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GOE 522 AIRFOIL (goe522-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 522 AIRFOIL (goe522-il)
Reynolds number: 200,000
Max Cl/Cd: 57.09 at α=6.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe522-il-200000.txt
Download as CSV file: xf-goe522-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 522 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
  ------ -------- --------- --------- -------- -------- --------
 -15.250  -0.6724   0.08057   0.07565  -0.0893   0.9953   0.0552
 -15.000  -0.7020   0.07155   0.06630  -0.0976   0.9923   0.0549
 -14.750  -0.7144   0.06569   0.06022  -0.1028   0.9882   0.0548
 -14.500  -0.7174   0.06106   0.05539  -0.1074   0.9839   0.0549
 -14.250  -0.7108   0.05729   0.05146  -0.1119   0.9805   0.0550
 -14.000  -0.7000   0.05391   0.04791  -0.1165   0.9778   0.0553
 -13.750  -0.6985   0.05128   0.04516  -0.1178   0.9709   0.0556
 -13.500  -0.6864   0.04863   0.04237  -0.1210   0.9668   0.0560
 -13.250  -0.6665   0.04612   0.03969  -0.1250   0.9639   0.0564
 -13.000  -0.6584   0.04438   0.03790  -0.1253   0.9564   0.0567
 -12.750  -0.6329   0.04297   0.03652  -0.1272   0.9519   0.0572
 -12.500  -0.6028   0.04134   0.03489  -0.1303   0.9489   0.0577
 -12.250  -0.5830   0.03971   0.03325  -0.1323   0.9441   0.0582
 -12.000  -0.5757   0.03814   0.03165  -0.1323   0.9357   0.0587
 -11.750  -0.5501   0.03634   0.02981  -0.1354   0.9321   0.0593
 -11.500  -0.5198   0.03448   0.02787  -0.1393   0.9296   0.0602
 -11.250  -0.5280   0.03322   0.02654  -0.1366   0.9174   0.0607
 -11.000  -0.5036   0.03159   0.02484  -0.1390   0.9136   0.0615
 -10.750  -0.4767   0.02998   0.02318  -0.1417   0.9111   0.0626
 -10.500  -0.5019   0.02961   0.02275  -0.1343   0.8971   0.0627
 -10.250  -0.4759   0.02833   0.02145  -0.1357   0.8940   0.0642
 -10.000  -0.4422   0.02712   0.02019  -0.1381   0.8921   0.0662
  -9.750  -0.4620   0.02698   0.02000  -0.1305   0.8787   0.0667
  -9.500  -0.4312   0.02590   0.01890  -0.1320   0.8757   0.0692
  -9.250  -0.3949   0.02484   0.01780  -0.1342   0.8736   0.0735
  -9.000  -0.3916   0.02442   0.01739  -0.1304   0.8648   0.0764
  -8.750  -0.3728   0.02370   0.01665  -0.1293   0.8585   0.0828
  -8.500  -0.3405   0.02276   0.01574  -0.1306   0.8555   0.0933
  -8.250  -0.3024   0.02193   0.01493  -0.1327   0.8532   0.1073
  -8.000  -0.2936   0.02177   0.01474  -0.1294   0.8443   0.1154
  -7.750  -0.2653   0.02134   0.01426  -0.1294   0.8385   0.1249
  -7.500  -0.2257   0.02081   0.01365  -0.1314   0.8352   0.1344
  -7.250  -0.1847   0.02021   0.01302  -0.1338   0.8324   0.1426
  -7.000  -0.1745   0.02016   0.01288  -0.1304   0.8227   0.1470
  -6.750  -0.1451   0.01961   0.01236  -0.1307   0.8169   0.1526
  -6.500  -0.1037   0.01909   0.01169  -0.1330   0.8130   0.1599
  -6.250  -0.0867   0.01872   0.01138  -0.1310   0.8042   0.1649
  -6.000  -0.0587   0.01830   0.01090  -0.1308   0.7966   0.1717
  -5.750  -0.0205   0.01766   0.01026  -0.1327   0.7915   0.1802
  -5.500  -0.0059   0.01747   0.01005  -0.1301   0.7808   0.1873
  -5.250   0.0257   0.01694   0.00955  -0.1307   0.7734   0.1968
