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GOE 501 AIRFOIL (goe501-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 501 AIRFOIL (goe501-il)
Reynolds number: 1,000,000
Max Cl/Cd: 137.89 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe501-il-1000000.txt
Download as CSV file: xf-goe501-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 501 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.6448   0.06407   0.06176  -0.1062   0.9895   0.0248
 -14.250  -0.6779   0.05272   0.05022  -0.1192   0.9854   0.0249
 -14.000  -0.6922   0.04299   0.04030  -0.1332   0.9820   0.0251
 -13.750  -0.6983   0.03448   0.03161  -0.1469   0.9743   0.0253
 -13.500  -0.6769   0.02708   0.02395  -0.1623   0.9696   0.0257
 -13.250  -0.6647   0.02236   0.01901  -0.1701   0.9606   0.0264
 -13.000  -0.6404   0.02126   0.01785  -0.1717   0.9566   0.0271
 -12.750  -0.6195   0.02049   0.01702  -0.1719   0.9516   0.0277
 -12.500  -0.5973   0.01978   0.01623  -0.1721   0.9465   0.0283
 -12.250  -0.5740   0.01904   0.01539  -0.1724   0.9421   0.0289
 -12.000  -0.5513   0.01838   0.01463  -0.1724   0.9372   0.0294
 -11.750  -0.5276   0.01787   0.01401  -0.1723   0.9320   0.0298
 -11.500  -0.5067   0.01670   0.01273  -0.1724   0.9269   0.0307
 -11.250  -0.4816   0.01626   0.01227  -0.1724   0.9223   0.0315
 -11.000  -0.4564   0.01587   0.01184  -0.1723   0.9167   0.0321
 -10.750  -0.4305   0.01546   0.01136  -0.1722   0.9115   0.0328
 -10.500  -0.4045   0.01503   0.01085  -0.1722   0.9062   0.0335
 -10.250  -0.3784   0.01469   0.01043  -0.1721   0.8996   0.0342
 -10.000  -0.3511   0.01443   0.01007  -0.1721   0.8937   0.0346
  -9.750  -0.3274   0.01349   0.00905  -0.1720   0.8856   0.0358
  -9.500  -0.3008   0.01315   0.00864  -0.1720   0.8777   0.0365
  -9.250  -0.2738   0.01293   0.00838  -0.1719   0.8685   0.0373
  -9.000  -0.2468   0.01267   0.00803  -0.1717   0.8593   0.0381
  -8.750  -0.2199   0.01239   0.00767  -0.1716   0.8496   0.0389
  -8.500  -0.1927   0.01216   0.00733  -0.1715   0.8410   0.0396
  -8.250  -0.1657   0.01184   0.00692  -0.1714   0.8327   0.0403
  -8.000  -0.1394   0.01130   0.00631  -0.1714   0.8252   0.0415
  -7.750  -0.1119   0.01108   0.00605  -0.1714   0.8176   0.0424
  -7.500  -0.0843   0.01090   0.00580  -0.1713   0.8109   0.0433
  -7.250  -0.0563   0.01073   0.00558  -0.1713   0.8046   0.0443
  -7.000  -0.0285   0.01058   0.00536  -0.1712   0.7988   0.0453
  -6.750  -0.0004   0.01044   0.00515  -0.1712   0.7935   0.0460
  -6.500   0.0270   0.00997   0.00463  -0.1712   0.7878   0.0474
  -6.250   0.0547   0.00976   0.00438  -0.1712   0.7822   0.0486
  -6.000   0.0830   0.00964   0.00422  -0.1712   0.7778   0.0498
  -5.750   0.1114   0.00951   0.00407  -0.1712   0.7734   0.0512
  -5.500   0.1397   0.00939   0.00390  -0.1712   0.7683   0.0524
  -5.250   0.1678   0.00933   0.00377  -0.1711   0.7634   0.0532
  -5.000   0.1959   0.00894   0.00336  -0.1712   0.7594   0.0553
