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S1223 RTL (s1223rtl-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: S1223 RTL (s1223rtl-il)
Reynolds number: 200,000
Max Cl/Cd: 64.59 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-s1223rtl-il-200000-n5.txt
Download as CSV file: xf-s1223rtl-il-200000-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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
  -9.500   0.0025   0.11944   0.11582  -0.0727   0.9379   0.0247
  -9.250   0.0097   0.11651   0.11290  -0.0756   0.9315   0.0248
  -9.000   0.0212   0.11359   0.11001  -0.0746   0.9232   0.0251
  -8.500   0.0412   0.10845   0.10491  -0.0756   0.9074   0.0262
  -8.250   0.0526   0.10562   0.10208  -0.0770   0.8998   0.0267
  -8.000   0.0628   0.10282   0.09929  -0.0782   0.8893   0.0273
  -7.750   0.0736   0.09991   0.09638  -0.0798   0.8782   0.0279
  -7.500   0.0874   0.09648   0.09294  -0.0834   0.8678   0.0285
  -7.250   0.1000   0.09298   0.08940  -0.0879   0.8554   0.0287
  -6.750   0.2592   0.07906   0.07352  -0.1235   0.5347   0.0306
  -6.500   0.2547   0.07811   0.07232  -0.1206   0.4864   0.0311
  -6.250   0.2528   0.07680   0.07092  -0.1186   0.4651   0.0317
  -6.000   0.2504   0.07538   0.06946  -0.1165   0.4506   0.0320
  -5.750   0.2403   0.07395   0.06805  -0.1143   0.4429   0.0328
  -5.500   0.2352   0.07261   0.06671  -0.1117   0.4345   0.0328
  -5.250   0.2269   0.07043   0.06457  -0.1106   0.4289   0.0331
  -5.000   0.2243   0.06674   0.06086  -0.1093   0.4236   0.0247
  -4.750   0.2290   0.06534   0.05945  -0.1076   0.4166   0.0243
  -4.500   0.2337   0.06327   0.05739  -0.1074   0.4109   0.0240
  -4.250   0.2414   0.06184   0.05595  -0.1073   0.4050   0.0267
  -3.750   0.4716   0.02632   0.01897  -0.1959   0.3938   0.0220
  -3.500   0.5506   0.02310   0.01492  -0.2099   0.3851   0.0230
  -3.250   0.6080   0.02149   0.01257  -0.2172   0.3786   0.0249
  -3.000   0.6436   0.02106   0.01206  -0.2192   0.3735   0.0263
  -2.750   0.6835   0.02040   0.01114  -0.2219   0.3687   0.0276
  -2.500   0.7217   0.01990   0.01035  -0.2241   0.3645   0.0288
  -2.250   0.7568   0.01965   0.01001  -0.2258   0.3607   0.0302
  -2.000   0.7917   0.01946   0.00971  -0.2272   0.3573   0.0327
  -1.750   0.8265   0.01930   0.00953  -0.2287   0.3536   0.0356
  -1.500   0.8618   0.01918   0.00931  -0.2303   0.3498   0.0385
  -1.250   0.8961   0.01915   0.00919  -0.2316   0.3463   0.0429
  -1.000   0.9297   0.01919   0.00911  -0.2328   0.3431   0.0497
  -0.750   0.9649   0.01924   0.00907  -0.2344   0.3404   0.0611
  -0.500   1.0024   0.01912   0.00905  -0.2365   0.3378   0.1044
  -0.250   1.0380   0.01907   0.00928  -0.2383   0.3351   0.2211
   0.000   1.0674   0.01924   0.00948  -0.2386   0.3325   0.2659
   0.250   1.0956   0.01946   0.00968  -0.2385   0.3299   0.3009
   0.500   1.1231   0.01972   0.00992  -0.2383   0.3274   0.3353
   0.750   1.1506   0.01999   0.01013  -0.2381   0.3250   0.3568
   1.000   1.1789   0.02031   0.01036  -0.2382   0.3225   0.3697
   1.250   1.2069   0.02054   0.01057  -0.2380   0.3205   0.3823
   1.500   1.2345   0.02077   0.01079  -0.2379   0.3186   0.3964
   1.750   1.2622   0.02101   0.01104  -0.2377   0.3165   0.4097
   2.000   1.2895   0.02127   0.01129  -0.2375   0.3144   0.4228
   2.250   1.3165   0.02154   0.01154  -0.2373   0.3124   0.4374
   2.500   1.3432   0.02182   0.01182  -0.2370   0.3104   0.4521
   2.750   1.3696   0.02211   0.01209  -0.2366   0.3083   0.4662
   3.000   1.3962   0.02245   0.01238  -0.2363   0.3064   0.4803
