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GOE 627 AIRFOIL (goe627-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 627 AIRFOIL (goe627-il)
Reynolds number: 1,000,000
Max Cl/Cd: 93.39 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe627-il-1000000.txt
Download as CSV file: xf-goe627-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 627 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.000  -0.7881   0.07200   0.06952  -0.0744   1.0000   0.0181
 -15.750  -0.8391   0.06090   0.05819  -0.0813   1.0000   0.0181
 -15.500  -0.8697   0.05409   0.05121  -0.0850   1.0000   0.0181
 -15.250  -0.8903   0.04744   0.04435  -0.0903   0.9992   0.0181
 -15.000  -0.9020   0.04192   0.03859  -0.0953   0.9974   0.0183
 -14.750  -0.9112   0.03746   0.03392  -0.0982   0.9954   0.0185
 -14.500  -0.9040   0.03513   0.03151  -0.0997   0.9940   0.0186
 -14.250  -0.8841   0.03443   0.03082  -0.1006   0.9929   0.0189
 -14.000  -0.8793   0.03263   0.02892  -0.1002   0.9901   0.0190
 -13.750  -0.8617   0.03194   0.02820  -0.1004   0.9881   0.0192
 -13.500  -0.8478   0.03062   0.02679  -0.1005   0.9861   0.0194
 -13.250  -0.8264   0.03005   0.02619  -0.1010   0.9847   0.0196
 -13.000  -0.8098   0.02869   0.02471  -0.1012   0.9834   0.0199
 -12.750  -0.7877   0.02787   0.02381  -0.1017   0.9824   0.0202
 -12.500  -0.7843   0.02712   0.02296  -0.0982   0.9770   0.0205
 -12.250  -0.7692   0.02604   0.02174  -0.0971   0.9741   0.0208
 -12.000  -0.7469   0.02506   0.02062  -0.0972   0.9723   0.0211
 -11.750  -0.7181   0.02425   0.01968  -0.0982   0.9710   0.0214
 -11.500  -0.6921   0.02226   0.01755  -0.0994   0.9701   0.0220
 -11.250  -0.6724   0.02154   0.01681  -0.0984   0.9667   0.0222
 -11.000  -0.6530   0.02102   0.01625  -0.0971   0.9629   0.0225
 -10.750  -0.6261   0.02054   0.01574  -0.0973   0.9612   0.0229
 -10.500  -0.5969   0.02004   0.01521  -0.0980   0.9599   0.0233
 -10.250  -0.5667   0.01939   0.01450  -0.0989   0.9588   0.0238
 -10.000  -0.5345   0.01877   0.01380  -0.1001   0.9580   0.0244
  -9.750  -0.5028   0.01816   0.01309  -0.1012   0.9570   0.0248
  -9.500  -0.4705   0.01767   0.01251  -0.1023   0.9559   0.0251
  -9.250  -0.4530   0.01656   0.01133  -0.1006   0.9519   0.0255
  -9.000  -0.4319   0.01585   0.01062  -0.0994   0.9478   0.0259
  -8.750  -0.4032   0.01535   0.01012  -0.0998   0.9453   0.0264
  -8.500  -0.3726   0.01488   0.00963  -0.1004   0.9431   0.0270
  -8.250  -0.3411   0.01443   0.00915  -0.1013   0.9408   0.0275
  -8.000  -0.3210   0.01404   0.00873  -0.0996   0.9354   0.0280
  -7.750  -0.2966   0.01360   0.00824  -0.0988   0.9297   0.0284
  -7.500  -0.2663   0.01315   0.00774  -0.0992   0.9252   0.0288
  -7.250  -0.2447   0.01286   0.00740  -0.0978   0.9189   0.0291
  -7.000  -0.2243   0.01222   0.00674  -0.0963   0.9123   0.0296
  -6.750  -0.1976   0.01163   0.00614  -0.0961   0.9068   0.0304
  -6.500  -0.1806   0.01133   0.00582  -0.0937   0.8982   0.0308
  -6.250  -0.1535   0.01099   0.00546  -0.0934   0.8917   0.0314
  -6.000  -0.1338   0.01073   0.00517  -0.0916   0.8824   0.0318
  -5.750  -0.1083   0.01043   0.00482  -0.0909   0.8737   0.0324
  -5.500  -0.0868   0.01020   0.00455  -0.0894   0.8623   0.0328
