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GOE 435 AIRFOIL (goe435-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 435 AIRFOIL (goe435-il)
Reynolds number: 500,000
Max Cl/Cd: 69.9 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe435-il-500000-n5.txt
Download as CSV file: xf-goe435-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 435 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.6044   0.09221   0.08672  -0.0693   0.7820   0.0621
 -16.000  -0.6005   0.08936   0.08378  -0.0707   0.7742   0.0623
 -15.750  -0.5976   0.08638   0.08072  -0.0721   0.7679   0.0625
 -15.500  -0.5947   0.08336   0.07764  -0.0736   0.7623   0.0627
 -15.250  -0.5931   0.08022   0.07443  -0.0751   0.7563   0.0628
 -15.000  -0.5923   0.07703   0.07116  -0.0766   0.7502   0.0630
 -14.500  -0.5973   0.06990   0.06389  -0.0801   0.7412   0.0635
 -14.250  -0.6000   0.06632   0.06026  -0.0819   0.7377   0.0638
 -14.000  -0.6025   0.06283   0.05671  -0.0836   0.7337   0.0640
 -13.750  -0.6054   0.05935   0.05315  -0.0853   0.7292   0.0643
 -13.500  -0.6059   0.05621   0.04994  -0.0869   0.7246   0.0646
 -13.250  -0.6066   0.05311   0.04675  -0.0885   0.7205   0.0648
 -13.000  -0.6058   0.05022   0.04379  -0.0900   0.7168   0.0651
 -12.750  -0.6044   0.04743   0.04095  -0.0914   0.7140   0.0655
 -12.500  -0.6026   0.04473   0.03820  -0.0929   0.7108   0.0658
 -12.250  -0.5997   0.04228   0.03569  -0.0941   0.7071   0.0662
 -12.000  -0.5966   0.03982   0.03317  -0.0954   0.7032   0.0666
 -11.750  -0.5914   0.03760   0.03088  -0.0966   0.6993   0.0670
 -11.500  -0.5857   0.03537   0.02858  -0.0978   0.6955   0.0674
 -11.250  -0.5784   0.03328   0.02641  -0.0991   0.6917   0.0678
 -11.000  -0.5695   0.03128   0.02437  -0.1004   0.6889   0.0682
 -10.750  -0.5589   0.02938   0.02243  -0.1017   0.6857   0.0686
 -10.500  -0.5468   0.02759   0.02059  -0.1030   0.6820   0.0690
 -10.250  -0.5352   0.02575   0.01870  -0.1045   0.6780   0.0696
 -10.000  -0.5260   0.02399   0.01688  -0.1056   0.6739   0.0703
  -9.750  -0.5104   0.02244   0.01525  -0.1074   0.6697   0.0711
  -9.500  -0.4899   0.02110   0.01384  -0.1096   0.6656   0.0721
  -9.250  -0.4658   0.01996   0.01267  -0.1118   0.6618   0.0734
  -9.000  -0.4398   0.01905   0.01172  -0.1137   0.6572   0.0748
  -8.750  -0.4137   0.01831   0.01093  -0.1151   0.6519   0.0769
  -8.500  -0.3883   0.01759   0.01015  -0.1161   0.6463   0.0807
  -8.250  -0.3660   0.01628   0.00897  -0.1177   0.6410   0.1041
  -8.000  -0.3372   0.01596   0.00879  -0.1185   0.6347   0.1353
  -7.750  -0.3079   0.01578   0.00860  -0.1189   0.6276   0.1400
  -7.500  -0.2789   0.01566   0.00842  -0.1193   0.6208   0.1435
  -7.250  -0.2492   0.01552   0.00824  -0.1197   0.6134   0.1453
  -7.000  -0.2203   0.01533   0.00802  -0.1201   0.6044   0.1471
  -6.750  -0.1912   0.01518   0.00785  -0.1205   0.5958   0.1489
  -6.500  -0.1620   0.01506   0.00769  -0.1209   0.5856   0.1507
