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GOE 383 AIRFOIL (goe383-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 383 AIRFOIL (goe383-il)
Reynolds number: 1,000,000
Max Cl/Cd: 106.06 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe383-il-1000000-n5.txt
Download as CSV file: xf-goe383-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 383 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     1.000 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -0.7552   0.11558   0.11284  -0.0549   1.0000   0.0254
 -19.000  -0.8162   0.10111   0.09812  -0.0637   1.0000   0.0255
 -18.750  -0.8510   0.09158   0.08843  -0.0697   0.9913   0.0255
 -18.500  -0.8768   0.08368   0.08038  -0.0749   0.9784   0.0256
 -18.250  -0.9007   0.07646   0.07301  -0.0794   0.9690   0.0256
 -18.000  -0.9210   0.07014   0.06655  -0.0831   0.9613   0.0257
 -17.750  -0.9392   0.06425   0.06052  -0.0865   0.9537   0.0257
 -17.500  -0.9536   0.05889   0.05503  -0.0896   0.9473   0.0258
 -17.250  -0.9655   0.05397   0.04998  -0.0925   0.9399   0.0258
 -17.000  -0.9739   0.04954   0.04542  -0.0951   0.9331   0.0259
 -16.750  -0.9796   0.04558   0.04134  -0.0974   0.9246   0.0259
 -16.500  -0.9827   0.04210   0.03773  -0.0992   0.9160   0.0260
 -16.250  -0.9835   0.03908   0.03458  -0.1006   0.9044   0.0260
 -16.000  -0.9819   0.03643   0.03181  -0.1017   0.8909   0.0261
 -15.750  -0.9789   0.03412   0.02935  -0.1023   0.8742   0.0261
 -15.500  -0.9737   0.03212   0.02720  -0.1027   0.8554   0.0262
 -15.250  -0.9668   0.03035   0.02528  -0.1028   0.8362   0.0262
 -15.000  -0.9585   0.02880   0.02358  -0.1028   0.8177   0.0263
 -14.750  -0.9488   0.02744   0.02207  -0.1025   0.7998   0.0263
 -14.500  -0.9380   0.02624   0.02074  -0.1021   0.7822   0.0264
 -14.250  -0.9260   0.02519   0.01956  -0.1015   0.7652   0.0264
 -14.000  -0.9130   0.02426   0.01852  -0.1007   0.7485   0.0265
 -13.750  -0.8990   0.02345   0.01757  -0.0998   0.7323   0.0265
 -13.500  -0.8842   0.02270   0.01672  -0.0988   0.7173   0.0266
 -13.250  -0.8684   0.02202   0.01594  -0.0977   0.7046   0.0266
 -13.000  -0.8557   0.02125   0.01507  -0.0961   0.6921   0.0267
 -12.750  -0.8436   0.02060   0.01434  -0.0941   0.6823   0.0269
 -12.250  -0.8070   0.01944   0.01305  -0.0919   0.6653   0.0271
 -12.000  -0.7865   0.01894   0.01249  -0.0911   0.6582   0.0272
 -11.750  -0.7650   0.01849   0.01197  -0.0903   0.6515   0.0274
 -11.500  -0.7428   0.01806   0.01149  -0.0896   0.6461   0.0275
 -11.250  -0.7197   0.01765   0.01105  -0.0890   0.6418   0.0276
 -11.000  -0.6962   0.01726   0.01062  -0.0884   0.6371   0.0278
 -10.750  -0.6723   0.01690   0.01021  -0.0878   0.6323   0.0279
 -10.250  -0.6234   0.01622   0.00944  -0.0869   0.6239   0.0282
 -10.000  -0.5983   0.01588   0.00908  -0.0864   0.6207   0.0284
  -9.750  -0.5730   0.01557   0.00872  -0.0860   0.6168   0.0286
  -9.500  -0.5476   0.01527   0.00838  -0.0857   0.6125   0.0287
  -9.250  -0.5220   0.01499   0.00805  -0.0853   0.6081   0.0289
  -8.750  -0.4698   0.01444   0.00743  -0.0847   0.6012   0.0293
  -8.500  -0.4433   0.01417   0.00714  -0.0844   0.5983   0.0295
  -8.250  -0.4166   0.01392   0.00686  -0.0842   0.5952   0.0297
  -8.000  -0.3898   0.01368   0.00659  -0.0839   0.5916   0.0299
  -7.750  -0.3628   0.01348   0.00635  -0.0837   0.5877   0.0301
