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GOE 592 AIRFOIL (goe592-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 592 AIRFOIL (goe592-il)
Reynolds number: 1,000,000
Max Cl/Cd: 124.5 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe592-il-1000000-n5.txt
Download as CSV file: xf-goe592-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 592 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.5929   0.02765   0.02426  -0.1759   0.8494   0.0254
 -13.750  -0.5928   0.02470   0.02108  -0.1755   0.8425   0.0257
 -13.500  -0.5819   0.02307   0.01931  -0.1748   0.8374   0.0258
 -13.250  -0.5670   0.02184   0.01797  -0.1740   0.8316   0.0261
 -13.000  -0.5499   0.02085   0.01684  -0.1732   0.8259   0.0263
 -12.750  -0.5314   0.01995   0.01582  -0.1725   0.8208   0.0266
 -12.500  -0.5117   0.01912   0.01490  -0.1718   0.8154   0.0268
 -12.250  -0.4914   0.01837   0.01402  -0.1711   0.8101   0.0270
 -12.000  -0.4702   0.01769   0.01322  -0.1704   0.8051   0.0273
 -11.750  -0.4479   0.01705   0.01249  -0.1699   0.8000   0.0275
 -11.500  -0.4252   0.01649   0.01181  -0.1692   0.7941   0.0278
 -11.000  -0.3781   0.01550   0.01061  -0.1681   0.7837   0.0282
 -10.750  -0.3547   0.01497   0.00999  -0.1676   0.7783   0.0285
 -10.500  -0.3313   0.01447   0.00940  -0.1669   0.7726   0.0288
 -10.250  -0.3069   0.01404   0.00890  -0.1664   0.7674   0.0291
 -10.000  -0.2819   0.01365   0.00845  -0.1660   0.7614   0.0294
  -9.750  -0.2570   0.01331   0.00803  -0.1654   0.7553   0.0298
  -9.500  -0.2315   0.01299   0.00763  -0.1650   0.7502   0.0301
  -9.250  -0.2057   0.01268   0.00726  -0.1646   0.7447   0.0304
  -9.000  -0.1802   0.01240   0.00690  -0.1641   0.7386   0.0308
  -8.750  -0.1544   0.01213   0.00656  -0.1637   0.7330   0.0312
  -8.500  -0.1282   0.01188   0.00624  -0.1633   0.7269   0.0316
  -8.250  -0.1022   0.01165   0.00594  -0.1629   0.7208   0.0319
  -8.000  -0.0762   0.01140   0.00561  -0.1625   0.7155   0.0323
  -7.750  -0.0501   0.01113   0.00530  -0.1621   0.7095   0.0328
  -7.500  -0.0241   0.01093   0.00505  -0.1616   0.7032   0.0333
  -7.250   0.0023   0.01074   0.00481  -0.1613   0.6978   0.0338
  -7.000   0.0291   0.01055   0.00459  -0.1609   0.6922   0.0344
  -6.750   0.0554   0.01040   0.00437  -0.1605   0.6861   0.0350
  -6.500   0.0818   0.01025   0.00417  -0.1601   0.6806   0.0356
  -6.250   0.1087   0.01011   0.00398  -0.1598   0.6753   0.0361
  -6.000   0.1351   0.00995   0.00378  -0.1594   0.6695   0.0369
  -5.750   0.1612   0.00983   0.00363  -0.1589   0.6641   0.0378
  -5.500   0.1883   0.00971   0.00349  -0.1587   0.6590   0.0388
  -5.250   0.2150   0.00961   0.00334  -0.1583   0.6535   0.0399
  -5.000   0.2412   0.00952   0.00321  -0.1578   0.6481   0.0408
  -4.750   0.2681   0.00941   0.00309  -0.1575   0.6436   0.0421
  -4.500   0.2950   0.00933   0.00299  -0.1572   0.6386   0.0434
  -4.250   0.3214   0.00927   0.00290  -0.1568   0.6334   0.0447