   3.250   1.4238   0.02284   0.01272  -0.2363   0.3044   0.4962
   3.500   1.4501   0.02315   0.01306  -0.2360   0.3027   0.5123
   3.750   1.4763   0.02345   0.01342  -0.2356   0.3010   0.5280
   4.000   1.5024   0.02376   0.01379  -0.2352   0.2993   0.5447
   4.250   1.5282   0.02409   0.01418  -0.2348   0.2975   0.5626
   4.500   1.5537   0.02443   0.01456  -0.2344   0.2957   0.5819
   4.750   1.5784   0.02476   0.01493  -0.2338   0.2940   0.6033
   5.000   1.6023   0.02508   0.01532  -0.2330   0.2923   0.6275
   5.500   1.6498   0.02574   0.01608  -0.2315   0.2889   0.7051
   5.750   1.6639   0.02576   0.01631  -0.2287   0.2875   1.0000
   6.000   1.6889   0.02623   0.01678  -0.2282   0.2861   1.0000
   6.250   1.7122   0.02667   0.01727  -0.2275   0.2846   1.0000
   6.500   1.7353   0.02713   0.01778  -0.2267   0.2831   1.0000
   6.750   1.7581   0.02760   0.01829  -0.2258   0.2815   1.0000
   7.000   1.7805   0.02808   0.01883  -0.2249   0.2798   1.0000
   7.250   1.8022   0.02857   0.01934  -0.2239   0.2782   1.0000
   7.500   1.8233   0.02905   0.01986  -0.2228   0.2766   1.0000
   7.750   1.8439   0.02954   0.02037  -0.2216   0.2750   1.0000
   8.000   1.8646   0.03005   0.02090  -0.2205   0.2735   1.0000
   8.250   1.8864   0.03059   0.02145  -0.2195   0.2722   1.0000
   8.500   1.9093   0.03118   0.02203  -0.2189   0.2710   1.0000
   8.750   1.9303   0.03181   0.02273  -0.2179   0.2697   1.0000
   9.000   1.9487   0.03246   0.02351  -0.2164   0.2683   1.0000
   9.250   1.9669   0.03313   0.02430  -0.2149   0.2669   1.0000
   9.500   1.9843   0.03381   0.02510  -0.2134   0.2653   1.0000
   9.750   2.0014   0.03450   0.02589  -0.2118   0.2636   1.0000
  10.000   2.0178   0.03520   0.02668  -0.2101   0.2620   1.0000
  10.250   2.0344   0.03591   0.02748  -0.2085   0.2605   1.0000
  10.500   2.0511   0.03664   0.02829  -0.2069   0.2593   1.0000
  10.750   2.0675   0.03739   0.02911  -0.2053   0.2581   1.0000
  11.000   2.0843   0.03815   0.02994  -0.2038   0.2569   1.0000
  11.250   2.1023   0.03893   0.03076  -0.2026   0.2558   1.0000
  11.500   2.1204   0.03978   0.03166  -0.2014   0.2546   1.0000
  11.750   2.1300   0.04092   0.03302  -0.1990   0.2533   1.0000
  12.000   2.1391   0.04211   0.03441  -0.1966   0.2517   1.0000
  12.250   2.1479   0.04333   0.03581  -0.1942   0.2501   1.0000
  12.500   2.1572   0.04457   0.03721  -0.1920   0.2485   1.0000
  12.750   2.1665   0.04584   0.03862  -0.1899   0.2471   1.0000
  13.000   2.1757   0.04713   0.04005  -0.1878   0.2458   1.0000
  13.250   2.1849   0.04843   0.04148  -0.1858   0.2446   1.0000
  13.500   2.1938   0.04974   0.04291  -0.1839   0.2434   1.0000
  13.750   2.2032   0.05105   0.04432  -0.1820   0.2422   1.0000
  14.000   2.2144   0.05224   0.04558  -0.1804   0.2410   1.0000
  14.250   2.2267   0.05348   0.04690  -0.1791   0.2397   1.0000
  14.500   2.2202   0.05616   0.04986  -0.1761   0.2384   1.0000
  14.750   2.2130   0.05902   0.05298  -0.1734   0.2368   1.0000
  15.000   2.2060   0.06203   0.05623  -0.1710   0.2353   1.0000
  15.250   2.1991   0.06516   0.05958  -0.1689   0.2338   1.0000
  15.500   2.1925   0.06836   0.06297  -0.1672   0.2322   1.0000
  15.750   2.1875   0.07147   0.06625  -0.1658   0.2306   1.0000
  16.000   2.1854   0.07431   0.06922  -0.1646   0.2291   1.0000
  16.250   2.1897   0.07638   0.07137  -0.1638   0.2274   1.0000
  16.500   2.2071   0.07692   0.07190  -0.1632   0.2256   1.0000
  16.750   2.1537   0.08677   0.08217  -0.1628   0.2235   1.0000
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