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GOE 704 AIRFOIL (goe704-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 704 AIRFOIL (goe704-il)
Reynolds number: 500,000
Max Cl/Cd: 72.68 at α=8°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe704-il-500000-n5.txt
Download as CSV file: xf-goe704-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 704 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.500  -1.0070   0.08435   0.08099  -0.0177   1.0000   0.0090
 -15.250  -1.0803   0.06797   0.06443  -0.0273   1.0000   0.0087
 -15.000  -1.1577   0.04559   0.04153  -0.0462   1.0000   0.0084
 -14.750  -1.1745   0.04084   0.03658  -0.0474   1.0000   0.0084
 -14.500  -1.1834   0.03776   0.03334  -0.0465   1.0000   0.0085
 -14.250  -1.1877   0.03542   0.03085  -0.0448   1.0000   0.0086
 -14.000  -1.1887   0.03350   0.02879  -0.0426   1.0000   0.0087
 -13.750  -1.1873   0.03187   0.02703  -0.0401   1.0000   0.0089
 -13.500  -1.1839   0.03046   0.02549  -0.0375   1.0000   0.0091
 -13.250  -1.1787   0.02922   0.02413  -0.0348   1.0000   0.0093
 -13.000  -1.1689   0.02805   0.02283  -0.0327   1.0000   0.0095
 -12.750  -1.1562   0.02697   0.02163  -0.0309   1.0000   0.0097
 -12.500  -1.1414   0.02599   0.02053  -0.0293   1.0000   0.0099
 -12.250  -1.1281   0.02482   0.01926  -0.0276   1.0000   0.0103
 -12.000  -1.1126   0.02376   0.01811  -0.0261   1.0000   0.0107
 -11.750  -1.0949   0.02287   0.01712  -0.0248   1.0000   0.0112
 -11.500  -1.0760   0.02206   0.01622  -0.0237   1.0000   0.0116
 -11.250  -1.0562   0.02130   0.01538  -0.0226   1.0000   0.0121
 -11.000  -1.0357   0.02060   0.01458  -0.0216   1.0000   0.0126
 -10.750  -1.0145   0.01995   0.01384  -0.0207   1.0000   0.0131
 -10.500  -0.9920   0.01912   0.01294  -0.0202   0.9923   0.0139
 -10.250  -0.9634   0.01840   0.01214  -0.0208   0.9742   0.0149
 -10.000  -0.9359   0.01779   0.01145  -0.0211   0.9561   0.0161
  -9.750  -0.9115   0.01723   0.01081  -0.0206   0.9364   0.0175
  -9.500  -0.8894   0.01670   0.01021  -0.0195   0.9171   0.0195
  -9.250  -0.8671   0.01625   0.00966  -0.0184   0.8994   0.0218
  -9.000  -0.8446   0.01579   0.00913  -0.0174   0.8827   0.0251
  -8.750  -0.8212   0.01536   0.00863  -0.0166   0.8673   0.0287
  -8.500  -0.7969   0.01499   0.00818  -0.0159   0.8534   0.0328
  -8.250  -0.7725   0.01459   0.00773  -0.0153   0.8413   0.0376
  -8.000  -0.7474   0.01424   0.00732  -0.0148   0.8302   0.0419
  -7.750  -0.7221   0.01391   0.00693  -0.0143   0.8196   0.0467
  -7.500  -0.6963   0.01359   0.00656  -0.0140   0.8101   0.0514
  -7.250  -0.6704   0.01329   0.00622  -0.0136   0.8019   0.0572
  -7.000  -0.6442   0.01298   0.00590  -0.0133   0.7938   0.0638
  -6.500  -0.5910   0.01249   0.00538  -0.0129   0.7795   0.0800
  -6.250  -0.5641   0.01229   0.00518  -0.0127   0.7732   0.0892
  -6.000  -0.5368   0.01213   0.00499  -0.0126   0.7675   0.0962
  -5.750  -0.5094   0.01197   0.00481  -0.0125   0.7614   0.1018
