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GOE 512 AIRFOIL (goe512-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 512 AIRFOIL (goe512-il)
Reynolds number: 1,000,000
Max Cl/Cd: 95.86 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe512-il-1000000.txt
Download as CSV file: xf-goe512-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 512 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.6951   0.06222   0.05997  -0.0842   0.9933   0.0125
 -13.750  -0.8165   0.03877   0.03607  -0.1056   0.9842   0.0121
 -13.500  -0.8168   0.03369   0.03073  -0.1072   0.9810   0.0123
 -13.250  -0.8140   0.03100   0.02784  -0.1059   0.9763   0.0123
 -13.000  -0.7995   0.02865   0.02529  -0.1062   0.9739   0.0125
 -12.750  -0.7778   0.02704   0.02351  -0.1068   0.9724   0.0126
 -12.500  -0.7522   0.02582   0.02216  -0.1076   0.9715   0.0128
 -12.250  -0.7482   0.02415   0.02030  -0.1045   0.9666   0.0131
 -12.000  -0.7356   0.02267   0.01869  -0.1027   0.9628   0.0135
 -11.750  -0.7124   0.02159   0.01752  -0.1026   0.9610   0.0137
 -11.500  -0.6840   0.02082   0.01669  -0.1033   0.9598   0.0141
 -11.250  -0.6553   0.01988   0.01566  -0.1040   0.9589   0.0143
 -11.000  -0.6228   0.01908   0.01477  -0.1053   0.9581   0.0148
 -10.750  -0.5900   0.01823   0.01382  -0.1067   0.9574   0.0152
 -10.500  -0.5745   0.01769   0.01319  -0.1043   0.9526   0.0155
 -10.250  -0.5513   0.01701   0.01241  -0.1035   0.9492   0.0157
 -10.000  -0.5249   0.01608   0.01137  -0.1035   0.9472   0.0162
  -9.750  -0.4943   0.01532   0.01057  -0.1043   0.9459   0.0169
  -9.500  -0.4585   0.01483   0.01004  -0.1061   0.9449   0.0176
  -9.250  -0.4226   0.01426   0.00941  -0.1078   0.9436   0.0182
  -9.000  -0.3877   0.01377   0.00885  -0.1093   0.9421   0.0188
  -8.750  -0.3758   0.01352   0.00854  -0.1058   0.9353   0.0192
  -8.500  -0.3497   0.01281   0.00779  -0.1055   0.9316   0.0202
  -8.250  -0.3163   0.01247   0.00743  -0.1066   0.9289   0.0213
  -8.000  -0.2821   0.01212   0.00703  -0.1079   0.9259   0.0223
  -7.750  -0.2664   0.01192   0.00678  -0.1050   0.9176   0.0229
  -7.500  -0.2365   0.01132   0.00615  -0.1054   0.9128   0.0242
  -7.250  -0.2147   0.01110   0.00590  -0.1040   0.9049   0.0252
  -7.000  -0.1844   0.01085   0.00560  -0.1043   0.8980   0.0265
  -6.750  -0.1601   0.01054   0.00524  -0.1034   0.8888   0.0277
  -6.500  -0.1295   0.01022   0.00489  -0.1039   0.8806   0.0294
  -6.250  -0.1043   0.01009   0.00472  -0.1031   0.8688   0.0310
  -6.000  -0.0771   0.00994   0.00449  -0.1027   0.8565   0.0322
  -5.750  -0.0521   0.00963   0.00413  -0.1020   0.8434   0.0342
  -5.500  -0.0266   0.00953   0.00397  -0.1013   0.8298   0.0360
  -5.250  -0.0022   0.00948   0.00383  -0.1004   0.8156   0.0375
  -5.000   0.0198   0.00927   0.00355  -0.0989   0.8005   0.0397
  -4.750   0.0416   0.00919   0.00342  -0.0974   0.7844   0.0416
  -4.500   0.0622   0.00916   0.00331  -0.0956   0.7644   0.0434
