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GOE 435 AIRFOIL (goe435-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 435 AIRFOIL (goe435-il)
Reynolds number: 500,000
Max Cl/Cd: 75.77 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe435-il-500000.txt
Download as CSV file: xf-goe435-il-500000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.8245   0.10577   0.10112  -0.0660   1.0000   0.0716
 -19.500  -0.8149   0.10373   0.09907  -0.0672   1.0000   0.0719
 -19.250  -0.8051   0.10171   0.09704  -0.0683   1.0000   0.0721
 -19.000  -0.7951   0.09972   0.09504  -0.0694   1.0000   0.0724
 -18.750  -0.7846   0.09780   0.09311  -0.0704   1.0000   0.0726
 -18.500  -0.7740   0.09590   0.09120  -0.0714   1.0000   0.0728
 -18.250  -0.7636   0.09397   0.08926  -0.0724   1.0000   0.0730
 -18.000  -0.7533   0.09202   0.08730  -0.0735   1.0000   0.0732
 -17.750  -0.7432   0.09002   0.08529  -0.0746   1.0000   0.0734
 -17.500  -0.7328   0.08805   0.08332  -0.0757   1.0000   0.0736
 -17.250  -0.7224   0.08611   0.08137  -0.0768   1.0000   0.0738
 -17.000  -0.7122   0.08412   0.07939  -0.0779   1.0000   0.0740
 -16.750  -0.6975   0.08193   0.07716  -0.0804   0.9761   0.0743
 -16.500  -0.6870   0.07973   0.07491  -0.0818   0.9526   0.0745
 -16.250  -0.6829   0.07779   0.07289  -0.0816   0.9262   0.0747
 -16.000  -0.6786   0.07591   0.07091  -0.0814   0.9010   0.0749
 -15.750  -0.6735   0.07391   0.06880  -0.0815   0.8785   0.0751
 -15.500  -0.6682   0.07176   0.06651  -0.0820   0.8601   0.0753
 -15.250  -0.6626   0.06956   0.06419  -0.0826   0.8442   0.0755
 -15.000  -0.6555   0.06742   0.06196  -0.0834   0.8315   0.0757
 -14.750  -0.6491   0.06532   0.05975  -0.0842   0.8205   0.0760
 -14.500  -0.6438   0.06297   0.05738  -0.0852   0.8128   0.0764
 -14.250  -0.6400   0.06050   0.05485  -0.0863   0.8050   0.0768
 -14.000  -0.6375   0.05791   0.05218  -0.0874   0.7974   0.0772
 -13.750  -0.6368   0.05502   0.04923  -0.0889   0.7913   0.0776
 -13.500  -0.6350   0.05230   0.04646  -0.0902   0.7857   0.0780
 -13.250  -0.6351   0.04938   0.04348  -0.0917   0.7803   0.0784
 -13.000  -0.6333   0.04678   0.04079  -0.0929   0.7750   0.0789
 -12.750  -0.6330   0.04406   0.03798  -0.0943   0.7694   0.0793
 -12.500  -0.6308   0.04156   0.03544  -0.0956   0.7657   0.0798
 -12.250  -0.6291   0.03899   0.03282  -0.0970   0.7613   0.0803
 -12.000  -0.6258   0.03659   0.03035  -0.0983   0.7566   0.0808
 -11.750  -0.6212   0.03430   0.02798  -0.0995   0.7519   0.0814
 -11.500  -0.6152   0.03209   0.02568  -0.1008   0.7472   0.0820
 -11.250  -0.6072   0.03002   0.02352  -0.1022   0.7426   0.0828
 -11.000  -0.6023   0.02748   0.02095  -0.1041   0.7393   0.0841
 -10.750  -0.5948   0.02516   0.01860  -0.1059   0.7353   0.0856
 -10.500  -0.5881   0.02319   0.01657  -0.1073   0.7310   0.0873
 -10.000  -0.5585   0.01854   0.01206  -0.1148   0.7219   0.1255
  -9.750  -0.5293   0.01831   0.01181  -0.1158   0.7168   0.1389
  -9.500  -0.4995   0.01815   0.01163  -0.1164   0.7136   0.1446
  -9.250  -0.4705   0.01787   0.01136  -0.1173   0.7095   0.1482
  -9.000  -0.4405   0.01774   0.01121  -0.1180   0.7050   0.1520
  -8.750  -0.4105   0.01764   0.01104  -0.1187   0.7002   0.1548
  -8.500  -0.3802   0.01764   0.01091  -0.1194   0.6949   0.1566
  -8.250  -0.3532   0.01726   0.01054  -0.1199   0.6896   0.1591
  -8.000  -0.3243   0.01703   0.01033  -0.1205   0.6850   0.1612
  -7.750  -0.2950   0.01686   0.01016  -0.1210   0.6796   0.1632
