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GOE 383 AIRFOIL (goe383-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 383 AIRFOIL (goe383-il)
Reynolds number: 500,000
Max Cl/Cd: 83.12 at α=6°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe383-il-500000-n5.txt
Download as CSV file: xf-goe383-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.6511   0.08575   0.08215  -0.0776   0.9746   0.0294
 -16.000  -0.7454   0.06260   0.05839  -0.0944   0.9566   0.0295
 -15.750  -0.7649   0.05649   0.05206  -0.0985   0.9469   0.0296
 -15.500  -0.7789   0.05159   0.04698  -0.1014   0.9366   0.0296
 -15.250  -0.7882   0.04744   0.04265  -0.1038   0.9256   0.0297
 -15.000  -0.7943   0.04398   0.03903  -0.1053   0.9140   0.0297
 -14.750  -0.7979   0.04104   0.03592  -0.1062   0.9004   0.0298
 -14.500  -0.7993   0.03850   0.03320  -0.1067   0.8844   0.0299
 -14.250  -0.7982   0.03631   0.03082  -0.1067   0.8669   0.0299
 -14.000  -0.7952   0.03441   0.02873  -0.1065   0.8486   0.0300
 -13.750  -0.7900   0.03275   0.02689  -0.1060   0.8305   0.0301
 -13.500  -0.7830   0.03132   0.02526  -0.1054   0.8129   0.0301
 -13.250  -0.7746   0.03000   0.02377  -0.1045   0.7959   0.0302
 -12.750  -0.7533   0.02767   0.02118  -0.1025   0.7634   0.0305
 -12.500  -0.7403   0.02672   0.02012  -0.1014   0.7496   0.0306
 -12.000  -0.7127   0.02516   0.01836  -0.0987   0.7243   0.0308
 -11.750  -0.6983   0.02453   0.01762  -0.0972   0.7133   0.0309
 -11.500  -0.6804   0.02387   0.01688  -0.0962   0.7034   0.0311
 -11.250  -0.6616   0.02327   0.01619  -0.0953   0.6941   0.0312
 -11.000  -0.6419   0.02268   0.01552  -0.0944   0.6866   0.0314
 -10.750  -0.6214   0.02211   0.01487  -0.0936   0.6792   0.0316
 -10.500  -0.6005   0.02157   0.01425  -0.0928   0.6725   0.0318
 -10.250  -0.5788   0.02104   0.01365  -0.0921   0.6669   0.0320
 -10.000  -0.5566   0.02053   0.01307  -0.0914   0.6612   0.0322
  -9.750  -0.5341   0.02004   0.01251  -0.0908   0.6557   0.0324
  -9.500  -0.5112   0.01958   0.01197  -0.0901   0.6509   0.0326
  -9.250  -0.4878   0.01913   0.01146  -0.0896   0.6469   0.0329
  -9.000  -0.4639   0.01869   0.01096  -0.0890   0.6430   0.0331
  -8.750  -0.4397   0.01828   0.01049  -0.0885   0.6383   0.0334
  -8.500  -0.4152   0.01791   0.01005  -0.0880   0.6332   0.0337
  -8.250  -0.3904   0.01760   0.00965  -0.0876   0.6282   0.0339
  -8.000  -0.3666   0.01714   0.00917  -0.0870   0.6242   0.0343
  -7.750  -0.3417   0.01675   0.00878  -0.0866   0.6204   0.0346
  -7.500  -0.3163   0.01641   0.00842  -0.0862   0.6160   0.0349
  -7.250  -0.2908   0.01610   0.00808  -0.0858   0.6121   0.0353
  -7.000  -0.2651   0.01582   0.00776  -0.0855   0.6086   0.0356
  -6.750  -0.2393   0.01555   0.00745  -0.0851   0.6053   0.0360
  -6.500  -0.2131   0.01528   0.00715  -0.0848   0.6023   0.0364
  -6.250  -0.1866   0.01501   0.00686  -0.0846   0.5997   0.0368
  -6.000  -0.1598   0.01475   0.00659  -0.0844   0.5970   0.0373
  -5.750  -0.1330   0.01452   0.00633  -0.0842   0.5942   0.0378
