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GOE 693 AIRFOIL (goe693-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 693 AIRFOIL (goe693-il)
Reynolds number: 500,000
Max Cl/Cd: 87.21 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe693-il-500000-n5.txt
Download as CSV file: xf-goe693-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 693 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
  ------ -------- --------- --------- -------- -------- --------
 -14.250  -1.0128   0.03859   0.03521  -0.0888   1.0000   0.0181
 -14.000  -1.0304   0.03528   0.03171  -0.0878   1.0000   0.0183
 -13.750  -1.0345   0.03312   0.02937  -0.0859   1.0000   0.0186
 -13.500  -1.0348   0.03147   0.02758  -0.0836   1.0000   0.0190
 -13.250  -1.0306   0.03026   0.02630  -0.0812   1.0000   0.0194
 -13.000  -1.0227   0.02931   0.02528  -0.0790   0.9999   0.0198
 -12.750  -0.9973   0.02826   0.02413  -0.0801   0.9976   0.0204
 -12.500  -0.9715   0.02716   0.02290  -0.0812   0.9954   0.0211
 -12.250  -0.9455   0.02603   0.02161  -0.0823   0.9934   0.0218
 -12.000  -0.9203   0.02497   0.02038  -0.0830   0.9905   0.0225
 -11.750  -0.8930   0.02405   0.01927  -0.0840   0.9880   0.0230
 -11.500  -0.8660   0.02296   0.01810  -0.0851   0.9857   0.0238
 -11.250  -0.8366   0.02223   0.01730  -0.0863   0.9838   0.0245
 -11.000  -0.8108   0.02159   0.01659  -0.0865   0.9797   0.0251
 -10.750  -0.7829   0.02094   0.01584  -0.0872   0.9762   0.0258
 -10.500  -0.7540   0.02028   0.01506  -0.0880   0.9733   0.0266
 -10.250  -0.7278   0.01965   0.01431  -0.0882   0.9690   0.0273
 -10.000  -0.7013   0.01908   0.01360  -0.0883   0.9642   0.0279
  -9.750  -0.6745   0.01829   0.01270  -0.0886   0.9601   0.0285
  -9.500  -0.6506   0.01761   0.01197  -0.0883   0.9541   0.0293
  -9.250  -0.6247   0.01711   0.01141  -0.0882   0.9484   0.0300
  -9.000  -0.5985   0.01664   0.01088  -0.0880   0.9432   0.0307
  -8.750  -0.5735   0.01618   0.01033  -0.0876   0.9359   0.0314
  -8.500  -0.5477   0.01570   0.00975  -0.0874   0.9295   0.0321
  -8.250  -0.5224   0.01527   0.00924  -0.0869   0.9212   0.0329
  -8.000  -0.4965   0.01485   0.00871  -0.0866   0.9137   0.0335
  -7.750  -0.4708   0.01444   0.00821  -0.0862   0.9044   0.0339
  -7.500  -0.4456   0.01389   0.00758  -0.0858   0.8950   0.0346
  -7.250  -0.4200   0.01343   0.00704  -0.0854   0.8842   0.0355
  -7.000  -0.3938   0.01306   0.00662  -0.0851   0.8727   0.0364
  -6.750  -0.3673   0.01276   0.00623  -0.0848   0.8614   0.0374
  -6.500  -0.3406   0.01247   0.00585  -0.0845   0.8502   0.0384
  -6.250  -0.3139   0.01219   0.00548  -0.0843   0.8383   0.0393
  -6.000  -0.2868   0.01194   0.00514  -0.0841   0.8264   0.0403
  -5.750  -0.2598   0.01170   0.00480  -0.0839   0.8154   0.0413
  -5.500  -0.2328   0.01142   0.00446  -0.0837   0.8052   0.0432
  -5.250  -0.2054   0.01119   0.00419  -0.0836   0.7954   0.0452
  -5.000  -0.1778   0.01101   0.00394  -0.0835   0.7865   0.0475
  -4.750  -0.1502   0.01083   0.00370  -0.0834   0.7774   0.0503
