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GOE 701 AIRFOIL (goe701-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 701 AIRFOIL (goe701-il)
Reynolds number: 500,000
Max Cl/Cd: 108.69 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe701-il-500000.txt
Download as CSV file: xf-goe701-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 701 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.500  -0.3322   0.14135   0.13887  -0.0388   1.0000   0.0340
 -13.250  -0.9040   0.03967   0.03663  -0.0929   0.9964   0.0319
 -13.000  -0.8938   0.03439   0.03090  -0.0990   0.9911   0.0326
 -12.750  -0.8738   0.03223   0.02868  -0.1010   0.9869   0.0336
 -12.500  -0.8419   0.03167   0.02814  -0.1029   0.9847   0.0345
 -12.250  -0.8114   0.03051   0.02686  -0.1054   0.9828   0.0357
 -12.000  -0.7910   0.02907   0.02520  -0.1060   0.9778   0.0369
 -11.750  -0.7674   0.02739   0.02324  -0.1074   0.9739   0.0381
 -11.500  -0.7380   0.02630   0.02215  -0.1090   0.9717   0.0392
 -11.250  -0.7029   0.02597   0.02182  -0.1109   0.9703   0.0403
 -11.000  -0.6773   0.02517   0.02091  -0.1113   0.9662   0.0415
 -10.750  -0.6524   0.02419   0.01974  -0.1117   0.9616   0.0427
 -10.500  -0.6229   0.02306   0.01837  -0.1130   0.9590   0.0439
 -10.250  -0.5912   0.02197   0.01727  -0.1147   0.9573   0.0453
 -10.000  -0.5554   0.02146   0.01675  -0.1167   0.9562   0.0466
  -9.750  -0.5194   0.02081   0.01599  -0.1188   0.9552   0.0481
  -9.500  -0.4992   0.02023   0.01527  -0.1175   0.9479   0.0493
  -9.250  -0.4674   0.01973   0.01459  -0.1185   0.9447   0.0503
  -9.000  -0.4383   0.01816   0.01295  -0.1197   0.9419   0.0521
  -8.750  -0.4040   0.01762   0.01238  -0.1212   0.9398   0.0535
  -8.500  -0.3836   0.01721   0.01189  -0.1197   0.9316   0.0547
  -8.250  -0.3534   0.01661   0.01118  -0.1202   0.9272   0.0561
  -8.000  -0.3211   0.01606   0.01049  -0.1212   0.9237   0.0573
  -7.750  -0.3017   0.01527   0.00957  -0.1196   0.9147   0.0585
  -7.500  -0.2733   0.01452   0.00878  -0.1198   0.9094   0.0601
  -7.250  -0.2483   0.01412   0.00833  -0.1192   0.9018   0.0613
  -7.000  -0.2210   0.01372   0.00787  -0.1189   0.8949   0.0628
  -6.750  -0.1935   0.01338   0.00743  -0.1188   0.8881   0.0645
  -6.500  -0.1675   0.01306   0.00700  -0.1182   0.8802   0.0658
  -6.250  -0.1406   0.01246   0.00632  -0.1180   0.8735   0.0675
  -6.000  -0.1160   0.01210   0.00595  -0.1172   0.8651   0.0694
  -5.750  -0.0873   0.01188   0.00566  -0.1173   0.8586   0.0716
  -5.500  -0.0624   0.01169   0.00542  -0.1165   0.8503   0.0737
  -5.250  -0.0338   0.01151   0.00513  -0.1164   0.8436   0.0756
  -5.000  -0.0100   0.01113   0.00477  -0.1155   0.8357   0.0787
  -4.750   0.0174   0.01100   0.00459  -0.1152   0.8289   0.0816
  -4.500   0.0439   0.01089   0.00443  -0.1148   0.8217   0.0849