  -5.000   0.0495   0.01663   0.00922  -0.1297   0.7637   0.2062
  -4.750   0.0764   0.01627   0.00886  -0.1294   0.7538   0.2186
  -4.500   0.1016   0.01601   0.00862  -0.1287   0.7432   0.2335
  -4.250   0.1287   0.01578   0.00837  -0.1283   0.7323   0.2516
  -4.000   0.1515   0.01568   0.00826  -0.1272   0.7203   0.2701
  -3.750   0.1821   0.01557   0.00805  -0.1274   0.7097   0.2898
  -3.500   0.2006   0.01554   0.00804  -0.1254   0.6963   0.3047
  -3.250   0.2298   0.01550   0.00790  -0.1255   0.6854   0.3209
  -3.000   0.2502   0.01557   0.00784  -0.1238   0.6726   0.3347
  -2.750   0.2747   0.01555   0.00783  -0.1230   0.6616   0.3478
  -2.500   0.2985   0.01557   0.00777  -0.1221   0.6509   0.3605
  -2.250   0.3228   0.01564   0.00781  -0.1213   0.6412   0.3726
  -2.000   0.3460   0.01566   0.00776  -0.1202   0.6317   0.3832
  -1.750   0.3728   0.01573   0.00777  -0.1199   0.6234   0.3935
  -1.500   0.3937   0.01581   0.00777  -0.1185   0.6144   0.4030
  -1.250   0.4229   0.01584   0.00777  -0.1186   0.6072   0.4136
  -1.000   0.4445   0.01597   0.00785  -0.1173   0.5998   0.4237
  -0.750   0.4681   0.01598   0.00789  -0.1164   0.5929   0.4323
  -0.500   0.4989   0.01610   0.00789  -0.1169   0.5871   0.4417
  -0.250   0.5211   0.01620   0.00797  -0.1158   0.5808   0.4506
   0.000   0.5436   0.01625   0.00807  -0.1148   0.5745   0.4599
   0.250   0.5719   0.01637   0.00808  -0.1148   0.5688   0.4706
   0.500   0.5988   0.01647   0.00820  -0.1146   0.5632   0.4808
   0.750   0.6186   0.01658   0.00833  -0.1130   0.5572   0.4927
   1.000   0.6423   0.01663   0.00839  -0.1122   0.5510   0.5045
   1.250   0.6759   0.01685   0.00846  -0.1133   0.5450   0.5204
   1.500   0.6905   0.01687   0.00866  -0.1107   0.5394   0.5333
   1.750   0.7112   0.01695   0.00876  -0.1093   0.5336   0.5496
   2.000   0.7376   0.01707   0.00883  -0.1090   0.5280   0.5684
   2.250   0.7639   0.01722   0.00902  -0.1087   0.5226   0.5877
   2.500   0.7786   0.01728   0.00922  -0.1062   0.5173   0.6068
   2.750   0.7991   0.01736   0.00936  -0.1047   0.5122   0.6284
   3.000   0.8247   0.01747   0.00949  -0.1043   0.5077   0.6524
   3.250   0.8554   0.01769   0.00972  -0.1048   0.5031   0.6794
   3.500   0.8661   0.01775   0.00997  -0.1015   0.4988   0.7060
   3.750   0.8816   0.01781   0.01018  -0.0991   0.4941   0.7380
   4.000   0.9019   0.01786   0.01036  -0.0975   0.4897   0.7803
   4.250   0.9334   0.01796   0.01055  -0.0980   0.4854   0.8425
   4.500   0.9931   0.01829   0.01105  -0.1046   0.4800   0.9356
   4.750   1.0267   0.01858   0.01134  -0.1064   0.4746   1.0000
   5.000   1.0445   0.01879   0.01147  -0.1047   0.4701   1.0000
   5.250   1.0702   0.01901   0.01158  -0.1045   0.4658   1.0000
   5.500   1.0948   0.01936   0.01184  -0.1041   0.4614   1.0000
   5.750   1.0977   0.01959   0.01214  -0.0997   0.4568   1.0000
   6.000   1.1099   0.01983   0.01236  -0.0970   0.4519   1.0000
   6.250   1.1300   0.02002   0.01248  -0.0957   0.4472   1.0000
   6.500   1.1594   0.02031   0.01264  -0.0962   0.4423   1.0000
   6.750   1.1583   0.02064   0.01306  -0.0913   0.4373   1.0000
