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GOE 629 AIRFOIL (goe629-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 629 AIRFOIL (goe629-il)
Reynolds number: 200,000
Max Cl/Cd: 66.25 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe629-il-200000-n5.txt
Download as CSV file: xf-goe629-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 629 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.000  -0.8358   0.06990   0.06542  -0.0724   1.0000   0.0503
 -14.750  -0.9228   0.05311   0.04829  -0.0836   1.0000   0.0491
 -14.500  -0.9515   0.04594   0.04094  -0.0886   1.0000   0.0494
 -14.250  -0.9698   0.04134   0.03618  -0.0911   1.0000   0.0501
 -14.000  -0.9832   0.03833   0.03305  -0.0912   1.0000   0.0511
 -13.750  -0.9956   0.03615   0.03073  -0.0895   1.0000   0.0521
 -13.500  -1.0079   0.03450   0.02894  -0.0864   1.0000   0.0532
 -13.250  -1.0218   0.03325   0.02753  -0.0818   1.0000   0.0543
 -13.000  -1.0333   0.03246   0.02670  -0.0766   1.0000   0.0551
 -12.750  -1.0354   0.03176   0.02597  -0.0727   1.0000   0.0562
 -12.500  -1.0346   0.03111   0.02525  -0.0692   1.0000   0.0575
 -12.250  -1.0325   0.03039   0.02441  -0.0657   1.0000   0.0591
 -12.000  -1.0291   0.02962   0.02348  -0.0625   1.0000   0.0608
 -11.750  -1.0075   0.02871   0.02240  -0.0626   0.9975   0.0630
 -11.500  -0.9799   0.02811   0.02176  -0.0637   0.9943   0.0649
 -11.250  -0.9535   0.02748   0.02099  -0.0644   0.9908   0.0673
 -11.000  -0.9275   0.02673   0.02002  -0.0651   0.9871   0.0700
 -10.750  -0.8997   0.02605   0.01926  -0.0660   0.9841   0.0724
 -10.500  -0.8718   0.02567   0.01884  -0.0668   0.9808   0.0750
 -10.250  -0.8465   0.02512   0.01817  -0.0669   0.9764   0.0776
 -10.000  -0.8186   0.02439   0.01723  -0.0676   0.9731   0.0798
  -9.750  -0.7887   0.02358   0.01629  -0.0687   0.9707   0.0816
  -9.500  -0.7656   0.02297   0.01567  -0.0683   0.9657   0.0834
  -9.250  -0.7382   0.02241   0.01505  -0.0687   0.9618   0.0852
  -9.000  -0.7078   0.02183   0.01437  -0.0696   0.9590   0.0873
  -8.750  -0.6755   0.02125   0.01365  -0.0709   0.9569   0.0896
  -8.500  -0.6534   0.02076   0.01302  -0.0699   0.9510   0.0913
  -8.250  -0.6255   0.02013   0.01239  -0.0703   0.9471   0.0933
  -8.000  -0.5937   0.01964   0.01189  -0.0714   0.9443   0.0956
  -7.750  -0.5587   0.01916   0.01134  -0.0730   0.9421   0.0982
  -7.500  -0.5344   0.01873   0.01083  -0.0723   0.9349   0.1005
  -7.250  -0.5005   0.01821   0.01019  -0.0736   0.9302   0.1029
  -7.000  -0.4643   0.01766   0.00966  -0.0753   0.9269   0.1058
  -6.750  -0.4376   0.01731   0.00930  -0.0752   0.9210   0.1087
  -6.500  -0.4101   0.01697   0.00890  -0.0751   0.9155   0.1119
  -6.250  -0.3779   0.01659   0.00843  -0.0759   0.9118   0.1152
  -6.000  -0.3444   0.01618   0.00805  -0.0771   0.9090   0.1189
  -5.750  -0.3229   0.01596   0.00782  -0.0758   0.9012   0.1226
  -5.500  -0.2924   0.01566   0.00746  -0.0762   0.8964   0.1274
