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GOE 498 AIRFOIL (goe498-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 498 AIRFOIL (goe498-il)
Reynolds number: 500,000
Max Cl/Cd: 105.79 at α=4.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe498-il-500000.txt
Download as CSV file: xf-goe498-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 498 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7349   0.07356   0.07012  -0.0892   1.0000   0.0410
 -15.500  -0.7824   0.06506   0.06144  -0.0939   1.0000   0.0410
 -15.250  -0.8177   0.05934   0.05559  -0.0960   1.0000   0.0411
 -15.000  -0.8520   0.05458   0.05073  -0.0968   1.0000   0.0412
 -14.750  -0.8752   0.05014   0.04616  -0.0989   0.9994   0.0413
 -14.500  -0.8742   0.04466   0.04049  -0.1066   0.9961   0.0416
 -14.250  -0.8582   0.04187   0.03769  -0.1109   0.9935   0.0422
 -14.000  -0.8441   0.03913   0.03490  -0.1151   0.9899   0.0427
 -13.750  -0.8287   0.03625   0.03195  -0.1201   0.9856   0.0431
 -13.500  -0.8080   0.03332   0.02892  -0.1266   0.9821   0.0437
 -13.250  -0.7957   0.03062   0.02606  -0.1312   0.9749   0.0443
 -13.000  -0.7701   0.02868   0.02396  -0.1349   0.9712   0.0450
 -12.750  -0.7412   0.02704   0.02214  -0.1383   0.9691   0.0457
 -12.500  -0.7209   0.02585   0.02079  -0.1392   0.9641   0.0462
 -12.250  -0.6975   0.02444   0.01938  -0.1402   0.9600   0.0471
 -12.000  -0.6653   0.02359   0.01853  -0.1422   0.9578   0.0480
 -11.750  -0.6311   0.02275   0.01764  -0.1445   0.9562   0.0489
 -11.500  -0.5959   0.02180   0.01660  -0.1470   0.9549   0.0500
 -11.250  -0.5588   0.02089   0.01555  -0.1498   0.9539   0.0511
 -11.000  -0.5408   0.02009   0.01467  -0.1487   0.9466   0.0519
 -10.750  -0.5088   0.01924   0.01384  -0.1502   0.9435   0.0529
 -10.500  -0.4731   0.01864   0.01322  -0.1522   0.9411   0.0542
 -10.250  -0.4370   0.01803   0.01252  -0.1541   0.9386   0.0557
 -10.000  -0.4146   0.01758   0.01197  -0.1533   0.9314   0.0568
  -9.750  -0.3856   0.01677   0.01115  -0.1540   0.9264   0.0582
  -9.500  -0.3522   0.01625   0.01060  -0.1553   0.9225   0.0596
  -9.250  -0.3282   0.01587   0.01019  -0.1547   0.9152   0.0611
  -9.000  -0.2998   0.01549   0.00971  -0.1548   0.9088   0.0628
  -8.750  -0.2690   0.01488   0.00906  -0.1556   0.9035   0.0647
  -8.500  -0.2470   0.01455   0.00873  -0.1545   0.8947   0.0663
  -8.250  -0.2182   0.01422   0.00832  -0.1546   0.8880   0.0684
  -8.000  -0.1917   0.01398   0.00799  -0.1542   0.8800   0.0701
  -7.750  -0.1676   0.01338   0.00740  -0.1536   0.8712   0.0723
  -7.500  -0.1404   0.01306   0.00704  -0.1535   0.8632   0.0745
  -7.250  -0.1149   0.01281   0.00672  -0.1529   0.8536   0.0768
  -7.000  -0.0883   0.01238   0.00624  -0.1526   0.8451   0.0794
  -6.750  -0.0634   0.01204   0.00589  -0.1520   0.8344   0.0819
  -6.500  -0.0365   0.01179   0.00557  -0.1516   0.8248   0.0845
  -6.250  -0.0105   0.01150   0.00521  -0.1511   0.8142   0.0872
  -6.000   0.0155   0.01116   0.00487  -0.1507   0.8044   0.0906
