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S1223 RTL (s1223rtl-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: S1223 RTL (s1223rtl-il)
Reynolds number: 1,000,000
Max Cl/Cd: 106.7 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-s1223rtl-il-1000000.txt
Download as CSV file: xf-s1223rtl-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.000   0.0740   0.10979   0.10801  -0.0969   0.9489   0.0119
  -9.750   0.0806   0.10648   0.10471  -0.0986   0.9437   0.0119
  -9.500   0.0849   0.10361   0.10185  -0.0977   0.9356   0.0121
  -9.250   0.0972   0.10088   0.09912  -0.0989   0.9279   0.0121
  -9.000   0.1231   0.09729   0.09549  -0.1036   0.9152   0.0123
  -8.750   0.2506   0.08668   0.08401  -0.1377   0.7921   0.0136
  -8.500   0.2414   0.08728   0.08320  -0.1331   0.4904   0.0139
  -8.250   0.2478   0.08495   0.08072  -0.1337   0.4544   0.0144
  -8.000   0.2478   0.08221   0.07792  -0.1345   0.4378   0.0147
  -7.750   0.2517   0.08000   0.07569  -0.1346   0.4258   0.0147
  -7.500   0.2554   0.07778   0.07344  -0.1343   0.4151   0.0148
  -7.250   0.2598   0.07565   0.07128  -0.1334   0.4036   0.0150
  -7.000   0.2669   0.07414   0.06975  -0.1326   0.3948   0.0151
  -6.750   0.2732   0.07270   0.06829  -0.1316   0.3882   0.0152
  -6.500   0.2778   0.07124   0.06682  -0.1305   0.3806   0.0154
  -6.250   0.2808   0.06969   0.06528  -0.1293   0.3770   0.0155
  -6.000   0.2818   0.06814   0.06376  -0.1278   0.3734   0.0156
  -5.750   0.2808   0.06678   0.06241  -0.1257   0.3698   0.0159
  -5.500   0.2752   0.06551   0.06116  -0.1228   0.3665   0.0160
  -5.250   0.2702   0.06401   0.05968  -0.1201   0.3626   0.0164
  -5.000   0.4702   0.01653   0.01054  -0.2289   0.3636   0.0150
  -4.750   0.5191   0.01524   0.00898  -0.2344   0.3580   0.0153
  -4.500   0.5571   0.01469   0.00829  -0.2369   0.3537   0.0157
  -4.250   0.5909   0.01442   0.00791  -0.2382   0.3490   0.0162
  -4.000   0.6259   0.01410   0.00743  -0.2398   0.3434   0.0169
  -3.750   0.6620   0.01373   0.00691  -0.2416   0.3397   0.0175
  -3.500   0.7009   0.01323   0.00628  -0.2440   0.3373   0.0182
  -3.250   0.7354   0.01299   0.00600  -0.2454   0.3344   0.0189
  -3.000   0.7677   0.01287   0.00582  -0.2462   0.3314   0.0197
  -2.750   0.8000   0.01278   0.00564  -0.2470   0.3281   0.0206
  -2.500   0.8325   0.01270   0.00547  -0.2479   0.3242   0.0214
  -2.250   0.8658   0.01260   0.00533  -0.2490   0.3215   0.0228
  -2.000   0.8962   0.01257   0.00527  -0.2493   0.3199   0.0245
  -1.750   0.9292   0.01246   0.00513  -0.2503   0.3179   0.0264
  -1.500   0.9595   0.01246   0.00509  -0.2507   0.3157   0.0285
  -1.250   0.9908   0.01243   0.00502  -0.2512   0.3135   0.0316
  -1.000   1.0209   0.01245   0.00501  -0.2516   0.3111   0.0363
  -0.750   1.0510   0.01249   0.00503  -0.2519   0.3085   0.0459
  -0.500   1.0835   0.01250   0.00512  -0.2529   0.3051   0.0960
  -0.250   1.1176   0.01240   0.00526  -0.2543   0.3035   0.2034
   0.000   1.1463   0.01245   0.00535  -0.2543   0.3023   0.2369
   0.250   1.1743   0.01252   0.00545  -0.2542   0.3009   0.2598
   0.500   1.2019   0.01262   0.00556  -0.2540   0.2992   0.2791
   0.750   1.2291   0.01272   0.00567  -0.2537   0.2974   0.2968
   1.000   1.2561   0.01285   0.00581  -0.2534   0.2957   0.3193
   1.250   1.2829   0.01299   0.00598  -0.2530   0.2938   0.3433
   1.500   1.3088   0.01316   0.00613  -0.2525   0.2918   0.3571
   1.750   1.3346   0.01338   0.00634  -0.2519   0.2894   0.3713
   2.000   1.3596   0.01365   0.00661  -0.2512   0.2868   0.3840
   2.250   1.3858   0.01377   0.00674  -0.2507   0.2861   0.3968
   2.500   1.4121   0.01390   0.00690  -0.2503   0.2851   0.4107
   2.750   1.4381   0.01404   0.00706  -0.2498   0.2839   0.4242
   3.250   1.4895   0.01435   0.00740  -0.2487   0.2809   0.4500
   3.500   1.5149   0.01452   0.00759  -0.2481   0.2795   0.4624
   3.750   1.5400   0.01472   0.00779  -0.2474   0.2780   0.4755
   4.000   1.5650   0.01493   0.00802  -0.2468   0.2764   0.4898
