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GOE 527 AIRFOIL (goe527-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 527 AIRFOIL (goe527-il)
Reynolds number: 200,000
Max Cl/Cd: 69.46 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe527-il-200000.txt
Download as CSV file: xf-goe527-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 527 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.2121   0.14787   0.14408  -0.0462   1.0000   0.0571
 -13.750  -0.2109   0.14529   0.14154  -0.0468   1.0000   0.0590
 -13.500  -0.2374   0.14297   0.13930  -0.0506   1.0000   0.0604
 -13.250  -0.2177   0.13971   0.13606  -0.0482   1.0000   0.0610
 -13.000  -0.2108   0.13768   0.13408  -0.0467   1.0000   0.0617
 -12.750  -0.2116   0.13617   0.13264  -0.0450   1.0000   0.0626
 -12.500  -0.2224   0.13572   0.13228  -0.0417   0.9999   0.0634
 -12.250  -0.2054   0.13116   0.12771  -0.0472   0.9968   0.0660
 -12.000  -0.2123   0.12527   0.12183  -0.0570   0.9912   0.0678
 -11.750  -0.1791   0.12139   0.11793  -0.0579   0.9873   0.0686
 -11.500  -0.1541   0.11774   0.11427  -0.0611   0.9832   0.0701
 -11.250  -0.1362   0.11389   0.11041  -0.0652   0.9771   0.0727
 -11.000  -0.1539   0.10725   0.10379  -0.0785   0.9692   0.0758
 -10.750  -0.1213   0.10377   0.10028  -0.0777   0.9633   0.0766
 -10.500  -0.0942   0.10041   0.09691  -0.0799   0.9571   0.0776
 -10.250  -0.0700   0.09684   0.09332  -0.0838   0.9509   0.0796
  -9.750  -0.0504   0.08549   0.08192  -0.1009   0.9337   0.0859
  -9.500  -0.0158   0.08266   0.07904  -0.1031   0.9257   0.0873
  -9.250   0.0118   0.07917   0.07549  -0.1078   0.9151   0.0894
  -9.000  -0.0428   0.06837   0.06454  -0.1297   0.8856   0.0954
  -8.750  -0.0124   0.06598   0.06217  -0.1269   0.8756   0.0963
  -8.500   0.0216   0.06497   0.06108  -0.1248   0.8663   0.0973
  -8.250  -0.1638   0.03929   0.03408  -0.1302   0.8380   0.0674
  -8.000  -0.1568   0.03622   0.03069  -0.1289   0.8286   0.0673
  -7.750  -0.1507   0.03356   0.02774  -0.1268   0.8172   0.0671
  -7.500  -0.1407   0.03093   0.02470  -0.1251   0.8083   0.0671
  -7.250  -0.1299   0.02872   0.02206  -0.1230   0.7982   0.0674
  -7.000  -0.1115   0.02688   0.01999  -0.1220   0.7903   0.0683
  -6.750  -0.0891   0.02629   0.01943  -0.1212   0.7805   0.0697
  -6.500  -0.0658   0.02540   0.01836  -0.1205   0.7729   0.0712
  -6.250  -0.0469   0.02425   0.01698  -0.1190   0.7630   0.0726
  -6.000  -0.0238   0.02299   0.01534  -0.1181   0.7558   0.0742
  -5.750  -0.0035   0.02208   0.01411  -0.1165   0.7465   0.0758
  -5.500   0.0218   0.02114   0.01316  -0.1162   0.7392   0.0778
  -5.250   0.0459   0.02075   0.01272  -0.1154   0.7311   0.0806
  -5.000   0.0706   0.02023   0.01196  -0.1145   0.7231   0.0840
  -4.750   0.0963   0.01946   0.01111  -0.1141   0.7162   0.0872
  -4.500   0.1202   0.01905   0.01069  -0.1132   0.7079   0.0910
  -4.250   0.1468   0.01859   0.01002  -0.1127   0.7017   0.0963
  -4.000   0.1710   0.01816   0.00967  -0.1120   0.6944   0.1020
