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GOE 703 AIRFOIL (goe703-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 703 AIRFOIL (goe703-il)
Reynolds number: 200,000
Max Cl/Cd: 63.26 at α=7.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe703-il-200000.txt
Download as CSV file: xf-goe703-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 703 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -0.7698   0.07321   0.06794  -0.0867   1.0000   0.0593
 -15.250  -0.8000   0.06785   0.06240  -0.0874   1.0000   0.0591
 -15.000  -0.8229   0.06358   0.05799  -0.0869   1.0000   0.0590
 -14.750  -0.8469   0.05980   0.05403  -0.0856   1.0000   0.0588
 -14.500  -0.8706   0.05646   0.05051  -0.0834   1.0000   0.0588
 -14.250  -0.8911   0.05357   0.04743  -0.0805   1.0000   0.0587
 -14.000  -0.9101   0.05109   0.04477  -0.0769   1.0000   0.0587
 -13.750  -0.9269   0.04889   0.04239  -0.0730   1.0000   0.0587
 -13.500  -0.9401   0.04698   0.04031  -0.0688   1.0000   0.0587
 -13.250  -0.9555   0.04536   0.03852  -0.0639   1.0000   0.0588
 -13.000  -0.9711   0.04398   0.03698  -0.0584   1.0000   0.0589
 -12.750  -0.9884   0.04296   0.03582  -0.0523   1.0000   0.0590
 -12.500  -1.0079   0.04221   0.03496  -0.0455   1.0000   0.0591
 -12.250  -1.0294   0.04169   0.03434  -0.0382   1.0000   0.0591
 -12.000  -1.0392   0.04087   0.03334  -0.0330   0.9985   0.0593
 -11.750  -1.0000   0.03835   0.03076  -0.0365   0.9957   0.0601
 -11.500  -0.9623   0.03680   0.02920  -0.0396   0.9924   0.0611
 -11.250  -0.9306   0.03537   0.02769  -0.0414   0.9875   0.0621
 -11.000  -0.8966   0.03400   0.02620  -0.0436   0.9829   0.0633
 -10.750  -0.8591   0.03254   0.02457  -0.0463   0.9796   0.0643
 -10.500  -0.8300   0.03130   0.02313  -0.0473   0.9725   0.0653
 -10.250  -0.7857   0.02976   0.02157  -0.0509   0.9694   0.0665
 -10.000  -0.7409   0.02852   0.02042  -0.0547   0.9669   0.0682
  -9.750  -0.7074   0.02751   0.01939  -0.0562   0.9598   0.0702
  -9.500  -0.6694   0.02652   0.01829  -0.0586   0.9549   0.0723
  -9.250  -0.6261   0.02525   0.01714  -0.0621   0.9520   0.0750
  -9.000  -0.5940   0.02437   0.01628  -0.0634   0.9446   0.0777
  -8.750  -0.5562   0.02330   0.01520  -0.0657   0.9394   0.0812
  -8.500  -0.5150   0.02224   0.01421  -0.0690   0.9356   0.0859
  -8.250  -0.4811   0.02127   0.01329  -0.0707   0.9274   0.0917
  -8.000  -0.4414   0.02027   0.01236  -0.0737   0.9208   0.1009
  -7.750  -0.4014   0.01931   0.01149  -0.0768   0.9137   0.1160
  -7.500  -0.3683   0.01845   0.01077  -0.0785   0.9025   0.1386
  -7.250  -0.3353   0.01780   0.01020  -0.0801   0.8907   0.1637
  -7.000  -0.3001   0.01734   0.00971  -0.0820   0.8790   0.1856
  -6.750  -0.2792   0.01706   0.00942  -0.0808   0.8633   0.2004
  -6.500  -0.2560   0.01678   0.00914  -0.0801   0.8498   0.2143
  -6.250  -0.2306   0.01653   0.00881  -0.0798   0.8375   0.2284
  -6.000  -0.2151   0.01639   0.00863  -0.0774   0.8229   0.2410
  -5.750  -0.1949   0.01614   0.00839  -0.0760   0.8111   0.2543
  -5.500  -0.1773   0.01592   0.00817  -0.0740   0.7990   0.2682
  -5.250  -0.1587   0.01575   0.00796  -0.0722   0.7883   0.2835
