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GOE 646 AIRFOIL (goe646-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 646 AIRFOIL (goe646-il)
Reynolds number: 200,000
Max Cl/Cd: 65.24 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe646-il-200000-n5.txt
Download as CSV file: xf-goe646-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 646 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.6813   0.09503   0.08985  -0.0789   1.0000   0.0500
 -16.500  -0.7139   0.08682   0.08144  -0.0831   1.0000   0.0506
 -16.250  -0.7232   0.08275   0.07732  -0.0846   1.0000   0.0511
 -16.000  -0.7265   0.07978   0.07435  -0.0853   1.0000   0.0516
 -15.750  -0.7338   0.07632   0.07087  -0.0863   1.0000   0.0522
 -15.500  -0.7430   0.07278   0.06728  -0.0873   1.0000   0.0527
 -15.250  -0.7542   0.06919   0.06365  -0.0881   1.0000   0.0533
 -15.000  -0.7668   0.06582   0.06022  -0.0886   1.0000   0.0538
 -14.750  -0.7806   0.06268   0.05703  -0.0885   1.0000   0.0544
 -14.500  -0.7964   0.05972   0.05402  -0.0880   1.0000   0.0548
 -14.250  -0.7947   0.05602   0.05020  -0.0914   0.9978   0.0557
 -14.000  -0.7866   0.05251   0.04660  -0.0955   0.9942   0.0567
 -13.750  -0.7775   0.04934   0.04340  -0.0992   0.9901   0.0576
 -13.500  -0.7687   0.04615   0.04015  -0.1030   0.9852   0.0586
 -13.250  -0.7571   0.04307   0.03697  -0.1072   0.9811   0.0599
 -13.000  -0.7505   0.04021   0.03400  -0.1100   0.9745   0.0612
 -12.750  -0.7384   0.03745   0.03112  -0.1136   0.9692   0.0627
 -12.500  -0.7300   0.03492   0.02855  -0.1163   0.9615   0.0639
 -12.250  -0.7146   0.03250   0.02605  -0.1199   0.9552   0.0655
 -12.000  -0.7044   0.03038   0.02380  -0.1220   0.9455   0.0672
 -11.750  -0.6850   0.02860   0.02187  -0.1245   0.9393   0.0692
 -11.500  -0.6755   0.02729   0.02052  -0.1240   0.9299   0.0706
 -11.250  -0.6522   0.02608   0.01923  -0.1254   0.9250   0.0730
 -11.000  -0.6224   0.02502   0.01802  -0.1274   0.9221   0.0762
 -10.750  -0.6078   0.02414   0.01713  -0.1266   0.9143   0.0782
 -10.500  -0.5820   0.02328   0.01621  -0.1276   0.9096   0.0812
 -10.250  -0.5513   0.02248   0.01529  -0.1292   0.9062   0.0846
 -10.000  -0.5231   0.02164   0.01444  -0.1304   0.9023   0.0877
  -9.750  -0.5057   0.02112   0.01385  -0.1291   0.8947   0.0907
  -9.500  -0.4781   0.02047   0.01313  -0.1298   0.8898   0.0942
  -9.250  -0.4460   0.01978   0.01242  -0.1314   0.8861   0.0984
  -9.000  -0.4244   0.01936   0.01192  -0.1306   0.8797   0.1023
  -8.750  -0.4030   0.01885   0.01141  -0.1299   0.8731   0.1061
  -8.500  -0.3733   0.01837   0.01086  -0.1306   0.8682   0.1112
  -8.250  -0.3443   0.01787   0.01035  -0.1313   0.8633   0.1166
  -8.000  -0.3261   0.01756   0.01000  -0.1296   0.8551   0.1221
  -7.750  -0.2990   0.01713   0.00956  -0.1297   0.8490   0.1289
  -7.500  -0.2677   0.01673   0.00911  -0.1306   0.8442   0.1374
  -7.250  -0.2502   0.01645   0.00885  -0.1287   0.8358   0.1451
  -7.000  -0.2238   0.01611   0.00850  -0.1286   0.8293   0.1541