  -5.500  -0.1064   0.01426   0.00606  -0.0839   0.5913   0.0382
  -5.250  -0.0798   0.01402   0.00581  -0.0837   0.5882   0.0388
  -5.000  -0.0529   0.01383   0.00560  -0.0835   0.5850   0.0395
  -4.750  -0.0259   0.01368   0.00541  -0.0833   0.5816   0.0402
  -4.500   0.0017   0.01348   0.00522  -0.0832   0.5790   0.0410
  -4.250   0.0295   0.01332   0.00505  -0.0831   0.5761   0.0419
  -4.000   0.0570   0.01313   0.00487  -0.0830   0.5730   0.0430
  -3.750   0.0845   0.01297   0.00472  -0.0829   0.5697   0.0443
  -3.500   0.1122   0.01284   0.00457  -0.0828   0.5664   0.0458
  -3.250   0.1397   0.01272   0.00443  -0.0827   0.5630   0.0473
  -3.000   0.1672   0.01259   0.00429  -0.0826   0.5596   0.0493
  -2.500   0.2230   0.01231   0.00405  -0.0825   0.5518   0.0553
  -2.250   0.2505   0.01218   0.00393  -0.0824   0.5476   0.0608
  -2.000   0.2766   0.01191   0.00379  -0.0821   0.5435   0.0887
  -1.750   0.3032   0.01172   0.00372  -0.0819   0.5396   0.1265
  -1.500   0.3308   0.01156   0.00366  -0.0819   0.5353   0.1477
  -1.250   0.3582   0.01142   0.00360  -0.0818   0.5302   0.1696
  -1.000   0.3847   0.01125   0.00354  -0.0816   0.5249   0.2038
  -0.750   0.4110   0.01108   0.00352  -0.0814   0.5195   0.2547
  -0.500   0.4381   0.01094   0.00350  -0.0814   0.5129   0.2946
  -0.250   0.4644   0.01084   0.00348  -0.0811   0.5057   0.3277
   0.000   0.4909   0.01073   0.00348  -0.0809   0.4992   0.3671
   0.250   0.5161   0.01050   0.00348  -0.0806   0.4916   0.4406
   0.500   0.5396   0.01024   0.00352  -0.0799   0.4844   0.5378
   0.750   0.5637   0.01005   0.00362  -0.0792   0.4767   0.6278
   1.000   0.5887   0.01008   0.00370  -0.0786   0.4685   0.6711
   1.250   0.6149   0.01013   0.00378  -0.0783   0.4609   0.6957
   1.500   0.6407   0.01023   0.00387  -0.0779   0.4532   0.7158
   1.750   0.6661   0.01030   0.00398  -0.0774   0.4471   0.7386
   2.000   0.6919   0.01037   0.00409  -0.0770   0.4412   0.7612
   2.250   0.7166   0.01046   0.00422  -0.0764   0.4352   0.7849
   2.500   0.7409   0.01057   0.00437  -0.0757   0.4299   0.8099
   2.750   0.7661   0.01065   0.00451  -0.0751   0.4250   0.8326
   3.000   0.7901   0.01078   0.00467  -0.0743   0.4194   0.8571
   3.500   0.8367   0.01110   0.00503  -0.0725   0.4072   0.9085
   3.750   0.8620   0.01128   0.00522  -0.0720   0.4014   0.9302
   4.000   0.8902   0.01152   0.00543  -0.0723   0.3967   0.9505
   4.250   0.9225   0.01175   0.00563  -0.0734   0.3929   0.9673
   4.500   0.9586   0.01194   0.00583  -0.0753   0.3892   0.9815
   4.750   0.9960   0.01218   0.00604  -0.0776   0.3852   0.9927
   5.000   1.0334   0.01244   0.00628  -0.0800   0.3812   0.9995
   5.250   1.0460   0.01264   0.00643  -0.0773   0.3779   1.0000
   5.500   1.0588   0.01282   0.00660  -0.0746   0.3748   1.0000
   5.750   1.0771   0.01299   0.00678  -0.0730   0.3718   1.0000
   6.000   1.0963   0.01319   0.00699  -0.0717   0.3686   1.0000
   6.250   1.1156   0.01344   0.00723  -0.0704   0.3653   1.0000