  -5.500  -0.4818   0.01184   0.00461  -0.0124   0.7561   0.1055
  -5.250  -0.4543   0.01168   0.00441  -0.0122   0.7512   0.1096
  -5.000  -0.4267   0.01152   0.00425  -0.0122   0.7460   0.1141
  -4.750  -0.3990   0.01140   0.00408  -0.0121   0.7411   0.1178
  -4.500  -0.3711   0.01131   0.00392  -0.0121   0.7368   0.1209
  -4.250  -0.3435   0.01113   0.00375  -0.0120   0.7320   0.1251
  -4.000  -0.3157   0.01100   0.00360  -0.0120   0.7272   0.1292
  -3.750  -0.2879   0.01090   0.00346  -0.0119   0.7230   0.1331
  -3.500  -0.2597   0.01080   0.00333  -0.0119   0.7186   0.1365
  -3.250  -0.2320   0.01064   0.00319  -0.0119   0.7138   0.1421
  -3.000  -0.2041   0.01053   0.00306  -0.0118   0.7088   0.1467
  -2.750  -0.1761   0.01044   0.00294  -0.0118   0.7021   0.1507
  -2.500  -0.1484   0.01032   0.00280  -0.0117   0.6931   0.1551
  -2.250  -0.1206   0.01021   0.00268  -0.0117   0.6848   0.1606
  -2.000  -0.0926   0.01011   0.00257  -0.0117   0.6786   0.1662
  -1.750  -0.0648   0.01001   0.00248  -0.0116   0.6733   0.1739
  -1.500  -0.0367   0.00989   0.00240  -0.0116   0.6675   0.1844
  -1.250  -0.0090   0.00976   0.00232  -0.0116   0.6614   0.1995
  -1.000   0.0186   0.00963   0.00226  -0.0116   0.6555   0.2204
  -0.750   0.0463   0.00949   0.00221  -0.0116   0.6485   0.2466
  -0.500   0.0738   0.00937   0.00216  -0.0115   0.6419   0.2746
  -0.250   0.1014   0.00923   0.00212  -0.0115   0.6334   0.3019
   0.000   0.1287   0.00911   0.00207  -0.0114   0.6231   0.3308
   0.250   0.1556   0.00898   0.00202  -0.0112   0.6084   0.3669
   0.750   0.2055   0.00841   0.00192  -0.0102   0.5801   0.5234
   1.000   0.2165   0.00731   0.00204  -0.0062   0.5682   0.8634
   1.250   0.2443   0.00744   0.00215  -0.0060   0.5515   0.8924
   1.500   0.2718   0.00759   0.00223  -0.0057   0.5312   0.9076
   1.750   0.2990   0.00778   0.00233  -0.0054   0.5066   0.9190
   2.000   0.3248   0.00798   0.00243  -0.0049   0.4816   0.9301
   2.250   0.3525   0.00827   0.00259  -0.0048   0.4525   0.9392
   2.500   0.3788   0.00858   0.00276  -0.0044   0.4201   0.9471
   2.750   0.4083   0.00893   0.00297  -0.0048   0.3904   0.9534
   3.000   0.4343   0.00919   0.00313  -0.0044   0.3692   0.9599
   3.250   0.4701   0.00951   0.00336  -0.0061   0.3487   0.9635
   3.500   0.5045   0.00982   0.00357  -0.0077   0.3294   0.9675
   3.750   0.5302   0.01004   0.00373  -0.0073   0.3137   0.9720
   4.000   0.5658   0.01030   0.00390  -0.0091   0.2981   0.9733
   4.250   0.6025   0.01055   0.00409  -0.0113   0.2838   0.9746
   4.500   0.6357   0.01077   0.00427  -0.0126   0.2707   0.9758
   4.750   0.6654   0.01095   0.00441  -0.0133   0.2598   0.9769
   5.000   0.6938   0.01113   0.00456  -0.0136   0.2499   0.9779
   5.500   0.7489   0.01151   0.00489  -0.0140   0.2316   0.9805
   5.750   0.7749   0.01172   0.00507  -0.0138   0.2237   0.9822
   6.000   0.8001   0.01191   0.00526  -0.0135   0.2156   0.9839
   6.250   0.8297   0.01215   0.00547  -0.0142   0.2074   0.9846
