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GOE 735 AIRFOIL (goe735-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 735 AIRFOIL (goe735-il)
Reynolds number: 200,000
Max Cl/Cd: 49.57 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe735-il-200000.txt
Download as CSV file: xf-goe735-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 735 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.2763   0.14355   0.14003  -0.0269   0.9182   0.0911
 -14.500  -0.7698   0.05523   0.05076  -0.0769   1.0000   0.0735
 -14.250  -0.8203   0.04898   0.04417  -0.0790   1.0000   0.0737
 -13.750  -0.6779   0.05327   0.04894  -0.0831   0.9141   0.0779
 -13.500  -0.7329   0.04689   0.04209  -0.0841   0.8894   0.0782
 -13.250  -0.7656   0.04363   0.03848  -0.0812   0.8722   0.0788
 -13.000  -0.7935   0.04122   0.03572  -0.0768   0.8582   0.0797
 -12.750  -0.8220   0.03910   0.03319  -0.0711   0.8456   0.0806
 -12.500  -0.8295   0.03761   0.03150  -0.0670   0.8346   0.0818
 -12.250  -0.8111   0.03729   0.03123  -0.0655   0.8252   0.0831
 -12.000  -0.8001   0.03688   0.03081  -0.0632   0.8151   0.0845
 -11.750  -0.7941   0.03619   0.02997  -0.0602   0.8062   0.0862
 -11.500  -0.7969   0.03491   0.02838  -0.0563   0.7971   0.0883
 -11.250  -0.7929   0.03366   0.02687  -0.0531   0.7885   0.0902
 -11.000  -0.7707   0.03335   0.02664  -0.0522   0.7798   0.0919
 -10.750  -0.7535   0.03295   0.02620  -0.0505   0.7707   0.0941
 -10.500  -0.7434   0.03213   0.02514  -0.0478   0.7632   0.0966
 -10.250  -0.7348   0.03098   0.02369  -0.0451   0.7540   0.0991
 -10.000  -0.7111   0.03053   0.02330  -0.0443   0.7463   0.1011
  -9.750  -0.6906   0.03019   0.02296  -0.0431   0.7368   0.1036
  -9.500  -0.6748   0.02954   0.02208  -0.0410   0.7285   0.1065
  -9.250  -0.6601   0.02863   0.02089  -0.0389   0.7208   0.1091
  -9.000  -0.6350   0.02801   0.02037  -0.0385   0.7114   0.1115
  -8.750  -0.6136   0.02766   0.01992  -0.0371   0.7043   0.1142
  -8.500  -0.5934   0.02714   0.01927  -0.0358   0.6943   0.1173
  -8.250  -0.5749   0.02645   0.01830  -0.0340   0.6866   0.1200
  -8.000  -0.5488   0.02574   0.01768  -0.0338   0.6780   0.1227
  -7.750  -0.5254   0.02534   0.01723  -0.0329   0.6692   0.1256
  -7.500  -0.5029   0.02492   0.01662  -0.0317   0.6620   0.1288
  -7.250  -0.4817   0.02462   0.01612  -0.0303   0.6523   0.1316
  -7.000  -0.4545   0.02357   0.01509  -0.0302   0.6449   0.1348
  -6.750  -0.4293   0.02318   0.01469  -0.0296   0.6363   0.1377
  -6.500  -0.4047   0.02276   0.01416  -0.0289   0.6282   0.1410
  -6.250  -0.3803   0.02240   0.01359  -0.0279   0.6212   0.1439
  -6.000  -0.3535   0.02161   0.01278  -0.0277   0.6121   0.1470
  -5.750  -0.3266   0.02110   0.01224  -0.0274   0.6051   0.1501
  -5.500  -0.3003   0.02074   0.01185  -0.0270   0.5974   0.1534
  -5.250  -0.2744   0.02041   0.01141  -0.0264   0.5898   0.1570
  -5.000  -0.2480   0.02006   0.01086  -0.0258   0.5836   0.1602
  -4.750  -0.2202   0.01944   0.01036  -0.0259   0.5755   0.1641
  -4.500  -0.1937   0.01912   0.01000  -0.0254   0.5686   0.1682
  -4.250  -0.1673   0.01892   0.00967  -0.0249   0.5628   0.1728
  -4.000  -0.1405   0.01853   0.00931  -0.0246   0.5557   0.1773
  -3.750  -0.1143   0.01816   0.00897  -0.0242   0.5494   0.1825
  -3.500  -0.0882   0.01801   0.00870  -0.0237   0.5439   0.1886
  -3.250  -0.0627   0.01770   0.00847  -0.0232   0.5372   0.1952
  -3.000  -0.0376   0.01744   0.00825  -0.0226   0.5312   0.2028
  -2.750  -0.0121   0.01726   0.00799  -0.0220   0.5262   0.2118
  -2.500   0.0118   0.01706   0.00789  -0.0212   0.5210   0.2232
  -2.250   0.0353   0.01682   0.00777  -0.0203   0.5153   0.2377
  -2.000   0.0586   0.01658   0.00760  -0.0194   0.5102   0.2584
  -1.750   0.0810   0.01635   0.00745  -0.0183   0.5056   0.2914
  -1.500   0.1002   0.01603   0.00745  -0.0167   0.5006   0.3460
  -1.250   0.1167   0.01560   0.00740  -0.0146   0.4957   0.4229
  -1.000   0.1289   0.01504   0.00737  -0.0115   0.4916   0.5428
