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GOE 547 AIRFOIL (goe547-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 547 AIRFOIL (goe547-il)
Reynolds number: 200,000
Max Cl/Cd: 82.37 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe547-il-200000-n5.txt
Download as CSV file: xf-goe547-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 547 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
  ------ -------- --------- --------- -------- -------- --------
 -10.750  -0.3917   0.10735   0.10365  -0.0446   1.0000   0.0244
 -10.500  -0.4026   0.10218   0.09855  -0.0458   1.0000   0.0252
 -10.250  -0.4082   0.09904   0.09546  -0.0454   1.0000   0.0254
 -10.000  -0.4141   0.09635   0.09281  -0.0447   1.0000   0.0256
  -9.750  -0.4166   0.09416   0.09067  -0.0440   0.9997   0.0259
  -9.500  -0.4033   0.09059   0.08709  -0.0478   0.9970   0.0266
  -9.250  -0.3897   0.08710   0.08359  -0.0517   0.9937   0.0277
  -9.000  -0.3817   0.08189   0.07838  -0.0572   0.9888   0.0287
  -8.750  -0.3783   0.07536   0.07186  -0.0643   0.9822   0.0297
  -8.500  -0.3826   0.06741   0.06393  -0.0731   0.9715   0.0299
  -8.250  -0.4083   0.04410   0.04009  -0.0989   0.9533   0.0301
  -8.000  -0.4077   0.03633   0.03162  -0.1029   0.9435   0.0315
  -7.750  -0.3885   0.03213   0.02675  -0.1052   0.9390   0.0327
  -7.500  -0.3717   0.02881   0.02294  -0.1056   0.9333   0.0335
  -7.250  -0.3496   0.02662   0.02048  -0.1061   0.9284   0.0344
  -7.000  -0.3203   0.02543   0.01914  -0.1073   0.9255   0.0357
  -6.750  -0.2890   0.02405   0.01752  -0.1089   0.9233   0.0369
  -6.500  -0.2663   0.02273   0.01592  -0.1085   0.9175   0.0377
  -6.250  -0.2384   0.02141   0.01434  -0.1090   0.9134   0.0385
  -6.000  -0.2074   0.02017   0.01286  -0.1100   0.9104   0.0392
  -5.750  -0.1742   0.01918   0.01166  -0.1114   0.9081   0.0405
  -5.500  -0.1500   0.01845   0.01076  -0.1108   0.9020   0.0415
  -5.250  -0.1206   0.01761   0.00977  -0.1113   0.8978   0.0421
  -5.000  -0.0883   0.01682   0.00884  -0.1123   0.8946   0.0427
  -4.750  -0.0594   0.01598   0.00795  -0.1127   0.8903   0.0436
  -4.500  -0.0339   0.01539   0.00732  -0.1124   0.8843   0.0446
  -4.250  -0.0032   0.01486   0.00675  -0.1131   0.8803   0.0458
  -4.000   0.0273   0.01443   0.00627  -0.1137   0.8762   0.0472
  -3.750   0.0521   0.01410   0.00589  -0.1131   0.8695   0.0488
  -3.500   0.0827   0.01377   0.00549  -0.1137   0.8649   0.0514
  -3.250   0.1105   0.01346   0.00516  -0.1137   0.8594   0.0547
  -3.000   0.1370   0.01321   0.00489  -0.1135   0.8533   0.0591
  -2.750   0.1678   0.01291   0.00454  -0.1140   0.8488   0.0667
  -2.500   0.1929   0.01271   0.00431  -0.1134   0.8420   0.0779
  -2.250   0.2208   0.01242   0.00402  -0.1135   0.8361   0.0925
  -2.000   0.2484   0.01205   0.00381  -0.1136   0.8308   0.1279
  -1.750   0.2727   0.01175   0.00376  -0.1130   0.8237   0.2064
  -1.500   0.3018   0.01148   0.00363  -0.1133   0.8186   0.2594
  -1.250   0.3255   0.01130   0.00361  -0.1125   0.8111   0.3085
  -1.000   0.3516   0.01099   0.00361  -0.1123   0.8053   0.3990
  -0.750   0.3761   0.01079   0.00363  -0.1116   0.7986   0.4734
  -0.500   0.4016   0.01066   0.00362  -0.1110   0.7918   0.5237
  -0.250   0.4281   0.01054   0.00360  -0.1106   0.7858   0.5693
   0.000   0.4517   0.01039   0.00363  -0.1096   0.7784   0.6254
   0.250   0.4784   0.01018   0.00359  -0.1092   0.7729   0.6896
   0.500   0.5335   0.00974   0.00371  -0.1145   0.7670   0.9129
   0.750   0.5887   0.00974   0.00367  -0.1205   0.7614   1.0000
   1.000   0.6131   0.00982   0.00369  -0.1198   0.7537   1.0000
   1.250   0.6384   0.00988   0.00367  -0.1191   0.7448   1.0000
   1.500   0.6613   0.00995   0.00368  -0.1179   0.7331   1.0000
   1.750   0.6847   0.01001   0.00367  -0.1169   0.7202   1.0000
   2.000   0.7079   0.01008   0.00366  -0.1157   0.7058   1.0000
   2.250   0.7310   0.01016   0.00366  -0.1145   0.6907   1.0000
   2.500   0.7543   0.01027   0.00371  -0.1134   0.6770   1.0000
   2.750   0.7783   0.01039   0.00378  -0.1126   0.6662   1.0000
   3.000   0.8022   0.01052   0.00387  -0.1117   0.6555   1.0000
