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GOE 648 AIRFOIL (goe648-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 648 AIRFOIL (goe648-il)
Reynolds number: 500,000
Max Cl/Cd: 80.69 at α=7.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe648-il-500000-n5.txt
Download as CSV file: xf-goe648-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 648 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.6917   0.10926   0.10606  -0.0533   1.0000   0.0198
 -17.000  -0.7456   0.09593   0.09257  -0.0608   1.0000   0.0200
 -16.750  -0.7947   0.08433   0.08081  -0.0675   1.0000   0.0200
 -16.500  -0.8398   0.07405   0.07036  -0.0734   1.0000   0.0200
 -16.250  -0.8809   0.06468   0.06083  -0.0789   1.0000   0.0200
 -16.000  -0.9159   0.05631   0.05231  -0.0839   1.0000   0.0200
 -15.750  -0.9411   0.04953   0.04537  -0.0880   1.0000   0.0201
 -15.500  -0.9602   0.04402   0.03973  -0.0912   1.0000   0.0202
 -15.250  -0.9756   0.03952   0.03510  -0.0933   1.0000   0.0203
 -15.000  -0.9866   0.03609   0.03156  -0.0943   1.0000   0.0205
 -14.750  -0.9957   0.03347   0.02884  -0.0941   1.0000   0.0207
 -14.500  -1.0073   0.03133   0.02660  -0.0926   1.0000   0.0209
 -14.250  -1.0232   0.02969   0.02487  -0.0893   1.0000   0.0210
 -14.000  -1.0139   0.02834   0.02340  -0.0891   0.9981   0.0215
 -13.750  -0.9953   0.02714   0.02208  -0.0898   0.9946   0.0219
 -13.500  -0.9761   0.02607   0.02090  -0.0900   0.9910   0.0224
 -13.250  -0.9550   0.02495   0.01974  -0.0904   0.9870   0.0229
 -13.000  -0.9294   0.02402   0.01875  -0.0913   0.9840   0.0235
 -12.750  -0.9018   0.02319   0.01785  -0.0924   0.9819   0.0242
 -12.500  -0.8805   0.02247   0.01704  -0.0919   0.9773   0.0249
 -12.250  -0.8553   0.02172   0.01620  -0.0922   0.9736   0.0255
 -12.000  -0.8276   0.02095   0.01536  -0.0930   0.9709   0.0262
 -11.750  -0.7984   0.02020   0.01458  -0.0940   0.9690   0.0269
 -11.500  -0.7774   0.01961   0.01394  -0.0931   0.9625   0.0275
 -11.250  -0.7479   0.01898   0.01324  -0.0938   0.9585   0.0283
 -11.000  -0.7147   0.01836   0.01254  -0.0952   0.9556   0.0292
 -10.750  -0.6916   0.01779   0.01192  -0.0945   0.9481   0.0299
 -10.500  -0.6615   0.01719   0.01129  -0.0954   0.9437   0.0309
 -10.250  -0.6276   0.01664   0.01070  -0.0968   0.9406   0.0318
 -10.000  -0.6015   0.01620   0.01020  -0.0966   0.9336   0.0327
  -9.750  -0.5705   0.01574   0.00967  -0.0974   0.9281   0.0336
  -9.500  -0.5374   0.01518   0.00908  -0.0987   0.9236   0.0347
  -9.250  -0.5116   0.01478   0.00866  -0.0983   0.9151   0.0357
  -9.000  -0.4801   0.01438   0.00820  -0.0991   0.9088   0.0370
  -8.750  -0.4520   0.01403   0.00779  -0.0991   0.9006   0.0381
  -8.500  -0.4234   0.01363   0.00735  -0.0993   0.8923   0.0394
  -8.250  -0.3963   0.01330   0.00699  -0.0991   0.8833   0.0407
  -8.000  -0.3676   0.01301   0.00662  -0.0992   0.8727   0.0423
  -7.750  -0.3421   0.01273   0.00628  -0.0986   0.8604   0.0438
  -7.500  -0.3161   0.01247   0.00598  -0.0981   0.8490   0.0456
  -7.250  -0.2901   0.01225   0.00569  -0.0975   0.8383   0.0477
  -7.000  -0.2651   0.01203   0.00543  -0.0968   0.8273   0.0498
  -6.750  -0.2396   0.01185   0.00519  -0.0961   0.8161   0.0523