  -4.000   0.3475   0.00921   0.00281  -0.1563   0.6286   0.0460
  -3.750   0.3747   0.00914   0.00274  -0.1561   0.6245   0.0476
  -3.500   0.4015   0.00909   0.00267  -0.1557   0.6198   0.0493
  -3.250   0.4278   0.00906   0.00261  -0.1553   0.6152   0.0509
  -3.000   0.4537   0.00904   0.00258  -0.1548   0.6108   0.0527
  -2.750   0.4808   0.00899   0.00254  -0.1545   0.6069   0.0545
  -2.500   0.5075   0.00896   0.00249  -0.1542   0.6026   0.0560
  -2.250   0.5335   0.00894   0.00245  -0.1537   0.5982   0.0575
  -1.750   0.5857   0.00892   0.00242  -0.1528   0.5900   0.0609
  -1.500   0.6122   0.00891   0.00240  -0.1525   0.5859   0.0625
  -1.250   0.6379   0.00890   0.00238  -0.1520   0.5815   0.0639
  -1.000   0.6627   0.00891   0.00238  -0.1513   0.5769   0.0655
  -0.750   0.6886   0.00891   0.00239  -0.1508   0.5732   0.0674
  -0.500   0.7146   0.00891   0.00239  -0.1504   0.5691   0.0692
  -0.250   0.7399   0.00894   0.00239  -0.1498   0.5646   0.0703
   0.000   0.7636   0.00894   0.00239  -0.1489   0.5596   0.0722
   0.250   0.7885   0.00895   0.00240  -0.1483   0.5558   0.0741
   0.500   0.8137   0.00895   0.00242  -0.1477   0.5516   0.0757
   0.750   0.8378   0.00899   0.00244  -0.1469   0.5468   0.0775
   1.000   0.8599   0.00905   0.00247  -0.1457   0.5417   0.0787
   1.250   0.8827   0.00905   0.00249  -0.1447   0.5374   0.0809
   1.500   0.9051   0.00907   0.00252  -0.1435   0.5326   0.0832
   1.750   0.9258   0.00912   0.00257  -0.1421   0.5270   0.0861
   2.000   0.9463   0.00920   0.00263  -0.1406   0.5221   0.0882
   2.250   0.9689   0.00923   0.00269  -0.1396   0.5170   0.0926
   2.500   0.9898   0.00933   0.00279  -0.1382   0.5107   0.0982
   2.750   1.0094   0.00944   0.00292  -0.1366   0.5042   0.1107
   3.000   1.0302   0.00952   0.00305  -0.1353   0.4963   0.1391
   3.250   1.0479   0.00969   0.00323  -0.1334   0.4872   0.1644
   3.750   1.0849   0.00996   0.00361  -0.1300   0.4689   0.2441
   4.000   1.1033   0.00999   0.00384  -0.1284   0.4607   0.3489
   4.500   1.1740   0.00943   0.00455  -0.1327   0.4422   1.0000
   4.750   1.1924   0.00971   0.00478  -0.1311   0.4337   1.0000
   5.000   1.2115   0.00997   0.00501  -0.1296   0.4253   1.0000
   5.250   1.2302   0.01027   0.00526  -0.1281   0.4173   1.0000
   5.500   1.2500   0.01053   0.00550  -0.1269   0.4104   1.0000
   5.750   1.2679   0.01087   0.00579  -0.1253   0.4030   1.0000
   6.000   1.2879   0.01116   0.00606  -0.1241   0.3952   1.0000
   6.250   1.3042   0.01158   0.00643  -0.1224   0.3854   1.0000
   6.500   1.3218   0.01198   0.00678  -0.1209   0.3744   1.0000
   6.750   1.3385   0.01242   0.00718  -0.1193   0.3635   1.0000
   7.000   1.3541   0.01293   0.00764  -0.1176   0.3534   1.0000
   7.250   1.3723   0.01335   0.00803  -0.1163   0.3446   1.0000
   7.500   1.3878   0.01389   0.00853  -0.1147   0.3344   1.0000
   7.750   1.4010   0.01457   0.00914  -0.1128   0.3204   1.0000
   8.000   1.4163   0.01517   0.00969  -0.1112   0.3082   1.0000
