391   0.02395  -0.0882   0.2908   1.0000
   9.000   1.5211   0.03486   0.02516  -0.0848   0.2863   1.0000
   9.250   1.5340   0.03576   0.02616  -0.0830   0.2810   1.0000
   9.500   1.5725   0.03673   0.02699  -0.0854   0.2751   1.0000
   9.750   1.5794   0.03792   0.02840  -0.0828   0.2717   1.0000
  10.000   1.5848   0.03909   0.02979  -0.0799   0.2679   1.0000
  10.250   1.5981   0.04020   0.03100  -0.0784   0.2638   1.0000
  10.500   1.6412   0.04128   0.03196  -0.0815   0.2585   1.0000
  10.750   1.6382   0.04268   0.03363  -0.0776   0.2554   1.0000
  11.000   1.6346   0.04412   0.03532  -0.0738   0.2519   1.0000
  11.250   1.6396   0.04546   0.03681  -0.0713   0.2480   1.0000
  11.500   1.6885   0.04634   0.03750  -0.0751   0.2414   1.0000
  11.750   1.6663   0.04805   0.03955  -0.0690   0.2387   1.0000
  12.000   1.6528   0.04982   0.04156  -0.0646   0.2347   1.0000
  12.250   1.6668   0.05049   0.04221  -0.0635   0.2286   1.0000
  12.500   1.6742   0.05185   0.04362  -0.0618   0.2229   1.0000
  12.750   1.6530   0.05417   0.04622  -0.0575   0.2191   1.0000
  13.000   1.6572   0.05526   0.04736  -0.0557   0.2134   1.0000
  13.250   1.6740   0.05634   0.04841  -0.0552   0.2075   1.0000
  13.500   1.6440   0.05969   0.05208  -0.0511   0.2044   1.0000
  13.750   1.6282   0.06249   0.05508  -0.0486   0.2003   1.0000
  14.000   1.6698   0.06181   0.05418  -0.0496   0.1926   1.0000
  14.250   1.6279   0.06658   0.05932  -0.0460   0.1904   1.0000
  14.500   1.5880   0.07198   0.06503  -0.0436   0.1877   1.0000
  14.750   1.5728   0.07548   0.06868  -0.0425   0.1834   1.0000
  15.000   1.4729   0.08951   0.08317  -0.0428   0.1841   1.0000
  15.250   1.4250   0.09901   0.09284  -0.0448   0.1812   1.0000
  15.500   1.3471   0.11530   0.10928  -0.0502   0.1785   1.0000
  15.750   1.5378   0.08864   0.08223  -0.0413   0.1651   1.0000
  16.000   1.4572   0.10253   0.09645  -0.0444   0.1645   1.0000
  16.250   1.0564   0.19701   0.19093  -0.0918   0.1650   1.0000
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