  -4.250   0.0696   0.01068   0.00419  -0.1142   0.8146   0.0889
  -4.000   0.0972   0.01061   0.00410  -0.1139   0.8082   0.0934
  -3.750   0.1231   0.01056   0.00401  -0.1133   0.8009   0.0978
  -3.500   0.1497   0.01034   0.00378  -0.1130   0.7946   0.1037
  -3.250   0.1758   0.01031   0.00373  -0.1124   0.7878   0.1091
  -3.000   0.2019   0.01018   0.00356  -0.1119   0.7811   0.1144
  -2.750   0.2288   0.01010   0.00346  -0.1116   0.7749   0.1197
  -2.500   0.2544   0.01004   0.00339  -0.1109   0.7679   0.1241
  -2.250   0.2812   0.00996   0.00325  -0.1106   0.7616   0.1281
  -2.000   0.3066   0.00983   0.00315  -0.1099   0.7549   0.1331
  -1.750   0.3327   0.00978   0.00309  -0.1094   0.7480   0.1377
  -1.500   0.3593   0.00977   0.00301  -0.1089   0.7408   0.1412
  -1.250   0.3836   0.00961   0.00288  -0.1080   0.7322   0.1462
  -1.000   0.4096   0.00957   0.00282  -0.1075   0.7243   0.1514
  -0.750   0.4346   0.00953   0.00277  -0.1067   0.7156   0.1564
  -0.500   0.4599   0.00946   0.00270  -0.1060   0.7074   0.1637
  -0.250   0.4845   0.00943   0.00267  -0.1051   0.6973   0.1719
   0.000   0.5090   0.00936   0.00262  -0.1043   0.6879   0.1813
   0.250   0.5339   0.00933   0.00258  -0.1035   0.6790   0.1932
   0.500   0.5589   0.00928   0.00257  -0.1028   0.6711   0.2087
   0.750   0.5834   0.00922   0.00255  -0.1020   0.6627   0.2262
   1.000   0.6076   0.00915   0.00255  -0.1011   0.6539   0.2473
   1.250   0.6313   0.00909   0.00255  -0.1002   0.6448   0.2777
   1.500   0.6538   0.00891   0.00261  -0.0990   0.6356   0.3522
   1.750   0.6635   0.00806   0.00267  -0.0954   0.6274   0.6767
   2.000   0.7861   0.00792   0.00312  -0.1154   0.6131   0.9911
   2.250   0.8429   0.00804   0.00316  -0.1217   0.5998   1.0000
   2.500   0.8634   0.00815   0.00321  -0.1201   0.5883   1.0000
   2.750   0.8833   0.00828   0.00326  -0.1184   0.5769   1.0000
   3.000   0.9035   0.00839   0.00333  -0.1167   0.5647   1.0000
   3.250   0.9233   0.00852   0.00341  -0.1150   0.5526   1.0000
   3.500   0.9423   0.00867   0.00350  -0.1131   0.5398   1.0000
   3.750   0.9606   0.00885   0.00361  -0.1110   0.5259   1.0000
   4.000   0.9782   0.00903   0.00373  -0.1089   0.5113   1.0000
   4.250   0.9956   0.00923   0.00386  -0.1067   0.4960   1.0000
   4.500   1.0128   0.00943   0.00400  -0.1045   0.4804   1.0000
   4.750   1.0289   0.00966   0.00416  -0.1020   0.4637   1.0000
   5.000   1.0440   0.00991   0.00433  -0.0994   0.4449   1.0000
   5.250   1.0585   0.01018   0.00452  -0.0967   0.4244   1.0000
   5.500   1.0714   0.01051   0.00474  -0.0937   0.4023   1.0000
   5.750   1.0817   0.01088   0.00499  -0.0902   0.3784   1.0000
   6.000   1.0894   0.01127   0.00526  -0.0862   0.3533   1.0000
   6.250   1.0972   0.01169   0.00555  -0.0823   0.3304   1.0000
   6.500   1.1074   0.01212   0.00587  -0.0789   0.3093   1.0000
