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S1223 RTL (s1223rtl-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: S1223 RTL (s1223rtl-il)
Reynolds number: 1,000,000
Max Cl/Cd: 106.75 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1223rtl-il-1000000-n5.txt
Download as CSV file: xf-s1223rtl-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: S1223 RTL                                       
  
 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
  ------ -------- --------- --------- -------- -------- --------
  -9.500   0.2120   0.09464   0.08989  -0.1343   0.3797   0.0086
  -7.500   0.1359   0.01960   0.01432  -0.2124   0.3856   0.0096
  -7.250   0.1911   0.01776   0.01219  -0.2212   0.3755   0.0098
  -7.000   0.2348   0.01677   0.01099  -0.2260   0.3673   0.0100
  -6.750   0.2750   0.01604   0.01007  -0.2295   0.3598   0.0101
  -6.500   0.3132   0.01545   0.00934  -0.2323   0.3547   0.0103
  -6.250   0.3506   0.01493   0.00867  -0.2348   0.3487   0.0105
  -6.000   0.3872   0.01449   0.00808  -0.2370   0.3425   0.0108
  -5.750   0.4230   0.01411   0.00756  -0.2389   0.3386   0.0111
  -5.500   0.4579   0.01378   0.00713  -0.2405   0.3353   0.0114
  -5.250   0.4913   0.01355   0.00679  -0.2417   0.3317   0.0117
  -5.000   0.5243   0.01336   0.00648  -0.2428   0.3281   0.0119
  -4.750   0.5607   0.01303   0.00605  -0.2448   0.3241   0.0124
  -4.500   0.5933   0.01288   0.00583  -0.2457   0.3212   0.0128
  -4.250   0.6255   0.01275   0.00565  -0.2466   0.3189   0.0132
  -4.000   0.6576   0.01263   0.00547  -0.2473   0.3161   0.0136
  -3.750   0.6895   0.01254   0.00530  -0.2481   0.3133   0.0141
  -3.500   0.7210   0.01247   0.00516  -0.2487   0.3106   0.0145
  -3.250   0.7528   0.01240   0.00501  -0.2494   0.3078   0.0150
  -3.000   0.7841   0.01235   0.00492  -0.2500   0.3048   0.0157
  -2.750   0.8145   0.01233   0.00486  -0.2504   0.3033   0.0165
  -2.500   0.8446   0.01231   0.00480  -0.2507   0.3019   0.0174
  -2.250   0.8751   0.01229   0.00475  -0.2511   0.3002   0.0186
  -2.000   0.9049   0.01229   0.00473  -0.2513   0.2982   0.0198
  -1.750   0.9342   0.01232   0.00471  -0.2514   0.2959   0.0211
  -1.500   0.9639   0.01234   0.00470  -0.2517   0.2935   0.0229
  -1.250   0.9928   0.01240   0.00471  -0.2517   0.2912   0.0250
  -1.000   1.0216   0.01246   0.00474  -0.2517   0.2889   0.0284
  -0.750   1.0503   0.01252   0.00479  -0.2517   0.2867   0.0334
  -0.500   1.0794   0.01255   0.00484  -0.2518   0.2859   0.0421
  -0.250   1.1090   0.01257   0.00490  -0.2521   0.2847   0.0620
   0.000   1.1401   0.01256   0.00497  -0.2527   0.2833   0.1073
   0.250   1.1715   0.01253   0.00508  -0.2535   0.2817   0.1788
   0.500   1.2000   0.01260   0.00520  -0.2535   0.2797   0.2135
   0.750   1.2275   0.01271   0.00532  -0.2533   0.2778   0.2352
   1.000   1.2552   0.01282   0.00546  -0.2531   0.2759   0.2644
   1.250   1.2824   0.01295   0.00562  -0.2529   0.2740   0.2940
   1.500   1.3087   0.01310   0.00577  -0.2524   0.2721   0.3062
   1.750   1.3345   0.01327   0.00593  -0.2519   0.2703   0.3170
   2.000   1.3608   0.01340   0.00608  -0.2514   0.2696   0.3279
   2.250   1.3867   0.01354   0.00622  -0.2509   0.2686   0.3377
   2.500   1.4128   0.01369   0.00639  -0.2504   0.2675   0.3501
   2.750   1.4386   0.01384   0.00655  -0.2499   0.2662   0.3619
   3.000   1.4642   0.01401   0.00673  -0.2493   0.2645   0.3735
   3.250   1.4896   0.01418   0.00691  -0.2487   0.2628   0.3839
   3.500   1.5148   0.01437   0.00710  -0.2481   0.2612   0.3951
   3.750   1.5400   0.01456   0.00731  -0.2475   0.2596   0.4072
   4.000   1.5649   0.01477   0.00752  -0.2468   0.2580   0.4194