  -5.000  -0.1413   0.01549   0.00772  -0.0702   0.7776   0.3004
  -4.750  -0.1251   0.01521   0.00751  -0.0680   0.7676   0.3199
  -4.500  -0.1107   0.01490   0.00727  -0.0654   0.7579   0.3444
  -4.250  -0.0981   0.01449   0.00703  -0.0625   0.7498   0.3750
  -4.000  -0.0932   0.01407   0.00685  -0.0580   0.7404   0.4158
  -3.750  -0.0915   0.01351   0.00660  -0.0528   0.7333   0.4838
  -3.500  -0.0929   0.01303   0.00661  -0.0467   0.7249   0.5785
  -3.250  -0.0258   0.01325   0.00736  -0.0535   0.7175   0.7114
  -3.000   0.0269   0.01395   0.00801  -0.0572   0.7112   0.7539
  -2.750   0.0593   0.01454   0.00860  -0.0572   0.7028   0.7752
  -2.500   0.0855   0.01498   0.00895  -0.0560   0.6958   0.7924
  -2.250   0.1080   0.01541   0.00927  -0.0542   0.6895   0.8077
  -2.000   0.1549   0.01630   0.01009  -0.0569   0.6815   0.8127
  -1.750   0.1980   0.01698   0.01065  -0.0589   0.6749   0.8193
  -1.500   0.2248   0.01738   0.01096  -0.0582   0.6686   0.8298
  -1.250   0.2699   0.01800   0.01153  -0.0608   0.6610   0.8343
  -1.000   0.2878   0.01821   0.01165  -0.0586   0.6549   0.8465
  -0.750   0.3401   0.01881   0.01214  -0.0627   0.6483   0.8497
  -0.500   0.3819   0.01925   0.01256  -0.0649   0.6411   0.8554
  -0.250   0.4060   0.01951   0.01274  -0.0639   0.6352   0.8659
   0.000   0.4602   0.01998   0.01310  -0.0685   0.6289   0.8702
   0.250   0.4766   0.02028   0.01342  -0.0661   0.6226   0.8827
   0.500   0.5297   0.02047   0.01354  -0.0707   0.6158   0.8862
   0.750   0.5763   0.02073   0.01367  -0.0741   0.6101   0.8924
   1.000   0.6014   0.02091   0.01391  -0.0735   0.6033   0.9026
   1.250   0.6478   0.02094   0.01391  -0.0770   0.5964   0.9086
   1.500   0.6689   0.02118   0.01406  -0.0758   0.5913   0.9184
   1.750   0.7081   0.02103   0.01393  -0.0782   0.5845   0.9218
   2.000   0.7395   0.02096   0.01386  -0.0791   0.5779   0.9269
   2.250   0.7578   0.02116   0.01399  -0.0774   0.5724   0.9351
   2.500   0.7973   0.02095   0.01378  -0.0799   0.5661   0.9384
   2.750   0.8277   0.02084   0.01370  -0.0807   0.5587   0.9438
   3.000   0.8477   0.02101   0.01382  -0.0793   0.5529   0.9512
   3.250   0.8857   0.02070   0.01350  -0.0816   0.5454   0.9549
   3.500   0.9146   0.02056   0.01337  -0.0821   0.5375   0.9603
   3.750   0.9404   0.02060   0.01333  -0.0819   0.5310   0.9667
   4.000   0.9741   0.02025   0.01304  -0.0834   0.5223   0.9713
   4.250   1.0020   0.02013   0.01289  -0.0837   0.5145   0.9769
   4.500   1.0353   0.01989   0.01264  -0.0851   0.5068   0.9826
   4.750   1.0671   0.01955   0.01232  -0.0862   0.4974   0.9881
   5.000   1.1077   0.01914   0.01185  -0.0891   0.4891   0.9953
   5.250   1.1404   0.01878   0.01156  -0.0906   0.4801   1.0000
   5.500   1.1584   0.01885   0.01156  -0.0890   0.4739   1.0000
   5.750   1.1723   0.01899   0.01178  -0.0866   0.4666   1.0000
   6.000   1.1870   0.01909   0.01190  -0.0844   0.4595   1.0000
   6.250   1.2051   0.01922   0.01195  -0.0828   0.4533   1.0000
   6.500   1.2163   0.01939   0.01224  -0.0800   0.4455   1.0000
   6.750   1.2309   0.01951   0.01234  -0.0777   0.4386   1.0000
   7.000   1.2443   0.01970   0.01255  -0.0752   0.4313   1.0000