  -3.750   0.1962   0.01775   0.00914  -0.1113   0.6873   0.1089
  -3.500   0.2234   0.01733   0.00871  -0.1111   0.6817   0.1163
  -3.250   0.2464   0.01696   0.00835  -0.1101   0.6744   0.1238
  -3.000   0.2719   0.01668   0.00808  -0.1096   0.6683   0.1319
  -2.750   0.2991   0.01636   0.00770  -0.1093   0.6633   0.1403
  -2.500   0.3221   0.01622   0.00760  -0.1084   0.6565   0.1489
  -2.250   0.3470   0.01594   0.00737  -0.1077   0.6505   0.1586
  -2.000   0.3745   0.01580   0.00716  -0.1075   0.6459   0.1699
  -1.750   0.3979   0.01566   0.00711  -0.1066   0.6402   0.1827
  -1.500   0.4219   0.01546   0.00700  -0.1058   0.6344   0.2008
  -1.250   0.4470   0.01514   0.00685  -0.1052   0.6296   0.2434
  -1.000   0.4678   0.01458   0.00687  -0.1041   0.6252   0.3925
  -0.750   0.4850   0.01421   0.00704  -0.1020   0.6197   0.5363
  -0.500   0.5044   0.01385   0.00712  -0.1000   0.6148   0.6606
  -0.250   0.5401   0.01353   0.00724  -0.1005   0.6104   0.8349
   0.000   0.6107   0.01374   0.00747  -0.1084   0.6048   0.9526
   0.250   0.6775   0.01389   0.00750  -0.1161   0.5987   0.9839
   0.500   0.7397   0.01394   0.00736  -0.1231   0.5935   1.0000
   0.750   0.7611   0.01412   0.00742  -0.1220   0.5891   1.0000
   1.000   0.7784   0.01426   0.00755  -0.1201   0.5830   1.0000
   1.250   0.8004   0.01433   0.00750  -0.1189   0.5771   1.0000
   1.500   0.8236   0.01446   0.00749  -0.1180   0.5714   1.0000
   1.750   0.8407   0.01458   0.00761  -0.1159   0.5646   1.0000
   2.000   0.8633   0.01469   0.00762  -0.1148   0.5592   1.0000
   2.250   0.8895   0.01489   0.00768  -0.1145   0.5552   1.0000
   2.500   0.9065   0.01511   0.00795  -0.1125   0.5501   1.0000
   2.750   0.9272   0.01529   0.00810  -0.1111   0.5449   1.0000
   3.000   0.9516   0.01544   0.00815  -0.1104   0.5403   1.0000
   3.250   0.9755   0.01567   0.00830  -0.1097   0.5358   1.0000
   3.500   0.9927   0.01587   0.00855  -0.1077   0.5301   1.0000
   3.750   1.0150   0.01604   0.00867  -0.1066   0.5250   1.0000
   4.000   1.0415   0.01621   0.00874  -0.1063   0.5206   1.0000
   4.250   1.0596   0.01648   0.00904  -0.1046   0.5154   1.0000
   4.500   1.0790   0.01668   0.00926  -0.1030   0.5098   1.0000
   4.750   1.1035   0.01683   0.00935  -0.1023   0.5050   1.0000
   5.000   1.1272   0.01708   0.00954  -0.1016   0.5001   1.0000
   5.250   1.1430   0.01731   0.00984  -0.0994   0.4941   1.0000
   5.500   1.1656   0.01746   0.00996  -0.0985   0.4886   1.0000
   5.750   1.1917   0.01766   0.01007  -0.0982   0.4835   1.0000
   6.000   1.2043   0.01787   0.01038  -0.0954   0.4764   1.0000
   6.250   1.2261   0.01799   0.01045  -0.0943   0.4702   1.0000
   6.500   1.2456   0.01819   0.01063  -0.0928   0.4638   1.0000
   6.750   1.2604   0.01837   0.01087  -0.0905   0.4565   1.0000
   7.000   1.2844   0.01849   0.01088  -0.0898   0.4502   1.0000
   7.250   1.2938   0.01875   0.01124  -0.0866   0.4424   1.0000
   7.500   1.3113   0.01891   0.01137  -0.0848   0.4355   1.0000
