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GOE 738 AIRFOIL (goe738-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 738 AIRFOIL (goe738-il)
Reynolds number: 1,000,000
Max Cl/Cd: 102.91 at α=7.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe738-il-1000000.txt
Download as CSV file: xf-goe738-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 738 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -1.1341   0.10775   0.10483  -0.0110   1.0000   0.0267
 -19.500  -1.1542   0.10020   0.09716  -0.0158   1.0000   0.0268
 -19.250  -1.1720   0.09326   0.09010  -0.0201   1.0000   0.0269
 -19.000  -1.1897   0.08644   0.08316  -0.0244   1.0000   0.0270
 -18.750  -1.2110   0.07941   0.07601  -0.0286   1.0000   0.0272
 -18.500  -1.2317   0.07276   0.06923  -0.0324   1.0000   0.0273
 -18.250  -1.2501   0.06655   0.06294  -0.0360   1.0000   0.0276
 -18.000  -1.2641   0.06106   0.05735  -0.0391   1.0000   0.0278
 -17.750  -1.2765   0.05596   0.05214  -0.0419   1.0000   0.0279
 -17.500  -1.2856   0.05148   0.04757  -0.0443   1.0000   0.0281
 -17.250  -1.2919   0.04753   0.04353  -0.0462   1.0000   0.0282
 -17.000  -1.2957   0.04409   0.04000  -0.0477   1.0000   0.0284
 -16.750  -1.2978   0.04101   0.03684  -0.0487   1.0000   0.0286
 -16.500  -1.2972   0.03842   0.03418  -0.0493   1.0000   0.0289
 -16.250  -1.2966   0.03602   0.03169  -0.0496   1.0000   0.0291
 -16.000  -1.2950   0.03386   0.02946  -0.0494   1.0000   0.0293
 -15.750  -1.2912   0.03205   0.02758  -0.0489   1.0000   0.0296
 -15.500  -1.2861   0.03047   0.02592  -0.0482   1.0000   0.0298
 -15.250  -1.2803   0.02904   0.02441  -0.0472   1.0000   0.0301
 -15.000  -1.2737   0.02776   0.02306  -0.0460   1.0000   0.0304
 -14.750  -1.2652   0.02669   0.02192  -0.0447   1.0000   0.0306
 -14.500  -1.2561   0.02572   0.02088  -0.0431   1.0000   0.0308
 -14.250  -1.2462   0.02484   0.01993  -0.0415   1.0000   0.0310
 -14.000  -1.2450   0.02350   0.01852  -0.0388   1.0000   0.0314
 -13.750  -1.2408   0.02242   0.01740  -0.0362   1.0000   0.0317
 -13.500  -1.2315   0.02165   0.01660  -0.0338   1.0000   0.0321
 -13.250  -1.2193   0.02103   0.01596  -0.0317   1.0000   0.0326
 -13.000  -1.1899   0.02038   0.01522  -0.0329   0.9207   0.0330
 -12.750  -1.1803   0.02010   0.01470  -0.0297   0.8576   0.0334
 -12.250  -1.1532   0.01928   0.01365  -0.0250   0.8189   0.0342
 -12.000  -1.1356   0.01884   0.01312  -0.0234   0.8063   0.0346
 -11.750  -1.1164   0.01844   0.01263  -0.0219   0.7956   0.0350
 -11.500  -1.0960   0.01809   0.01219  -0.0207   0.7857   0.0353
 -11.250  -1.0793   0.01744   0.01147  -0.0189   0.7769   0.0359
 -11.000  -1.0609   0.01687   0.01085  -0.0174   0.7684   0.0366
 -10.750  -1.0398   0.01646   0.01040  -0.0162   0.7609   0.0372
 -10.500  -1.0176   0.01608   0.00998  -0.0152   0.7533   0.0378
 -10.250  -0.9950   0.01575   0.00959  -0.0142   0.7460   0.0385
 -10.000  -0.9718   0.01541   0.00920  -0.0134   0.7396   0.0391
  -9.750  -0.9481   0.01510   0.00883  -0.0125   0.7327   0.0397
  -9.500  -0.9238   0.01485   0.00851  -0.0118   0.7260   0.0402
  -9.250  -0.9026   0.01428   0.00792  -0.0106   0.7202   0.0414
  -9.000  -0.8786   0.01394   0.00756  -0.0098   0.7137   0.0424
  -8.750  -0.8539   0.01370   0.00726  -0.0091   0.7075   0.0435
  -8.500  -0.8286   0.01342   0.00697  -0.0085   0.7020   0.0445
  -8.250  -0.8030   0.01319   0.00669  -0.0080   0.6957   0.0454
