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GOE 535 AIRFOIL (goe535-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 535 AIRFOIL (goe535-il)
Reynolds number: 200,000
Max Cl/Cd: 68.07 at α=7°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe535-il-200000.txt
Download as CSV file: xf-goe535-il-200000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 535 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -11.250  -0.2152   0.12486   0.12108  -0.0363   1.0000   0.0761
 -11.000  -0.2160   0.12287   0.11914  -0.0355   1.0000   0.0777
 -10.500  -0.2652   0.11767   0.11409  -0.0377   1.0000   0.0809
 -10.250  -0.2591   0.11605   0.11252  -0.0347   1.0000   0.0812
 -10.000  -0.2267   0.11269   0.10915  -0.0369   0.9974   0.0820
  -9.750  -0.1994   0.10920   0.10565  -0.0405   0.9939   0.0835
  -9.500  -0.1790   0.10525   0.10170  -0.0455   0.9895   0.0861
  -9.250  -0.1809   0.09839   0.09484  -0.0560   0.9827   0.0897
  -9.000  -0.0243   0.08524   0.08182  -0.0712   0.9574   0.0961
  -8.750  -0.0301   0.07804   0.07462  -0.0790   0.9523   0.0992
  -8.500   0.0003   0.07528   0.07186  -0.0799   0.9461   0.1005
  -8.250  -0.2017   0.05602   0.05224  -0.1053   0.9391   0.0810
  -8.000  -0.1679   0.05328   0.04951  -0.1086   0.9353   0.0816
  -7.750  -0.1758   0.03624   0.03148  -0.1332   0.9172   0.0768
  -7.500  -0.1574   0.03186   0.02657  -0.1366   0.9038   0.0775
  -7.250  -0.1258   0.02837   0.02252  -0.1403   0.8960   0.0791
  -7.000  -0.1017   0.02608   0.01967  -0.1412   0.8826   0.0810
  -6.750  -0.0710   0.02492   0.01862  -0.1418   0.8717   0.0830
  -6.500  -0.0387   0.02386   0.01742  -0.1427   0.8605   0.0856
  -6.250  -0.0128   0.02268   0.01588  -0.1426   0.8456   0.0882
  -6.000   0.0153   0.02133   0.01432  -0.1428   0.8324   0.0904
  -5.750   0.0452   0.02060   0.01356  -0.1429   0.8195   0.0932
  -5.500   0.0711   0.02000   0.01277  -0.1424   0.8043   0.0964
  -5.250   0.0979   0.01917   0.01171  -0.1420   0.7903   0.0994
  -5.000   0.1260   0.01853   0.01102  -0.1418   0.7770   0.1024
  -4.750   0.1515   0.01811   0.01048  -0.1410   0.7619   0.1059
  -4.500   0.1780   0.01772   0.00987  -0.1404   0.7480   0.1090
  -4.250   0.2050   0.01708   0.00922  -0.1400   0.7358   0.1126
  -4.000   0.2300   0.01676   0.00885  -0.1392   0.7214   0.1163
  -3.750   0.2567   0.01654   0.00846  -0.1385   0.7083   0.1197
  -3.500   0.2824   0.01601   0.00791  -0.1378   0.6955   0.1236
  -3.250   0.3075   0.01574   0.00764  -0.1370   0.6819   0.1277
  -3.000   0.3344   0.01559   0.00734  -0.1364   0.6701   0.1319
  -2.750   0.3591   0.01522   0.00700  -0.1356   0.6571   0.1365
  -2.500   0.3850   0.01505   0.00680  -0.1349   0.6449   0.1417
  -2.250   0.4111   0.01488   0.00655  -0.1341   0.6331   0.1477
  -2.000   0.4363   0.01468   0.00639  -0.1334   0.6211   0.1557
  -1.750   0.4629   0.01454   0.00619  -0.1329   0.6108   0.1664
  -1.500   0.4880   0.01432   0.00607  -0.1321   0.5993   0.1870
  -1.250   0.5130   0.01380   0.00601  -0.1317   0.5898   0.3119
  -1.000   0.5382   0.01402   0.00637  -0.1307   0.5791   0.3964
  -0.750   0.5650   0.01433   0.00657  -0.1300   0.5702   0.4252
  -0.500   0.5908   0.01459   0.00682  -0.1291   0.5609   0.4434
  -0.250   0.6171   0.01481   0.00696  -0.1284   0.5522   0.4580
   0.000   0.6437   0.01509   0.00716  -0.1277   0.5443   0.4714
   0.250   0.6693   0.01527   0.00735  -0.1269   0.5360   0.4820
   0.500   0.6966   0.01556   0.00749  -0.1264   0.5291   0.4946
   0.750   0.7218   0.01576   0.00776  -0.1255   0.5216   0.5051
   1.000   0.7480   0.01598   0.00790  -0.1249   0.5144   0.5167
   1.250   0.7751   0.01621   0.00807  -0.1244   0.5083   0.5254
   1.500   0.8004   0.01643   0.00828  -0.1236   0.5016   0.5365
   1.750   0.8254   0.01657   0.00847  -0.1227   0.4949   0.5469
   2.000   0.8527   0.01683   0.00860  -0.1224   0.4891   0.5588
   2.250   0.8776   0.01697   0.00881  -0.1216   0.4831   0.5665
   2.500   0.9033   0.01709   0.00890  -0.1210   0.4766   0.5728
   2.750   0.9303   0.01723   0.00894  -0.1207   0.4709   0.5785
   3.000   0.9565   0.01740   0.00910  -0.1202   0.4651   0.5839
   3.250   0.9810   0.01750   0.00923  -0.1194   0.4585   0.5896
