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GOE 498 AIRFOIL (goe498-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 498 AIRFOIL (goe498-il)
Reynolds number: 1,000,000
Max Cl/Cd: 123.83 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe498-il-1000000.txt
Download as CSV file: xf-goe498-il-1000000.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 =     1.000 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -0.7437   0.11358   0.11101  -0.0695   1.0000   0.0305
 -18.750  -0.7648   0.10667   0.10402  -0.0733   1.0000   0.0308
 -18.500  -0.7819   0.10065   0.09792  -0.0765   1.0000   0.0310
 -18.250  -0.7986   0.09482   0.09201  -0.0797   1.0000   0.0313
 -18.000  -0.8150   0.08921   0.08633  -0.0826   1.0000   0.0315
 -17.750  -0.8311   0.08379   0.08083  -0.0854   1.0000   0.0318
 -17.500  -0.8465   0.07863   0.07558  -0.0880   1.0000   0.0320
 -17.250  -0.8593   0.07411   0.07100  -0.0901   1.0000   0.0322
 -17.000  -0.8736   0.06954   0.06635  -0.0922   1.0000   0.0324
 -16.750  -0.8882   0.06520   0.06194  -0.0939   1.0000   0.0325
 -16.500  -0.9056   0.06088   0.05754  -0.0954   1.0000   0.0327
 -16.250  -0.9252   0.05701   0.05361  -0.0961   1.0000   0.0327
 -16.000  -0.9375   0.05281   0.04933  -0.0987   0.9995   0.0329
 -15.750  -0.9389   0.04775   0.04420  -0.1049   0.9975   0.0333
 -15.500  -0.9364   0.04284   0.03922  -0.1115   0.9948   0.0336
 -15.250  -0.9305   0.03821   0.03452  -0.1181   0.9919   0.0339
 -15.000  -0.9247   0.03382   0.03003  -0.1241   0.9869   0.0343
 -14.750  -0.9096   0.02995   0.02607  -0.1308   0.9834   0.0346
 -14.500  -0.8945   0.02603   0.02204  -0.1381   0.9787   0.0350
 -14.250  -0.8716   0.02316   0.01903  -0.1442   0.9732   0.0355
 -14.000  -0.8434   0.02177   0.01756  -0.1471   0.9710   0.0360
 -13.750  -0.8129   0.02066   0.01637  -0.1497   0.9694   0.0365
 -13.500  -0.7800   0.01984   0.01546  -0.1521   0.9683   0.0369
 -13.250  -0.7603   0.01859   0.01415  -0.1529   0.9625   0.0376
 -13.000  -0.7321   0.01768   0.01321  -0.1543   0.9589   0.0383
 -12.750  -0.7004   0.01697   0.01246  -0.1560   0.9563   0.0390
 -12.500  -0.6669   0.01633   0.01177  -0.1579   0.9539   0.0397
 -12.250  -0.6443   0.01585   0.01124  -0.1574   0.9476   0.0403
 -12.000  -0.6154   0.01540   0.01072  -0.1580   0.9429   0.0410
 -11.750  -0.5843   0.01484   0.01009  -0.1592   0.9387   0.0418
 -11.500  -0.5635   0.01425   0.00947  -0.1584   0.9316   0.0427
 -11.250  -0.5365   0.01382   0.00901  -0.1585   0.9257   0.0436
 -11.000  -0.5084   0.01347   0.00860  -0.1588   0.9202   0.0445
 -10.750  -0.4847   0.01316   0.00824  -0.1580   0.9139   0.0453
 -10.500  -0.4575   0.01289   0.00790  -0.1579   0.9080   0.0461
 -10.250  -0.4321   0.01242   0.00739  -0.1577   0.9022   0.0475
 -10.000  -0.4079   0.01213   0.00710  -0.1570   0.8958   0.0487
  -9.750  -0.3810   0.01190   0.00682  -0.1568   0.8895   0.0500
  -9.500  -0.3537   0.01170   0.00655  -0.1566   0.8836   0.0512
  -9.250  -0.3294   0.01134   0.00618  -0.1559   0.8767   0.0527
  -9.000  -0.3027   0.01110   0.00591  -0.1556   0.8695   0.0542
  -8.750  -0.2761   0.01092   0.00569  -0.1552   0.8624   0.0558
  -8.500  -0.2493   0.01077   0.00549  -0.1548   0.8540   0.0571
  -8.250  -0.2233   0.01047   0.00516  -0.1544   0.8458   0.0591
  -8.000  -0.1969   0.01030   0.00498  -0.1540   0.8357   0.0609