   7.000   1.1686   0.02092   0.01335  -0.0885   0.4319   1.0000
   7.250   1.1872   0.02113   0.01349  -0.0871   0.4269   1.0000
   7.500   1.2074   0.02144   0.01374  -0.0860   0.4218   1.0000
   7.750   1.2090   0.02190   0.01428  -0.0820   0.4160   1.0000
   8.000   1.2208   0.02222   0.01459  -0.0797   0.4103   1.0000
   8.250   1.2464   0.02243   0.01465  -0.0795   0.4048   1.0000
   8.500   1.2443   0.02308   0.01543  -0.0752   0.3985   1.0000
   8.750   1.2524   0.02356   0.01591  -0.0726   0.3919   1.0000
   9.000   1.2760   0.02381   0.01601  -0.0721   0.3860   1.0000
   9.250   1.2719   0.02470   0.01703  -0.0681   0.3786   1.0000
   9.500   1.2823   0.02526   0.01755  -0.0660   0.3719   1.0000
   9.750   1.2944   0.02589   0.01814  -0.0642   0.3651   1.0000
  10.000   1.2977   0.02681   0.01911  -0.0615   0.3575   1.0000
  10.250   1.3159   0.02728   0.01945  -0.0606   0.3512   1.0000
  10.500   1.3178   0.02843   0.02068  -0.0580   0.3439   1.0000
  10.750   1.3273   0.02929   0.02152  -0.0562   0.3376   1.0000
  11.000   1.3449   0.02993   0.02205  -0.0554   0.3320   1.0000
  11.250   1.3479   0.03120   0.02341  -0.0532   0.3259   1.0000
  11.500   1.3592   0.03211   0.02429  -0.0519   0.3207   1.0000
  11.750   1.3838   0.03251   0.02454  -0.0518   0.3163   1.0000
  12.000   1.3870   0.03393   0.02609  -0.0499   0.3121   1.0000
  12.250   1.3959   0.03509   0.02731  -0.0486   0.3079   1.0000
  12.500   1.4102   0.03598   0.02818  -0.0478   0.3044   1.0000
  12.750   1.4344   0.03641   0.02852  -0.0477   0.3013   1.0000
  13.000   1.4484   0.03743   0.02957  -0.0469   0.2982   1.0000
  13.250   1.4517   0.03901   0.03126  -0.0454   0.2951   1.0000
  13.500   1.4599   0.04033   0.03264  -0.0442   0.2919   1.0000
  13.750   1.4723   0.04139   0.03372  -0.0434   0.2889   1.0000
  14.000   1.4913   0.04209   0.03440  -0.0431   0.2865   1.0000
  14.250   1.5258   0.04201   0.03420  -0.0438   0.2839   1.0000
  14.500   1.5211   0.04417   0.03653  -0.0420   0.2817   1.0000
  14.750   1.5190   0.04629   0.03880  -0.0405   0.2793   1.0000
  15.000   1.5220   0.04813   0.04073  -0.0395   0.2768   1.0000
  15.250   1.5300   0.04965   0.04231  -0.0387   0.2747   1.0000
  15.500   1.5434   0.05075   0.04343  -0.0383   0.2725   1.0000
  15.750   1.5634   0.05141   0.04408  -0.0381   0.2705   1.0000
  16.000   1.5936   0.05146   0.04408  -0.0384   0.2687   1.0000
  16.250   1.6013   0.05317   0.04588  -0.0378   0.2672   1.0000
  16.500   1.5808   0.05697   0.04991  -0.0361   0.2655   1.0000
  16.750   1.5609   0.06104   0.05419  -0.0348   0.2637   1.0000
  17.000   1.5374   0.06567   0.05901  -0.0338   0.2613   1.0000
  17.250   1.5243   0.06949   0.06297  -0.0333   0.2589   1.0000
  17.500   1.5293   0.07156   0.06509  -0.0331   0.2570   1.0000
  17.750   1.5484   0.07221   0.06575  -0.0330   0.2554   1.0000
  18.000   1.5844   0.07118   0.06466  -0.0331   0.2539   1.0000
  18.250   1.5966   0.07265   0.06617  -0.0330   0.2518   1.0000
  18.500   0.9451   0.17389   0.16858  -0.0610   0.2094   1.0000
  18.750   0.9663   0.17361   0.16831  -0.0606   0.2073   1.0000
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