  -7.500  -0.3360   0.01326   0.00610  -0.0835   0.5842   0.0303
  -7.250  -0.3095   0.01300   0.00581  -0.0833   0.5813   0.0307
  -7.000  -0.2821   0.01275   0.00557  -0.0831   0.5799   0.0310
  -6.750  -0.2545   0.01253   0.00535  -0.0830   0.5781   0.0313
  -6.500  -0.2268   0.01233   0.00514  -0.0829   0.5759   0.0316
  -6.250  -0.1989   0.01215   0.00495  -0.0828   0.5732   0.0319
  -6.000  -0.1710   0.01198   0.00477  -0.0828   0.5702   0.0323
  -5.750  -0.1431   0.01183   0.00459  -0.0827   0.5671   0.0327
  -5.500  -0.1152   0.01168   0.00443  -0.0826   0.5641   0.0331
  -5.250  -0.0872   0.01156   0.00427  -0.0826   0.5611   0.0335
  -5.000  -0.0588   0.01141   0.00413  -0.0826   0.5591   0.0338
  -4.750  -0.0305   0.01125   0.00397  -0.0826   0.5570   0.0343
  -4.500  -0.0022   0.01109   0.00382  -0.0826   0.5543   0.0349
  -4.250   0.0262   0.01096   0.00369  -0.0826   0.5510   0.0356
  -4.000   0.0546   0.01085   0.00358  -0.0826   0.5472   0.0363
  -3.750   0.0828   0.01077   0.00347  -0.0826   0.5431   0.0371
  -3.500   0.1113   0.01068   0.00337  -0.0826   0.5396   0.0378
  -3.250   0.1399   0.01056   0.00326  -0.0827   0.5366   0.0390
  -3.000   0.1686   0.01046   0.00318  -0.0828   0.5327   0.0405
  -2.750   0.1971   0.01038   0.00310  -0.0828   0.5282   0.0420
  -2.500   0.2252   0.01031   0.00302  -0.0828   0.5233   0.0442
  -2.250   0.2538   0.01024   0.00295  -0.0829   0.5190   0.0466
  -2.000   0.2823   0.01016   0.00288  -0.0830   0.5135   0.0499
  -1.750   0.3103   0.01010   0.00282  -0.0829   0.5062   0.0543
  -1.500   0.3382   0.01003   0.00275  -0.0829   0.4991   0.0620
  -1.250   0.3645   0.00980   0.00268  -0.0827   0.4900   0.1086
  -1.000   0.3919   0.00976   0.00266  -0.0826   0.4816   0.1271
  -0.750   0.4193   0.00971   0.00264  -0.0826   0.4722   0.1446
  -0.500   0.4464   0.00969   0.00264  -0.0825   0.4636   0.1627
  -0.250   0.4731   0.00960   0.00264  -0.0823   0.4548   0.1973
   0.000   0.4992   0.00950   0.00266  -0.0821   0.4467   0.2484
   0.250   0.5263   0.00948   0.00270  -0.0820   0.4388   0.2776
   0.500   0.5527   0.00950   0.00276  -0.0818   0.4311   0.3051
   0.750   0.5800   0.00944   0.00279  -0.0818   0.4261   0.3413
   1.250   0.6305   0.00905   0.00291  -0.0812   0.4156   0.5208
   1.500   0.6562   0.00893   0.00300  -0.0809   0.4111   0.5957
   1.750   0.6834   0.00893   0.00309  -0.0808   0.4069   0.6310
   2.000   0.7102   0.00898   0.00319  -0.0806   0.4018   0.6581
   2.250   0.7361   0.00909   0.00331  -0.0803   0.3955   0.6835
   2.500   0.7632   0.00915   0.00341  -0.0802   0.3907   0.7046
   2.750   0.7899   0.00921   0.00351  -0.0800   0.3857   0.7255
   3.000   0.8159   0.00930   0.00364  -0.0797   0.3809   0.7486
   3.250   0.8417   0.00941   0.00377  -0.0794   0.3767   0.7686
   3.500   0.8684   0.00947   0.00388  -0.0793   0.3741   0.7870
   3.750   0.8949   0.00951   0.00400  -0.0790   0.3716   0.8092
   4.000   0.9206   0.00958   0.00413  -0.0787   0.3685   0.8344
   4.250   0.9455   0.00966   0.00428  -0.0782   0.3650   0.8593
   4.500   0.9692   0.00978   0.00445  -0.0774   0.3613   0.8866
   4.750   0.9920   0.00992   0.00463  -0.0765   0.3578   0.9124
   5.000   1.0166   0.01001   0.00479  -0.0758   0.3558   0.9387
   5.250   1.0450   0.01015   0.00495  -0.0760   0.3529   0.9656
   5.500   1.0791   0.01034   0.00514  -0.0776   0.3491   0.9830