  -6.750  -0.1937   0.01580   0.00813  -0.1290   0.8237   0.1638
  -6.500  -0.1743   0.01556   0.00791  -0.1274   0.8146   0.1724
  -6.250  -0.1459   0.01528   0.00759  -0.1275   0.8076   0.1819
  -6.000  -0.1214   0.01508   0.00735  -0.1268   0.7994   0.1915
  -5.750  -0.0964   0.01486   0.00714  -0.1262   0.7908   0.2007
  -5.500  -0.0681   0.01467   0.00689  -0.1262   0.7835   0.2103
  -5.250  -0.0450   0.01452   0.00675  -0.1252   0.7740   0.2190
  -5.000  -0.0156   0.01436   0.00651  -0.1253   0.7664   0.2283
  -4.750   0.0071   0.01425   0.00640  -0.1242   0.7560   0.2370
  -4.500   0.0359   0.01413   0.00619  -0.1242   0.7473   0.2455
  -4.250   0.0593   0.01404   0.00609  -0.1231   0.7361   0.2536
  -4.000   0.0868   0.01395   0.00591  -0.1229   0.7264   0.2619
  -3.750   0.1115   0.01388   0.00583  -0.1221   0.7156   0.2695
  -3.500   0.1387   0.01383   0.00568  -0.1218   0.7063   0.2779
  -3.250   0.1639   0.01378   0.00562  -0.1211   0.6963   0.2861
  -3.000   0.1908   0.01378   0.00553  -0.1207   0.6875   0.2960
  -2.750   0.2161   0.01375   0.00549  -0.1201   0.6783   0.3040
  -2.500   0.2431   0.01375   0.00541  -0.1197   0.6702   0.3119
  -2.250   0.2685   0.01375   0.00534  -0.1191   0.6613   0.3185
  -2.000   0.2950   0.01373   0.00529  -0.1187   0.6538   0.3243
  -1.750   0.3208   0.01374   0.00527  -0.1181   0.6468   0.3311
  -1.500   0.3470   0.01378   0.00523  -0.1176   0.6399   0.3377
  -1.000   0.3981   0.01380   0.00522  -0.1164   0.6254   0.3502
  -0.750   0.4236   0.01386   0.00518  -0.1158   0.6174   0.3572
  -0.500   0.4489   0.01388   0.00520  -0.1152   0.6103   0.3634
  -0.250   0.4730   0.01390   0.00523  -0.1143   0.6028   0.3704
   0.000   0.4987   0.01398   0.00522  -0.1137   0.5957   0.3778
   0.250   0.5230   0.01400   0.00527  -0.1129   0.5892   0.3848
   0.500   0.5472   0.01403   0.00532  -0.1121   0.5829   0.3926
   0.750   0.5727   0.01410   0.00535  -0.1115   0.5774   0.4005
   1.000   0.5983   0.01415   0.00541  -0.1110   0.5724   0.4085
   1.250   0.6220   0.01419   0.00550  -0.1101   0.5671   0.4172
   1.500   0.6461   0.01423   0.00558  -0.1093   0.5618   0.4259
   1.750   0.6709   0.01429   0.00565  -0.1086   0.5566   0.4364
   2.000   0.6953   0.01435   0.00574  -0.1078   0.5515   0.4472
   2.250   0.7175   0.01440   0.00587  -0.1066   0.5457   0.4593
   2.500   0.7406   0.01445   0.00599  -0.1056   0.5403   0.4733
   2.750   0.7646   0.01452   0.00610  -0.1048   0.5353   0.4909
   3.000   0.7864   0.01458   0.00626  -0.1035   0.5298   0.5119
   3.250   0.8070   0.01463   0.00643  -0.1020   0.5235   0.5362
   3.500   0.8285   0.01471   0.00657  -0.1007   0.5176   0.5633
   3.750   0.8498   0.01480   0.00674  -0.0993   0.5120   0.5927
   4.000   0.8680   0.01487   0.00693  -0.0973   0.5055   0.6204
   4.250   0.8866   0.01495   0.00706  -0.0954   0.4986   0.6464
   4.500   0.9039   0.01505   0.00720  -0.0932   0.4909   0.6698
   4.750   0.9188   0.01515   0.00737  -0.0907   0.4814   0.6917
   5.000   0.9343   0.01526   0.00754  -0.0882   0.4724   0.7163