  -6.500  -0.2145   0.01168   0.00497  -0.0953   0.8052   0.0549
  -6.250  -0.1893   0.01150   0.00477  -0.0946   0.7955   0.0578
  -6.000  -0.1640   0.01137   0.00458  -0.0939   0.7843   0.0611
  -5.750  -0.1391   0.01122   0.00439  -0.0931   0.7716   0.0642
  -5.500  -0.1142   0.01110   0.00422  -0.0922   0.7583   0.0674
  -5.250  -0.0891   0.01100   0.00404  -0.0914   0.7452   0.0702
  -5.000  -0.0646   0.01085   0.00386  -0.0905   0.7310   0.0733
  -4.750  -0.0400   0.01076   0.00371  -0.0896   0.7146   0.0766
  -4.500  -0.0159   0.01071   0.00355  -0.0886   0.6953   0.0795
  -4.250   0.0071   0.01062   0.00338  -0.0874   0.6741   0.0830
  -3.750   0.0550   0.01054   0.00313  -0.0854   0.6380   0.0896
  -3.500   0.0793   0.01045   0.00301  -0.0844   0.6231   0.0948
  -3.000   0.1279   0.01033   0.00282  -0.0826   0.5956   0.1106
  -2.500   0.1755   0.01015   0.00267  -0.0807   0.5662   0.1486
  -2.250   0.1995   0.01008   0.00261  -0.0798   0.5510   0.1706
  -2.000   0.2233   0.01000   0.00257  -0.0788   0.5371   0.1964
  -1.750   0.2472   0.00995   0.00254  -0.0779   0.5229   0.2234
  -1.500   0.2708   0.00991   0.00251  -0.0769   0.5077   0.2488
  -1.250   0.2946   0.00989   0.00250  -0.0759   0.4912   0.2756
  -1.000   0.3179   0.00989   0.00250  -0.0749   0.4728   0.3024
  -0.750   0.3407   0.00991   0.00251  -0.0738   0.4506   0.3288
  -0.500   0.3625   0.00996   0.00253  -0.0725   0.4241   0.3599
  -0.250   0.3836   0.01000   0.00258  -0.0711   0.3984   0.4037
   0.000   0.4047   0.01001   0.00266  -0.0697   0.3776   0.4575
   0.250   0.4266   0.01005   0.00275  -0.0684   0.3621   0.5030
   0.500   0.4489   0.01012   0.00284  -0.0672   0.3494   0.5388
   0.750   0.4722   0.01018   0.00293  -0.0661   0.3397   0.5679
   1.000   0.4946   0.01026   0.00302  -0.0649   0.3312   0.5972
   1.250   0.5180   0.01028   0.00311  -0.0638   0.3250   0.6259
   1.500   0.5400   0.01029   0.00321  -0.0625   0.3192   0.6636
   1.750   0.5600   0.01029   0.00336  -0.0607   0.3136   0.7193
   2.000   0.5816   0.01029   0.00347  -0.0592   0.3092   0.7651
   2.250   0.6040   0.01033   0.00358  -0.0579   0.3045   0.7969
   2.750   0.6501   0.01045   0.00384  -0.0556   0.2950   0.8664
   3.000   0.7085   0.01060   0.00409  -0.0621   0.2904   0.9248
   3.250   0.7860   0.01090   0.00436  -0.0728   0.2844   0.9803
   3.500   0.8205   0.01116   0.00456  -0.0743   0.2799   1.0000
   3.750   0.8405   0.01134   0.00469  -0.0727   0.2766   1.0000
   4.000   0.8621   0.01146   0.00480  -0.0714   0.2742   1.0000
   4.250   0.8834   0.01160   0.00493  -0.0700   0.2713   1.0000
   4.500   0.9042   0.01175   0.00507  -0.0685   0.2679   1.0000
   4.750   0.9245   0.01193   0.00522  -0.0670   0.2642   1.0000
   5.000   0.9439   0.01214   0.00539  -0.0653   0.2608   1.0000
   5.250   0.9635   0.01231   0.00555  -0.0637   0.2584   1.0000
   5.500   0.9834   0.01245   0.00570  -0.0620   0.2556   1.0000
   5.750   1.0029   0.01262   0.00586  -0.0604   0.2523   1.0000
   6.000   1.0219   0.01281   0.00604  -0.0587   0.2488   1.0000
   6.250   1.0404   0.01303   0.00624  -0.0569   0.2453   1.0000
   6.500   1.0595   0.01325   0.00645  -0.0553   0.2423   1.0000
