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GOE 693 AIRFOIL (goe693-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 693 AIRFOIL (goe693-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.26 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe693-il-1000000-n5.txt
Download as CSV file: xf-goe693-il-1000000-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 =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.7208   0.12992   0.12797  -0.0247   1.0000   0.0143
 -16.250  -0.7944   0.11134   0.10925  -0.0347   1.0000   0.0146
 -16.000  -1.2087   0.03474   0.03154  -0.0922   1.0000   0.0107
 -15.750  -1.2203   0.03204   0.02868  -0.0907   1.0000   0.0109
 -15.500  -1.2203   0.03009   0.02659  -0.0892   1.0000   0.0112
 -15.250  -1.2142   0.02848   0.02486  -0.0878   1.0000   0.0115
 -15.000  -1.2060   0.02714   0.02341  -0.0862   1.0000   0.0118
 -14.750  -1.1980   0.02600   0.02217  -0.0841   1.0000   0.0121
 -14.500  -1.1806   0.02471   0.02079  -0.0838   0.9984   0.0128
 -14.250  -1.1574   0.02356   0.01956  -0.0844   0.9963   0.0135
 -14.000  -1.1323   0.02257   0.01848  -0.0851   0.9948   0.0143
 -13.750  -1.1071   0.02169   0.01751  -0.0857   0.9927   0.0149
 -13.500  -1.0827   0.02087   0.01661  -0.0859   0.9898   0.0156
 -13.250  -1.0568   0.02014   0.01584  -0.0864   0.9872   0.0164
 -13.000  -1.0296   0.01950   0.01514  -0.0869   0.9849   0.0171
 -12.750  -1.0036   0.01891   0.01448  -0.0872   0.9820   0.0179
 -12.500  -0.9785   0.01836   0.01385  -0.0871   0.9781   0.0184
 -12.250  -0.9522   0.01784   0.01325  -0.0873   0.9747   0.0188
 -12.000  -0.9268   0.01726   0.01262  -0.0873   0.9714   0.0196
 -11.750  -0.9021   0.01682   0.01216  -0.0870   0.9667   0.0203
 -11.500  -0.8768   0.01642   0.01171  -0.0868   0.9623   0.0209
 -11.250  -0.8514   0.01603   0.01126  -0.0865   0.9584   0.0216
 -11.000  -0.8265   0.01564   0.01080  -0.0861   0.9533   0.0221
 -10.750  -0.8014   0.01528   0.01036  -0.0858   0.9481   0.0225
 -10.500  -0.7758   0.01495   0.00996  -0.0854   0.9433   0.0229
 -10.250  -0.7505   0.01455   0.00950  -0.0851   0.9376   0.0234
 -10.000  -0.7258   0.01407   0.00896  -0.0847   0.9314   0.0241
  -9.750  -0.7001   0.01369   0.00854  -0.0844   0.9251   0.0247
  -9.500  -0.6742   0.01337   0.00817  -0.0841   0.9173   0.0253
  -9.250  -0.6480   0.01308   0.00782  -0.0838   0.9097   0.0259
  -9.000  -0.6217   0.01279   0.00747  -0.0836   0.9006   0.0265
  -8.750  -0.5952   0.01252   0.00712  -0.0833   0.8905   0.0270
  -8.500  -0.5686   0.01227   0.00679  -0.0831   0.8790   0.0275
  -8.250  -0.5420   0.01204   0.00647  -0.0828   0.8659   0.0279
  -8.000  -0.5154   0.01179   0.00612  -0.0826   0.8523   0.0283
  -7.750  -0.4891   0.01142   0.00566  -0.0823   0.8391   0.0292
  -7.500  -0.4622   0.01115   0.00531  -0.0822   0.8261   0.0298
  -7.250  -0.4351   0.01091   0.00500  -0.0821   0.8135   0.0304
  -7.000  -0.4078   0.01071   0.00472  -0.0819   0.8013   0.0310
  -6.750  -0.3804   0.01052   0.00446  -0.0819   0.7898   0.0316
  -6.500  -0.3526   0.01034   0.00421  -0.0818   0.7795   0.0323
  -6.250  -0.3247   0.01018   0.00399  -0.0818   0.7706   0.0330
  -6.000  -0.2968   0.01002   0.00377  -0.0818   0.7616   0.0336
