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GOE 682 AIRFOIL (goe682-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 682 AIRFOIL (goe682-il)
Reynolds number: 1,000,000
Max Cl/Cd: 112.64 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe682-il-1000000-n5.txt
Download as CSV file: xf-goe682-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 682 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -1.0685   0.03329   0.03067  -0.0951   1.0000   0.0118
 -14.500  -1.0787   0.03017   0.02737  -0.0935   1.0000   0.0120
 -14.250  -1.0642   0.02770   0.02474  -0.0948   0.9986   0.0125
 -14.000  -1.0417   0.02581   0.02269  -0.0966   0.9964   0.0132
 -13.750  -1.0170   0.02426   0.02100  -0.0981   0.9943   0.0137
 -13.500  -0.9931   0.02296   0.01957  -0.0990   0.9914   0.0143
 -13.250  -0.9653   0.02196   0.01851  -0.1002   0.9885   0.0150
 -13.000  -0.9354   0.02112   0.01759  -0.1016   0.9862   0.0157
 -12.750  -0.9065   0.02036   0.01675  -0.1026   0.9837   0.0165
 -12.500  -0.8807   0.01964   0.01593  -0.1029   0.9800   0.0171
 -12.250  -0.8525   0.01890   0.01508  -0.1037   0.9775   0.0176
 -12.000  -0.8224   0.01821   0.01433  -0.1049   0.9757   0.0182
 -11.750  -0.7935   0.01772   0.01381  -0.1055   0.9725   0.0187
 -11.500  -0.7645   0.01730   0.01334  -0.1061   0.9687   0.0192
 -11.250  -0.7335   0.01685   0.01283  -0.1071   0.9657   0.0197
 -11.000  -0.7037   0.01643   0.01235  -0.1078   0.9621   0.0203
 -10.750  -0.6748   0.01600   0.01185  -0.1083   0.9569   0.0209
 -10.500  -0.6440   0.01555   0.01130  -0.1092   0.9525   0.0213
 -10.250  -0.6166   0.01514   0.01080  -0.1093   0.9453   0.0216
 -10.000  -0.5878   0.01474   0.01031  -0.1097   0.9389   0.0218
  -9.750  -0.5628   0.01409   0.00957  -0.1095   0.9306   0.0225
  -9.500  -0.5361   0.01372   0.00914  -0.1094   0.9226   0.0230
  -9.250  -0.5094   0.01343   0.00879  -0.1092   0.9136   0.0234
  -9.000  -0.4830   0.01319   0.00849  -0.1089   0.9042   0.0239
  -8.750  -0.4567   0.01294   0.00817  -0.1086   0.8950   0.0244
  -8.500  -0.4308   0.01267   0.00782  -0.1082   0.8853   0.0249
  -8.250  -0.4050   0.01235   0.00742  -0.1078   0.8762   0.0253
  -8.000  -0.3794   0.01206   0.00702  -0.1074   0.8661   0.0257
  -7.750  -0.3535   0.01179   0.00666  -0.1069   0.8560   0.0261
  -7.500  -0.3277   0.01151   0.00629  -0.1065   0.8459   0.0264
  -7.250  -0.3019   0.01125   0.00593  -0.1060   0.8359   0.0266
  -7.000  -0.2758   0.01100   0.00560  -0.1056   0.8267   0.0267
  -6.750  -0.2507   0.01062   0.00512  -0.1050   0.8156   0.0271
  -6.500  -0.2256   0.01027   0.00467  -0.1045   0.8028   0.0278
  -6.250  -0.1999   0.01003   0.00436  -0.1039   0.7889   0.0284
  -6.000  -0.1740   0.00983   0.00408  -0.1035   0.7752   0.0288
  -5.750  -0.1480   0.00966   0.00383  -0.1030   0.7611   0.0292
  -5.500  -0.1219   0.00950   0.00359  -0.1025   0.7469   0.0296
  -5.250  -0.0957   0.00936   0.00337  -0.1020   0.7345   0.0301
  -5.000  -0.0692   0.00921   0.00315  -0.1017   0.7235   0.0306
  -4.750  -0.0424   0.00906   0.00295  -0.1013   0.7139   0.0311
  -4.500  -0.0157   0.00893   0.00276  -0.1010   0.7046   0.0316