  -7.500  -0.2655   0.01674   0.00999  -0.1215   0.6740   0.1653
  -7.250  -0.2363   0.01665   0.00980  -0.1219   0.6680   0.1668
  -7.000  -0.2067   0.01653   0.00964  -0.1224   0.6623   0.1681
  -6.750  -0.1769   0.01643   0.00951  -0.1229   0.6556   0.1690
  -6.500  -0.1488   0.01610   0.00913  -0.1231   0.6487   0.1704
  -6.250  -0.1211   0.01576   0.00876  -0.1233   0.6416   0.1721
  -6.000  -0.0923   0.01548   0.00852  -0.1237   0.6336   0.1736
  -5.750  -0.0636   0.01529   0.00828  -0.1240   0.6253   0.1748
  -5.500  -0.0346   0.01514   0.00810  -0.1243   0.6169   0.1763
  -5.250  -0.0056   0.01498   0.00791  -0.1246   0.6077   0.1774
  -5.000   0.0231   0.01487   0.00772  -0.1248   0.5994   0.1784
  -4.750   0.0524   0.01472   0.00756  -0.1251   0.5914   0.1793
  -4.500   0.0813   0.01462   0.00739  -0.1254   0.5839   0.1802
  -4.250   0.1103   0.01453   0.00724  -0.1256   0.5773   0.1810
  -4.000   0.1396   0.01444   0.00712  -0.1259   0.5705   0.1818
  -3.750   0.1685   0.01441   0.00701  -0.1261   0.5637   0.1826
  -3.500   0.1976   0.01440   0.00694  -0.1263   0.5574   0.1834
  -3.250   0.2268   0.01424   0.00678  -0.1266   0.5518   0.1844
  -3.000   0.2555   0.01407   0.00657  -0.1269   0.5466   0.1855
  -2.750   0.2842   0.01397   0.00643  -0.1272   0.5413   0.1866
  -2.500   0.3134   0.01387   0.00631  -0.1275   0.5364   0.1877
  -2.250   0.3429   0.01374   0.00621  -0.1279   0.5322   0.1890
  -2.000   0.3724   0.01367   0.00613  -0.1282   0.5282   0.1904
  -1.750   0.4017   0.01363   0.00607  -0.1285   0.5242   0.1920
  -1.500   0.4310   0.01364   0.00603  -0.1288   0.5201   0.1935
  -1.250   0.4607   0.01366   0.00602  -0.1292   0.5164   0.1949
  -1.000   0.4904   0.01360   0.00598  -0.1295   0.5138   0.1962
  -0.750   0.5201   0.01357   0.00596  -0.1298   0.5106   0.1974
  -0.500   0.5495   0.01355   0.00594  -0.1301   0.5071   0.1983
  -0.250   0.5788   0.01355   0.00592  -0.1304   0.5036   0.1993
   0.000   0.6081   0.01354   0.00588  -0.1307   0.5000   0.2015
   0.250   0.6379   0.01361   0.00591  -0.1311   0.4958   0.2041
   0.500   0.6673   0.01356   0.00591  -0.1314   0.4931   0.2069
   0.750   0.6964   0.01351   0.00591  -0.1317   0.4901   0.2103
   1.000   0.7254   0.01349   0.00592  -0.1319   0.4866   0.2145
   1.250   0.7545   0.01341   0.00590  -0.1322   0.4832   0.2252
   1.500   0.7842   0.01307   0.00588  -0.1331   0.4794   0.3108
   1.750   0.8129   0.01321   0.00610  -0.1333   0.4751   0.3545
   2.000   0.8414   0.01336   0.00628  -0.1334   0.4713   0.3686
   2.250   0.8691   0.01345   0.00642  -0.1333   0.4680   0.3795
   2.500   0.8967   0.01355   0.00653  -0.1332   0.4642   0.3859
   2.750   0.9239   0.01364   0.00666  -0.1330   0.4600   0.3924
   3.000   0.9503   0.01381   0.00681  -0.1327   0.4553   0.3986
   3.250   0.9767   0.01403   0.00698  -0.1325   0.4504   0.4030
   3.500   1.0028   0.01413   0.00710  -0.1321   0.4463   0.4060
   3.750   1.0286   0.01416   0.00719  -0.1318   0.4413   0.4111
   4.000   1.0529   0.01429   0.00732  -0.1312   0.4358   0.4153
   4.250   1.0759   0.01449   0.00750  -0.1304   0.4300   0.4190
   4.500   1.0995   0.01459   0.00766  -0.1297   0.4238   0.4230
   4.750   1.1184   0.01477   0.00781  -0.1282   0.4169   0.4260
   5.000   1.1366   0.01503   0.00803  -0.1266   0.4100   0.4285
   5.250   1.1578   0.01528   0.00829  -0.1256   0.4013   0.4306
   5.500   1.1764   0.01562   0.00861  -0.1244   0.3921   0.4350