  -8.000  -0.7792   0.01282   0.00628  -0.0071   0.6895   0.0468
  -7.750  -0.7539   0.01252   0.00598  -0.0065   0.6843   0.0484
  -7.500  -0.7280   0.01229   0.00574  -0.0060   0.6784   0.0499
  -7.250  -0.7017   0.01212   0.00550  -0.0055   0.6722   0.0513
  -7.000  -0.6765   0.01180   0.00518  -0.0049   0.6666   0.0535
  -6.750  -0.6503   0.01157   0.00496  -0.0044   0.6606   0.0558
  -6.500  -0.6236   0.01141   0.00475  -0.0040   0.6547   0.0577
  -6.250  -0.5978   0.01115   0.00448  -0.0035   0.6492   0.0604
  -6.000  -0.5712   0.01093   0.00427  -0.0031   0.6433   0.0631
  -5.750  -0.5441   0.01080   0.00409  -0.0027   0.6370   0.0654
  -5.500  -0.5180   0.01055   0.00385  -0.0022   0.6310   0.0690
  -5.250  -0.4910   0.01036   0.00367  -0.0018   0.6251   0.0724
  -5.000  -0.4643   0.01018   0.00347  -0.0014   0.6190   0.0765
  -4.750  -0.4376   0.00999   0.00328  -0.0010   0.6132   0.0814
  -4.500  -0.4107   0.00979   0.00310  -0.0007   0.6074   0.0875
  -4.250  -0.3841   0.00958   0.00292  -0.0002   0.6009   0.0965
  -4.000  -0.3579   0.00936   0.00276   0.0002   0.5947   0.1130
  -3.750  -0.3311   0.00914   0.00263   0.0006   0.5887   0.1325
  -3.500  -0.3040   0.00899   0.00252   0.0009   0.5826   0.1475
  -3.250  -0.2767   0.00888   0.00242   0.0012   0.5766   0.1594
  -3.000  -0.2492   0.00873   0.00232   0.0014   0.5709   0.1717
  -2.750  -0.2218   0.00862   0.00223   0.0017   0.5638   0.1835
  -2.500  -0.1943   0.00851   0.00214   0.0020   0.5567   0.1964
  -2.250  -0.1669   0.00838   0.00205   0.0022   0.5494   0.2119
  -2.000  -0.1399   0.00827   0.00197   0.0026   0.5425   0.2316
  -1.750  -0.1127   0.00809   0.00190   0.0029   0.5369   0.2572
  -1.500  -0.0859   0.00792   0.00183   0.0032   0.5305   0.2882
  -1.250  -0.0595   0.00777   0.00176   0.0036   0.5241   0.3236
  -1.000  -0.0331   0.00754   0.00170   0.0040   0.5188   0.3703
  -0.750  -0.0077   0.00729   0.00164   0.0046   0.5124   0.4303
  -0.500   0.0171   0.00705   0.00160   0.0053   0.5057   0.4945
  -0.250   0.0427   0.00683   0.00157   0.0059   0.4999   0.5524
   0.000   0.0685   0.00669   0.00156   0.0065   0.4928   0.6011
   0.250   0.0940   0.00656   0.00156   0.0072   0.4867   0.6451
   0.500   0.1197   0.00643   0.00157   0.0078   0.4816   0.6903
   0.750   0.1456   0.00635   0.00159   0.0085   0.4762   0.7282
   1.000   0.1721   0.00634   0.00162   0.0090   0.4705   0.7546
   1.250   0.1994   0.00629   0.00165   0.0094   0.4660   0.7773
   1.500   0.2266   0.00627   0.00168   0.0098   0.4607   0.7977
   1.750   0.2537   0.00628   0.00171   0.0102   0.4551   0.8170
   2.000   0.2813   0.00627   0.00176   0.0105   0.4504   0.8359
   2.250   0.3090   0.00626   0.00180   0.0108   0.4451   0.8566
   2.500   0.3370   0.00627   0.00185   0.0110   0.4395   0.8773
   2.750   0.3665   0.00630   0.00192   0.0109   0.4341   0.8971
   3.250   0.4424   0.00646   0.00214   0.0071   0.4204   0.9409
   3.750   0.5207   0.00674   0.00238   0.0027   0.4044   0.9617
   4.000   0.5538   0.00689   0.00250   0.0018   0.3962   0.9686
   4.250   0.5913   0.00706   0.00262  -0.0002   0.3848   0.9712
   4.500   0.6274   0.00720   0.00273  -0.0018   0.3739   0.9744
   4.750   0.6591   0.00738   0.00286  -0.0025   0.3619   0.9793
   5.000   0.6941   0.00758   0.00299  -0.0041   0.3462   0.9818
   5.250   0.7306   0.00783   0.00313  -0.0060   0.3235   0.9836
   5.500   0.7657   0.00815   0.00332  -0.0077   0.2993   0.9859