  -5.250  -0.2596   0.01529   0.00709  -0.0772   0.8928   0.1319
  -5.000  -0.2360   0.01507   0.00687  -0.0763   0.8851   0.1365
  -4.750  -0.2060   0.01483   0.00657  -0.0766   0.8795   0.1425
  -4.250  -0.1504   0.01433   0.00608  -0.0764   0.8670   0.1540
  -4.000  -0.1196   0.01411   0.00579  -0.0768   0.8613   0.1599
  -3.750  -0.0929   0.01383   0.00556  -0.0765   0.8540   0.1655
  -3.500  -0.0651   0.01363   0.00534  -0.0763   0.8464   0.1718
  -3.250  -0.0352   0.01342   0.00511  -0.0766   0.8402   0.1783
  -3.000  -0.0102   0.01323   0.00495  -0.0759   0.8314   0.1849
  -2.750   0.0208   0.01304   0.00472  -0.0763   0.8249   0.1921
  -2.500   0.0449   0.01287   0.00459  -0.0754   0.8148   0.1986
  -2.250   0.0741   0.01269   0.00440  -0.0755   0.8070   0.2070
  -2.000   0.0992   0.01254   0.00429  -0.0748   0.7969   0.2162
  -1.750   0.1269   0.01239   0.00416  -0.0746   0.7883   0.2279
  -1.250   0.1783   0.01208   0.00396  -0.0734   0.7664   0.2639
  -1.000   0.2044   0.01191   0.00386  -0.0729   0.7541   0.2888
  -0.750   0.2301   0.01177   0.00375  -0.0722   0.7406   0.3145
  -0.500   0.2542   0.01162   0.00368  -0.0713   0.7258   0.3437
  -0.250   0.2782   0.01148   0.00362  -0.0703   0.7104   0.3791
   0.000   0.3017   0.01133   0.00358  -0.0693   0.6956   0.4223
   0.250   0.3249   0.01117   0.00357  -0.0681   0.6824   0.4719
   0.500   0.3476   0.01101   0.00356  -0.0669   0.6699   0.5285
   0.750   0.3691   0.01082   0.00359  -0.0654   0.6573   0.5972
   1.000   0.3900   0.01059   0.00367  -0.0636   0.6454   0.6868
   1.250   0.4177   0.01044   0.00382  -0.0630   0.6339   0.7925
   1.500   0.4675   0.01052   0.00401  -0.0670   0.6209   0.8754
   1.750   0.5157   0.01068   0.00416  -0.0710   0.6078   0.9175
   2.000   0.5545   0.01084   0.00428  -0.0730   0.5963   0.9409
   2.250   0.5945   0.01102   0.00439  -0.0754   0.5850   0.9590
   2.500   0.6358   0.01122   0.00453  -0.0781   0.5726   0.9773
   2.750   0.6814   0.01140   0.00466  -0.0818   0.5603   0.9917
   3.000   0.7233   0.01156   0.00477  -0.0848   0.5492   1.0000
   3.250   0.7426   0.01172   0.00487  -0.0830   0.5380   1.0000
   3.500   0.7617   0.01187   0.00499  -0.0812   0.5257   1.0000
   3.750   0.7803   0.01205   0.00512  -0.0793   0.5123   1.0000
   4.000   0.7984   0.01225   0.00525  -0.0773   0.4978   1.0000
   4.250   0.8160   0.01245   0.00539  -0.0752   0.4816   1.0000
   4.500   0.8336   0.01265   0.00554  -0.0731   0.4651   1.0000
   4.750   0.8506   0.01286   0.00570  -0.0709   0.4464   1.0000
   5.000   0.8672   0.01309   0.00587  -0.0686   0.4260   1.0000
   5.250   0.8834   0.01335   0.00606  -0.0663   0.4061   1.0000
   5.500   0.8995   0.01362   0.00626  -0.0640   0.3883   1.0000
   5.750   0.9147   0.01394   0.00649  -0.0615   0.3705   1.0000
   6.000   0.9289   0.01429   0.00675  -0.0589   0.3525   1.0000
   6.250   0.9428   0.01467   0.00704  -0.0562   0.3354   1.0000
   6.500   0.9564   0.01507   0.00735  -0.0535   0.3185   1.0000
