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GOE 523 AIRFOIL (goe523-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 523 AIRFOIL (goe523-il)
Reynolds number: 200,000
Max Cl/Cd: 71.49 at α=1.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe523-il-200000-n5.txt
Download as CSV file: xf-goe523-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 523 AIRFOIL                                 
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500   0.2989   0.09798   0.09367  -0.1601   0.8973   0.0465
 -10.250   0.2946   0.09595   0.09166  -0.1602   0.8905   0.0467
 -10.000   0.3017   0.09315   0.08887  -0.1616   0.8854   0.0470
  -9.750   0.3305   0.09075   0.08645  -0.1623   0.8833   0.0481
  -9.500   0.3513   0.08802   0.08369  -0.1655   0.8809   0.0494
  -9.250   0.3542   0.08631   0.08200  -0.1647   0.8741   0.0505
  -9.000   0.3591   0.08383   0.07951  -0.1662   0.8679   0.0522
  -8.750   0.3576   0.07699   0.07258  -0.1720   0.8637   0.0411
  -8.500   0.3494   0.07529   0.07091  -0.1693   0.8541   0.0411
  -8.250   0.3608   0.07211   0.06770  -0.1718   0.8490   0.0411
  -8.000   0.3675   0.07007   0.06566  -0.1716   0.8421   0.0410
  -7.750   0.3739   0.06822   0.06380  -0.1711   0.8338   0.0408
  -7.500   0.3847   0.06582   0.06136  -0.1722   0.8266   0.0404
  -7.250   0.3819   0.06389   0.05943  -0.1706   0.8163   0.0402
  -7.000   0.3779   0.06193   0.05747  -0.1690   0.8064   0.0399
  -6.750   0.3738   0.05951   0.05502  -0.1681   0.7971   0.0397
  -6.500   0.3557   0.05783   0.05337  -0.1640   0.7853   0.0396
  -6.000   0.4090   0.02425   0.01812  -0.2280   0.7640   0.0398
  -5.750   0.4584   0.02222   0.01564  -0.2346   0.7574   0.0403
  -5.500   0.4962   0.02096   0.01404  -0.2378   0.7488   0.0409
  -5.250   0.5370   0.01996   0.01283  -0.2411   0.7414   0.0415
  -5.000   0.5662   0.01941   0.01222  -0.2419   0.7318   0.0424
  -4.750   0.6019   0.01884   0.01151  -0.2438   0.7233   0.0435
  -4.500   0.6335   0.01833   0.01085  -0.2449   0.7134   0.0444
  -4.250   0.6666   0.01784   0.01020  -0.2462   0.7043   0.0452
  -4.000   0.6987   0.01743   0.00965  -0.2472   0.6950   0.0461
  -3.750   0.7300   0.01710   0.00920  -0.2481   0.6859   0.0470
  -3.500   0.7620   0.01680   0.00884  -0.2492   0.6768   0.0481
  -3.250   0.7923   0.01660   0.00857  -0.2499   0.6678   0.0494
  -3.000   0.8230   0.01645   0.00831  -0.2506   0.6593   0.0516
  -2.750   0.8534   0.01632   0.00810  -0.2513   0.6516   0.0540
  -2.500   0.8830   0.01623   0.00794  -0.2519   0.6434   0.0568
  -2.000   0.9417   0.01612   0.00767  -0.2529   0.6279   0.0656
  -1.750   0.9725   0.01608   0.00756  -0.2537   0.6207   0.0762
  -1.500   1.0007   0.01602   0.00758  -0.2540   0.6138   0.1017
  -1.250   1.0279   0.01604   0.00763  -0.2542   0.6065   0.1386
  -1.000   1.0560   0.01612   0.00766  -0.2544   0.5998   0.1645
  -0.750   1.0802   0.01617   0.00778  -0.2539   0.5923   0.1933
  -0.500   1.1067   0.01624   0.00795  -0.2539   0.5851   0.2488
  -0.250   1.1317   0.01635   0.00814  -0.2536   0.5785   0.3046
   0.000   1.1545   0.01649   0.00835  -0.2528   0.5711   0.3422
   0.250   1.1786   0.01670   0.00853  -0.2522   0.5642   0.3740
   0.500   1.2001   0.01690   0.00878  -0.2511   0.5569   0.3990
   0.750   1.2217   0.01714   0.00901  -0.2500   0.5495   0.4210
   1.000   1.2436   0.01741   0.00925  -0.2490   0.5427   0.4432
   1.250   1.2640   0.01768   0.00953  -0.2477   0.5350   0.4626
   1.500   1.2846   0.01799   0.00979  -0.2464   0.5279   0.4798
   1.750   1.3044   0.01830   0.01010  -0.2451   0.5203   0.4973
   2.000   1.3239   0.01865   0.01041  -0.2437   0.5128   0.5149
   2.250   1.3435   0.01901   0.01074  -0.2423   0.5059   0.5314
   2.500   1.3620   0.01939   0.01111  -0.2408   0.4981   0.5439
   2.750   1.3808   0.01981   0.01145  -0.2393   0.4912   0.5567
   3.000   1.3997   0.02021   0.01185  -0.2379   0.4839   0.5704
   3.250   1.4173   0.02066   0.01227  -0.2363   0.4768   0.5812
   3.500   1.4362   0.02112   0.01269  -0.2350   0.4702   0.5922
