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GOE 600 AIRFOIL (goe600-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 600 AIRFOIL (goe600-il)
Reynolds number: 1,000,000
Max Cl/Cd: 86.04 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe600-il-1000000-n5.txt
Download as CSV file: xf-goe600-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 600 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -1.0598   0.09369   0.09089  -0.0215   1.0000   0.0055
 -17.000  -1.1221   0.07867   0.07566  -0.0297   1.0000   0.0054
 -16.750  -1.1667   0.06717   0.06397  -0.0363   1.0000   0.0053
 -16.500  -1.1959   0.05852   0.05513  -0.0416   1.0000   0.0053
 -16.250  -1.2159   0.05161   0.04807  -0.0460   1.0000   0.0053
 -16.000  -1.2279   0.04616   0.04247  -0.0494   1.0000   0.0053
 -15.750  -1.2353   0.04156   0.03773  -0.0523   1.0000   0.0054
 -15.500  -1.2383   0.03780   0.03384  -0.0545   1.0000   0.0054
 -15.250  -1.2379   0.03475   0.03066  -0.0560   1.0000   0.0055
 -15.000  -1.2358   0.03222   0.02802  -0.0567   1.0000   0.0055
 -14.750  -1.2318   0.03020   0.02589  -0.0568   1.0000   0.0056
 -14.500  -1.2308   0.02821   0.02379  -0.0560   1.0000   0.0057
 -14.250  -1.2283   0.02662   0.02209  -0.0544   1.0000   0.0058
 -14.000  -1.2232   0.02539   0.02078  -0.0523   1.0000   0.0059
 -13.750  -1.2126   0.02435   0.01966  -0.0507   1.0000   0.0061
 -13.500  -1.1983   0.02339   0.01863  -0.0496   1.0000   0.0062
 -13.250  -1.1822   0.02252   0.01769  -0.0486   1.0000   0.0064
 -13.000  -1.1647   0.02171   0.01681  -0.0476   1.0000   0.0065
 -12.750  -1.1462   0.02096   0.01598  -0.0468   1.0000   0.0067
 -12.500  -1.1268   0.02024   0.01520  -0.0460   1.0000   0.0069
 -12.250  -1.1068   0.01957   0.01447  -0.0453   1.0000   0.0071
 -12.000  -1.0830   0.01891   0.01375  -0.0453   0.9948   0.0073
 -11.750  -1.0560   0.01828   0.01304  -0.0459   0.9854   0.0075
 -11.500  -1.0294   0.01766   0.01234  -0.0463   0.9752   0.0076
 -11.250  -1.0050   0.01695   0.01157  -0.0463   0.9635   0.0080
 -11.000  -0.9817   0.01640   0.01095  -0.0459   0.9518   0.0084
 -10.750  -0.9587   0.01591   0.01040  -0.0453   0.9412   0.0088
 -10.500  -0.9354   0.01548   0.00990  -0.0447   0.9315   0.0092
 -10.250  -0.9114   0.01506   0.00942  -0.0442   0.9229   0.0096
 -10.000  -0.8872   0.01469   0.00896  -0.0437   0.9146   0.0100
  -9.750  -0.8628   0.01424   0.00845  -0.0434   0.9066   0.0106
  -9.500  -0.8384   0.01381   0.00796  -0.0429   0.8990   0.0113
  -9.250  -0.8129   0.01343   0.00753  -0.0427   0.8918   0.0120
  -9.000  -0.7873   0.01309   0.00713  -0.0425   0.8847   0.0127
  -8.750  -0.7611   0.01277   0.00675  -0.0423   0.8776   0.0134
  -8.500  -0.7354   0.01240   0.00634  -0.0421   0.8698   0.0150
  -8.250  -0.7091   0.01208   0.00599  -0.0420   0.8617   0.0167
  -8.000  -0.6828   0.01176   0.00564  -0.0418   0.8532   0.0192
  -7.750  -0.6560   0.01148   0.00533  -0.0418   0.8442   0.0222
  -7.500  -0.6293   0.01120   0.00504  -0.0417   0.8354   0.0262
  -7.250  -0.6021   0.01097   0.00477  -0.0417   0.8253   0.0292
  -7.000  -0.5748   0.01073   0.00453  -0.0417   0.8148   0.0328
  -6.750  -0.5472   0.01057   0.00431  -0.0417   0.8036   0.0348
  -6.500  -0.5199   0.01035   0.00405  -0.0417   0.7917   0.0379