  -5.750   0.0423   0.01096   0.00459  -0.1504   0.7943   0.0939
  -5.500   0.0686   0.01071   0.00431  -0.1499   0.7844   0.0978
  -5.250   0.0954   0.01051   0.00407  -0.1496   0.7747   0.1025
  -5.000   0.1220   0.01033   0.00387  -0.1492   0.7658   0.1084
  -4.750   0.1490   0.01017   0.00369  -0.1488   0.7571   0.1170
  -4.500   0.1759   0.01001   0.00357  -0.1485   0.7488   0.1312
  -4.250   0.2028   0.00988   0.00346  -0.1482   0.7403   0.1503
  -4.000   0.2302   0.00980   0.00335  -0.1479   0.7328   0.1666
  -3.750   0.2569   0.00968   0.00327  -0.1475   0.7247   0.1802
  -3.500   0.2841   0.00965   0.00319  -0.1472   0.7160   0.1926
  -3.250   0.3104   0.00958   0.00313  -0.1466   0.7066   0.2038
  -3.000   0.3372   0.00955   0.00307  -0.1462   0.6977   0.2168
  -2.750   0.3641   0.00950   0.00305  -0.1458   0.6900   0.2303
  -2.500   0.3911   0.00946   0.00302  -0.1454   0.6824   0.2439
  -2.250   0.4185   0.00949   0.00300  -0.1451   0.6753   0.2591
  -2.000   0.4453   0.00944   0.00300  -0.1447   0.6680   0.2739
  -1.750   0.4721   0.00943   0.00300  -0.1443   0.6604   0.2887
  -1.500   0.4990   0.00945   0.00300  -0.1439   0.6530   0.3015
  -1.250   0.5256   0.00945   0.00300  -0.1434   0.6444   0.3139
  -1.000   0.5520   0.00948   0.00301  -0.1429   0.6366   0.3260
  -0.750   0.5787   0.00947   0.00302  -0.1424   0.6289   0.3370
  -0.500   0.6048   0.00948   0.00303  -0.1419   0.6206   0.3488
  -0.250   0.6312   0.00951   0.00305  -0.1413   0.6125   0.3597
   0.000   0.6570   0.00952   0.00307  -0.1407   0.6035   0.3714
   0.250   0.6829   0.00957   0.00310  -0.1401   0.5955   0.3830
   0.500   0.7091   0.00959   0.00314  -0.1396   0.5875   0.3965
   0.750   0.7345   0.00965   0.00319  -0.1389   0.5798   0.4110
   1.000   0.7606   0.00966   0.00325  -0.1384   0.5721   0.4256
   1.250   0.7859   0.00973   0.00331  -0.1377   0.5639   0.4411
   1.500   0.8113   0.00977   0.00340  -0.1371   0.5561   0.4585
   1.750   0.8364   0.00982   0.00348  -0.1364   0.5478   0.4779
   2.000   0.8610   0.00992   0.00359  -0.1356   0.5402   0.4990
   2.250   0.8863   0.00996   0.00370  -0.1349   0.5323   0.5230
   2.500   0.9104   0.01008   0.00381  -0.1340   0.5243   0.5463
   2.750   0.9350   0.01015   0.00394  -0.1332   0.5162   0.5689
   3.000   0.9583   0.01025   0.00406  -0.1322   0.5073   0.5921
   3.250   0.9820   0.01033   0.00420  -0.1313   0.4995   0.6155
   3.500   1.0052   0.01041   0.00433  -0.1302   0.4909   0.6390
   4.000   1.0491   0.01053   0.00461  -0.1276   0.4731   0.7039
   4.250   1.0666   0.01047   0.00479  -0.1254   0.4644   0.7908
   4.500   1.0992   0.01039   0.00495  -0.1263   0.4539   1.0000
   4.750   1.1198   0.01060   0.00510  -0.1248   0.4452   1.0000
   5.000   1.1402   0.01079   0.00526  -0.1233   0.4357   1.0000
   5.250   1.1598   0.01102   0.00544  -0.1216   0.4264   1.0000
   5.500   1.1793   0.01126   0.00563  -0.1200   0.4167   1.0000
   5.750   1.1988   0.01151   0.00585  -0.1184   0.4080   1.0000