  -5.750  -0.2687   0.00986   0.00355  -0.0818   0.7535   0.0341
  -5.500  -0.2409   0.00966   0.00330  -0.0818   0.7452   0.0356
  -5.250  -0.2127   0.00949   0.00311  -0.0819   0.7382   0.0371
  -5.000  -0.1845   0.00934   0.00293  -0.0819   0.7315   0.0386
  -4.750  -0.1563   0.00922   0.00277  -0.0820   0.7247   0.0401
  -4.500  -0.1279   0.00909   0.00261  -0.0821   0.7166   0.0424
  -4.250  -0.0998   0.00896   0.00245  -0.0821   0.7087   0.0460
  -4.000  -0.0713   0.00884   0.00232  -0.0822   0.7016   0.0499
  -3.750  -0.0432   0.00871   0.00219  -0.0823   0.6947   0.0563
  -3.500  -0.0147   0.00859   0.00208  -0.0824   0.6881   0.0635
  -3.250   0.0138   0.00849   0.00199  -0.0825   0.6812   0.0716
  -3.000   0.0422   0.00841   0.00192  -0.0826   0.6738   0.0798
  -2.750   0.0707   0.00834   0.00184  -0.0827   0.6650   0.0861
  -2.500   0.0993   0.00829   0.00178  -0.0828   0.6578   0.0915
  -2.250   0.1280   0.00826   0.00172  -0.0829   0.6505   0.0941
  -2.000   0.1566   0.00821   0.00166  -0.0831   0.6432   0.0990
  -1.750   0.1851   0.00817   0.00161  -0.0832   0.6339   0.1039
  -1.500   0.2136   0.00816   0.00156  -0.0833   0.6235   0.1076
  -1.250   0.2420   0.00815   0.00152  -0.0834   0.6140   0.1121
  -1.000   0.2707   0.00809   0.00148  -0.0835   0.6058   0.1197
  -0.500   0.3277   0.00803   0.00143  -0.0838   0.5894   0.1353
  -0.250   0.3561   0.00801   0.00141  -0.0839   0.5814   0.1453
   0.000   0.3845   0.00797   0.00140  -0.0840   0.5717   0.1638
   0.250   0.4127   0.00793   0.00141  -0.0841   0.5613   0.1870
   0.500   0.4407   0.00790   0.00142  -0.0842   0.5492   0.2141
   0.750   0.4685   0.00788   0.00144  -0.0842   0.5357   0.2455
   1.000   0.4962   0.00786   0.00147  -0.0843   0.5202   0.2831
   1.250   0.5236   0.00785   0.00151  -0.0843   0.5008   0.3299
   1.500   0.5500   0.00785   0.00159  -0.0842   0.4748   0.3972
   1.750   0.5750   0.00787   0.00172  -0.0838   0.4355   0.4983
   2.000   0.5992   0.00794   0.00189  -0.0834   0.3930   0.6038
   2.250   0.6238   0.00796   0.00204  -0.0829   0.3642   0.7008
   2.500   0.6484   0.00790   0.00218  -0.0823   0.3461   0.7918
   2.750   0.6690   0.00777   0.00234  -0.0805   0.3316   0.9125
   3.000   0.7061   0.00790   0.00248  -0.0825   0.3189   0.9862
   3.250   0.7465   0.00807   0.00260  -0.0854   0.3082   1.0000
   3.500   0.7718   0.00823   0.00271  -0.0849   0.2997   1.0000
   3.750   0.7975   0.00837   0.00281  -0.0845   0.2914   1.0000
   4.000   0.8231   0.00853   0.00293  -0.0841   0.2821   1.0000
   4.250   0.8485   0.00873   0.00306  -0.0837   0.2696   1.0000
   4.500   0.8734   0.00898   0.00322  -0.0832   0.2497   1.0000
   4.750   0.8951   0.00948   0.00349  -0.0823   0.2039   1.0000
   5.000   0.9182   0.00988   0.00376  -0.0815   0.1800   1.0000
   5.250   0.9429   0.01014   0.00396  -0.0810   0.1707   1.0000
   5.500   0.9686   0.01033   0.00414  -0.0807   0.1667   1.0000
   5.750   0.9939   0.01054   0.00434  -0.0803   0.1628   1.0000
   6.000   1.0190   0.01077   0.00455  -0.0799   0.1583   1.0000
   6.250   1.0444   0.01097   0.00475  -0.0795   0.1547   1.0000
   6.500   1.0698   0.01116   0.00495  -0.0792   0.1511   1.0000
   6.750   1.0942   0.01143   0.00519  -0.0786   0.1450   1.0000
