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GOE 533 AIRFOIL (goe533-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 533 AIRFOIL (goe533-il)
Reynolds number: 1,000,000
Max Cl/Cd: 121.74 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe533-il-1000000-n5.txt
Download as CSV file: xf-goe533-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 533 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.750  -0.8134   0.04213   0.03956  -0.0878   1.0000   0.0190
 -13.500  -0.8402   0.03622   0.03347  -0.0922   1.0000   0.0190
 -13.250  -0.8437   0.03178   0.02885  -0.0985   0.9918   0.0191
 -12.750  -0.8043   0.02723   0.02401  -0.1053   0.9763   0.0195
 -12.500  -0.7734   0.02606   0.02276  -0.1081   0.9712   0.0197
 -12.250  -0.7415   0.02495   0.02157  -0.1108   0.9636   0.0198
 -12.000  -0.7081   0.02397   0.02050  -0.1134   0.9537   0.0199
 -11.750  -0.6747   0.02315   0.01959  -0.1157   0.9382   0.0201
 -11.500  -0.6476   0.02239   0.01868  -0.1167   0.9144   0.0203
 -11.250  -0.6264   0.02172   0.01783  -0.1163   0.8848   0.0205
 -11.000  -0.6072   0.02111   0.01702  -0.1154   0.8518   0.0207
 -10.750  -0.5886   0.02041   0.01610  -0.1144   0.8175   0.0209
 -10.500  -0.5694   0.01977   0.01522  -0.1134   0.7818   0.0211
 -10.250  -0.5493   0.01910   0.01432  -0.1125   0.7492   0.0213
 -10.000  -0.5280   0.01843   0.01344  -0.1118   0.7232   0.0215
  -9.750  -0.5056   0.01780   0.01263  -0.1113   0.7023   0.0217
  -9.500  -0.4820   0.01727   0.01194  -0.1108   0.6854   0.0219
  -9.250  -0.4578   0.01678   0.01131  -0.1104   0.6719   0.0221
  -9.000  -0.4329   0.01630   0.01070  -0.1100   0.6606   0.0223
  -8.750  -0.4078   0.01582   0.01010  -0.1097   0.6512   0.0224
  -8.500  -0.3824   0.01536   0.00954  -0.1094   0.6424   0.0225
  -8.250  -0.3573   0.01477   0.00884  -0.1091   0.6355   0.0227
  -8.000  -0.3321   0.01414   0.00813  -0.1088   0.6289   0.0230
  -7.750  -0.3062   0.01371   0.00762  -0.1085   0.6226   0.0232
  -7.500  -0.2796   0.01334   0.00721  -0.1083   0.6176   0.0234
  -7.250  -0.2527   0.01302   0.00684  -0.1081   0.6123   0.0236
  -7.000  -0.2259   0.01272   0.00649  -0.1079   0.6070   0.0238
  -6.750  -0.1989   0.01245   0.00616  -0.1077   0.6020   0.0240
  -6.500  -0.1714   0.01218   0.00586  -0.1076   0.5976   0.0243
  -6.250  -0.1440   0.01194   0.00557  -0.1075   0.5925   0.0247
  -6.000  -0.1168   0.01169   0.00526  -0.1073   0.5873   0.0250
  -5.750  -0.0894   0.01142   0.00495  -0.1071   0.5825   0.0252
  -5.500  -0.0618   0.01117   0.00465  -0.1070   0.5776   0.0254
  -5.250  -0.0342   0.01094   0.00438  -0.1068   0.5728   0.0257
  -5.000  -0.0066   0.01072   0.00411  -0.1067   0.5682   0.0260
  -4.750   0.0213   0.01052   0.00387  -0.1066   0.5640   0.0262
  -4.500   0.0493   0.01033   0.00366  -0.1065   0.5594   0.0264
  -4.250   0.0772   0.01017   0.00345  -0.1063   0.5541   0.0266
  -4.000   0.1047   0.00994   0.00318  -0.1062   0.5495   0.0269