   5.750   0.8000   0.00845   0.00352  -0.0092   0.2791   0.9886
   6.000   0.8328   0.00875   0.00374  -0.0104   0.2638   0.9915
   6.500   0.9032   0.00921   0.00410  -0.0138   0.2436   0.9951
   6.750   0.9386   0.00945   0.00429  -0.0156   0.2354   0.9971
   7.000   0.9742   0.00961   0.00445  -0.0174   0.2299   0.9988
   7.250   1.0072   0.00985   0.00465  -0.0187   0.2229   1.0000
   7.500   1.0293   0.01004   0.00484  -0.0177   0.2176   1.0000
   7.750   1.0517   0.01022   0.00501  -0.0167   0.2131   1.0000
   8.000   1.0735   0.01046   0.00524  -0.0157   0.2078   1.0000
   8.250   1.0953   0.01070   0.00547  -0.0147   0.2029   1.0000
   8.500   1.1180   0.01088   0.00566  -0.0138   0.1983   1.0000
   8.750   1.1393   0.01115   0.00591  -0.0128   0.1919   1.0000
   9.000   1.1609   0.01140   0.00616  -0.0118   0.1859   1.0000
   9.250   1.1818   0.01169   0.00642  -0.0107   0.1772   1.0000
   9.500   1.2019   0.01203   0.00672  -0.0095   0.1663   1.0000
   9.750   1.2191   0.01252   0.00711  -0.0079   0.1496   1.0000
  10.000   1.2330   0.01318   0.00765  -0.0060   0.1318   1.0000
  10.250   1.2465   0.01381   0.00820  -0.0039   0.1192   1.0000
  10.750   1.2709   0.01503   0.00934   0.0005   0.1006   1.0000
  11.000   1.2810   0.01568   0.00996   0.0029   0.0922   1.0000
  11.250   1.2829   0.01638   0.01063   0.0067   0.0849   1.0000
  11.750   1.2860   0.01829   0.01253   0.0125   0.0740   1.0000
  12.000   1.2923   0.01947   0.01370   0.0140   0.0705   1.0000
  12.250   1.3011   0.02061   0.01487   0.0151   0.0677   1.0000
  12.500   1.3104   0.02180   0.01608   0.0161   0.0657   1.0000
  12.750   1.3178   0.02321   0.01750   0.0170   0.0638   1.0000
  13.000   1.3250   0.02467   0.01899   0.0177   0.0623   1.0000
  13.250   1.3319   0.02622   0.02058   0.0184   0.0611   1.0000
  13.500   1.3418   0.02755   0.02197   0.0189   0.0604   1.0000
  13.750   1.3506   0.02899   0.02347   0.0193   0.0595   1.0000
  14.000   1.3573   0.03066   0.02519   0.0198   0.0587   1.0000
  14.250   1.3631   0.03243   0.02699   0.0201   0.0576   1.0000
  14.500   1.3667   0.03443   0.02903   0.0204   0.0566   1.0000
  14.750   1.3691   0.03659   0.03123   0.0207   0.0558   1.0000
  15.000   1.3691   0.03901   0.03372   0.0208   0.0549   1.0000
  15.250   1.3679   0.04162   0.03638   0.0209   0.0541   1.0000
  15.500   1.3744   0.04354   0.03837   0.0208   0.0537   1.0000
  15.750   1.3803   0.04557   0.04046   0.0207   0.0532   1.0000
  16.000   1.3835   0.04794   0.04290   0.0205   0.0527   1.0000
  16.250   1.3876   0.05023   0.04524   0.0203   0.0519   1.0000
  16.500   1.3902   0.05272   0.04780   0.0199   0.0512   1.0000
  16.750   1.3906   0.05552   0.05065   0.0195   0.0505   1.0000
  17.000   1.3904   0.05840   0.05358   0.0189   0.0499   1.0000
  17.250   1.3884   0.06154   0.05677   0.0183   0.0493   1.0000
  17.500   1.3836   0.06508   0.06038   0.0175   0.0487   1.0000
  17.750   1.3761   0.06900   0.06436   0.0166   0.0479   1.0000
  18.000   1.3762   0.07200   0.06743   0.0158   0.0475   1.0000
  18.250   1.3808   0.07450   0.07001   0.0152   0.0469   1.0000
  18.500   1.3821   0.07743   0.07300   0.0144   0.0464   1.0000
  18.750   1.3809   0.08069   0.07633   0.0135   0.0458   1.0000
  19.000   1.3796   0.08399   0.07969   0.0125   0.0451   1.0000
  19.250   1.3779   0.08737   0.08313   0.0114   0.0445   1.0000
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