  -4.250   0.0814   0.00909   0.00314  -0.0936   0.7425   0.0456
  -4.000   0.0985   0.00905   0.00300  -0.0911   0.7176   0.0480
  -3.750   0.1165   0.00907   0.00292  -0.0887   0.6930   0.0503
  -3.500   0.1343   0.00913   0.00286  -0.0864   0.6707   0.0521
  -3.250   0.1532   0.00902   0.00269  -0.0843   0.6539   0.0563
  -3.000   0.1741   0.00900   0.00262  -0.0826   0.6404   0.0596
  -2.750   0.1949   0.00897   0.00252  -0.0810   0.6274   0.0635
  -2.500   0.2149   0.00891   0.00243  -0.0791   0.6146   0.0689
  -2.250   0.2353   0.00890   0.00235  -0.0774   0.6022   0.0734
  -2.000   0.2559   0.00879   0.00225  -0.0757   0.5900   0.0833
  -1.750   0.2736   0.00863   0.00216  -0.0734   0.5769   0.1137
  -1.500   0.2882   0.00844   0.00209  -0.0705   0.5631   0.1637
  -1.250   0.3036   0.00835   0.00212  -0.0678   0.5477   0.2125
  -1.000   0.3227   0.00843   0.00215  -0.0658   0.5309   0.2327
  -0.750   0.3411   0.00854   0.00219  -0.0636   0.5087   0.2423
  -0.500   0.3607   0.00868   0.00224  -0.0617   0.4896   0.2497
  -0.250   0.3797   0.00881   0.00228  -0.0598   0.4716   0.2553
   0.000   0.4005   0.00894   0.00236  -0.0582   0.4588   0.2613
   0.250   0.4215   0.00907   0.00242  -0.0566   0.4481   0.2651
   0.500   0.4431   0.00920   0.00248  -0.0552   0.4391   0.2682
   0.750   0.4640   0.00926   0.00252  -0.0537   0.4318   0.2730
   1.000   0.4862   0.00934   0.00258  -0.0524   0.4250   0.2762
   1.250   0.5072   0.00946   0.00265  -0.0510   0.4181   0.2789
   1.500   0.5306   0.00953   0.00270  -0.0499   0.4132   0.2815
   1.750   0.5530   0.00964   0.00277  -0.0488   0.4076   0.2834
   2.000   0.5726   0.00969   0.00282  -0.0470   0.4021   0.2883
   2.250   0.5954   0.00975   0.00288  -0.0459   0.3975   0.2917
   2.500   0.6175   0.00981   0.00294  -0.0447   0.3924   0.2940
   2.750   0.6385   0.00992   0.00301  -0.0433   0.3869   0.2953
   3.000   0.6607   0.00999   0.00307  -0.0421   0.3822   0.2968
   3.250   0.6833   0.01006   0.00314  -0.0411   0.3767   0.2982
   3.500   0.7039   0.01015   0.00320  -0.0396   0.3707   0.3004
   3.750   0.7249   0.01022   0.00327  -0.0382   0.3649   0.3030
   4.000   0.7461   0.01029   0.00335  -0.0369   0.3583   0.3059
   4.250   0.7662   0.01042   0.00345  -0.0354   0.3511   0.3076
   4.500   0.7882   0.01050   0.00353  -0.0343   0.3441   0.3098
   4.750   0.8080   0.01066   0.00364  -0.0328   0.3352   0.3119
   5.000   0.8292   0.01078   0.00375  -0.0315   0.3261   0.3135
   5.250   0.8481   0.01094   0.00388  -0.0298   0.3154   0.3163
   5.500   0.8661   0.01114   0.00404  -0.0280   0.3033   0.3190
   5.750   0.8844   0.01135   0.00420  -0.0263   0.2912   0.3220
   6.000   0.9025   0.01157   0.00439  -0.0246   0.2798   0.3251
   6.250   0.9202   0.01182   0.00460  -0.0228   0.2701   0.3291
   6.500   0.9374   0.01205   0.00482  -0.0209   0.2618   0.3355
   6.750   0.9548   0.01227   0.00504  -0.0191   0.2548   0.3446