   8.250   1.4291   0.01591   0.01037  -0.1094   0.2952   1.0000
   8.500   1.4406   0.01674   0.01113  -0.1074   0.2801   1.0000
   8.750   1.4502   0.01770   0.01202  -0.1053   0.2640   1.0000
   9.000   1.4608   0.01864   0.01289  -0.1034   0.2501   1.0000
   9.250   1.4696   0.01971   0.01389  -0.1013   0.2358   1.0000
   9.500   1.4785   0.02081   0.01492  -0.0994   0.2219   1.0000
   9.750   1.4876   0.02194   0.01600  -0.0975   0.2092   1.0000
  10.000   1.4973   0.02305   0.01707  -0.0958   0.1974   1.0000
  10.250   1.5070   0.02421   0.01819  -0.0942   0.1874   1.0000
  10.500   1.5120   0.02572   0.01963  -0.0921   0.1715   1.0000
  10.750   1.5143   0.02745   0.02127  -0.0899   0.1531   1.0000
  11.000   1.5139   0.02944   0.02315  -0.0876   0.1339   1.0000
  11.250   1.5142   0.03145   0.02509  -0.0855   0.1177   1.0000
  11.500   1.5178   0.03328   0.02688  -0.0838   0.1073   1.0000
  11.750   1.5234   0.03496   0.02854  -0.0823   0.1001   1.0000
  12.000   1.5312   0.03652   0.03012  -0.0811   0.0954   1.0000
  12.250   1.5383   0.03816   0.03175  -0.0799   0.0912   1.0000
  12.500   1.5462   0.03976   0.03338  -0.0788   0.0883   1.0000
  12.750   1.5556   0.04124   0.03488  -0.0778   0.0861   1.0000
  13.000   1.5636   0.04287   0.03654  -0.0768   0.0842   1.0000
  13.250   1.5717   0.04449   0.03820  -0.0759   0.0825   1.0000
  13.500   1.5786   0.04628   0.04001  -0.0749   0.0809   1.0000
  13.750   1.5855   0.04805   0.04182  -0.0740   0.0791   1.0000
  14.000   1.5924   0.04986   0.04367  -0.0732   0.0779   1.0000
  14.250   1.6012   0.05148   0.04534  -0.0725   0.0772   1.0000
  14.500   1.6079   0.05334   0.04725  -0.0717   0.0763   1.0000
  14.750   1.6152   0.05512   0.04909  -0.0710   0.0754   1.0000
  15.000   1.6202   0.05718   0.05118  -0.0702   0.0741   1.0000
  15.250   1.6247   0.05929   0.05332  -0.0695   0.0725   1.0000
  15.500   1.6285   0.06149   0.05557  -0.0688   0.0714   1.0000
  15.750   1.6304   0.06388   0.05799  -0.0680   0.0694   1.0000
  16.000   1.6353   0.06598   0.06015  -0.0675   0.0686   1.0000
  16.250   1.6410   0.06802   0.06225  -0.0670   0.0677   1.0000
  16.500   1.6457   0.07017   0.06445  -0.0665   0.0668   1.0000
  16.750   1.6485   0.07254   0.06687  -0.0660   0.0656   1.0000
  17.000   1.6521   0.07481   0.06919  -0.0655   0.0649   1.0000
  17.250   1.6525   0.07746   0.07189  -0.0650   0.0635   1.0000
  17.500   1.6544   0.07994   0.07441  -0.0646   0.0625   1.0000
  17.750   1.6530   0.08285   0.07737  -0.0643   0.0611   1.0000
  18.000   1.6566   0.08517   0.07975  -0.0640   0.0604   1.0000
  18.250   1.6581   0.08779   0.08243  -0.0638   0.0595   1.0000
  18.500   1.6604   0.09027   0.08498  -0.0636   0.0588   1.0000
  18.750   1.6606   0.09304   0.08781  -0.0635   0.0578   1.0000
  19.000   1.6612   0.09574   0.09056  -0.0634   0.0566   1.0000
  19.250   1.6601   0.09873   0.09360  -0.0635   0.0556   1.0000
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