   4.250   1.5896   0.01500   0.00775  -0.2461   0.2562   0.4310
   4.500   1.6141   0.01523   0.00799  -0.2454   0.2547   0.4412
   4.750   1.6389   0.01542   0.00822  -0.2448   0.2540   0.4529
   5.000   1.6638   0.01561   0.00845  -0.2441   0.2531   0.4658
   5.250   1.6882   0.01582   0.00869  -0.2434   0.2519   0.4781
   5.500   1.7123   0.01604   0.00894  -0.2426   0.2506   0.4900
   5.750   1.7362   0.01627   0.00921  -0.2419   0.2490   0.5032
   6.000   1.7599   0.01651   0.00948  -0.2411   0.2476   0.5172
   6.500   1.8069   0.01704   0.01007  -0.2394   0.2448   0.5483
   6.750   1.8303   0.01732   0.01039  -0.2386   0.2433   0.5664
   7.000   1.8535   0.01763   0.01073  -0.2378   0.2417   0.5872
   7.250   1.8765   0.01796   0.01111  -0.2369   0.2399   0.6121
   7.500   1.9004   0.01821   0.01145  -0.2363   0.2392   0.6436
   7.750   1.9251   0.01847   0.01183  -0.2358   0.2382   0.7006
   8.250   1.9672   0.01882   0.01255  -0.2334   0.2359   1.0000
   8.500   1.9889   0.01916   0.01291  -0.2323   0.2347   1.0000
   8.750   2.0103   0.01951   0.01329  -0.2312   0.2335   1.0000
   9.000   2.0315   0.01988   0.01368  -0.2301   0.2321   1.0000
   9.250   2.0522   0.02028   0.01410  -0.2289   0.2308   1.0000
   9.500   2.0722   0.02071   0.01454  -0.2276   0.2294   1.0000
   9.750   2.0919   0.02116   0.01502  -0.2263   0.2278   1.0000
  10.000   2.1112   0.02166   0.01553  -0.2250   0.2261   1.0000
  10.250   2.1313   0.02208   0.01600  -0.2238   0.2250   1.0000
  10.500   2.1511   0.02251   0.01648  -0.2225   0.2241   1.0000
  10.750   2.1706   0.02295   0.01698  -0.2212   0.2232   1.0000
  11.000   2.1898   0.02342   0.01749  -0.2200   0.2222   1.0000
  11.250   2.2089   0.02390   0.01803  -0.2187   0.2210   1.0000
  11.500   2.2272   0.02443   0.01860  -0.2173   0.2198   1.0000
  11.750   2.2450   0.02498   0.01920  -0.2158   0.2184   1.0000
  12.000   2.2626   0.02556   0.01983  -0.2144   0.2170   1.0000
  12.250   2.2795   0.02620   0.02050  -0.2129   0.2154   1.0000
  12.500   2.2954   0.02690   0.02124  -0.2112   0.2138   1.0000
  12.750   2.3104   0.02767   0.02205  -0.2095   0.2117   1.0000
  13.000   2.3280   0.02824   0.02269  -0.2082   0.2105   1.0000
  13.250   2.3447   0.02887   0.02339  -0.2068   0.2085   1.0000
  13.500   2.3605   0.02958   0.02416  -0.2053   0.2065   1.0000
  13.750   2.3756   0.03035   0.02498  -0.2037   0.2043   1.0000
  14.000   2.3888   0.03127   0.02594  -0.2020   0.2015   1.0000
  14.250   2.4009   0.03231   0.02700  -0.2001   0.1981   1.0000
  14.500   2.4157   0.03311   0.02789  -0.1987   0.1963   1.0000
  14.750   2.4270   0.03423   0.02901  -0.1969   0.1894   1.0000
  15.000   2.4351   0.03566   0.03043  -0.1948   0.1804   1.0000
  15.250   2.4392   0.03747   0.03221  -0.1924   0.1708   1.0000
  15.500   2.4400   0.03963   0.03435  -0.1897   0.1603   1.0000
  15.750   2.4425   0.04168   0.03641  -0.1874   0.1519   1.0000
  16.000   2.4344   0.04485   0.03955  -0.1844   0.1392   1.0000
  16.250   2.4239   0.04837   0.04307  -0.1814   0.1280   1.0000
  16.500   2.3987   0.05372   0.04840  -0.1780   0.1124   1.0000
  16.750   2.3790   0.05876   0.05348  -0.1756   0.1031   1.0000
  17.000   2.3440   0.06610   0.06087  -0.1735   0.0911   1.0000
  17.250   2.3041   0.07488   0.06975  -0.1727   0.0819   1.0000
  17.500   2.2652   0.08440   0.07944  -0.1735   0.0767   1.0000
  17.750   2.2327   0.09374   0.08898  -0.1756   0.0757   1.0000
  18.000   2.2000   0.10363   0.09911  -0.1786   0.0759   1.0000
  18.250   2.1468   0.11734   0.11308  -0.1835   0.0753   1.0000
  18.500   2.1066   0.12834   0.12429  -0.1876   0.0760   1.0000
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