  -4.250   0.0112   0.00881   0.00258  -0.1006   0.6946   0.0321
  -4.000   0.0382   0.00871   0.00242  -0.1003   0.6854   0.0325
  -3.750   0.0649   0.00860   0.00225  -0.1000   0.6762   0.0331
  -3.500   0.0920   0.00845   0.00208  -0.0997   0.6687   0.0347
  -3.250   0.1190   0.00836   0.00197  -0.0994   0.6604   0.0361
  -3.000   0.1462   0.00828   0.00186  -0.0991   0.6529   0.0373
  -2.750   0.1733   0.00822   0.00175  -0.0989   0.6446   0.0387
  -2.500   0.2007   0.00816   0.00166  -0.0986   0.6375   0.0398
  -2.250   0.2277   0.00808   0.00157  -0.0983   0.6297   0.0428
  -2.000   0.2548   0.00803   0.00150  -0.0981   0.6201   0.0460
  -1.750   0.2816   0.00802   0.00145  -0.0977   0.6095   0.0486
  -1.500   0.3087   0.00796   0.00139  -0.0975   0.5996   0.0535
  -1.250   0.3357   0.00793   0.00135  -0.0972   0.5904   0.0582
  -1.000   0.3625   0.00792   0.00131  -0.0968   0.5795   0.0646
  -0.750   0.3896   0.00788   0.00127  -0.0966   0.5690   0.0722
  -0.500   0.4163   0.00785   0.00124  -0.0963   0.5582   0.0842
  -0.250   0.4424   0.00778   0.00122  -0.0959   0.5447   0.1164
   0.000   0.4683   0.00775   0.00124  -0.0954   0.5268   0.1532
   0.250   0.4942   0.00780   0.00126  -0.0950   0.5057   0.1757
   0.500   0.5200   0.00785   0.00130  -0.0945   0.4870   0.1973
   0.750   0.5461   0.00790   0.00134  -0.0941   0.4722   0.2167
   1.000   0.5722   0.00794   0.00139  -0.0937   0.4582   0.2408
   1.250   0.5981   0.00799   0.00145  -0.0933   0.4442   0.2672
   1.500   0.6240   0.00803   0.00151  -0.0929   0.4311   0.2959
   1.750   0.6495   0.00800   0.00159  -0.0925   0.4208   0.3568
   2.000   0.6722   0.00758   0.00171  -0.0916   0.4119   0.5824
   2.250   0.6864   0.00689   0.00187  -0.0886   0.4042   0.8841
   2.500   0.7521   0.00697   0.00200  -0.0970   0.3907   0.9942
   2.750   0.7802   0.00711   0.00209  -0.0970   0.3805   1.0000
   3.000   0.8046   0.00726   0.00218  -0.0963   0.3691   1.0000
   3.250   0.8289   0.00743   0.00228  -0.0955   0.3565   1.0000
   3.500   0.8533   0.00760   0.00239  -0.0948   0.3433   1.0000
   3.750   0.8775   0.00779   0.00250  -0.0940   0.3285   1.0000
   4.000   0.9012   0.00801   0.00264  -0.0932   0.3112   1.0000
   4.250   0.9246   0.00826   0.00280  -0.0923   0.2917   1.0000
   4.500   0.9476   0.00854   0.00297  -0.0914   0.2722   1.0000
   4.750   0.9706   0.00881   0.00317  -0.0905   0.2553   1.0000
   5.000   0.9936   0.00910   0.00337  -0.0896   0.2398   1.0000
   5.250   1.0174   0.00932   0.00355  -0.0888   0.2307   1.0000
   5.500   1.0414   0.00953   0.00372  -0.0881   0.2235   1.0000
   5.750   1.0655   0.00973   0.00391  -0.0874   0.2178   1.0000
   6.000   1.0893   0.00994   0.00410  -0.0866   0.2105   1.0000
   6.250   1.1126   0.01019   0.00431  -0.0858   0.2025   1.0000
   6.500   1.1363   0.01040   0.00451  -0.0851   0.1962   1.0000
   6.750   1.1592   0.01066   0.00474  -0.0842   0.1889   1.0000
   7.000   1.1830   0.01085   0.00494  -0.0835   0.1843   1.0000
   7.250   1.2052   0.01114   0.00518  -0.0825   0.1756   1.0000
   7.500   1.2281   0.01137   0.00541  -0.0816   0.1682   1.0000