  -4.500  -0.1225   0.01063   0.00348  -0.0834   0.7692   0.0549
  -4.250  -0.0947   0.01048   0.00328  -0.0834   0.7614   0.0597
  -4.000  -0.0668   0.01032   0.00313  -0.0834   0.7546   0.0669
  -3.750  -0.0388   0.01019   0.00300  -0.0834   0.7468   0.0748
  -3.500  -0.0108   0.01011   0.00288  -0.0834   0.7391   0.0820
  -3.250   0.0173   0.01002   0.00279  -0.0834   0.7307   0.0892
  -3.000   0.0455   0.00998   0.00268  -0.0834   0.7233   0.0941
  -2.750   0.0736   0.00987   0.00258  -0.0835   0.7158   0.1004
  -2.500   0.1018   0.00982   0.00249  -0.0835   0.7092   0.1058
  -2.250   0.1303   0.00976   0.00240  -0.0836   0.7022   0.1096
  -1.750   0.1865   0.00962   0.00224  -0.0836   0.6860   0.1225
  -1.250   0.2427   0.00949   0.00211  -0.0837   0.6699   0.1374
  -1.000   0.2706   0.00944   0.00205  -0.0837   0.6613   0.1476
  -0.750   0.2987   0.00937   0.00200  -0.0837   0.6514   0.1602
  -0.500   0.3266   0.00930   0.00197  -0.0838   0.6433   0.1806
  -0.250   0.3547   0.00920   0.00194  -0.0838   0.6365   0.2083
   0.000   0.3826   0.00911   0.00193  -0.0839   0.6300   0.2422
   0.250   0.4106   0.00898   0.00193  -0.0840   0.6225   0.2852
   0.500   0.4379   0.00885   0.00193  -0.0840   0.6145   0.3417
   0.750   0.4652   0.00861   0.00195  -0.0840   0.6059   0.4299
   1.000   0.4912   0.00828   0.00199  -0.0838   0.5977   0.5613
   1.250   0.5157   0.00788   0.00206  -0.0832   0.5886   0.7092
   1.500   0.5383   0.00759   0.00213  -0.0818   0.5791   0.8326
   1.750   0.5682   0.00752   0.00224  -0.0817   0.5676   0.9416
   2.000   0.6060   0.00761   0.00229  -0.0839   0.5541   0.9756
   2.250   0.6458   0.00776   0.00235  -0.0866   0.5360   0.9959
   2.500   0.6765   0.00792   0.00242  -0.0873   0.5150   1.0000
   2.750   0.7002   0.00814   0.00250  -0.0865   0.4884   1.0000
   3.000   0.7229   0.00846   0.00263  -0.0855   0.4519   1.0000
   3.250   0.7450   0.00885   0.00281  -0.0845   0.4136   1.0000
   3.500   0.7682   0.00919   0.00300  -0.0837   0.3852   1.0000
   3.750   0.7923   0.00946   0.00317  -0.0830   0.3671   1.0000
   4.000   0.8170   0.00970   0.00334  -0.0825   0.3524   1.0000
   4.250   0.8420   0.00992   0.00351  -0.0820   0.3406   1.0000
   4.500   0.8668   0.01016   0.00369  -0.0815   0.3292   1.0000
   4.750   0.8917   0.01039   0.00388  -0.0810   0.3188   1.0000
   5.000   0.9169   0.01060   0.00407  -0.0806   0.3095   1.0000
   5.250   0.9416   0.01084   0.00428  -0.0801   0.2991   1.0000
   5.500   0.9661   0.01110   0.00449  -0.0796   0.2865   1.0000
   5.750   0.9907   0.01136   0.00471  -0.0790   0.2731   1.0000
   6.000   1.0147   0.01164   0.00495  -0.0785   0.2578   1.0000
   6.250   1.0376   0.01200   0.00522  -0.0777   0.2350   1.0000
   6.500   1.0582   0.01252   0.00557  -0.0766   0.2022   1.0000
   6.750   1.0792   0.01300   0.00595  -0.0756   0.1846   1.0000
   7.000   1.1006   0.01343   0.00633  -0.0746   0.1737   1.0000
   7.250   1.1226   0.01381   0.00668  -0.0737   0.1659   1.0000