   6.500   1.1345   0.01374   0.00750  -0.0691   0.3618   1.0000
   6.750   1.1527   0.01409   0.00783  -0.0678   0.3582   1.0000
   7.000   1.1743   0.01435   0.00811  -0.0671   0.3550   1.0000
   7.250   1.1955   0.01464   0.00842  -0.0663   0.3512   1.0000
   7.500   1.2154   0.01499   0.00877  -0.0654   0.3474   1.0000
   7.750   1.2343   0.01540   0.00917  -0.0644   0.3435   1.0000
   8.000   1.2524   0.01586   0.00962  -0.0634   0.3397   1.0000
   8.250   1.2733   0.01623   0.01001  -0.0627   0.3353   1.0000
   8.500   1.2915   0.01671   0.01050  -0.0618   0.3296   1.0000
   8.750   1.3070   0.01735   0.01110  -0.0606   0.3242   1.0000
   9.000   1.3261   0.01784   0.01162  -0.0598   0.3192   1.0000
   9.250   1.3429   0.01846   0.01225  -0.0589   0.3131   1.0000
   9.500   1.3566   0.01927   0.01304  -0.0577   0.3070   1.0000
   9.750   1.3734   0.01995   0.01373  -0.0569   0.3000   1.0000
  10.000   1.3850   0.02095   0.01471  -0.0556   0.2927   1.0000
  10.250   1.3996   0.02181   0.01558  -0.0547   0.2860   1.0000
  10.500   1.4096   0.02300   0.01675  -0.0535   0.2780   1.0000
  10.750   1.4202   0.02418   0.01793  -0.0524   0.2696   1.0000
  11.000   1.4265   0.02571   0.01943  -0.0511   0.2611   1.0000
  11.250   1.4349   0.02713   0.02085  -0.0500   0.2523   1.0000
  11.500   1.4406   0.02880   0.02250  -0.0489   0.2450   1.0000
  11.750   1.4473   0.03045   0.02415  -0.0479   0.2375   1.0000
  12.000   1.4514   0.03235   0.02604  -0.0468   0.2307   1.0000
  12.250   1.4574   0.03414   0.02784  -0.0459   0.2237   1.0000
  12.500   1.4600   0.03625   0.02994  -0.0450   0.2177   1.0000
  12.750   1.4670   0.03802   0.03174  -0.0443   0.2124   1.0000
  13.000   1.4715   0.04003   0.03376  -0.0435   0.2075   1.0000
  13.250   1.4754   0.04214   0.03589  -0.0428   0.2034   1.0000
  13.500   1.4827   0.04394   0.03773  -0.0423   0.1992   1.0000
  13.750   1.4863   0.04612   0.03993  -0.0417   0.1948   1.0000
  14.000   1.4876   0.04853   0.04236  -0.0411   0.1908   1.0000
  14.250   1.4950   0.05039   0.04428  -0.0407   0.1875   1.0000
  14.500   1.5006   0.05244   0.04635  -0.0403   0.1836   1.0000
  14.750   1.5014   0.05500   0.04894  -0.0398   0.1798   1.0000
  15.000   1.5051   0.05727   0.05125  -0.0395   0.1763   1.0000
  15.250   1.5085   0.05961   0.05364  -0.0392   0.1721   1.0000
  15.500   1.5088   0.06230   0.05635  -0.0388   0.1674   1.0000
  15.750   1.5091   0.06505   0.05914  -0.0386   0.1632   1.0000
  16.000   1.5098   0.06774   0.06187  -0.0384   0.1577   1.0000
  16.250   1.5058   0.07101   0.06516  -0.0382   0.1524   1.0000
  16.500   1.5034   0.07414   0.06832  -0.0381   0.1455   1.0000
  16.750   1.4971   0.07779   0.07198  -0.0381   0.1380   1.0000
  17.000   1.4852   0.08213   0.07632  -0.0382   0.1274   1.0000
  17.250   1.4544   0.08884   0.08294  -0.0384   0.1041   1.0000
  17.500   1.4208   0.09610   0.09012  -0.0389   0.0844   1.0000
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