   3.500   1.0072   0.01766   0.00930  -0.1190   0.4525   0.5958
   3.750   1.0344   0.01786   0.00945  -0.1188   0.4469   0.6013
   4.000   1.0575   0.01797   0.00965  -0.1178   0.4409   0.6084
   4.250   1.0828   0.01812   0.00978  -0.1172   0.4351   0.6161
   4.500   1.1099   0.01831   0.00992  -0.1169   0.4300   0.6234
   4.750   1.1344   0.01855   0.01020  -0.1163   0.4246   0.6319
   5.000   1.1580   0.01866   0.01040  -0.1154   0.4188   0.6402
   5.250   1.1832   0.01882   0.01055  -0.1149   0.4134   0.6506
   5.500   1.2103   0.01911   0.01079  -0.1147   0.4083   0.6620
   5.750   1.2319   0.01925   0.01110  -0.1136   0.4027   0.6758
   6.000   1.2575   0.01940   0.01134  -0.1131   0.3971   0.6936
   6.250   1.2857   0.01955   0.01154  -0.1132   0.3919   0.7210
   6.500   1.3215   0.01952   0.01194  -0.1150   0.3857   1.0000
   6.750   1.3439   0.01981   0.01223  -0.1141   0.3797   1.0000
   7.000   1.3683   0.02010   0.01243  -0.1135   0.3743   1.0000
   7.250   1.3928   0.02054   0.01280  -0.1130   0.3689   1.0000
   7.500   1.4116   0.02086   0.01320  -0.1114   0.3630   1.0000
   7.750   1.4332   0.02116   0.01347  -0.1103   0.3575   1.0000
   8.000   1.4596   0.02161   0.01377  -0.1101   0.3523   1.0000
   8.250   1.4741   0.02197   0.01428  -0.1079   0.3464   1.0000
   8.500   1.4926   0.02229   0.01461  -0.1063   0.3405   1.0000
   8.750   1.5162   0.02269   0.01487  -0.1056   0.3352   1.0000
   9.000   1.5287   0.02312   0.01543  -0.1031   0.3291   1.0000
   9.250   1.5431   0.02347   0.01580  -0.1009   0.3231   1.0000
   9.500   1.5639   0.02387   0.01608  -0.0998   0.3175   1.0000
   9.750   1.5709   0.02437   0.01670  -0.0964   0.3118   1.0000
  10.000   1.5809   0.02480   0.01717  -0.0936   0.3059   1.0000
  10.250   1.5994   0.02528   0.01753  -0.0923   0.3005   1.0000
  10.500   1.6063   0.02592   0.01829  -0.0893   0.2950   1.0000
  10.750   1.6152   0.02652   0.01895  -0.0867   0.2894   1.0000
  11.000   1.6306   0.02709   0.01943  -0.0851   0.2843   1.0000
  11.250   1.6389   0.02790   0.02033  -0.0827   0.2792   1.0000
  11.500   1.6462   0.02872   0.02123  -0.0803   0.2741   1.0000
  11.750   1.6580   0.02947   0.02195  -0.0785   0.2695   1.0000
  12.000   1.6701   0.03033   0.02281  -0.0769   0.2647   1.0000
  12.250   1.6729   0.03145   0.02407  -0.0744   0.2597   1.0000
  12.500   1.6799   0.03247   0.02512  -0.0724   0.2550   1.0000
  12.750   1.6972   0.03324   0.02575  -0.0715   0.2504   1.0000
  13.000   1.6963   0.03476   0.02747  -0.0692   0.2464   1.0000
  13.250   1.7006   0.03615   0.02896  -0.0674   0.2422   1.0000
  13.500   1.7080   0.03739   0.03022  -0.0660   0.2383   1.0000
  13.750   1.7220   0.03839   0.03114  -0.0650   0.2342   1.0000
  14.000   1.7194   0.04038   0.03332  -0.0633   0.2306   1.0000
  14.250   1.7205   0.04222   0.03527  -0.0620   0.2265   1.0000
  14.500   1.7257   0.04380   0.03688  -0.0609   0.2227   1.0000
  14.750   1.7376   0.04499   0.03800  -0.0600   0.2188   1.0000
  15.000   1.7306   0.04769   0.04091  -0.0589   0.2153   1.0000
  15.250   1.7285   0.05009   0.04343  -0.0581   0.2114   1.0000
  15.500   1.7316   0.05207   0.04544  -0.0574   0.2076   1.0000
  15.750   1.7390   0.05371   0.04705  -0.0567   0.2037   1.0000
  16.000   1.7273   0.05735   0.05090  -0.0564   0.1998   1.0000
  16.250   1.7221   0.06043   0.05409  -0.0562   0.1957   1.0000
  16.500   1.7281   0.06225   0.05584  -0.0558   0.1913   1.0000
  16.750   1.7173   0.06619   0.05995  -0.0560   0.1872   1.0000
  17.000   1.7052   0.07043   0.06434  -0.0565   0.1825   1.0000
  17.250   1.7061   0.07301   0.06689  -0.0565   0.1778   1.0000
  17.500   1.6917   0.07780   0.07183  -0.0574   0.1730   1.0000
  17.750   1.6775   0.08272   0.07688  -0.0586   0.1677   1.0000
  18.000   1.6774   0.08559   0.07967  -0.0589   0.1621   1.0000
  18.250   1.6530   0.09227   0.08658  -0.0610   0.1563   1.0000
  18.500   1.6546   0.09493   0.08911  -0.0614   0.1502   1.0000
  18.750   1.6267   0.10250   0.09692  -0.0642   0.1440   1.0000
  19.000   1.6265   0.10555   0.09983  -0.0649   0.1381   1.0000
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