   6.500   0.8594   0.01236   0.00568  -0.0149   0.2007   0.9853
   6.750   0.8884   0.01261   0.00592  -0.0155   0.1945   0.9862
   7.000   0.9170   0.01284   0.00616  -0.0160   0.1866   0.9871
   7.250   0.9445   0.01314   0.00643  -0.0163   0.1773   0.9882
   7.500   0.9716   0.01344   0.00672  -0.0165   0.1679   0.9894
   7.750   0.9984   0.01374   0.00700  -0.0167   0.1587   0.9907
   8.000   1.0240   0.01409   0.00732  -0.0167   0.1475   0.9922
   8.250   1.0489   0.01447   0.00767  -0.0166   0.1342   0.9937
   8.500   1.0740   0.01503   0.00810  -0.0168   0.1091   0.9947
   8.750   1.0975   0.01579   0.00870  -0.0168   0.0880   0.9959
   9.000   1.1234   0.01627   0.00919  -0.0171   0.0818   0.9972
   9.250   1.1479   0.01686   0.00977  -0.0172   0.0747   0.9986
   9.500   1.1734   0.01729   0.01023  -0.0173   0.0685   0.9998
   9.750   1.1862   0.01781   0.01075  -0.0150   0.0606   1.0000
  10.000   1.1841   0.01887   0.01158  -0.0102   0.0313   1.0000
  10.250   1.1840   0.01968   0.01235  -0.0057   0.0221   1.0000
  10.500   1.1822   0.02028   0.01296  -0.0007   0.0190   1.0000
  10.750   1.1834   0.02085   0.01358   0.0036   0.0174   1.0000
  11.000   1.1891   0.02160   0.01436   0.0066   0.0159   1.0000
  11.250   1.1974   0.02246   0.01527   0.0089   0.0146   1.0000
  11.500   1.2083   0.02330   0.01619   0.0107   0.0138   1.0000
  11.750   1.2189   0.02427   0.01722   0.0122   0.0131   1.0000
  12.000   1.2286   0.02538   0.01840   0.0136   0.0124   1.0000
  12.250   1.2372   0.02666   0.01975   0.0149   0.0118   1.0000
  12.500   1.2439   0.02817   0.02133   0.0161   0.0113   1.0000
  12.750   1.2534   0.02952   0.02277   0.0170   0.0110   1.0000
  13.000   1.2618   0.03101   0.02435   0.0178   0.0106   1.0000
  13.250   1.2689   0.03266   0.02610   0.0185   0.0102   1.0000
  13.500   1.2751   0.03446   0.02797   0.0191   0.0099   1.0000
  13.750   1.2801   0.03641   0.03001   0.0196   0.0096   1.0000
  14.000   1.2835   0.03857   0.03225   0.0200   0.0093   1.0000
  14.250   1.2847   0.04103   0.03480   0.0203   0.0090   1.0000
  14.500   1.2832   0.04383   0.03770   0.0205   0.0088   1.0000
  14.750   1.2782   0.04713   0.04111   0.0204   0.0086   1.0000
  15.000   1.2752   0.05034   0.04443   0.0201   0.0084   1.0000
  15.250   1.2723   0.05368   0.04788   0.0196   0.0083   1.0000
  15.500   1.2681   0.05735   0.05167   0.0188   0.0082   1.0000
  15.750   1.2624   0.06140   0.05583   0.0177   0.0081   1.0000
  16.000   1.2550   0.06580   0.06037   0.0164   0.0080   1.0000
  16.250   1.2465   0.07054   0.06523   0.0149   0.0079   1.0000
  16.500   1.2362   0.07568   0.07050   0.0130   0.0078   1.0000
  16.750   1.2250   0.08104   0.07598   0.0110   0.0077   1.0000
  17.000   1.2125   0.08670   0.08177   0.0089   0.0077   1.0000
  17.250   1.2000   0.09245   0.08763   0.0066   0.0076   1.0000
  17.500   1.1872   0.09831   0.09360   0.0043   0.0075   1.0000
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