  -6.250  -0.4923   0.01017   0.00383  -0.0418   0.7798   0.0407
  -6.000  -0.4643   0.01003   0.00363  -0.0419   0.7691   0.0427
  -5.750  -0.4364   0.00987   0.00342  -0.0419   0.7599   0.0454
  -5.500  -0.4085   0.00968   0.00320  -0.0420   0.7511   0.0492
  -5.250  -0.3803   0.00953   0.00301  -0.0422   0.7438   0.0527
  -5.000  -0.3521   0.00936   0.00283  -0.0423   0.7365   0.0584
  -4.750  -0.3242   0.00914   0.00263  -0.0425   0.7301   0.0698
  -4.500  -0.2964   0.00887   0.00248  -0.0426   0.7237   0.0977
  -4.250  -0.2677   0.00879   0.00237  -0.0428   0.7177   0.1044
  -4.000  -0.2391   0.00866   0.00225  -0.0430   0.7128   0.1123
  -3.750  -0.2102   0.00858   0.00215  -0.0433   0.7078   0.1167
  -3.500  -0.1814   0.00851   0.00206  -0.0435   0.7020   0.1212
  -3.250  -0.1526   0.00841   0.00196  -0.0437   0.6958   0.1272
  -3.000  -0.1238   0.00835   0.00187  -0.0440   0.6888   0.1322
  -2.750  -0.0950   0.00828   0.00179  -0.0442   0.6829   0.1383
  -2.500  -0.0660   0.00819   0.00171  -0.0445   0.6771   0.1452
  -2.250  -0.0372   0.00810   0.00163  -0.0447   0.6716   0.1554
  -2.000  -0.0085   0.00795   0.00155  -0.0449   0.6668   0.1752
  -1.750   0.0192   0.00756   0.00142  -0.0452   0.6610   0.2544
  -1.500   0.0473   0.00732   0.00135  -0.0454   0.6550   0.3080
  -1.250   0.0759   0.00715   0.00130  -0.0457   0.6492   0.3481
  -1.000   0.1047   0.00702   0.00127  -0.0460   0.6429   0.3803
  -0.750   0.1334   0.00693   0.00124  -0.0462   0.6377   0.4087
  -0.500   0.1624   0.00683   0.00123  -0.0465   0.6326   0.4349
  -0.250   0.1913   0.00676   0.00122  -0.0468   0.6266   0.4597
   0.000   0.2202   0.00670   0.00122  -0.0470   0.6209   0.4843
   0.250   0.2493   0.00664   0.00123  -0.0473   0.6143   0.5079
   0.750   0.3071   0.00662   0.00125  -0.0478   0.5964   0.5422
   1.000   0.3355   0.00667   0.00127  -0.0480   0.5758   0.5584
   1.250   0.3637   0.00673   0.00130  -0.0481   0.5490   0.5763
   1.500   0.3917   0.00684   0.00135  -0.0482   0.5198   0.5917
   1.750   0.4187   0.00706   0.00143  -0.0482   0.4734   0.6080
   2.000   0.4455   0.00730   0.00156  -0.0482   0.4321   0.6249
   2.500   0.5004   0.00756   0.00178  -0.0483   0.3868   0.6697
   2.750   0.5278   0.00764   0.00189  -0.0483   0.3684   0.6988
   3.000   0.5553   0.00771   0.00201  -0.0483   0.3529   0.7294
   3.250   0.5826   0.00777   0.00213  -0.0483   0.3385   0.7609
   3.500   0.6093   0.00782   0.00226  -0.0482   0.3239   0.8024
   3.750   0.6346   0.00788   0.00241  -0.0477   0.3051   0.8509
   4.000   0.6585   0.00801   0.00258  -0.0468   0.2829   0.8970
   4.250   0.6816   0.00823   0.00277  -0.0458   0.2553   0.9343
   4.500   0.7088   0.00846   0.00294  -0.0458   0.2333   0.9620
   4.750   0.7395   0.00878   0.00315  -0.0466   0.2080   0.9804
   5.000   0.7711   0.00909   0.00336  -0.0477   0.1858   0.9930
   5.250   0.8019   0.00938   0.00357  -0.0487   0.1695   1.0000
   5.500   0.8273   0.00963   0.00377  -0.0484   0.1562   1.0000
   5.750   0.8527   0.00991   0.00399  -0.0481   0.1425   1.0000
   6.000   0.8773   0.01027   0.00425  -0.0477   0.1236   1.0000
   6.250   0.9013   0.01067   0.00454  -0.0472   0.1019   1.0000
   6.500   0.9255   0.01106   0.00485  -0.0468   0.0875   1.0000
   6.750   0.9504   0.01138   0.00513  -0.0464   0.0792   1.0000