   6.750   1.1190   0.01255   0.00620  -0.0759   0.2926   1.0000
   7.000   1.1321   0.01296   0.00655  -0.0732   0.2795   1.0000
   7.250   1.1449   0.01342   0.00693  -0.0706   0.2675   1.0000
   7.500   1.1606   0.01379   0.00728  -0.0685   0.2583   1.0000
   7.750   1.1752   0.01422   0.00768  -0.0663   0.2507   1.0000
   8.000   1.1913   0.01460   0.00806  -0.0643   0.2428   1.0000
   8.250   1.2056   0.01508   0.00850  -0.0622   0.2358   1.0000
   8.500   1.2230   0.01544   0.00888  -0.0605   0.2294   1.0000
   8.750   1.2377   0.01594   0.00936  -0.0585   0.2238   1.0000
   9.000   1.2540   0.01637   0.00981  -0.0568   0.2185   1.0000
   9.250   1.2710   0.01679   0.01026  -0.0553   0.2132   1.0000
   9.500   1.2847   0.01738   0.01082  -0.0533   0.2073   1.0000
   9.750   1.3019   0.01781   0.01129  -0.0519   0.2021   1.0000
  10.000   1.3180   0.01831   0.01182  -0.0504   0.1965   1.0000
  10.250   1.3311   0.01898   0.01246  -0.0485   0.1898   1.0000
  10.500   1.3488   0.01942   0.01296  -0.0473   0.1843   1.0000
  10.750   1.3627   0.02009   0.01362  -0.0457   0.1778   1.0000
  11.000   1.3782   0.02069   0.01425  -0.0443   0.1713   1.0000
  11.250   1.3915   0.02143   0.01498  -0.0427   0.1630   1.0000
  11.500   1.4056   0.02214   0.01571  -0.0413   0.1544   1.0000
  11.750   1.4171   0.02305   0.01658  -0.0397   0.1446   1.0000
  12.000   1.4264   0.02412   0.01760  -0.0380   0.1309   1.0000
  12.250   1.4329   0.02542   0.01882  -0.0361   0.1149   1.0000
  12.500   1.4343   0.02714   0.02042  -0.0338   0.0964   1.0000
  12.750   1.4338   0.02905   0.02222  -0.0316   0.0773   1.0000
  13.000   1.4210   0.03203   0.02495  -0.0288   0.0439   1.0000
  13.250   1.4170   0.03444   0.02733  -0.0267   0.0361   1.0000
  13.500   1.4193   0.03642   0.02936  -0.0253   0.0336   1.0000
  13.750   1.4198   0.03863   0.03164  -0.0239   0.0317   1.0000
  14.000   1.4223   0.04074   0.03384  -0.0228   0.0303   1.0000
  14.250   1.4246   0.04291   0.03610  -0.0218   0.0292   1.0000
  14.500   1.4244   0.04540   0.03868  -0.0209   0.0282   1.0000
  14.750   1.4197   0.04845   0.04181  -0.0201   0.0272   1.0000
  15.000   1.4108   0.05207   0.04553  -0.0194   0.0264   1.0000
  15.250   1.4123   0.05465   0.04822  -0.0191   0.0258   1.0000
  15.500   1.4107   0.05765   0.05132  -0.0188   0.0253   1.0000
  15.750   1.4083   0.06083   0.05460  -0.0187   0.0247   1.0000
  16.000   1.4027   0.06448   0.05836  -0.0188   0.0241   1.0000
  16.250   1.3965   0.06829   0.06227  -0.0190   0.0237   1.0000
  16.500   1.3885   0.07245   0.06652  -0.0195   0.0233   1.0000
  16.750   1.3777   0.07705   0.07122  -0.0202   0.0229   1.0000
  17.000   1.3639   0.08216   0.07642  -0.0211   0.0225   1.0000
  17.250   1.3464   0.08789   0.08225  -0.0223   0.0221   1.0000
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