  -0.750   0.1470   0.01454   0.00747  -0.0090   0.4878   0.6892
  -0.500   0.2034   0.01472   0.00803  -0.0136   0.4823   0.8172
  -0.250   0.2581   0.01514   0.00848  -0.0180   0.4762   0.8608
   0.000   0.3056   0.01557   0.00879  -0.0210   0.4711   0.8844
   0.250   0.3479   0.01613   0.00917  -0.0230   0.4668   0.9004
   0.500   0.3856   0.01663   0.00967  -0.0244   0.4622   0.9150
   0.750   0.4366   0.01712   0.01010  -0.0283   0.4571   0.9246
   1.000   0.4804   0.01747   0.01034  -0.0310   0.4527   0.9349
   1.250   0.5247   0.01785   0.01055  -0.0338   0.4486   0.9457
   1.500   0.5799   0.01827   0.01095  -0.0389   0.4437   0.9549
   1.750   0.6387   0.01860   0.01125  -0.0447   0.4386   0.9682
   2.000   0.6876   0.01876   0.01133  -0.0488   0.4344   0.9790
   2.250   0.7396   0.01872   0.01115  -0.0536   0.4307   0.9862
   2.500   0.7881   0.01882   0.01118  -0.0580   0.4270   0.9945
   2.750   0.8296   0.01877   0.01119  -0.0612   0.4227   1.0000
   3.000   0.8496   0.01892   0.01133  -0.0602   0.4191   1.0000
   3.250   0.8702   0.01905   0.01142  -0.0593   0.4160   1.0000
   3.500   0.8916   0.01921   0.01150  -0.0585   0.4133   1.0000
   3.750   0.9135   0.01948   0.01166  -0.0578   0.4107   1.0000
   4.000   0.9324   0.01982   0.01206  -0.0567   0.4079   1.0000
   4.250   0.9506   0.02012   0.01244  -0.0555   0.4048   1.0000
   4.500   0.9696   0.02038   0.01273  -0.0543   0.4015   1.0000
   4.750   0.9897   0.02058   0.01291  -0.0533   0.3986   1.0000
   5.000   1.0109   0.02075   0.01302  -0.0524   0.3959   1.0000
   5.250   1.0332   0.02099   0.01318  -0.0516   0.3935   1.0000
   5.500   1.0531   0.02147   0.01364  -0.0506   0.3910   1.0000
   5.750   1.0679   0.02190   0.01420  -0.0489   0.3882   1.0000
   6.000   1.0835   0.02232   0.01470  -0.0473   0.3851   1.0000
   6.250   1.1007   0.02266   0.01506  -0.0459   0.3822   1.0000
   6.500   1.1200   0.02291   0.01530  -0.0447   0.3795   1.0000
   6.750   1.1412   0.02317   0.01550  -0.0437   0.3773   1.0000
   7.000   1.1643   0.02349   0.01574  -0.0431   0.3750   1.0000
   7.250   1.1785   0.02411   0.01642  -0.0413   0.3724   1.0000
   7.500   1.1873   0.02472   0.01717  -0.0388   0.3695   1.0000
   7.750   1.1982   0.02526   0.01779  -0.0365   0.3665   1.0000
   8.000   1.2120   0.02569   0.01825  -0.0345   0.3638   1.0000
   8.250   1.2306   0.02595   0.01848  -0.0332   0.3613   1.0000
   8.500   1.2536   0.02615   0.01862  -0.0325   0.3590   1.0000
   8.750   1.2800   0.02656   0.01893  -0.0325   0.3567   1.0000
   9.000   1.2799   0.02740   0.01993  -0.0287   0.3542   1.0000
   9.250   1.2777   0.02826   0.02094  -0.0248   0.3513   1.0000
   9.500   1.2792   0.02899   0.02175  -0.0213   0.3485   1.0000
   9.750   1.2867   0.02955   0.02234  -0.0186   0.3460   1.0000
  10.000   1.3033   0.02988   0.02266  -0.0171   0.3437   1.0000
  10.250   1.3311   0.02999   0.02271  -0.0172   0.3416   1.0000
  10.500   1.3641   0.03035   0.02297  -0.0181   0.3391   1.0000
  10.750   1.3287   0.03177   0.02460  -0.0098   0.3368   1.0000
  11.000   1.2847   0.03371   0.02671  -0.0017   0.3339   1.0000
  11.250   1.2581   0.03589   0.02901   0.0028   0.3307   1.0000
  11.500   1.2595   0.03707   0.03023   0.0048   0.3280   1.0000
  11.750   1.2859   0.03706   0.03019   0.0050   0.3259   1.0000
  12.000   1.3295   0.03638   0.02943   0.0040   0.3242   1.0000
  12.250   1.3476   0.03715   0.03020   0.0047   0.3218   1.0000
  12.500   1.0444   0.06329   0.05696   0.0128   0.3056   1.0000
  12.750   1.0914   0.06051   0.05416   0.0135   0.3055   1.0000
  13.000   1.1428   0.05756   0.05117   0.0141   0.3054   1.0000
  13.250   1.2053   0.05380   0.04736   0.0144   0.3054   1.0000
  13.500   1.2921   0.04859   0.04203   0.0139   0.3058   1.0000
  14.000   0.6897   0.13380   0.12793  -0.0024   0.2414   1.0000
  14.250   0.7581   0.12617   0.12027   0.0008   0.2445   1.0000
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