  -3.750   0.1328   0.00972   0.00294  -0.1061   0.5453   0.0274
  -3.500   0.1609   0.00957   0.00277  -0.1061   0.5396   0.0278
  -3.250   0.1888   0.00946   0.00262  -0.1060   0.5335   0.0283
  -3.000   0.2171   0.00935   0.00249  -0.1059   0.5282   0.0288
  -2.750   0.2454   0.00925   0.00238  -0.1058   0.5223   0.0294
  -2.500   0.2734   0.00918   0.00227  -0.1057   0.5161   0.0300
  -2.250   0.3017   0.00910   0.00216  -0.1057   0.5099   0.0305
  -2.000   0.3298   0.00904   0.00207  -0.1056   0.5019   0.0310
  -1.750   0.3578   0.00898   0.00197  -0.1055   0.4943   0.0317
  -1.500   0.3858   0.00892   0.00189  -0.1054   0.4856   0.0327
  -1.250   0.4138   0.00890   0.00183  -0.1052   0.4764   0.0338
  -1.000   0.4414   0.00891   0.00179  -0.1051   0.4639   0.0351
  -0.750   0.4691   0.00893   0.00176  -0.1049   0.4521   0.0366
  -0.500   0.4969   0.00893   0.00174  -0.1048   0.4428   0.0400
  -0.250   0.5246   0.00894   0.00173  -0.1047   0.4341   0.0467
   0.000   0.5522   0.00881   0.00172  -0.1046   0.4262   0.0926
   0.250   0.5797   0.00881   0.00173  -0.1045   0.4172   0.1166
   0.500   0.6071   0.00863   0.00174  -0.1045   0.4103   0.1954
   0.750   0.6343   0.00847   0.00176  -0.1044   0.4030   0.2815
   1.000   0.6610   0.00819   0.00183  -0.1044   0.3967   0.4189
   1.250   0.6884   0.00818   0.00191  -0.1043   0.3895   0.4692
   1.500   0.7156   0.00821   0.00199  -0.1041   0.3821   0.5066
   1.750   0.7430   0.00821   0.00206  -0.1039   0.3755   0.5410
   2.000   0.7700   0.00826   0.00216  -0.1037   0.3680   0.5714
   2.250   0.7971   0.00830   0.00227  -0.1035   0.3610   0.6092
   2.500   0.8242   0.00838   0.00238  -0.1033   0.3540   0.6348
   2.750   0.8513   0.00849   0.00248  -0.1031   0.3483   0.6493
   3.000   0.8789   0.00858   0.00257  -0.1030   0.3435   0.6613
   3.250   0.9060   0.00868   0.00267  -0.1028   0.3383   0.6718
   3.500   0.9329   0.00880   0.00278  -0.1026   0.3331   0.6816
   3.750   0.9602   0.00889   0.00289  -0.1024   0.3292   0.6935
   4.000   0.9871   0.00898   0.00300  -0.1022   0.3245   0.7069
   4.250   1.0135   0.00912   0.00314  -0.1019   0.3184   0.7174
   4.500   1.0402   0.00923   0.00326  -0.1017   0.3131   0.7266
   4.750   1.0666   0.00935   0.00339  -0.1014   0.3072   0.7365
   5.000   1.0922   0.00952   0.00355  -0.1011   0.2990   0.7481
   5.250   1.1179   0.00966   0.00371  -0.1007   0.2902   0.7641
   5.500   1.1426   0.00979   0.00388  -0.1001   0.2833   0.7913
   5.750   1.1699   0.00961   0.00405  -0.1000   0.2768   0.9536
   6.000   1.1972   0.00985   0.00424  -0.1000   0.2675   1.0000
   6.250   1.2218   0.01011   0.00445  -0.0995   0.2558   1.0000
   6.500   1.2452   0.01045   0.00470  -0.0989   0.2402   1.0000
   6.750   1.2678   0.01083   0.00499  -0.0981   0.2226   1.0000
   7.000   1.2888   0.01131   0.00535  -0.0971   0.2012   1.0000
   7.250   1.3100   0.01175   0.00570  -0.0961   0.1867   1.0000
   7.500   1.3321   0.01211   0.00602  -0.0952   0.1780   1.0000