   7.000   0.9754   0.01169   0.00540  -0.0461   0.0730   1.0000
   7.250   1.0009   0.01193   0.00566  -0.0458   0.0688   1.0000
   7.500   1.0251   0.01229   0.00598  -0.0454   0.0607   1.0000
   7.750   1.0471   0.01283   0.00638  -0.0446   0.0410   1.0000
   8.000   1.0696   0.01331   0.00680  -0.0440   0.0323   1.0000
   8.250   1.0927   0.01373   0.00721  -0.0434   0.0284   1.0000
   8.500   1.1163   0.01408   0.00758  -0.0428   0.0261   1.0000
   8.750   1.1396   0.01444   0.00796  -0.0423   0.0244   1.0000
   9.000   1.1618   0.01487   0.00839  -0.0416   0.0223   1.0000
   9.250   1.1841   0.01527   0.00881  -0.0409   0.0206   1.0000
   9.500   1.2064   0.01566   0.00922  -0.0402   0.0190   1.0000
   9.750   1.2273   0.01612   0.00968  -0.0393   0.0170   1.0000
  10.000   1.2479   0.01658   0.01016  -0.0383   0.0156   1.0000
  10.250   1.2678   0.01704   0.01064  -0.0373   0.0143   1.0000
  10.500   1.2862   0.01757   0.01117  -0.0361   0.0129   1.0000
  10.750   1.3025   0.01809   0.01171  -0.0344   0.0119   1.0000
  11.000   1.3184   0.01862   0.01229  -0.0327   0.0112   1.0000
  11.250   1.3337   0.01923   0.01293  -0.0311   0.0104   1.0000
  11.500   1.3481   0.01992   0.01364  -0.0294   0.0097   1.0000
  11.750   1.3623   0.02066   0.01442  -0.0279   0.0091   1.0000
  12.000   1.3771   0.02137   0.01519  -0.0265   0.0088   1.0000
  12.250   1.3913   0.02216   0.01603  -0.0251   0.0084   1.0000
  12.500   1.4046   0.02303   0.01695  -0.0237   0.0080   1.0000
  12.750   1.4172   0.02398   0.01795  -0.0224   0.0077   1.0000
  13.000   1.4287   0.02503   0.01905  -0.0211   0.0073   1.0000
  13.250   1.4391   0.02621   0.02028  -0.0197   0.0070   1.0000
  13.500   1.4486   0.02749   0.02163  -0.0184   0.0067   1.0000
  13.750   1.4592   0.02871   0.02292  -0.0174   0.0066   1.0000
  14.000   1.4691   0.03004   0.02431  -0.0163   0.0064   1.0000
  14.250   1.4780   0.03148   0.02583  -0.0154   0.0062   1.0000
  14.500   1.4861   0.03303   0.02746  -0.0145   0.0060   1.0000
  14.750   1.4931   0.03473   0.02922  -0.0137   0.0058   1.0000
  15.000   1.4991   0.03658   0.03115  -0.0130   0.0056   1.0000
  15.250   1.5037   0.03859   0.03323  -0.0123   0.0055   1.0000
  15.500   1.5069   0.04079   0.03551  -0.0118   0.0054   1.0000
  15.750   1.5088   0.04319   0.03799  -0.0113   0.0052   1.0000
  16.000   1.5088   0.04583   0.04072  -0.0110   0.0051   1.0000
  16.250   1.5066   0.04883   0.04381  -0.0108   0.0050   1.0000
  16.500   1.5033   0.05208   0.04716  -0.0108   0.0049   1.0000
  16.750   1.5016   0.05525   0.05043  -0.0110   0.0048   1.0000
  17.000   1.4985   0.05866   0.05395  -0.0115   0.0048   1.0000
  17.250   1.4940   0.06241   0.05782  -0.0121   0.0047   1.0000
  17.500   1.4879   0.06649   0.06201  -0.0130   0.0047   1.0000
  17.750   1.4800   0.07098   0.06661  -0.0142   0.0046   1.0000
  18.000   1.4701   0.07590   0.07165  -0.0157   0.0046   1.0000
  18.250   1.4585   0.08124   0.07711  -0.0175   0.0046   1.0000
  18.500   1.4453   0.08700   0.08300  -0.0197   0.0045   1.0000
  18.750   1.4303   0.09314   0.08926  -0.0221   0.0045   1.0000
  19.000   1.4132   0.09971   0.09596  -0.0248   0.0045   1.0000
  19.250   1.3946   0.10667   0.10306  -0.0277   0.0044   1.0000
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