   6.000   1.2178   0.01178   0.00607  -0.1167   0.3983   1.0000
   6.250   1.2369   0.01206   0.00632  -0.1151   0.3896   1.0000
   6.500   1.2552   0.01236   0.00658  -0.1133   0.3804   1.0000
   6.750   1.2737   0.01267   0.00686  -0.1116   0.3715   1.0000
   7.000   1.2913   0.01301   0.00717  -0.1098   0.3625   1.0000
   7.250   1.3092   0.01335   0.00749  -0.1081   0.3540   1.0000
   7.500   1.3261   0.01374   0.00784  -0.1063   0.3449   1.0000
   7.750   1.3434   0.01411   0.00820  -0.1046   0.3369   1.0000
   8.000   1.3592   0.01455   0.00860  -0.1027   0.3270   1.0000
   8.250   1.3752   0.01499   0.00902  -0.1008   0.3167   1.0000
   8.500   1.3880   0.01557   0.00953  -0.0985   0.3053   1.0000
   8.750   1.4036   0.01606   0.01001  -0.0967   0.2940   1.0000
   9.000   1.4182   0.01660   0.01053  -0.0948   0.2836   1.0000
   9.250   1.4298   0.01729   0.01117  -0.0926   0.2702   1.0000
   9.500   1.4407   0.01805   0.01186  -0.0904   0.2545   1.0000
   9.750   1.4500   0.01892   0.01266  -0.0880   0.2361   1.0000
  10.000   1.4567   0.01996   0.01361  -0.0855   0.2174   1.0000
  10.250   1.4636   0.02105   0.01462  -0.0830   0.2035   1.0000
  10.500   1.4704   0.02219   0.01571  -0.0807   0.1936   1.0000
  10.750   1.4799   0.02322   0.01673  -0.0788   0.1874   1.0000
  11.000   1.4873   0.02441   0.01791  -0.0768   0.1818   1.0000
  11.250   1.4969   0.02550   0.01902  -0.0751   0.1775   1.0000
  11.500   1.5063   0.02665   0.02019  -0.0735   0.1733   1.0000
  11.750   1.5130   0.02802   0.02157  -0.0717   0.1691   1.0000
  12.000   1.5189   0.02949   0.02305  -0.0700   0.1651   1.0000
  12.250   1.5310   0.03058   0.02420  -0.0689   0.1619   1.0000
  12.500   1.5398   0.03193   0.02560  -0.0676   0.1583   1.0000
  12.750   1.5455   0.03357   0.02725  -0.0662   0.1546   1.0000
  13.000   1.5502   0.03534   0.02905  -0.0649   0.1509   1.0000
  13.250   1.5632   0.03647   0.03027  -0.0641   0.1472   1.0000
  13.500   1.5706   0.03812   0.03195  -0.0631   0.1427   1.0000
  13.750   1.5727   0.04027   0.03411  -0.0620   0.1379   1.0000
  14.000   1.5855   0.04150   0.03541  -0.0614   0.1316   1.0000
  14.250   1.5895   0.04359   0.03750  -0.0605   0.1233   1.0000
  14.500   1.5913   0.04594   0.03981  -0.0597   0.1068   1.0000
  14.750   1.5814   0.04956   0.04330  -0.0588   0.0894   1.0000
  15.000   1.5725   0.05318   0.04689  -0.0581   0.0814   1.0000
  15.250   1.5635   0.05696   0.05068  -0.0576   0.0762   1.0000
  15.500   1.5585   0.06043   0.05420  -0.0573   0.0723   1.0000
  15.750   1.5493   0.06450   0.05830  -0.0572   0.0693   1.0000
  16.000   1.5476   0.06773   0.06162  -0.0572   0.0666   1.0000
  16.250   1.5422   0.07152   0.06546  -0.0573   0.0641   1.0000
  16.500   1.5320   0.07603   0.07001  -0.0578   0.0621   1.0000
  16.750   1.5313   0.07936   0.07344  -0.0581   0.0603   1.0000
  17.000   1.5288   0.08299   0.07714  -0.0586   0.0585   1.0000
  17.250   1.5240   0.08699   0.08119  -0.0593   0.0570   1.0000
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