   7.750   1.3539   0.01247   0.00634  -0.0943   0.1708   1.0000
   8.000   1.3762   0.01278   0.00664  -0.0935   0.1656   1.0000
   8.250   1.3984   0.01308   0.00694  -0.0926   0.1615   1.0000
   8.500   1.4199   0.01340   0.00725  -0.0917   0.1579   1.0000
   8.750   1.4408   0.01373   0.00759  -0.0906   0.1541   1.0000
   9.000   1.4624   0.01400   0.00788  -0.0897   0.1518   1.0000
   9.250   1.4835   0.01428   0.00818  -0.0887   0.1494   1.0000
   9.500   1.5012   0.01462   0.00852  -0.0871   0.1449   1.0000
   9.750   1.5152   0.01508   0.00896  -0.0848   0.1382   1.0000
  10.000   1.5313   0.01545   0.00934  -0.0830   0.1319   1.0000
  10.250   1.5427   0.01604   0.00988  -0.0805   0.1203   1.0000
  10.500   1.5309   0.01769   0.01125  -0.0750   0.0807   1.0000
  10.750   1.5345   0.01874   0.01226  -0.0718   0.0702   1.0000
  11.000   1.5427   0.01961   0.01314  -0.0695   0.0650   1.0000
  11.250   1.5509   0.02055   0.01409  -0.0673   0.0612   1.0000
  11.500   1.5616   0.02139   0.01497  -0.0656   0.0590   1.0000
  11.750   1.5712   0.02236   0.01597  -0.0639   0.0570   1.0000
  12.000   1.5784   0.02354   0.01717  -0.0621   0.0547   1.0000
  12.250   1.5857   0.02479   0.01846  -0.0605   0.0524   1.0000
  12.500   1.5955   0.02594   0.01967  -0.0593   0.0513   1.0000
  12.750   1.6037   0.02727   0.02105  -0.0581   0.0499   1.0000
  13.000   1.6103   0.02881   0.02263  -0.0570   0.0483   1.0000
  13.250   1.6146   0.03063   0.02448  -0.0560   0.0462   1.0000
  13.500   1.6194   0.03248   0.02638  -0.0551   0.0445   1.0000
  13.750   1.6260   0.03426   0.02822  -0.0545   0.0434   1.0000
  14.000   1.6308   0.03625   0.03027  -0.0539   0.0418   1.0000
  14.250   1.6333   0.03852   0.03258  -0.0534   0.0400   1.0000
  14.500   1.6341   0.04101   0.03512  -0.0529   0.0383   1.0000
  14.750   1.6371   0.04333   0.03751  -0.0526   0.0370   1.0000
  15.000   1.6381   0.04591   0.04014  -0.0523   0.0350   1.0000
  15.250   1.6350   0.04897   0.04324  -0.0522   0.0324   1.0000
  15.500   1.6327   0.05204   0.04636  -0.0521   0.0294   1.0000
  15.750   1.6275   0.05553   0.04988  -0.0522   0.0262   1.0000
  16.000   1.6193   0.05950   0.05389  -0.0525   0.0225   1.0000
  16.250   1.6111   0.06361   0.05804  -0.0530   0.0198   1.0000
  16.500   1.6042   0.06768   0.06218  -0.0536   0.0181   1.0000
  16.750   1.5968   0.07194   0.06650  -0.0544   0.0167   1.0000
  17.000   1.5915   0.07601   0.07065  -0.0553   0.0158   1.0000
  17.250   1.5854   0.08028   0.07500  -0.0563   0.0151   1.0000
  17.500   1.5777   0.08486   0.07965  -0.0575   0.0143   1.0000
  17.750   1.5721   0.08923   0.08411  -0.0588   0.0138   1.0000
  18.000   1.5661   0.09374   0.08871  -0.0602   0.0132   1.0000
  18.250   1.5599   0.09833   0.09338  -0.0617   0.0129   1.0000
  18.500   1.5532   0.10303   0.09817  -0.0633   0.0124   1.0000
  18.750   1.5465   0.10781   0.10302  -0.0651   0.0119   1.0000
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