   3.250   0.8258   0.01066   0.00402  -0.1107   0.6455   1.0000
   3.500   0.8499   0.01080   0.00415  -0.1099   0.6363   1.0000
   3.750   0.8736   0.01096   0.00430  -0.1090   0.6265   1.0000
   4.000   0.8965   0.01112   0.00448  -0.1079   0.6148   1.0000
   4.250   0.9188   0.01129   0.00464  -0.1067   0.6009   1.0000
   4.500   0.9401   0.01149   0.00481  -0.1053   0.5835   1.0000
   4.750   0.9609   0.01170   0.00499  -0.1037   0.5650   1.0000
   5.000   0.9810   0.01191   0.00520  -0.1021   0.5440   1.0000
   5.250   0.9994   0.01218   0.00541  -0.1002   0.5171   1.0000
   5.500   1.0157   0.01251   0.00564  -0.0978   0.4816   1.0000
   5.750   1.0276   0.01300   0.00592  -0.0946   0.4361   1.0000
   6.000   1.0381   0.01358   0.00631  -0.0913   0.3926   1.0000
   6.250   1.0461   0.01430   0.00678  -0.0877   0.3475   1.0000
   6.500   1.0538   0.01501   0.00729  -0.0840   0.3099   1.0000
   6.750   1.0624   0.01571   0.00782  -0.0806   0.2759   1.0000
   7.000   1.0717   0.01642   0.00838  -0.0774   0.2436   1.0000
   7.250   1.0816   0.01716   0.00896  -0.0744   0.2112   1.0000
   7.500   1.0915   0.01794   0.00960  -0.0716   0.1729   1.0000
   7.750   1.0993   0.01890   0.01031  -0.0685   0.1352   1.0000
   8.000   1.1099   0.01974   0.01106  -0.0660   0.1169   1.0000
   8.250   1.1218   0.02054   0.01183  -0.0636   0.1021   1.0000
   8.500   1.1346   0.02131   0.01258  -0.0615   0.0813   1.0000
   8.750   1.1441   0.02231   0.01343  -0.0591   0.0603   1.0000
   9.000   1.1530   0.02337   0.01444  -0.0566   0.0460   1.0000
   9.250   1.1625   0.02442   0.01548  -0.0542   0.0335   1.0000
   9.500   1.1715   0.02554   0.01656  -0.0519   0.0256   1.0000
   9.750   1.1808   0.02668   0.01772  -0.0497   0.0223   1.0000
  10.000   1.1899   0.02785   0.01895  -0.0476   0.0206   1.0000
  10.250   1.1993   0.02903   0.02024  -0.0456   0.0192   1.0000
  10.500   1.2079   0.03029   0.02160  -0.0436   0.0181   1.0000
  10.750   1.2145   0.03173   0.02313  -0.0416   0.0168   1.0000
  11.000   1.2179   0.03348   0.02499  -0.0394   0.0159   1.0000
  11.250   1.2223   0.03519   0.02681  -0.0375   0.0154   1.0000
  11.500   1.2281   0.03683   0.02858  -0.0357   0.0150   1.0000
  11.750   1.2331   0.03859   0.03047  -0.0341   0.0146   1.0000
  12.000   1.2368   0.04053   0.03253  -0.0324   0.0142   1.0000
  12.250   1.2408   0.04251   0.03463  -0.0310   0.0139   1.0000
  12.500   1.2446   0.04456   0.03680  -0.0296   0.0134   1.0000
  12.750   1.2484   0.04665   0.03900  -0.0284   0.0130   1.0000
  13.000   1.2514   0.04889   0.04134  -0.0273   0.0125   1.0000
  13.250   1.2541   0.05120   0.04378  -0.0264   0.0121   1.0000
  13.500   1.2556   0.05373   0.04641  -0.0255   0.0118   1.0000
  13.750   1.2548   0.05662   0.04939  -0.0247   0.0114   1.0000
  14.000   1.2552   0.05958   0.05245  -0.0239   0.0112   1.0000
  14.250   1.2571   0.06230   0.05535  -0.0234   0.0110   1.0000
  14.500   1.2580   0.06523   0.05845  -0.0230   0.0109   1.0000
  14.750   1.2576   0.06841   0.06182  -0.0229   0.0108   1.0000
  15.000   1.2555   0.07189   0.06549  -0.0229   0.0106   1.0000
  15.250   1.2525   0.07558   0.06937  -0.0232   0.0105   1.0000
  15.500   1.2473   0.07968   0.07368  -0.0238   0.0104   1.0000
  15.750   1.2407   0.08414   0.07834  -0.0247   0.0103   1.0000
  16.000   1.2327   0.08896   0.08337  -0.0260   0.0102   1.0000
  16.250   1.2231   0.09419   0.08880  -0.0278   0.0101   1.0000
  16.500   1.2117   0.09995   0.09477  -0.0301   0.0101   1.0000
  16.750   1.2000   0.10602   0.10104  -0.0328   0.0101   1.0000
  17.000   1.1858   0.11285   0.10808  -0.0362   0.0100   1.0000
  17.250   1.1713   0.12006   0.11549  -0.0401   0.0100   1.0000
  17.500   1.1558   0.12783   0.12346  -0.0447   0.0101   1.0000
  17.750   1.1385   0.13649   0.13231  -0.0500   0.0101   1.0000
  18.000   1.1197   0.14597   0.14197  -0.0560   0.0101   1.0000
  18.250   1.0999   0.15628   0.15245  -0.0626   0.0103   1.0000
  18.500   1.0742   0.16912   0.16545  -0.0707   0.0104   1.0000
  18.750   1.0370   0.18762   0.18408  -0.0815   0.0108   1.0000
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