   7.750   1.3260   0.01918   0.01166  -0.0826   0.4285   1.0000
   8.000   1.3364   0.01942   0.01193  -0.0796   0.4210   1.0000
   8.250   1.3532   0.01967   0.01212  -0.0778   0.4142   1.0000
   8.500   1.3566   0.02003   0.01255  -0.0737   0.4060   1.0000
   8.750   1.3727   0.02030   0.01273  -0.0718   0.3985   1.0000
   9.000   1.3749   0.02078   0.01330  -0.0679   0.3896   1.0000
   9.250   1.3901   0.02116   0.01358  -0.0660   0.3820   1.0000
   9.500   1.3939   0.02179   0.01430  -0.0627   0.3735   1.0000
   9.750   1.4095   0.02226   0.01465  -0.0611   0.3661   1.0000
  10.000   1.4123   0.02303   0.01553  -0.0579   0.3577   1.0000
  10.500   1.4298   0.02451   0.01701  -0.0536   0.3424   1.0000
  10.750   1.4424   0.02521   0.01764  -0.0520   0.3359   1.0000
  11.000   1.4512   0.02611   0.01859  -0.0500   0.3294   1.0000
  11.250   1.4599   0.02702   0.01954  -0.0482   0.3233   1.0000
  11.500   1.4780   0.02765   0.02006  -0.0474   0.3178   1.0000
  11.750   1.4813   0.02885   0.02140  -0.0452   0.3121   1.0000
  12.000   1.4908   0.02984   0.02242  -0.0437   0.3068   1.0000
  12.250   1.5107   0.03044   0.02291  -0.0432   0.3018   1.0000
  12.500   1.5124   0.03185   0.02448  -0.0412   0.2969   1.0000
  12.750   1.5194   0.03304   0.02573  -0.0397   0.2919   1.0000
  13.000   1.5376   0.03371   0.02632  -0.0391   0.2872   1.0000
  13.250   1.5423   0.03513   0.02786  -0.0376   0.2827   1.0000
  13.500   1.5461   0.03660   0.02943  -0.0361   0.2779   1.0000
  13.750   1.5571   0.03767   0.03050  -0.0352   0.2734   1.0000
  14.000   1.5716   0.03863   0.03144  -0.0344   0.2688   1.0000
  14.250   1.5687   0.04063   0.03361  -0.0329   0.2642   1.0000
  14.500   1.5744   0.04212   0.03515  -0.0318   0.2595   1.0000
  14.750   1.5983   0.04245   0.03536  -0.0316   0.2545   1.0000
  15.000   1.5866   0.04523   0.03836  -0.0300   0.2501   1.0000
  15.250   1.5873   0.04720   0.04042  -0.0290   0.2451   1.0000
  15.500   1.6063   0.04777   0.04089  -0.0286   0.2399   1.0000
  15.750   1.5954   0.05080   0.04411  -0.0275   0.2351   1.0000
  16.000   1.5927   0.05323   0.04663  -0.0267   0.2298   1.0000
  16.250   1.6112   0.05377   0.04704  -0.0263   0.2244   1.0000
  16.500   1.5955   0.05754   0.05103  -0.0256   0.2196   1.0000
  16.750   1.5910   0.06033   0.05391  -0.0252   0.2144   1.0000
  17.000   1.6100   0.06076   0.05420  -0.0249   0.2091   1.0000
  17.250   1.5915   0.06520   0.05888  -0.0247   0.2048   1.0000
  17.500   1.5857   0.06838   0.06217  -0.0247   0.2003   1.0000
  17.750   1.5942   0.06991   0.06365  -0.0246   0.1958   1.0000
  18.000   1.5899   0.07306   0.06691  -0.0246   0.1918   1.0000
  18.250   1.5766   0.07738   0.07140  -0.0251   0.1875   1.0000
  18.500   1.5768   0.08008   0.07415  -0.0254   0.1836   1.0000
  18.750   1.5902   0.08103   0.07502  -0.0253   0.1796   1.0000
  19.000   1.5707   0.08643   0.08066  -0.0264   0.1764   1.0000
  19.250   1.5602   0.09071   0.08509  -0.0273   0.1726   1.0000
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