   6.750   1.0803   0.01344   0.00665  -0.0539   0.2395   1.0000
   7.000   1.1005   0.01364   0.00687  -0.0526   0.2363   1.0000
   7.250   1.1200   0.01388   0.00710  -0.0511   0.2325   1.0000
   7.500   1.1388   0.01416   0.00736  -0.0496   0.2288   1.0000
   7.750   1.1585   0.01442   0.00762  -0.0482   0.2248   1.0000
   8.000   1.1785   0.01467   0.00788  -0.0469   0.2198   1.0000
   8.250   1.1967   0.01499   0.00818  -0.0454   0.2144   1.0000
   8.500   1.2153   0.01532   0.00850  -0.0440   0.2105   1.0000
   8.750   1.2350   0.01561   0.00882  -0.0428   0.2066   1.0000
   9.000   1.2536   0.01595   0.00916  -0.0414   0.2023   1.0000
   9.250   1.2705   0.01637   0.00957  -0.0399   0.1979   1.0000
   9.500   1.2892   0.01674   0.00995  -0.0386   0.1940   1.0000
   9.750   1.3070   0.01714   0.01037  -0.0373   0.1893   1.0000
  10.000   1.3229   0.01765   0.01086  -0.0358   0.1843   1.0000
  10.250   1.3400   0.01812   0.01134  -0.0345   0.1804   1.0000
  10.500   1.3572   0.01859   0.01185  -0.0332   0.1765   1.0000
  10.750   1.3730   0.01915   0.01241  -0.0318   0.1725   1.0000
  11.000   1.3874   0.01980   0.01306  -0.0304   0.1688   1.0000
  11.250   1.4042   0.02034   0.01364  -0.0292   0.1657   1.0000
  11.500   1.4196   0.02097   0.01430  -0.0280   0.1618   1.0000
  11.750   1.4335   0.02170   0.01505  -0.0267   0.1583   1.0000
  12.000   1.4466   0.02251   0.01587  -0.0253   0.1548   1.0000
  12.250   1.4618   0.02321   0.01662  -0.0242   0.1518   1.0000
  12.500   1.4758   0.02400   0.01745  -0.0231   0.1488   1.0000
  12.750   1.4879   0.02493   0.01841  -0.0219   0.1452   1.0000
  13.000   1.4983   0.02600   0.01950  -0.0207   0.1418   1.0000
  13.250   1.5118   0.02689   0.02045  -0.0198   0.1388   1.0000
  13.500   1.5234   0.02794   0.02154  -0.0188   0.1351   1.0000
  13.750   1.5324   0.02921   0.02283  -0.0177   0.1315   1.0000
  14.000   1.5417   0.03049   0.02415  -0.0167   0.1284   1.0000
  14.250   1.5522   0.03170   0.02543  -0.0159   0.1253   1.0000
  14.500   1.5592   0.03323   0.02699  -0.0150   0.1206   1.0000
  14.750   1.5643   0.03498   0.02877  -0.0141   0.1166   1.0000
  15.000   1.5708   0.03664   0.03049  -0.0135   0.1118   1.0000
  15.250   1.5710   0.03896   0.03281  -0.0127   0.1055   1.0000
  15.500   1.5753   0.04097   0.03488  -0.0123   0.1011   1.0000
  15.750   1.5728   0.04370   0.03763  -0.0118   0.0952   1.0000
  16.000   1.5701   0.04655   0.04052  -0.0116   0.0880   1.0000
  16.250   1.5638   0.04991   0.04392  -0.0115   0.0819   1.0000
  16.500   1.5546   0.05370   0.04774  -0.0117   0.0760   1.0000
  16.750   1.5409   0.05812   0.05220  -0.0121   0.0698   1.0000
  17.000   1.5289   0.06250   0.05665  -0.0127   0.0665   1.0000
  17.250   1.5146   0.06729   0.06151  -0.0136   0.0634   1.0000
  17.500   1.4996   0.07228   0.06660  -0.0146   0.0616   1.0000
  17.750   1.4848   0.07739   0.07181  -0.0158   0.0601   1.0000
  18.000   1.4705   0.08253   0.07706  -0.0172   0.0588   1.0000
  18.250   1.4543   0.08800   0.08264  -0.0188   0.0577   1.0000
  18.500   1.4351   0.09402   0.08877  -0.0206   0.0564   1.0000
  18.750   1.4182   0.09978   0.09464  -0.0225   0.0556   1.0000
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