  -6.250  -0.1331   0.01498   0.00754  -0.1212   0.5762   0.1523
  -6.000  -0.1040   0.01490   0.00740  -0.1215   0.5665   0.1537
  -5.750  -0.0752   0.01484   0.00727  -0.1217   0.5582   0.1549
  -5.500  -0.0458   0.01479   0.00716  -0.1220   0.5507   0.1559
  -5.250  -0.0169   0.01475   0.00705  -0.1222   0.5433   0.1565
  -5.000   0.0117   0.01462   0.00688  -0.1225   0.5371   0.1574
  -4.750   0.0410   0.01446   0.00671  -0.1229   0.5318   0.1584
  -4.500   0.0701   0.01434   0.00657  -0.1233   0.5270   0.1594
  -4.250   0.0992   0.01426   0.00646  -0.1236   0.5224   0.1603
  -3.750   0.1577   0.01412   0.00628  -0.1242   0.5136   0.1624
  -3.500   0.1872   0.01407   0.00621  -0.1246   0.5090   0.1637
  -3.250   0.2164   0.01403   0.00615  -0.1248   0.5041   0.1647
  -3.000   0.2452   0.01401   0.00608  -0.1250   0.4994   0.1655
  -2.500   0.3039   0.01393   0.00596  -0.1256   0.4922   0.1668
  -2.250   0.3335   0.01388   0.00591  -0.1259   0.4884   0.1675
  -2.000   0.3629   0.01386   0.00587  -0.1262   0.4846   0.1683
  -1.750   0.3921   0.01387   0.00585  -0.1264   0.4811   0.1691
  -1.500   0.4210   0.01384   0.00580  -0.1267   0.4778   0.1702
  -1.250   0.4497   0.01380   0.00574  -0.1269   0.4744   0.1716
  -1.000   0.4791   0.01375   0.00570  -0.1272   0.4719   0.1730
  -0.750   0.5089   0.01369   0.00566  -0.1276   0.4696   0.1743
  -0.500   0.5385   0.01364   0.00564  -0.1279   0.4667   0.1752
  -0.250   0.5677   0.01362   0.00562  -0.1282   0.4633   0.1762
   0.000   0.5966   0.01362   0.00562  -0.1284   0.4600   0.1772
   0.250   0.6252   0.01365   0.00563  -0.1285   0.4568   0.1784
   0.500   0.6532   0.01369   0.00565  -0.1285   0.4533   0.1797
   0.750   0.6816   0.01373   0.00569  -0.1287   0.4501   0.1809
   1.000   0.7107   0.01373   0.00571  -0.1289   0.4469   0.1821
   1.250   0.7393   0.01375   0.00574  -0.1290   0.4433   0.1833
   1.750   0.7945   0.01383   0.00583  -0.1290   0.4348   0.1882
   2.000   0.8210   0.01391   0.00589  -0.1288   0.4304   0.1915
   2.250   0.8492   0.01392   0.00595  -0.1289   0.4261   0.1956
   2.750   0.9026   0.01394   0.00607  -0.1288   0.4151   0.2266
   3.000   0.9300   0.01374   0.00622  -0.1292   0.4094   0.3366
   3.250   0.9554   0.01387   0.00638  -0.1289   0.4018   0.3492
   3.500   0.9763   0.01410   0.00658  -0.1277   0.3937   0.3582
   3.750   0.9982   0.01428   0.00675  -0.1267   0.3851   0.3638
   4.000   1.0162   0.01457   0.00702  -0.1252   0.3754   0.3689
   4.250   1.0362   0.01491   0.00734  -0.1241   0.3641   0.3740
   4.500   1.0550   0.01537   0.00774  -0.1229   0.3529   0.3787
   4.750   1.0720   0.01593   0.00822  -0.1215   0.3417   0.3826
   5.000   1.0912   0.01641   0.00867  -0.1204   0.3325   0.3855
   5.250   1.1079   0.01700   0.00924  -0.1192   0.3243   0.3890
   5.500   1.1272   0.01751   0.00975  -0.1183   0.3173   0.3927
   5.750   1.1436   0.01817   0.01039  -0.1170   0.3102   0.3961
   6.000   1.1611   0.01880   0.01101  -0.1160   0.3043   0.3994