  -4.750   0.2244   0.00879   0.00321  -0.1713   0.7554   0.0569
  -4.500   0.2528   0.00869   0.00309  -0.1713   0.7511   0.0587
  -4.250   0.2811   0.00863   0.00298  -0.1712   0.7468   0.0603
  -4.000   0.3097   0.00857   0.00289  -0.1713   0.7433   0.0614
  -3.750   0.3382   0.00830   0.00260  -0.1713   0.7395   0.0640
  -3.500   0.3666   0.00817   0.00246  -0.1714   0.7351   0.0663
  -3.250   0.3947   0.00811   0.00235  -0.1713   0.7299   0.0686
  -3.000   0.4231   0.00804   0.00226  -0.1713   0.7251   0.0705
  -2.750   0.4513   0.00791   0.00211  -0.1712   0.7190   0.0730
  -2.500   0.4791   0.00781   0.00197  -0.1711   0.7128   0.0770
  -2.250   0.5075   0.00771   0.00188  -0.1711   0.7076   0.0807
  -2.000   0.5358   0.00762   0.00178  -0.1711   0.7020   0.0863
  -1.750   0.5636   0.00749   0.00170  -0.1710   0.6964   0.1045
  -1.500   0.5918   0.00734   0.00169  -0.1710   0.6907   0.1488
  -1.250   0.6198   0.00729   0.00167  -0.1709   0.6836   0.1641
  -1.000   0.6474   0.00727   0.00165  -0.1708   0.6762   0.1760
  -0.750   0.6752   0.00724   0.00163  -0.1707   0.6671   0.1867
  -0.250   0.7292   0.00720   0.00163  -0.1701   0.6430   0.2271
   0.000   0.7553   0.00722   0.00166  -0.1697   0.6231   0.2547
   0.250   0.7793   0.00735   0.00172  -0.1689   0.5925   0.2803
   0.500   0.8024   0.00758   0.00183  -0.1679   0.5620   0.3019
   0.750   0.8266   0.00778   0.00195  -0.1671   0.5398   0.3222
   1.000   0.8518   0.00793   0.00207  -0.1665   0.5253   0.3377
   1.250   0.8770   0.00808   0.00218  -0.1660   0.5138   0.3510
   1.500   0.9033   0.00818   0.00228  -0.1656   0.5043   0.3652
   1.750   0.9289   0.00831   0.00239  -0.1651   0.4955   0.3786
   2.000   0.9551   0.00840   0.00249  -0.1647   0.4873   0.3915
   2.250   0.9805   0.00852   0.00261  -0.1642   0.4796   0.4079
   2.500   1.0070   0.00857   0.00271  -0.1639   0.4732   0.4273
   2.750   1.0324   0.00868   0.00283  -0.1634   0.4661   0.4467
   3.000   1.0583   0.00873   0.00295  -0.1630   0.4601   0.4766
   3.250   1.0840   0.00877   0.00310  -0.1626   0.4537   0.5300
   3.500   1.1084   0.00886   0.00328  -0.1619   0.4468   0.5859
   3.750   1.1342   0.00887   0.00341  -0.1615   0.4411   0.6393
   4.000   1.1581   0.00887   0.00358  -0.1608   0.4338   0.7178
   4.250   1.1818   0.00858   0.00374  -0.1598   0.4266   1.0000
   4.500   1.2065   0.00875   0.00387  -0.1592   0.4187   1.0000
   4.750   1.2303   0.00894   0.00402  -0.1584   0.4096   1.0000
   5.000   1.2539   0.00913   0.00418  -0.1576   0.4003   1.0000
   5.250   1.2774   0.00932   0.00433  -0.1568   0.3917   1.0000
   5.500   1.2994   0.00957   0.00452  -0.1557   0.3813   1.0000
   5.750   1.3216   0.00977   0.00469  -0.1546   0.3703   1.0000
   6.000   1.3414   0.01002   0.00489  -0.1531   0.3584   1.0000
   6.250   1.3598   0.01032   0.00513  -0.1513   0.3439   1.0000
   6.500   1.3768   0.01069   0.00540  -0.1493   0.3251   1.0000