   5.750   1.1955   0.01600   0.00899  -0.1233   0.3808   0.4387
   6.000   1.2121   0.01651   0.00948  -0.1220   0.3695   0.4419
   6.250   1.2255   0.01721   0.01011  -0.1203   0.3583   0.4448
   6.500   1.2409   0.01787   0.01074  -0.1189   0.3475   0.4476
   6.750   1.2544   0.01867   0.01149  -0.1174   0.3382   0.4503
   7.000   1.2680   0.01950   0.01228  -0.1160   0.3297   0.4533
   7.250   1.2812   0.02040   0.01313  -0.1146   0.3227   0.4556
   7.500   1.2976   0.02114   0.01390  -0.1137   0.3167   0.4601
   7.750   1.3107   0.02210   0.01485  -0.1126   0.3110   0.4639
   8.000   1.3241   0.02307   0.01583  -0.1115   0.3061   0.4675
   8.250   1.3415   0.02384   0.01665  -0.1108   0.3019   0.4716
   8.500   1.3555   0.02484   0.01765  -0.1098   0.2974   0.4756
   8.750   1.3668   0.02602   0.01881  -0.1087   0.2929   0.4793
   9.000   1.3789   0.02717   0.01996  -0.1077   0.2888   0.4829
   9.250   1.3963   0.02800   0.02088  -0.1072   0.2854   0.4898
   9.500   1.4102   0.02908   0.02202  -0.1065   0.2817   0.4960
   9.750   1.4218   0.03031   0.02326  -0.1056   0.2780   0.5027
  10.000   1.4310   0.03172   0.02466  -0.1045   0.2743   0.5098
  10.250   1.4445   0.03286   0.02589  -0.1039   0.2712   0.5222
  10.500   1.4601   0.03389   0.02702  -0.1034   0.2686   0.5373
  10.750   1.4740   0.03505   0.02829  -0.1029   0.2657   0.5589
  11.000   1.4855   0.03640   0.02974  -0.1022   0.2627   0.5878
  11.250   1.4960   0.03782   0.03127  -0.1015   0.2596   0.6237
  11.500   1.5045   0.03934   0.03286  -0.1005   0.2560   0.6613
  11.750   1.5173   0.04068   0.03436  -0.1000   0.2538   0.6960
  12.000   1.5297   0.04200   0.03580  -0.0995   0.2512   0.7244
  12.250   1.5407   0.04346   0.03734  -0.0988   0.2485   0.7468
  12.500   1.5492   0.04513   0.03906  -0.0981   0.2457   0.7654
  12.750   1.5574   0.04682   0.04077  -0.0974   0.2430   0.7826
  13.000   1.5655   0.04841   0.04238  -0.0965   0.2400   0.7992
  13.250   1.5755   0.05002   0.04411  -0.0960   0.2382   0.8173
  13.500   1.5859   0.05155   0.04577  -0.0955   0.2361   0.8405
  13.750   1.5910   0.05286   0.04731  -0.0940   0.2339   1.0000
  14.000   1.5993   0.05475   0.04922  -0.0937   0.2316   1.0000
  14.250   1.6076   0.05662   0.05108  -0.0933   0.2293   1.0000
  14.500   1.6146   0.05859   0.05303  -0.0929   0.2268   1.0000
  14.750   1.6236   0.06027   0.05468  -0.0924   0.2243   1.0000
  15.000   1.6321   0.06222   0.05670  -0.0922   0.2227   1.0000
  15.250   1.6399   0.06423   0.05877  -0.0920   0.2208   1.0000
  15.500   1.6469   0.06633   0.06091  -0.0918   0.2188   1.0000
  15.750   1.6546   0.06834   0.06294  -0.0916   0.2167   1.0000
  16.000   1.6606   0.07051   0.06512  -0.0914   0.2147   1.0000
  16.250   1.6666   0.07260   0.06720  -0.0911   0.2125   1.0000
  16.500   1.6768   0.07412   0.06868  -0.0907   0.2101   1.0000
  16.750   1.6817   0.07653   0.07119  -0.0907   0.2086   1.0000
  17.000   1.6855   0.07905   0.07378  -0.0907   0.2067   1.0000
  17.250   1.6910   0.08136   0.07614  -0.0907   0.2047   1.0000
  17.500   1.6952   0.08381   0.07862  -0.0907   0.2026   1.0000
  17.750   1.6992   0.08622   0.08104  -0.0907   0.2006   1.0000
  18.000   1.7058   0.08826   0.08307  -0.0907   0.1987   1.0000
  18.250   1.7168   0.08966   0.08444  -0.0905   0.1966   1.0000
  18.500   1.7194   0.09235   0.08722  -0.0907   0.1953   1.0000
  18.750   1.7212   0.09512   0.09008  -0.0909   0.1937   1.0000
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