   6.250   1.1787   0.01945   0.01165  -0.1151   0.2985   0.4025
   6.500   1.1937   0.02027   0.01243  -0.1139   0.2926   0.4047
   6.750   1.2100   0.02104   0.01320  -0.1129   0.2876   0.4067
   7.000   1.2279   0.02174   0.01392  -0.1122   0.2826   0.4100
   7.250   1.2430   0.02263   0.01483  -0.1113   0.2777   0.4135
   7.500   1.2568   0.02363   0.01582  -0.1103   0.2734   0.4166
   7.750   1.2742   0.02442   0.01665  -0.1097   0.2704   0.4193
   8.000   1.2918   0.02522   0.01748  -0.1090   0.2673   0.4220
   8.250   1.3074   0.02616   0.01844  -0.1083   0.2641   0.4245
   8.500   1.3216   0.02721   0.01951  -0.1075   0.2608   0.4271
   8.750   1.3336   0.02843   0.02073  -0.1066   0.2575   0.4294
   9.000   1.3478   0.02953   0.02185  -0.1059   0.2546   0.4326
   9.250   1.3639   0.03047   0.02284  -0.1053   0.2517   0.4367
   9.500   1.3774   0.03164   0.02406  -0.1047   0.2485   0.4404
   9.750   1.3896   0.03291   0.02536  -0.1039   0.2452   0.4440
  10.000   1.4000   0.03435   0.02681  -0.1031   0.2422   0.4479
  10.250   1.4100   0.03584   0.02832  -0.1023   0.2394   0.4520
  10.750   1.4377   0.03824   0.03086  -0.1013   0.2348   0.4646
  11.000   1.4493   0.03967   0.03234  -0.1007   0.2322   0.4727
  11.250   1.4601   0.04116   0.03388  -0.1001   0.2296   0.4809
  11.500   1.4678   0.04297   0.03575  -0.0994   0.2269   0.4916
  11.750   1.4757   0.04476   0.03758  -0.0988   0.2243   0.5035
  12.000   1.4887   0.04614   0.03906  -0.0984   0.2220   0.5183
  12.500   1.5086   0.04950   0.04261  -0.0976   0.2169   0.5592
  12.750   1.5159   0.05147   0.04466  -0.0971   0.2143   0.5827
  13.000   1.5215   0.05360   0.04687  -0.0967   0.2118   0.6062
  13.250   1.5288   0.05558   0.04894  -0.0962   0.2097   0.6305
  13.500   1.5386   0.05736   0.05084  -0.0959   0.2079   0.6562
  13.750   1.5478   0.05916   0.05275  -0.0956   0.2058   0.6813
  14.000   1.5552   0.06118   0.05487  -0.0952   0.2036   0.7037
  14.250   1.5607   0.06339   0.05715  -0.0948   0.2015   0.7224
  14.500   1.5657   0.06565   0.05947  -0.0945   0.1993   0.7391
  14.750   1.5681   0.06822   0.06209  -0.0941   0.1973   0.7527
  15.000   1.5757   0.07024   0.06418  -0.0939   0.1956   0.7660
  15.250   1.5835   0.07225   0.06628  -0.0937   0.1939   0.7797
  15.500   1.5896   0.07445   0.06855  -0.0935   0.1920   0.7933
  15.750   1.5957   0.07661   0.07080  -0.0933   0.1900   0.8088
  16.000   1.5995   0.07903   0.07331  -0.0931   0.1880   0.8297
  16.250   1.5987   0.08123   0.07572  -0.0921   0.1862   0.9638
  16.500   1.6020   0.08378   0.07827  -0.0921   0.1843   1.0000
  16.750   1.6075   0.08609   0.08063  -0.0920   0.1827   1.0000
  17.000   1.6133   0.08840   0.08298  -0.0921   0.1810   1.0000
  17.250   1.6188   0.09070   0.08533  -0.0921   0.1789   1.0000
  17.500   1.6229   0.09318   0.08783  -0.0922   0.1766   1.0000
  17.750   1.6224   0.09624   0.09092  -0.0924   0.1743   1.0000
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