   7.000   1.1104   0.01191   0.00615  -0.0485   0.2410   0.9850
   7.250   1.1501   0.01225   0.00649  -0.0515   0.2376   0.9903
   7.500   1.1898   0.01264   0.00686  -0.0546   0.2340   0.9947
   7.750   1.2326   0.01305   0.00723  -0.0585   0.2291   0.9976
   8.000   1.2752   0.01335   0.00754  -0.0622   0.2260   0.9995
   8.250   1.2999   0.01356   0.00776  -0.0620   0.2231   1.0000
   8.500   1.3143   0.01379   0.00801  -0.0597   0.2201   1.0000
   8.750   1.3276   0.01407   0.00829  -0.0572   0.2175   1.0000
   9.000   1.3392   0.01442   0.00863  -0.0545   0.2142   1.0000
   9.250   1.3517   0.01476   0.00899  -0.0519   0.2117   1.0000
   9.500   1.3683   0.01497   0.00924  -0.0501   0.2104   1.0000
   9.750   1.3842   0.01521   0.00952  -0.0482   0.2086   1.0000
  10.000   1.3996   0.01549   0.00982  -0.0463   0.2062   1.0000
  10.250   1.4140   0.01582   0.01017  -0.0443   0.2037   1.0000
  10.500   1.4264   0.01625   0.01060  -0.0419   0.2001   1.0000
  10.750   1.4381   0.01673   0.01109  -0.0396   0.1969   1.0000
  11.000   1.4556   0.01698   0.01139  -0.0381   0.1952   1.0000
  11.250   1.4720   0.01729   0.01174  -0.0366   0.1919   1.0000
  11.500   1.4862   0.01771   0.01217  -0.0348   0.1880   1.0000
  11.750   1.4978   0.01827   0.01273  -0.0326   0.1838   1.0000
  12.000   1.5134   0.01867   0.01316  -0.0311   0.1800   1.0000
  12.250   1.5270   0.01918   0.01367  -0.0294   0.1732   1.0000
  12.500   1.5381   0.01983   0.01431  -0.0274   0.1650   1.0000
  12.750   1.5453   0.02073   0.01514  -0.0250   0.1515   1.0000
  13.000   1.5421   0.02224   0.01650  -0.0216   0.1306   1.0000
  13.250   1.5392   0.02383   0.01801  -0.0184   0.1153   1.0000
  13.500   1.5345   0.02564   0.01976  -0.0152   0.1009   1.0000
  13.750   1.5205   0.02821   0.02220  -0.0116   0.0800   1.0000
  14.000   1.4974   0.03170   0.02554  -0.0078   0.0551   1.0000
  14.250   1.4674   0.03615   0.02989  -0.0044   0.0301   1.0000
  14.500   1.4508   0.03985   0.03359  -0.0025   0.0193   1.0000
  14.750   1.4463   0.04261   0.03641  -0.0014   0.0169   1.0000
  15.000   1.4453   0.04514   0.03902  -0.0007   0.0160   1.0000
  15.250   1.4411   0.04808   0.04204  -0.0001   0.0149   1.0000
  15.500   1.4370   0.05109   0.04513   0.0004   0.0144   1.0000
  15.750   1.4286   0.05469   0.04883   0.0007   0.0136   1.0000
  16.000   1.4252   0.05780   0.05203   0.0008   0.0134   1.0000
  16.250   1.4197   0.06125   0.05557   0.0008   0.0129   1.0000
  16.500   1.4134   0.06486   0.05927   0.0006   0.0127   1.0000
  16.750   1.4049   0.06885   0.06336   0.0002   0.0124   1.0000
  17.000   1.3946   0.07318   0.06779  -0.0004   0.0121   1.0000
  17.250   1.3828   0.07779   0.07251  -0.0011   0.0119   1.0000
  17.500   1.3686   0.08279   0.07761  -0.0020   0.0115   1.0000
  17.750   1.3521   0.08821   0.08314  -0.0031   0.0113   1.0000
  18.000   1.3386   0.09329   0.08833  -0.0043   0.0112   1.0000
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