  -5.250  -0.0635   0.01000   0.00430  -0.0883   0.8504   0.0333
  -5.000  -0.0404   0.00984   0.00407  -0.0871   0.8354   0.0339
  -4.750  -0.0211   0.00952   0.00366  -0.0852   0.8173   0.0347
  -4.500  -0.0005   0.00935   0.00342  -0.0834   0.7982   0.0354
  -4.250   0.0203   0.00923   0.00323  -0.0818   0.7795   0.0362
  -4.000   0.0407   0.00916   0.00306  -0.0800   0.7598   0.0370
  -3.750   0.0606   0.00910   0.00291  -0.0781   0.7399   0.0378
  -3.500   0.0810   0.00907   0.00278  -0.0763   0.7209   0.0386
  -3.250   0.1005   0.00898   0.00262  -0.0744   0.7016   0.0400
  -3.000   0.1201   0.00894   0.00251  -0.0725   0.6816   0.0418
  -2.750   0.1401   0.00892   0.00242  -0.0706   0.6623   0.0439
  -2.500   0.1601   0.00889   0.00233  -0.0688   0.6445   0.0476
  -2.250   0.1795   0.00879   0.00224  -0.0669   0.6279   0.0628
  -2.000   0.1942   0.00842   0.00212  -0.0641   0.6125   0.1451
  -1.750   0.2099   0.00816   0.00204  -0.0616   0.5968   0.2155
  -1.500   0.2263   0.00796   0.00201  -0.0592   0.5807   0.2855
  -1.250   0.2443   0.00784   0.00198  -0.0571   0.5641   0.3348
  -1.000   0.2598   0.00764   0.00195  -0.0545   0.5471   0.4058
  -0.750   0.2730   0.00740   0.00193  -0.0514   0.5294   0.4956
  -0.500   0.2827   0.00718   0.00193  -0.0475   0.5100   0.5869
  -0.250   0.2922   0.00700   0.00194  -0.0435   0.4925   0.6660
   0.000   0.3026   0.00690   0.00198  -0.0396   0.4740   0.7332
   0.250   0.3157   0.00687   0.00205  -0.0362   0.4567   0.7865
   0.500   0.3314   0.00691   0.00214  -0.0334   0.4403   0.8307
   0.750   0.3505   0.00698   0.00225  -0.0314   0.4243   0.8681
   1.000   0.3755   0.00709   0.00237  -0.0306   0.4091   0.8988
   1.250   0.4106   0.00727   0.00252  -0.0321   0.3934   0.9237
   1.500   0.4553   0.00753   0.00272  -0.0357   0.3772   0.9417
   1.750   0.4910   0.00776   0.00287  -0.0375   0.3628   0.9518
   2.000   0.5294   0.00800   0.00301  -0.0398   0.3491   0.9560
   2.250   0.5698   0.00828   0.00320  -0.0427   0.3354   0.9607
   2.500   0.6004   0.00851   0.00337  -0.0432   0.3253   0.9687
   2.750   0.6394   0.00878   0.00357  -0.0457   0.3147   0.9713
   3.000   0.6758   0.00907   0.00377  -0.0476   0.3041   0.9742
   3.250   0.7100   0.00929   0.00394  -0.0490   0.2960   0.9782
   3.500   0.7406   0.00955   0.00413  -0.0497   0.2871   0.9823
   3.750   0.7793   0.00975   0.00428  -0.0522   0.2795   0.9838
   4.000   0.8167   0.01001   0.00447  -0.0544   0.2714   0.9859
   4.250   0.8516   0.01019   0.00462  -0.0561   0.2660   0.9881
   4.500   0.8840   0.01038   0.00477  -0.0573   0.2607   0.9907
   4.750   0.9138   0.01063   0.00497  -0.0580   0.2546   0.9933
   5.000   0.9487   0.01077   0.00509  -0.0597   0.2507   0.9947
   5.250   0.9828   0.01092   0.00521  -0.0613   0.2464   0.9964
   5.500   1.0157   0.01113   0.00537  -0.0627   0.2411   0.9982
   5.750   1.0487   0.01133   0.00555  -0.0641   0.2367   0.9996
   6.000   1.0656   0.01141   0.00565  -0.0621   0.2346   1.0000
   6.250   1.0740   0.01151   0.00575  -0.0584   0.2321   1.0000
   6.500   1.0833   0.01163   0.00587  -0.0548   0.2296   1.0000
   6.750   1.0942   0.01180   0.00603  -0.0516   0.2269   1.0000