   4.250   1.5896   0.01517   0.00826  -0.2461   0.2745   0.5029
   4.500   1.6135   0.01548   0.00857  -0.2453   0.2723   0.5161
   4.750   1.6374   0.01581   0.00892  -0.2445   0.2703   0.5303
   5.000   1.6627   0.01597   0.00913  -0.2439   0.2696   0.5467
   5.250   1.6877   0.01615   0.00935  -0.2433   0.2686   0.5641
   5.500   1.7124   0.01634   0.00960  -0.2427   0.2674   0.5824
   5.750   1.7370   0.01655   0.00987  -0.2421   0.2662   0.6045
   6.000   1.7617   0.01678   0.01016  -0.2415   0.2649   0.6331
   6.250   1.7867   0.01700   0.01046  -0.2410   0.2636   0.6749
   6.500   1.8085   0.01695   0.01080  -0.2398   0.2623   1.0000
   6.750   1.8314   0.01724   0.01109  -0.2389   0.2608   1.0000
   7.000   1.8539   0.01758   0.01141  -0.2379   0.2593   1.0000
   7.250   1.8756   0.01798   0.01180  -0.2368   0.2572   1.0000
   7.500   1.8966   0.01849   0.01230  -0.2356   0.2548   1.0000
   7.750   1.9194   0.01874   0.01259  -0.2346   0.2541   1.0000
   8.000   1.9417   0.01903   0.01291  -0.2337   0.2534   1.0000
   8.250   1.9638   0.01933   0.01325  -0.2326   0.2524   1.0000
   8.500   1.9856   0.01965   0.01360  -0.2316   0.2513   1.0000
   8.750   2.0073   0.01999   0.01397  -0.2306   0.2502   1.0000
   9.000   2.0288   0.02034   0.01434  -0.2295   0.2490   1.0000
   9.250   2.0498   0.02070   0.01474  -0.2284   0.2477   1.0000
   9.500   2.0701   0.02111   0.01517  -0.2271   0.2464   1.0000
   9.750   2.0899   0.02155   0.01563  -0.2258   0.2449   1.0000
  10.000   2.1091   0.02205   0.01614  -0.2245   0.2432   1.0000
  10.250   2.1273   0.02268   0.01677  -0.2230   0.2410   1.0000
  10.500   2.1460   0.02325   0.01739  -0.2216   0.2396   1.0000
  10.750   2.1658   0.02366   0.01786  -0.2204   0.2390   1.0000
  11.000   2.1854   0.02409   0.01835  -0.2191   0.2381   1.0000
  11.250   2.2048   0.02455   0.01887  -0.2179   0.2372   1.0000
  11.500   2.2235   0.02504   0.01942  -0.2166   0.2360   1.0000
  11.750   2.2418   0.02555   0.01998  -0.2152   0.2348   1.0000
  12.000   2.2600   0.02608   0.02057  -0.2139   0.2335   1.0000
  12.250   2.2776   0.02665   0.02118  -0.2124   0.2322   1.0000
  12.500   2.2940   0.02730   0.02188  -0.2109   0.2309   1.0000
  12.750   2.3093   0.02803   0.02264  -0.2092   0.2290   1.0000
  13.000   2.3228   0.02897   0.02360  -0.2073   0.2265   1.0000
  13.250   2.3386   0.02966   0.02436  -0.2058   0.2249   1.0000
  13.500   2.3557   0.03023   0.02502  -0.2045   0.2237   1.0000
  13.750   2.3725   0.03085   0.02571  -0.2031   0.2222   1.0000
  14.000   2.3883   0.03152   0.02645  -0.2017   0.2203   1.0000
  14.250   2.4035   0.03224   0.02723  -0.2002   0.2180   1.0000
  14.500   2.4168   0.03316   0.02819  -0.1986   0.2160   1.0000
  14.750   2.4254   0.03444   0.02948  -0.1964   0.2114   1.0000
  15.000   2.4451   0.03479   0.02991  -0.1957   0.2071   1.0000
  15.250   2.4568   0.03584   0.03098  -0.1940   0.2026   1.0000
  15.500   2.4650   0.03724   0.03240  -0.1920   0.1980   1.0000
  15.750   2.4789   0.03815   0.03340  -0.1907   0.1954   1.0000
  16.000   2.4893   0.03939   0.03468  -0.1891   0.1909   1.0000
  16.250   2.4942   0.04116   0.03647  -0.1870   0.1860   1.0000
  16.500   2.5040   0.04250   0.03788  -0.1855   0.1814   1.0000
  16.750   2.5075   0.04448   0.03989  -0.1835   0.1755   1.0000
  17.000   2.5108   0.04653   0.04199  -0.1816   0.1702   1.0000
  17.250   2.5113   0.04890   0.04441  -0.1797   0.1639   1.0000
  17.500   2.5072   0.05186   0.04740  -0.1776   0.1569   1.0000
  17.750   2.4937   0.05599   0.05154  -0.1753   0.1469   1.0000
  18.000   2.4733   0.06118   0.05676  -0.1732   0.1367   1.0000
  18.250   2.4564   0.06619   0.06184  -0.1718   0.1292   1.0000
  18.500   2.4252   0.07349   0.06922  -0.1708   0.1207   1.0000
  18.750   2.3833   0.08301   0.07887  -0.1712   0.1136   1.0000
  19.000   2.3549   0.09110   0.08714  -0.1725   0.1114   1.0000
  19.250   2.3125   0.10212   0.09837  -0.1756   0.1090   1.0000
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