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GOE 766 AIRFOIL (goe766-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 766 AIRFOIL (goe766-il)
Reynolds number: 1,000,000
Max Cl/Cd: 97.97 at α=6.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe766-il-1000000.txt
Download as CSV file: xf-goe766-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 766 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -1.1300   0.09612   0.09349  -0.0160   1.0000   0.0205
 -18.000  -1.1767   0.08372   0.08090  -0.0236   1.0000   0.0205
 -17.750  -1.2111   0.07385   0.07085  -0.0299   1.0000   0.0205
 -17.500  -1.2377   0.06554   0.06237  -0.0353   1.0000   0.0206
 -17.250  -1.2579   0.05854   0.05521  -0.0398   1.0000   0.0206
 -17.000  -1.2661   0.05364   0.05018  -0.0430   1.0000   0.0208
 -16.750  -1.2773   0.04871   0.04510  -0.0458   1.0000   0.0210
 -16.500  -1.2810   0.04508   0.04134  -0.0476   1.0000   0.0211
 -16.250  -1.2813   0.04208   0.03823  -0.0488   1.0000   0.0213
 -16.000  -1.2807   0.03942   0.03544  -0.0495   1.0000   0.0215
 -15.750  -1.2782   0.03716   0.03307  -0.0498   1.0000   0.0216
 -15.500  -1.2896   0.03377   0.02952  -0.0494   1.0000   0.0219
 -15.250  -1.2911   0.03159   0.02725  -0.0485   1.0000   0.0221
 -15.000  -1.2864   0.03011   0.02572  -0.0473   1.0000   0.0224
 -14.750  -1.2792   0.02894   0.02449  -0.0459   1.0000   0.0226
 -14.500  -1.2712   0.02790   0.02340  -0.0443   1.0000   0.0229
 -14.250  -1.2595   0.02722   0.02269  -0.0427   1.0000   0.0232
 -14.000  -1.2506   0.02634   0.02174  -0.0407   1.0000   0.0235
 -13.750  -1.2400   0.02565   0.02099  -0.0386   1.0000   0.0238
 -13.500  -1.2303   0.02492   0.02018  -0.0362   1.0000   0.0241
 -13.250  -1.2202   0.02429   0.01947  -0.0336   1.0000   0.0244
 -13.000  -1.2094   0.02368   0.01879  -0.0310   1.0000   0.0247
 -12.750  -1.1951   0.02308   0.01812  -0.0290   1.0000   0.0250
 -12.500  -1.1783   0.02263   0.01759  -0.0273   1.0000   0.0252
 -12.250  -1.1694   0.02125   0.01611  -0.0247   1.0000   0.0257
 -12.000  -1.1547   0.02045   0.01527  -0.0228   1.0000   0.0261
 -11.750  -1.1370   0.01991   0.01471  -0.0211   1.0000   0.0265
 -11.500  -1.1178   0.01948   0.01427  -0.0197   1.0000   0.0269
 -11.250  -1.0981   0.01909   0.01385  -0.0183   1.0000   0.0274
 -11.000  -1.0785   0.01864   0.01336  -0.0168   1.0000   0.0278
 -10.750  -1.0590   0.01816   0.01282  -0.0153   1.0000   0.0282
 -10.500  -1.0392   0.01769   0.01230  -0.0138   1.0000   0.0286
 -10.250  -1.0185   0.01730   0.01186  -0.0125   1.0000   0.0290
 -10.000  -0.9972   0.01697   0.01148  -0.0111   1.0000   0.0292
  -9.750  -0.9818   0.01599   0.01046  -0.0090   1.0000   0.0300
  -9.500  -0.9624   0.01547   0.00992  -0.0074   1.0000   0.0305
  -9.250  -0.9420   0.01506   0.00951  -0.0060   1.0000   0.0310
  -9.000  -0.9213   0.01470   0.00913  -0.0045   1.0000   0.0315
  -8.750  -0.9005   0.01434   0.00875  -0.0030   1.0000   0.0320
  -8.500  -0.8794   0.01401   0.00840  -0.0016   1.0000   0.0326
  -8.250  -0.8583   0.01372   0.00808  -0.0001   1.0000   0.0331
  -8.000  -0.8375   0.01340   0.00773   0.0014   1.0000   0.0335
  -7.750  -0.8168   0.01311   0.00741   0.0030   1.0000   0.0339
  -7.500  -0.8004   0.01245   0.00673   0.0052   1.0000   0.0348
  -7.250  -0.7812   0.01209   0.00638   0.0070   1.0000   0.0355
  -7.000  -0.7488   0.01177   0.00606   0.0061   0.9986   0.0362