   7.500   1.1439   0.01421   0.00707  -0.0727   0.1589   1.0000
   7.750   1.1659   0.01456   0.00744  -0.0718   0.1532   1.0000
   8.000   1.1871   0.01494   0.00781  -0.0708   0.1449   1.0000
   8.250   1.2080   0.01533   0.00819  -0.0698   0.1375   1.0000
   8.500   1.2286   0.01571   0.00857  -0.0687   0.1284   1.0000
   8.750   1.2473   0.01617   0.00898  -0.0673   0.1120   1.0000
   9.000   1.2598   0.01688   0.00953  -0.0649   0.0903   1.0000
   9.250   1.2748   0.01746   0.01009  -0.0630   0.0832   1.0000
   9.500   1.2898   0.01806   0.01069  -0.0611   0.0764   1.0000
   9.750   1.3045   0.01871   0.01134  -0.0592   0.0687   1.0000
  10.000   1.3195   0.01935   0.01199  -0.0574   0.0601   1.0000
  10.250   1.3268   0.02050   0.01298  -0.0548   0.0394   1.0000
  10.500   1.3352   0.02162   0.01405  -0.0524   0.0289   1.0000
  10.750   1.3462   0.02261   0.01505  -0.0504   0.0240   1.0000
  11.000   1.3574   0.02361   0.01607  -0.0486   0.0209   1.0000
  11.250   1.3694   0.02458   0.01710  -0.0470   0.0189   1.0000
  11.500   1.3799   0.02570   0.01826  -0.0453   0.0173   1.0000
  11.750   1.3917   0.02675   0.01937  -0.0438   0.0164   1.0000
  12.000   1.4026   0.02790   0.02059  -0.0424   0.0155   1.0000
  12.250   1.4123   0.02918   0.02192  -0.0410   0.0147   1.0000
  12.500   1.4204   0.03063   0.02344  -0.0395   0.0139   1.0000
  12.750   1.4280   0.03217   0.02506  -0.0382   0.0133   1.0000
  13.000   1.4368   0.03364   0.02661  -0.0370   0.0128   1.0000
  13.250   1.4445   0.03526   0.02831  -0.0359   0.0123   1.0000
  13.500   1.4512   0.03700   0.03013  -0.0349   0.0119   1.0000
  13.750   1.4567   0.03889   0.03210  -0.0339   0.0115   1.0000
  14.000   1.4607   0.04098   0.03427  -0.0330   0.0112   1.0000
  14.250   1.4630   0.04329   0.03666  -0.0322   0.0109   1.0000
  14.500   1.4628   0.04591   0.03939  -0.0314   0.0106   1.0000
  14.750   1.4625   0.04865   0.04222  -0.0308   0.0103   1.0000
  15.000   1.4642   0.05125   0.04493  -0.0304   0.0102   1.0000
  15.250   1.4647   0.05404   0.04783  -0.0301   0.0100   1.0000
  15.500   1.4641   0.05703   0.05093  -0.0299   0.0098   1.0000
  15.750   1.4627   0.06021   0.05421  -0.0299   0.0095   1.0000
  16.000   1.4604   0.06361   0.05771  -0.0300   0.0093   1.0000
  16.250   1.4575   0.06717   0.06139  -0.0304   0.0091   1.0000
  16.500   1.4528   0.07105   0.06537  -0.0309   0.0090   1.0000
  16.750   1.4476   0.07510   0.06953  -0.0315   0.0088   1.0000
  17.000   1.4414   0.07941   0.07396  -0.0324   0.0087   1.0000
  17.250   1.4344   0.08396   0.07862  -0.0335   0.0085   1.0000
  17.500   1.4255   0.08886   0.08364  -0.0349   0.0084   1.0000
  17.750   1.4156   0.09402   0.08891  -0.0364   0.0083   1.0000
  18.000   1.4047   0.09947   0.09447  -0.0382   0.0082   1.0000
  18.250   1.3932   0.10508   0.10019  -0.0402   0.0081   1.0000
  18.500   1.3806   0.11093   0.10615  -0.0423   0.0081   1.0000
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