   7.000   1.1050   0.01202   0.00623  -0.0484   0.2238   1.0000
   7.250   1.1184   0.01221   0.00642  -0.0457   0.2215   1.0000
   7.500   1.1351   0.01235   0.00659  -0.0437   0.2200   1.0000
   7.750   1.1513   0.01252   0.00678  -0.0416   0.2180   1.0000
   8.000   1.1676   0.01271   0.00698  -0.0396   0.2160   1.0000
   8.250   1.1839   0.01294   0.00721  -0.0376   0.2133   1.0000
   8.500   1.1995   0.01322   0.00747  -0.0356   0.2106   1.0000
   8.750   1.2134   0.01356   0.00781  -0.0333   0.2075   1.0000
   9.000   1.2317   0.01378   0.00806  -0.0317   0.2061   1.0000
   9.250   1.2508   0.01399   0.00830  -0.0304   0.2045   1.0000
   9.500   1.2694   0.01423   0.00857  -0.0290   0.2027   1.0000
   9.750   1.2875   0.01450   0.00885  -0.0276   0.2005   1.0000
  10.000   1.3051   0.01480   0.00917  -0.0261   0.1983   1.0000
  10.250   1.3218   0.01517   0.00954  -0.0246   0.1958   1.0000
  10.500   1.3363   0.01564   0.01001  -0.0227   0.1927   1.0000
  10.750   1.3564   0.01588   0.01029  -0.0218   0.1907   1.0000
  11.000   1.3758   0.01616   0.01062  -0.0208   0.1888   1.0000
  11.250   1.3940   0.01651   0.01098  -0.0196   0.1858   1.0000
  11.500   1.4107   0.01693   0.01140  -0.0183   0.1822   1.0000
  11.750   1.4250   0.01748   0.01194  -0.0167   0.1782   1.0000
  12.000   1.4440   0.01782   0.01234  -0.0157   0.1764   1.0000
  12.250   1.4624   0.01820   0.01275  -0.0148   0.1728   1.0000
  12.500   1.4784   0.01871   0.01326  -0.0135   0.1688   1.0000
  12.750   1.4918   0.01936   0.01391  -0.0120   0.1644   1.0000
  13.000   1.5094   0.01981   0.01440  -0.0111   0.1603   1.0000
  13.250   1.5231   0.02048   0.01506  -0.0098   0.1550   1.0000
  13.500   1.5362   0.02121   0.01579  -0.0084   0.1495   1.0000
  13.750   1.5482   0.02201   0.01660  -0.0070   0.1429   1.0000
  14.000   1.5590   0.02291   0.01750  -0.0056   0.1371   1.0000
  14.250   1.5674   0.02400   0.01856  -0.0040   0.1292   1.0000
  14.500   1.5742   0.02522   0.01977  -0.0024   0.1211   1.0000
  14.750   1.5794   0.02660   0.02113  -0.0008   0.1144   1.0000
  15.000   1.5859   0.02793   0.02248   0.0006   0.1088   1.0000
  15.250   1.5897   0.02953   0.02408   0.0020   0.1035   1.0000
  15.500   1.5952   0.03106   0.02564   0.0031   0.0994   1.0000
  15.750   1.5963   0.03299   0.02758   0.0044   0.0947   1.0000
  16.000   1.6015   0.03467   0.02931   0.0053   0.0920   1.0000
  16.250   1.6052   0.03653   0.03121   0.0061   0.0893   1.0000
  16.500   1.6064   0.03867   0.03340   0.0068   0.0867   1.0000
  16.750   1.6055   0.04109   0.03586   0.0075   0.0838   1.0000
  17.000   1.6098   0.04307   0.03791   0.0078   0.0821   1.0000
  17.250   1.6092   0.04560   0.04050   0.0082   0.0793   1.0000
  17.500   1.6053   0.04854   0.04349   0.0084   0.0768   1.0000
  17.750   1.6004   0.05165   0.04667   0.0084   0.0739   1.0000
  18.000   1.5984   0.05454   0.04963   0.0083   0.0713   1.0000
  18.250   1.5891   0.05834   0.05348   0.0081   0.0682   1.0000
  18.500   1.5782   0.06241   0.05762   0.0076   0.0650   1.0000
  18.750   1.5658   0.06676   0.06203   0.0069   0.0607   1.0000
  19.000   1.5445   0.07237   0.06769   0.0058   0.0557   1.0000
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