  -7.750  -0.1701   0.01019   0.00480  -0.1536   0.8251   0.0626
  -7.500  -0.1441   0.01000   0.00454  -0.1530   0.8124   0.0644
  -7.250  -0.1181   0.00980   0.00432  -0.1525   0.7997   0.0664
  -7.000  -0.0918   0.00970   0.00415  -0.1520   0.7869   0.0682
  -6.500  -0.0395   0.00945   0.00376  -0.1509   0.7621   0.0719
  -6.250  -0.0135   0.00933   0.00358  -0.1504   0.7512   0.0742
  -6.000   0.0134   0.00923   0.00344  -0.1500   0.7419   0.0762
  -5.750   0.0402   0.00919   0.00332  -0.1496   0.7332   0.0777
  -5.500   0.0672   0.00898   0.00310  -0.1493   0.7258   0.0806
  -5.250   0.0938   0.00888   0.00295  -0.1488   0.7177   0.0832
  -5.000   0.1213   0.00880   0.00283  -0.1486   0.7109   0.0856
  -4.750   0.1485   0.00865   0.00267  -0.1483   0.7038   0.0893
  -4.500   0.1750   0.00857   0.00255  -0.1478   0.6956   0.0935
  -4.250   0.2024   0.00841   0.00242  -0.1475   0.6882   0.1006
  -4.000   0.2288   0.00826   0.00231  -0.1471   0.6794   0.1183
  -3.750   0.2558   0.00813   0.00225  -0.1468   0.6718   0.1414
  -3.500   0.2833   0.00805   0.00219  -0.1465   0.6645   0.1545
  -3.250   0.3101   0.00800   0.00213  -0.1461   0.6574   0.1656
  -3.000   0.3380   0.00794   0.00208  -0.1459   0.6512   0.1745
  -2.750   0.3653   0.00789   0.00203  -0.1456   0.6434   0.1834
  -2.500   0.3919   0.00786   0.00200  -0.1451   0.6351   0.1938
  -2.250   0.4195   0.00779   0.00196  -0.1449   0.6272   0.2071
  -2.000   0.4461   0.00777   0.00194  -0.1444   0.6189   0.2221
  -1.750   0.4735   0.00773   0.00193  -0.1441   0.6111   0.2391
  -1.500   0.5002   0.00773   0.00194  -0.1437   0.6022   0.2554
  -1.250   0.5271   0.00772   0.00195  -0.1433   0.5942   0.2709
  -1.000   0.5540   0.00773   0.00196  -0.1429   0.5855   0.2837
  -0.750   0.5804   0.00778   0.00198  -0.1424   0.5767   0.2939
  -0.500   0.6075   0.00778   0.00201  -0.1420   0.5686   0.3052
   0.000   0.6607   0.00786   0.00207  -0.1411   0.5526   0.3263
   0.250   0.6867   0.00794   0.00211  -0.1406   0.5440   0.3344
   0.500   0.7134   0.00797   0.00216  -0.1401   0.5366   0.3450
   0.750   0.7398   0.00803   0.00221  -0.1397   0.5288   0.3549
   1.000   0.7654   0.00809   0.00227  -0.1391   0.5212   0.3675
   1.250   0.7922   0.00813   0.00233  -0.1387   0.5141   0.3795
   1.500   0.8175   0.00820   0.00240  -0.1380   0.5062   0.3940
   1.750   0.8437   0.00824   0.00247  -0.1375   0.4990   0.4094
   2.000   0.8692   0.00831   0.00255  -0.1369   0.4906   0.4254
   2.250   0.8942   0.00839   0.00264  -0.1362   0.4824   0.4434
   2.500   0.9193   0.00846   0.00274  -0.1355   0.4725   0.4639
   2.750   0.9437   0.00855   0.00285  -0.1347   0.4638   0.4880
   3.000   0.9684   0.00863   0.00297  -0.1340   0.4544   0.5110
   3.250   0.9923   0.00874   0.00309  -0.1331   0.4450   0.5317
   3.500   1.0160   0.00886   0.00322  -0.1321   0.4345   0.5534
   3.750   1.0395   0.00898   0.00335  -0.1312   0.4252   0.5742
   4.000   1.0615   0.00912   0.00349  -0.1299   0.4143   0.5938
   4.250   1.0835   0.00924   0.00362  -0.1287   0.4046   0.6117
   4.500   1.1031   0.00940   0.00379  -0.1270   0.3939   0.6336
   4.750   1.1246   0.00951   0.00394  -0.1256   0.3842   0.6574
   5.000   1.1439   0.00966   0.00414  -0.1239   0.3741   0.6939
   5.250   1.1595   0.00957   0.00438  -0.1213   0.3647   0.8248
   5.500   1.1912   0.00962   0.00461  -0.1222   0.3550   1.0000