   7.750   1.2496   0.01168   0.00568  -0.0806   0.1586   1.0000
   8.000   1.2695   0.01207   0.00598  -0.0793   0.1432   1.0000
   8.250   1.2862   0.01263   0.00640  -0.0774   0.1197   1.0000
   8.500   1.2987   0.01340   0.00699  -0.0749   0.0900   1.0000
   8.750   1.3110   0.01406   0.00755  -0.0723   0.0725   1.0000
   9.000   1.3232   0.01465   0.00806  -0.0697   0.0582   1.0000
   9.250   1.3311   0.01545   0.00874  -0.0664   0.0382   1.0000
   9.500   1.3386   0.01631   0.00950  -0.0631   0.0220   1.0000
   9.750   1.3514   0.01692   0.01009  -0.0608   0.0170   1.0000
  10.000   1.3659   0.01745   0.01064  -0.0589   0.0152   1.0000
  10.250   1.3797   0.01804   0.01125  -0.0569   0.0135   1.0000
  10.500   1.3945   0.01857   0.01182  -0.0551   0.0128   1.0000
  10.750   1.4082   0.01918   0.01246  -0.0532   0.0118   1.0000
  11.000   1.4210   0.01987   0.01317  -0.0513   0.0112   1.0000
  11.250   1.4328   0.02063   0.01398  -0.0493   0.0103   1.0000
  11.500   1.4461   0.02132   0.01471  -0.0477   0.0099   1.0000
  11.750   1.4584   0.02210   0.01554  -0.0460   0.0096   1.0000
  12.000   1.4700   0.02295   0.01644  -0.0443   0.0091   1.0000
  12.250   1.4808   0.02388   0.01741  -0.0427   0.0088   1.0000
  12.500   1.4906   0.02492   0.01850  -0.0410   0.0084   1.0000
  12.750   1.4990   0.02610   0.01973  -0.0394   0.0080   1.0000
  13.000   1.5063   0.02742   0.02111  -0.0378   0.0077   1.0000
  13.250   1.5159   0.02860   0.02235  -0.0365   0.0075   1.0000
  13.500   1.5242   0.02993   0.02374  -0.0353   0.0073   1.0000
  13.750   1.5319   0.03136   0.02523  -0.0341   0.0071   1.0000
  14.000   1.5382   0.03295   0.02689  -0.0330   0.0069   1.0000
  14.250   1.5439   0.03466   0.02867  -0.0320   0.0067   1.0000
  14.500   1.5491   0.03647   0.03054  -0.0311   0.0064   1.0000
  14.750   1.5526   0.03851   0.03265  -0.0303   0.0062   1.0000
  15.000   1.5549   0.04072   0.03494  -0.0296   0.0061   1.0000
  15.250   1.5553   0.04322   0.03751  -0.0290   0.0059   1.0000
  15.500   1.5537   0.04605   0.04043  -0.0286   0.0058   1.0000
  15.750   1.5521   0.04897   0.04344  -0.0284   0.0057   1.0000
  16.000   1.5521   0.05177   0.04633  -0.0283   0.0056   1.0000
  16.250   1.5509   0.05483   0.04947  -0.0284   0.0055   1.0000
  16.500   1.5479   0.05819   0.05293  -0.0286   0.0055   1.0000
  16.750   1.5439   0.06177   0.05662  -0.0291   0.0054   1.0000
  17.000   1.5384   0.06565   0.06060  -0.0297   0.0053   1.0000
  17.250   1.5327   0.06969   0.06474  -0.0305   0.0052   1.0000
  17.500   1.5258   0.07403   0.06918  -0.0316   0.0052   1.0000
  17.750   1.5188   0.07845   0.07370  -0.0328   0.0051   1.0000
  18.000   1.5073   0.08371   0.07908  -0.0344   0.0051   1.0000
  18.250   1.4980   0.08874   0.08422  -0.0361   0.0050   1.0000
  18.500   1.4857   0.09436   0.08995  -0.0381   0.0050   1.0000
  18.750   1.4765   0.09954   0.09523  -0.0401   0.0049   1.0000
  19.000   1.4609   0.10597   0.10179  -0.0427   0.0049   1.0000
  19.250   1.4497   0.11174   0.10766  -0.0452   0.0049   1.0000
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