   3.750   1.4542   0.02158   0.01314  -0.2335   0.4632   0.6001
   4.000   1.4720   0.02211   0.01358  -0.2321   0.4569   0.6094
   4.250   1.4907   0.02258   0.01408  -0.2308   0.4509   0.6164
   4.500   1.5089   0.02310   0.01458  -0.2295   0.4449   0.6242
   4.750   1.5270   0.02366   0.01507  -0.2282   0.4395   0.6312
   5.000   1.5455   0.02418   0.01563  -0.2270   0.4343   0.6384
   5.250   1.5634   0.02475   0.01619  -0.2257   0.4287   0.6464
   5.500   1.5807   0.02535   0.01676  -0.2244   0.4236   0.6525
   5.750   1.5988   0.02595   0.01735  -0.2232   0.4190   0.6600
   6.000   1.6164   0.02654   0.01800  -0.2219   0.4143   0.6680
   6.250   1.6335   0.02718   0.01865  -0.2207   0.4096   0.6779
   6.500   1.6505   0.02784   0.01930  -0.2194   0.4053   0.6870
   6.750   1.6678   0.02851   0.01999  -0.2182   0.4013   0.6954
   7.000   1.6841   0.02920   0.02074  -0.2169   0.3967   0.7016
   7.250   1.6997   0.02993   0.02150  -0.2155   0.3920   0.7084
   7.500   1.7149   0.03073   0.02228  -0.2141   0.3876   0.7155
   7.750   1.7302   0.03151   0.02310  -0.2128   0.3835   0.7221
   8.000   1.7451   0.03233   0.02399  -0.2115   0.3789   0.7296
   8.250   1.7592   0.03319   0.02491  -0.2100   0.3745   0.7373
   8.500   1.7731   0.03410   0.02583  -0.2086   0.3705   0.7464
   8.750   1.7876   0.03498   0.02675  -0.2073   0.3668   0.7561
   9.000   1.8013   0.03592   0.02781  -0.2060   0.3626   0.7678
   9.250   1.8139   0.03691   0.02891  -0.2045   0.3584   0.7852
   9.500   1.8231   0.03783   0.02995  -0.2026   0.3541   0.8927
   9.750   1.8338   0.03901   0.03114  -0.2010   0.3498   1.0000
  10.000   1.8445   0.04032   0.03254  -0.1996   0.3446   1.0000
  10.250   1.8540   0.04173   0.03399  -0.1981   0.3394   1.0000
  10.500   1.8633   0.04318   0.03542  -0.1967   0.3348   1.0000
  10.750   1.8731   0.04465   0.03697  -0.1954   0.3302   1.0000
  11.000   1.8822   0.04620   0.03860  -0.1940   0.3255   1.0000
  11.250   1.8909   0.04781   0.04024  -0.1927   0.3212   1.0000
  11.500   1.8997   0.04942   0.04185  -0.1914   0.3175   1.0000
  11.750   1.9091   0.05107   0.04361  -0.1903   0.3136   1.0000
  12.000   1.9172   0.05284   0.04548  -0.1891   0.3097   1.0000
  12.250   1.9252   0.05464   0.04733  -0.1880   0.3059   1.0000
  12.500   1.9326   0.05650   0.04922  -0.1868   0.3025   1.0000
  12.750   1.9398   0.05844   0.05124  -0.1858   0.2988   1.0000
  13.000   1.9446   0.06069   0.05361  -0.1847   0.2943   1.0000
  13.250   1.9482   0.06307   0.05604  -0.1836   0.2895   1.0000
  13.750   1.9526   0.06832   0.06142  -0.1816   0.2796   1.0000
  14.000   1.9530   0.07123   0.06442  -0.1807   0.2741   1.0000
  14.250   1.9540   0.07405   0.06723  -0.1798   0.2692   1.0000
  14.500   1.9544   0.07713   0.07046  -0.1792   0.2644   1.0000
  14.750   1.9552   0.08016   0.07359  -0.1786   0.2599   1.0000
  15.000   1.9557   0.08322   0.07669  -0.1780   0.2556   1.0000
  15.250   1.9563   0.08630   0.07985  -0.1776   0.2516   1.0000
  15.500   1.9558   0.08963   0.08332  -0.1773   0.2473   1.0000
  15.750   1.9537   0.09317   0.08695  -0.1770   0.2427   1.0000
  16.000   1.9525   0.09652   0.09033  -0.1768   0.2382   1.0000
  16.250   1.9500   0.10022   0.09418  -0.1768   0.2339   1.0000
  16.500   1.9466   0.10406   0.09814  -0.1769   0.2294   1.0000
  16.750   1.9438   0.10777   0.10192  -0.1770   0.2249   1.0000
  17.000   1.9415   0.11141   0.10564  -0.1773   0.2209   1.0000
  17.250   1.9368   0.11553   0.10991  -0.1778   0.2164   1.0000
  17.500   1.9316   0.11967   0.11415  -0.1783   0.2114   1.0000
  17.750   1.9261   0.12385   0.11839  -0.1790   0.2062   1.0000
  18.000   1.9184   0.12850   0.12319  -0.1800   0.2006   1.0000
  18.250   1.9106   0.13310   0.12785  -0.1810   0.1943   1.0000
  18.500   1.9026   0.13781   0.13269  -0.1823   0.1879   1.0000
  18.750   1.8918   0.14296   0.13790  -0.1838   0.1797   1.0000
  19.000   1.8810   0.14816   0.14321  -0.1855   0.1703   1.0000
  19.250   1.8683   0.15365   0.14874  -0.1875   0.1581   1.0000
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