  -6.750  -0.7129   0.01149   0.00578   0.0045   0.9962   0.0373
  -6.500  -0.6764   0.01121   0.00549   0.0027   0.9936   0.0383
  -6.250  -0.6429   0.01094   0.00521   0.0017   0.9900   0.0389
  -6.000  -0.6096   0.01043   0.00471   0.0006   0.9857   0.0404
  -5.750  -0.5728   0.01012   0.00441  -0.0012   0.9821   0.0419
  -5.500  -0.5412   0.00986   0.00416  -0.0018   0.9744   0.0432
  -5.250  -0.5019   0.00964   0.00393  -0.0040   0.9686   0.0447
  -5.000  -0.4632   0.00923   0.00354  -0.0062   0.9549   0.0476
  -4.750  -0.4207   0.00898   0.00325  -0.0090   0.9238   0.0504
  -4.500  -0.3923   0.00883   0.00298  -0.0088   0.8764   0.0536
  -4.250  -0.3695   0.00879   0.00277  -0.0074   0.8171   0.0573
  -4.000  -0.3482   0.00883   0.00257  -0.0057   0.7449   0.0623
  -3.750  -0.3255   0.00882   0.00240  -0.0044   0.6887   0.0701
  -3.500  -0.3020   0.00870   0.00223  -0.0033   0.6460   0.0870
  -3.250  -0.2781   0.00855   0.00211  -0.0024   0.6111   0.1161
  -3.000  -0.2531   0.00847   0.00201  -0.0016   0.5807   0.1360
  -2.750  -0.2274   0.00843   0.00192  -0.0010   0.5533   0.1499
  -2.500  -0.2014   0.00839   0.00184  -0.0004   0.5300   0.1632
  -2.250  -0.1754   0.00831   0.00175   0.0001   0.5111   0.1793
  -2.000  -0.1498   0.00819   0.00166   0.0007   0.4950   0.2042
  -1.750  -0.1249   0.00795   0.00157   0.0015   0.4812   0.2526
  -1.500  -0.1017   0.00757   0.00147   0.0024   0.4694   0.3409
  -1.250  -0.0776   0.00731   0.00140   0.0033   0.4580   0.4099
  -1.000  -0.0541   0.00700   0.00133   0.0042   0.4474   0.4872
  -0.750  -0.0317   0.00667   0.00131   0.0055   0.4375   0.5829
  -0.500  -0.0076   0.00652   0.00130   0.0065   0.4272   0.6430
  -0.250   0.0174   0.00641   0.00130   0.0074   0.4186   0.6838
   0.000   0.0425   0.00634   0.00131   0.0082   0.4094   0.7193
   0.250   0.0678   0.00626   0.00132   0.0091   0.4012   0.7537
   0.500   0.0936   0.00624   0.00134   0.0098   0.3919   0.7792
   0.750   0.1198   0.00621   0.00137   0.0105   0.3833   0.8037
   1.000   0.1454   0.00620   0.00140   0.0113   0.3733   0.8323
   1.250   0.1714   0.00617   0.00145   0.0120   0.3635   0.8639
   1.500   0.1983   0.00620   0.00151   0.0126   0.3526   0.8909
   1.750   0.2270   0.00626   0.00157   0.0127   0.3413   0.9093
   2.000   0.2573   0.00633   0.00164   0.0125   0.3299   0.9253
   2.250   0.2888   0.00645   0.00172   0.0120   0.3178   0.9396
   2.500   0.3245   0.00662   0.00183   0.0105   0.3043   0.9493
   2.750   0.3585   0.00677   0.00193   0.0094   0.2922   0.9579
   3.000   0.3936   0.00695   0.00205   0.0081   0.2806   0.9652
   3.250   0.4280   0.00714   0.00219   0.0069   0.2703   0.9707
   3.500   0.4660   0.00731   0.00231   0.0049   0.2623   0.9732
   3.750   0.5015   0.00748   0.00244   0.0034   0.2536   0.9761
   4.000   0.5342   0.00765   0.00256   0.0025   0.2451   0.9804
   4.250   0.5690   0.00782   0.00269   0.0011   0.2386   0.9831
   4.500   0.6060   0.00793   0.00279  -0.0007   0.2326   0.9847
   4.750   0.6408   0.00810   0.00291  -0.0022   0.2260   0.9866
   5.000   0.6754   0.00821   0.00301  -0.0035   0.2211   0.9887
   5.250   0.7089   0.00834   0.00312  -0.0046   0.2147   0.9912
   5.500   0.7410   0.00852   0.00327  -0.0055   0.2081   0.9935
   5.750   0.7765   0.00860   0.00336  -0.0070   0.2024   0.9948
   6.000   0.8110   0.00877   0.00348  -0.0085   0.1940   0.9964