   5.750   1.2111   0.00988   0.00481  -0.1207   0.3452   1.0000
   6.000   1.2312   0.01013   0.00502  -0.1192   0.3355   1.0000
   6.250   1.2509   0.01040   0.00524  -0.1176   0.3271   1.0000
   6.500   1.2707   0.01066   0.00547  -0.1161   0.3183   1.0000
   6.750   1.2892   0.01098   0.00573  -0.1144   0.3086   1.0000
   7.000   1.3090   0.01125   0.00597  -0.1130   0.2995   1.0000
   7.250   1.3256   0.01163   0.00629  -0.1110   0.2876   1.0000
   7.500   1.3421   0.01204   0.00662  -0.1091   0.2731   1.0000
   7.750   1.3583   0.01246   0.00697  -0.1072   0.2585   1.0000
   8.000   1.3714   0.01301   0.00741  -0.1048   0.2392   1.0000
   8.250   1.3784   0.01384   0.00806  -0.1015   0.2088   1.0000
   8.500   1.3868   0.01463   0.00873  -0.0986   0.1882   1.0000
   8.750   1.3984   0.01531   0.00934  -0.0962   0.1776   1.0000
   9.000   1.4131   0.01585   0.00987  -0.0943   0.1726   1.0000
   9.250   1.4264   0.01648   0.01048  -0.0923   0.1674   1.0000
   9.500   1.4422   0.01701   0.01102  -0.0907   0.1642   1.0000
   9.750   1.4582   0.01754   0.01156  -0.0892   0.1618   1.0000
  10.000   1.4735   0.01812   0.01215  -0.0876   0.1592   1.0000
  10.250   1.4866   0.01882   0.01286  -0.0858   0.1561   1.0000
  10.500   1.4994   0.01957   0.01361  -0.0840   0.1528   1.0000
  10.750   1.5141   0.02022   0.01429  -0.0825   0.1506   1.0000
  11.000   1.5306   0.02080   0.01491  -0.0813   0.1489   1.0000
  11.250   1.5455   0.02148   0.01562  -0.0799   0.1464   1.0000
  11.500   1.5581   0.02232   0.01646  -0.0784   0.1433   1.0000
  11.750   1.5689   0.02329   0.01745  -0.0767   0.1398   1.0000
  12.000   1.5823   0.02412   0.01831  -0.0753   0.1370   1.0000
  12.250   1.5975   0.02486   0.01909  -0.0742   0.1339   1.0000
  12.500   1.6083   0.02592   0.02014  -0.0728   0.1286   1.0000
  12.750   1.6191   0.02701   0.02124  -0.0714   0.1230   1.0000
  13.000   1.6267   0.02837   0.02255  -0.0699   0.1124   1.0000
  13.250   1.6220   0.03070   0.02473  -0.0677   0.0907   1.0000
  13.500   1.6162   0.03327   0.02724  -0.0656   0.0792   1.0000
  13.750   1.6162   0.03547   0.02944  -0.0641   0.0732   1.0000
  14.000   1.6166   0.03772   0.03170  -0.0627   0.0689   1.0000
  14.250   1.6199   0.03979   0.03381  -0.0617   0.0653   1.0000
  14.500   1.6197   0.04223   0.03626  -0.0606   0.0619   1.0000
  14.750   1.6239   0.04429   0.03837  -0.0597   0.0589   1.0000
  15.000   1.6247   0.04675   0.04085  -0.0589   0.0563   1.0000
  15.250   1.6272   0.04912   0.04327  -0.0583   0.0538   1.0000
  15.500   1.6287   0.05162   0.04581  -0.0577   0.0518   1.0000
  15.750   1.6274   0.05447   0.04869  -0.0572   0.0495   1.0000
  16.000   1.6300   0.05697   0.05125  -0.0568   0.0481   1.0000
  16.250   1.6306   0.05976   0.05408  -0.0566   0.0466   1.0000
  16.500   1.6291   0.06283   0.05719  -0.0564   0.0451   1.0000
  16.750   1.6265   0.06609   0.06051  -0.0563   0.0439   1.0000
  17.000   1.6275   0.06900   0.06350  -0.0564   0.0430   1.0000
  17.250   1.6278   0.07202   0.06659  -0.0565   0.0421   1.0000
  17.500   1.6257   0.07541   0.07003  -0.0568   0.0412   1.0000
  17.750   1.6217   0.07911   0.07380  -0.0572   0.0404   1.0000
  18.000   1.6162   0.08307   0.07782  -0.0578   0.0396   1.0000
  18.250   1.6104   0.08715   0.08197  -0.0585   0.0389   1.0000
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