   5.750   1.1122   0.01057   0.00534  -0.0790   0.3448   0.9936
   6.000   1.1423   0.01082   0.00556  -0.0799   0.3407   1.0000
   6.250   1.1596   0.01095   0.00570  -0.0781   0.3384   1.0000
   6.500   1.1794   0.01112   0.00587  -0.0767   0.3355   1.0000
   6.750   1.1995   0.01134   0.00608  -0.0756   0.3313   1.0000
   7.000   1.2180   0.01165   0.00635  -0.0742   0.3256   1.0000
   7.250   1.2387   0.01192   0.00661  -0.0733   0.3204   1.0000
   7.500   1.2594   0.01221   0.00689  -0.0724   0.3146   1.0000
   7.750   1.2781   0.01261   0.00725  -0.0713   0.3086   1.0000
   8.000   1.2987   0.01294   0.00757  -0.0704   0.3030   1.0000
   8.250   1.3172   0.01337   0.00798  -0.0694   0.2956   1.0000
   8.500   1.3355   0.01384   0.00842  -0.0683   0.2890   1.0000
   8.750   1.3525   0.01439   0.00894  -0.0672   0.2803   1.0000
   9.000   1.3680   0.01502   0.00953  -0.0659   0.2710   1.0000
   9.250   1.3812   0.01581   0.01026  -0.0644   0.2607   1.0000
   9.500   1.3939   0.01665   0.01106  -0.0629   0.2500   1.0000
   9.750   1.4071   0.01751   0.01188  -0.0616   0.2411   1.0000
  10.250   1.4323   0.01940   0.01373  -0.0591   0.2262   1.0000
  10.750   1.4546   0.02160   0.01590  -0.0567   0.2120   1.0000
  11.000   1.4621   0.02302   0.01729  -0.0554   0.2043   1.0000
  11.250   1.4739   0.02418   0.01844  -0.0544   0.1987   1.0000
  11.500   1.4828   0.02556   0.01981  -0.0534   0.1932   1.0000
  11.750   1.4932   0.02688   0.02115  -0.0525   0.1894   1.0000
  12.000   1.5051   0.02812   0.02241  -0.0518   0.1858   1.0000
  12.250   1.5144   0.02958   0.02389  -0.0510   0.1819   1.0000
  12.500   1.5212   0.03128   0.02559  -0.0501   0.1779   1.0000
  12.750   1.5321   0.03266   0.02701  -0.0495   0.1746   1.0000
  13.000   1.5384   0.03448   0.02883  -0.0487   0.1695   1.0000
  13.250   1.5426   0.03649   0.03085  -0.0479   0.1647   1.0000
  13.500   1.5491   0.03830   0.03267  -0.0472   0.1595   1.0000
  13.750   1.5506   0.04062   0.03499  -0.0464   0.1543   1.0000
  14.000   1.5559   0.04259   0.03699  -0.0457   0.1492   1.0000
  14.250   1.5546   0.04522   0.03961  -0.0449   0.1428   1.0000
  14.500   1.5536   0.04783   0.04222  -0.0442   0.1351   1.0000
  14.750   1.5452   0.05118   0.04553  -0.0432   0.1234   1.0000
  15.000   1.5148   0.05681   0.05105  -0.0417   0.0980   1.0000
  15.250   1.4884   0.06223   0.05642  -0.0406   0.0808   1.0000
  15.500   1.4780   0.06614   0.06033  -0.0401   0.0743   1.0000
  15.750   1.4730   0.06954   0.06377  -0.0398   0.0709   1.0000
  16.000   1.4697   0.07277   0.06704  -0.0397   0.0681   1.0000
  16.250   1.4685   0.07584   0.07015  -0.0396   0.0661   1.0000
  16.500   1.4665   0.07903   0.07340  -0.0396   0.0640   1.0000
  16.750   1.4634   0.08237   0.07678  -0.0397   0.0621   1.0000
  17.000   1.4627   0.08546   0.07992  -0.0398   0.0605   1.0000
  17.250   1.4622   0.08853   0.08304  -0.0400   0.0587   1.0000
  17.500   1.4577   0.09213   0.08669  -0.0403   0.0569   1.0000
  17.750   1.4573   0.09524   0.08985  -0.0407   0.0553   1.0000
  18.000   1.4542   0.09873   0.09339  -0.0411   0.0535   1.0000
  18.250   1.4521   0.10205   0.09674  -0.0415   0.0515   1.0000
  18.500   1.4482   0.10567   0.10042  -0.0421   0.0498   1.0000
  18.750   1.4473   0.10889   0.10368  -0.0427   0.0478   1.0000
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