   6.750   1.3904   0.01121   0.00578  -0.1467   0.2988   1.0000
   7.000   1.3968   0.01208   0.00638  -0.1431   0.2520   1.0000
   7.250   1.3964   0.01333   0.00727  -0.1384   0.1946   1.0000
   7.500   1.4109   0.01389   0.00776  -0.1363   0.1824   1.0000
   7.750   1.4283   0.01432   0.00818  -0.1346   0.1766   1.0000
   8.000   1.4457   0.01475   0.00860  -0.1329   0.1726   1.0000
   8.250   1.4624   0.01523   0.00907  -0.1312   0.1681   1.0000
   8.500   1.4795   0.01569   0.00954  -0.1296   0.1643   1.0000
   8.750   1.4982   0.01606   0.00995  -0.1283   0.1618   1.0000
   9.000   1.5156   0.01652   0.01042  -0.1268   0.1584   1.0000
   9.250   1.5310   0.01709   0.01098  -0.1250   0.1543   1.0000
   9.500   1.5453   0.01772   0.01161  -0.1232   0.1494   1.0000
   9.750   1.5649   0.01808   0.01201  -0.1221   0.1469   1.0000
  10.000   1.5819   0.01858   0.01254  -0.1207   0.1429   1.0000
  10.250   1.5960   0.01927   0.01321  -0.1189   0.1368   1.0000
  10.500   1.6123   0.01983   0.01379  -0.1175   0.1317   1.0000
  10.750   1.6252   0.02062   0.01453  -0.1157   0.1202   1.0000
  11.000   1.6278   0.02207   0.01577  -0.1128   0.0917   1.0000
  11.250   1.6298   0.02362   0.01724  -0.1100   0.0778   1.0000
  11.500   1.6377   0.02484   0.01845  -0.1079   0.0717   1.0000
  11.750   1.6456   0.02609   0.01972  -0.1059   0.0676   1.0000
  12.000   1.6547   0.02731   0.02096  -0.1042   0.0641   1.0000
  12.250   1.6650   0.02846   0.02215  -0.1026   0.0618   1.0000
  12.500   1.6732   0.02982   0.02353  -0.1010   0.0592   1.0000
  12.750   1.6798   0.03135   0.02508  -0.0993   0.0561   1.0000
  13.000   1.6902   0.03260   0.02639  -0.0980   0.0546   1.0000
  13.250   1.6997   0.03396   0.02781  -0.0967   0.0527   1.0000
  13.500   1.7071   0.03555   0.02942  -0.0954   0.0505   1.0000
  13.750   1.7125   0.03737   0.03126  -0.0940   0.0481   1.0000
  14.000   1.7214   0.03890   0.03285  -0.0929   0.0464   1.0000
  14.250   1.7293   0.04056   0.03455  -0.0919   0.0443   1.0000
  14.500   1.7329   0.04268   0.03669  -0.0907   0.0413   1.0000
  14.750   1.7395   0.04456   0.03862  -0.0898   0.0388   1.0000
  15.000   1.7420   0.04691   0.04096  -0.0888   0.0348   1.0000
  15.250   1.7445   0.04931   0.04339  -0.0879   0.0308   1.0000
  15.500   1.7440   0.05214   0.04624  -0.0871   0.0267   1.0000
  15.750   1.7424   0.05519   0.04931  -0.0864   0.0234   1.0000
  16.000   1.7392   0.05851   0.05266  -0.0858   0.0208   1.0000
  16.250   1.7391   0.06158   0.05579  -0.0855   0.0195   1.0000
  16.500   1.7364   0.06507   0.05934  -0.0853   0.0182   1.0000
  16.750   1.7332   0.06874   0.06308  -0.0853   0.0173   1.0000
  17.000   1.7329   0.07209   0.06652  -0.0854   0.0166   1.0000
  17.250   1.7311   0.07573   0.07023  -0.0857   0.0161   1.0000
  17.500   1.7280   0.07963   0.07422  -0.0861   0.0155   1.0000
  17.750   1.7225   0.08396   0.07862  -0.0867   0.0149   1.0000
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