   6.250   0.8456   0.00887   0.00358  -0.0099   0.1867   0.9981
   6.500   0.8795   0.00905   0.00371  -0.0112   0.1771   0.9995
   6.750   0.9062   0.00925   0.00385  -0.0111   0.1653   1.0000
   7.000   0.9276   0.00949   0.00403  -0.0098   0.1515   1.0000
   7.250   0.9483   0.00980   0.00426  -0.0085   0.1361   1.0000
   7.500   0.9687   0.01014   0.00453  -0.0071   0.1213   1.0000
   7.750   0.9890   0.01051   0.00483  -0.0057   0.1086   1.0000
   8.000   1.0092   0.01089   0.00515  -0.0043   0.0975   1.0000
   8.250   1.0292   0.01128   0.00549  -0.0028   0.0877   1.0000
   8.500   1.0494   0.01166   0.00583  -0.0014   0.0797   1.0000
   8.750   1.0702   0.01200   0.00615  -0.0001   0.0740   1.0000
   9.000   1.0901   0.01241   0.00654   0.0013   0.0684   1.0000
   9.250   1.1111   0.01272   0.00686   0.0026   0.0652   1.0000
   9.500   1.1307   0.01316   0.00727   0.0040   0.0614   1.0000
   9.750   1.1514   0.01350   0.00764   0.0053   0.0589   1.0000
  10.000   1.1718   0.01385   0.00801   0.0066   0.0565   1.0000
  10.250   1.1909   0.01431   0.00846   0.0081   0.0540   1.0000
  10.500   1.2101   0.01475   0.00893   0.0095   0.0521   1.0000
  10.750   1.2307   0.01508   0.00930   0.0108   0.0507   1.0000
  11.000   1.2501   0.01549   0.00972   0.0121   0.0490   1.0000
  11.250   1.2681   0.01599   0.01024   0.0137   0.0474   1.0000
  11.500   1.2843   0.01660   0.01088   0.0154   0.0457   1.0000
  11.750   1.3038   0.01696   0.01129   0.0167   0.0448   1.0000
  12.000   1.3225   0.01738   0.01175   0.0181   0.0437   1.0000
  12.250   1.3399   0.01785   0.01225   0.0196   0.0426   1.0000
  12.500   1.3553   0.01842   0.01284   0.0213   0.0414   1.0000
  12.750   1.3666   0.01919   0.01364   0.0236   0.0402   1.0000
  13.000   1.3799   0.01980   0.01431   0.0256   0.0395   1.0000
  13.250   1.3926   0.02026   0.01483   0.0278   0.0388   1.0000
  13.500   1.4025   0.02081   0.01543   0.0303   0.0381   1.0000
  13.750   1.4126   0.02144   0.01610   0.0326   0.0373   1.0000
  14.000   1.4212   0.02223   0.01693   0.0347   0.0366   1.0000
  14.250   1.4273   0.02326   0.01802   0.0367   0.0359   1.0000
  14.500   1.4296   0.02467   0.01949   0.0385   0.0351   1.0000
  14.750   1.4297   0.02647   0.02138   0.0397   0.0344   1.0000
  15.000   1.4377   0.02788   0.02287   0.0402   0.0341   1.0000
  15.250   1.4438   0.02964   0.02472   0.0403   0.0336   1.0000
  15.500   1.4487   0.03175   0.02691   0.0399   0.0330   1.0000
  15.750   1.4505   0.03445   0.02971   0.0390   0.0325   1.0000
  16.000   1.4512   0.03746   0.03281   0.0376   0.0320   1.0000
  16.250   1.4461   0.04137   0.03682   0.0358   0.0317   1.0000
  16.500   1.4395   0.04548   0.04102   0.0338   0.0312   1.0000
  16.750   1.4259   0.05050   0.04614   0.0316   0.0309   1.0000
  17.000   1.4084   0.05594   0.05169   0.0292   0.0306   1.0000
  17.250   1.3876   0.06181   0.05766   0.0267   0.0303   1.0000
  17.500   1.3658   0.06779   0.06374   0.0241   0.0300   1.0000
  17.750   1.3478   0.07339   0.06944   0.0218   0.0298   1.0000
  18.000   1.3373   0.07821   0.07436   0.0196   0.0296   1.0000
  18.250   1.3265   0.08313   0.07936   0.0175   0.0293   1.0000
  18.500   1.3148   0.08822   0.08454   0.0152   0.0291   1.0000
  18.750   1.3043   0.09324   0.08965   0.0130   0.0288   1.0000
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