   7.000   1.1186   0.01168   0.00543  -0.0781   0.1399   1.0000
   7.250   1.1434   0.01189   0.00565  -0.0777   0.1344   1.0000
   7.500   1.1662   0.01224   0.00593  -0.0770   0.1204   1.0000
   8.000   1.2071   0.01323   0.00668  -0.0747   0.0846   1.0000
   8.250   1.2285   0.01363   0.00705  -0.0738   0.0779   1.0000
   8.500   1.2507   0.01395   0.00739  -0.0729   0.0736   1.0000
   8.750   1.2712   0.01437   0.00779  -0.0718   0.0683   1.0000
   9.000   1.2921   0.01473   0.00815  -0.0708   0.0632   1.0000
   9.250   1.3047   0.01552   0.00879  -0.0684   0.0413   1.0000
   9.500   1.3146   0.01633   0.00950  -0.0655   0.0273   1.0000
   9.750   1.3287   0.01694   0.01011  -0.0634   0.0217   1.0000
  10.000   1.3443   0.01751   0.01068  -0.0616   0.0187   1.0000
  10.250   1.3598   0.01810   0.01128  -0.0599   0.0166   1.0000
  10.500   1.3756   0.01869   0.01189  -0.0582   0.0152   1.0000
  10.750   1.3903   0.01936   0.01258  -0.0565   0.0138   1.0000
  11.000   1.4057   0.02000   0.01326  -0.0550   0.0130   1.0000
  11.250   1.4208   0.02068   0.01397  -0.0535   0.0123   1.0000
  11.500   1.4348   0.02144   0.01476  -0.0519   0.0116   1.0000
  11.750   1.4481   0.02228   0.01563  -0.0503   0.0109   1.0000
  12.000   1.4605   0.02320   0.01659  -0.0487   0.0104   1.0000
  12.250   1.4740   0.02406   0.01751  -0.0473   0.0101   1.0000
  12.500   1.4868   0.02500   0.01850  -0.0459   0.0097   1.0000
  12.750   1.4989   0.02602   0.01957  -0.0446   0.0094   1.0000
  13.000   1.5100   0.02713   0.02072  -0.0432   0.0090   1.0000
  13.250   1.5203   0.02835   0.02199  -0.0419   0.0087   1.0000
  13.500   1.5295   0.02970   0.02339  -0.0406   0.0083   1.0000
  13.750   1.5368   0.03123   0.02498  -0.0393   0.0080   1.0000
  14.000   1.5461   0.03264   0.02646  -0.0382   0.0078   1.0000
  14.250   1.5547   0.03415   0.02803  -0.0372   0.0076   1.0000
  14.500   1.5622   0.03579   0.02974  -0.0362   0.0074   1.0000
  14.750   1.5689   0.03753   0.03155  -0.0353   0.0072   1.0000
  15.000   1.5746   0.03940   0.03349  -0.0344   0.0071   1.0000
  15.250   1.5796   0.04141   0.03557  -0.0336   0.0069   1.0000
  15.500   1.5836   0.04355   0.03779  -0.0330   0.0067   1.0000
  15.750   1.5866   0.04585   0.04015  -0.0323   0.0066   1.0000
  16.000   1.5885   0.04833   0.04271  -0.0318   0.0064   1.0000
  16.250   1.5893   0.05100   0.04546  -0.0314   0.0063   1.0000
  16.500   1.5885   0.05393   0.04847  -0.0311   0.0062   1.0000
  16.750   1.5856   0.05716   0.05179  -0.0309   0.0060   1.0000
  17.000   1.5809   0.06072   0.05545  -0.0310   0.0059   1.0000
  17.250   1.5789   0.06404   0.05886  -0.0311   0.0059   1.0000
  17.500   1.5756   0.06762   0.06254  -0.0315   0.0058   1.0000
  17.750   1.5706   0.07147   0.06649  -0.0320   0.0058   1.0000
  18.000   1.5647   0.07555   0.07068  -0.0326   0.0057   1.0000
  18.250   1.5578   0.07987   0.07510  -0.0335   0.0056   1.0000
  18.500   1.5495   0.08450   0.07985  -0.0346   0.0056   1.0000
  18.750   1.5397   0.08942   0.08487  -0.0359   0.0055   1.0000
  19.000   1.5292   0.09452   0.09009  -0.0373   0.0055   1.0000
  19.250   1.5169   0.10004   0.09572  -0.0391   0.0054   1.0000
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