   7.250   1.2547   0.01985   0.01274  -0.0722   0.4230   1.0000
   7.500   1.2678   0.02004   0.01287  -0.0697   0.4155   1.0000
   7.750   1.2750   0.02024   0.01316  -0.0660   0.4066   1.0000
   8.000   1.2865   0.02045   0.01327  -0.0632   0.3989   1.0000
   8.250   1.2903   0.02069   0.01363  -0.0590   0.3900   1.0000
   8.500   1.2979   0.02094   0.01382  -0.0555   0.3822   1.0000
   8.750   1.3004   0.02123   0.01419  -0.0511   0.3743   1.0000
   9.000   1.3020   0.02151   0.01446  -0.0465   0.3664   1.0000
   9.250   1.2974   0.02180   0.01477  -0.0408   0.3591   1.0000
   9.500   1.2904   0.02209   0.01509  -0.0347   0.3516   1.0000
   9.750   1.2852   0.02246   0.01542  -0.0291   0.3439   1.0000
  10.000   1.2776   0.02287   0.01591  -0.0233   0.3357   1.0000
  10.250   1.2739   0.02337   0.01633  -0.0183   0.3281   1.0000
  10.500   1.2660   0.02394   0.01700  -0.0128   0.3193   1.0000
  11.000   1.2527   0.02535   0.01843  -0.0029   0.3017   1.0000
  11.250   1.2457   0.02621   0.01922   0.0018   0.2931   1.0000
  11.500   1.2377   0.02716   0.02023   0.0064   0.2831   1.0000
  11.750   1.2302   0.02823   0.02127   0.0107   0.2739   1.0000
  12.000   1.2223   0.02940   0.02244   0.0148   0.2642   1.0000
  12.250   1.2150   0.03066   0.02370   0.0186   0.2547   1.0000
  12.500   1.2073   0.03204   0.02502   0.0222   0.2458   1.0000
  12.750   1.2017   0.03343   0.02644   0.0254   0.2369   1.0000
  13.000   1.1960   0.03490   0.02783   0.0285   0.2296   1.0000
  13.250   1.1937   0.03630   0.02928   0.0311   0.2225   1.0000
  13.500   1.1905   0.03780   0.03075   0.0336   0.2162   1.0000
  13.750   1.1894   0.03925   0.03218   0.0359   0.2105   1.0000
  14.000   1.1883   0.04079   0.03376   0.0379   0.2046   1.0000
  14.250   1.1877   0.04229   0.03519   0.0399   0.1994   1.0000
  14.500   1.1886   0.04381   0.03676   0.0416   0.1945   1.0000
  14.750   1.1891   0.04543   0.03842   0.0432   0.1898   1.0000
  15.000   1.1911   0.04690   0.03984   0.0447   0.1853   1.0000
  15.250   1.1937   0.04842   0.04139   0.0461   0.1811   1.0000
  15.500   1.1941   0.05021   0.04326   0.0473   0.1769   1.0000
  15.750   1.1955   0.05192   0.04496   0.0485   0.1726   1.0000
  16.000   1.2010   0.05325   0.04624   0.0497   0.1685   1.0000
  16.250   1.1984   0.05550   0.04863   0.0506   0.1643   1.0000
  16.500   1.1979   0.05756   0.05072   0.0514   0.1599   1.0000
  16.750   1.2018   0.05911   0.05219   0.0523   0.1551   1.0000
  17.000   1.1967   0.06181   0.05504   0.0529   0.1507   1.0000
  17.250   1.1938   0.06426   0.05750   0.0534   0.1457   1.0000
  17.500   1.1934   0.06646   0.05970   0.0539   0.1409   1.0000
  17.750   1.1864   0.06956   0.06291   0.0541   0.1355   1.0000
  18.000   1.1866   0.07172   0.06497   0.0545   0.1301   1.0000
  18.250   1.1768   0.07535   0.06875   0.0544   0.1248   1.0000
  18.500   1.1772   0.07756   0.07084   0.0546   0.1196   1.0000
  18.750   1.1675   0.08132   0.07476   0.0543   0.1146   1.0000
  19.000   1.1653   0.08406   0.07748   0.0541   0.1104   1.0000
  19.250   1.1632   0.08682   0.08027   0.0540   0.1064   1.0000
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