   6.750   0.9703   0.01546   0.00768  -0.0509   0.3023   1.0000
   7.000   0.9845   0.01585   0.00803  -0.0484   0.2871   1.0000
   7.250   0.9982   0.01621   0.00837  -0.0458   0.2731   1.0000
   7.500   1.0112   0.01659   0.00872  -0.0431   0.2585   1.0000
   7.750   1.0234   0.01702   0.00910  -0.0403   0.2415   1.0000
   8.000   1.0344   0.01752   0.00954  -0.0374   0.2220   1.0000
   8.250   1.0454   0.01808   0.01001  -0.0346   0.2015   1.0000
   8.500   1.0551   0.01874   0.01056  -0.0318   0.1812   1.0000
   8.750   1.0645   0.01946   0.01119  -0.0290   0.1637   1.0000
   9.000   1.0752   0.02017   0.01184  -0.0265   0.1502   1.0000
   9.250   1.0866   0.02087   0.01252  -0.0242   0.1387   1.0000
   9.500   1.0979   0.02160   0.01323  -0.0220   0.1291   1.0000
   9.750   1.1088   0.02237   0.01399  -0.0198   0.1192   1.0000
  10.000   1.1205   0.02314   0.01477  -0.0178   0.1103   1.0000
  10.250   1.1306   0.02401   0.01564  -0.0157   0.1017   1.0000
  10.750   1.1494   0.02595   0.01756  -0.0117   0.0851   1.0000
  11.000   1.1579   0.02703   0.01865  -0.0098   0.0776   1.0000
  11.250   1.1650   0.02824   0.01985  -0.0079   0.0708   1.0000
  11.500   1.1736   0.02939   0.02105  -0.0062   0.0641   1.0000
  11.750   1.1806   0.03070   0.02239  -0.0045   0.0588   1.0000
  12.000   1.1867   0.03213   0.02383  -0.0029   0.0547   1.0000
  12.250   1.1927   0.03361   0.02536  -0.0014   0.0516   1.0000
  12.500   1.1981   0.03520   0.02699  -0.0001   0.0491   1.0000
  12.750   1.2018   0.03698   0.02881   0.0012   0.0472   1.0000
  13.000   1.2060   0.03879   0.03069   0.0023   0.0458   1.0000
  13.250   1.2100   0.04067   0.03266   0.0033   0.0445   1.0000
  13.500   1.2129   0.04273   0.03479   0.0042   0.0432   1.0000
  13.750   1.2149   0.04495   0.03708   0.0048   0.0423   1.0000
  14.000   1.2155   0.04738   0.03958   0.0054   0.0415   1.0000
  14.250   1.2148   0.05004   0.04230   0.0058   0.0408   1.0000
  14.500   1.2154   0.05264   0.04499   0.0060   0.0401   1.0000
  14.750   1.2170   0.05520   0.04766   0.0062   0.0394   1.0000
  15.000   1.2180   0.05791   0.05047   0.0062   0.0388   1.0000
  15.250   1.2184   0.06074   0.05339   0.0061   0.0380   1.0000
  15.500   1.2182   0.06369   0.05643   0.0059   0.0372   1.0000
  15.750   1.2179   0.06671   0.05953   0.0055   0.0367   1.0000
  16.000   1.2168   0.06989   0.06278   0.0051   0.0362   1.0000
  16.250   1.2154   0.07313   0.06609   0.0045   0.0356   1.0000
  16.500   1.2141   0.07635   0.06935   0.0041   0.0351   1.0000
  16.750   1.2139   0.07952   0.07261   0.0035   0.0346   1.0000
  17.000   1.2140   0.08274   0.07594   0.0028   0.0342   1.0000
  17.250   1.2136   0.08610   0.07943   0.0019   0.0336   1.0000
  17.500   1.2128   0.08953   0.08297   0.0010   0.0331   1.0000
  17.750   1.2114   0.09310   0.08665  -0.0001   0.0325   1.0000
  18.000   1.2104   0.09665   0.09029  -0.0012   0.0321   1.0000
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