   5.250   0.9499   0.01537   0.00776  -0.0858   0.4617   0.7466
   5.500   0.9698   0.01544   0.00801  -0.0842   0.4522   0.8023
   5.750   1.0165   0.01558   0.00832  -0.0884   0.4398   1.0000
   6.000   1.0331   0.01585   0.00858  -0.0864   0.4293   1.0000
   6.250   1.0478   0.01617   0.00883  -0.0842   0.4186   1.0000
   6.500   1.0621   0.01652   0.00913  -0.0819   0.4062   1.0000
   6.750   1.0761   0.01691   0.00947  -0.0796   0.3940   1.0000
   7.000   1.0886   0.01737   0.00986  -0.0772   0.3819   1.0000
   7.250   1.1009   0.01787   0.01029  -0.0748   0.3704   1.0000
   7.500   1.1144   0.01838   0.01075  -0.0727   0.3602   1.0000
   7.750   1.1263   0.01898   0.01128  -0.0704   0.3510   1.0000
   8.000   1.1407   0.01953   0.01180  -0.0686   0.3425   1.0000
   8.250   1.1527   0.02018   0.01240  -0.0665   0.3341   1.0000
   8.500   1.1661   0.02082   0.01301  -0.0646   0.3259   1.0000
   8.750   1.1783   0.02153   0.01368  -0.0627   0.3179   1.0000
   9.000   1.1907   0.02225   0.01438  -0.0608   0.3104   1.0000
   9.250   1.2031   0.02300   0.01511  -0.0591   0.3022   1.0000
   9.500   1.2137   0.02386   0.01591  -0.0571   0.2954   1.0000
   9.750   1.2276   0.02458   0.01668  -0.0557   0.2881   1.0000
  10.000   1.2383   0.02548   0.01756  -0.0539   0.2811   1.0000
  10.250   1.2504   0.02635   0.01843  -0.0524   0.2748   1.0000
  10.500   1.2634   0.02718   0.01930  -0.0510   0.2689   1.0000
  10.750   1.2739   0.02817   0.02029  -0.0495   0.2630   1.0000
  11.000   1.2855   0.02914   0.02127  -0.0481   0.2578   1.0000
  11.250   1.2974   0.03011   0.02229  -0.0468   0.2517   1.0000
  11.500   1.3058   0.03130   0.02348  -0.0453   0.2455   1.0000
  11.750   1.3161   0.03243   0.02464  -0.0440   0.2397   1.0000
  12.000   1.3260   0.03361   0.02587  -0.0428   0.2338   1.0000
  12.250   1.3332   0.03501   0.02726  -0.0415   0.2283   1.0000
  12.500   1.3427   0.03629   0.02861  -0.0404   0.2225   1.0000
  12.750   1.3505   0.03774   0.03010  -0.0393   0.2165   1.0000
  13.250   1.3646   0.04089   0.03331  -0.0373   0.2053   1.0000
  13.500   1.3700   0.04267   0.03511  -0.0363   0.1994   1.0000
  13.750   1.3749   0.04453   0.03699  -0.0355   0.1940   1.0000
  14.000   1.3814   0.04633   0.03885  -0.0348   0.1884   1.0000
  14.250   1.3847   0.04844   0.04098  -0.0341   0.1832   1.0000
  14.500   1.3897   0.05043   0.04303  -0.0335   0.1783   1.0000
  14.750   1.3943   0.05252   0.04517  -0.0329   0.1731   1.0000
  15.000   1.3953   0.05498   0.04765  -0.0324   0.1681   1.0000
  15.250   1.3995   0.05719   0.04993  -0.0321   0.1630   1.0000
  15.500   1.4010   0.05973   0.05252  -0.0318   0.1573   1.0000
  15.750   1.4005   0.06249   0.05530  -0.0315   0.1522   1.0000
  16.000   1.4023   0.06508   0.05797  -0.0314   0.1460   1.0000
  16.250   1.3982   0.06837   0.06126  -0.0314   0.1402   1.0000
  16.500   1.3996   0.07110   0.06409  -0.0314   0.1335   1.0000
  16.750   1.3952   0.07455   0.06757  -0.0316   0.1271   1.0000
  17.000   1.3928   0.07782   0.07091  -0.0318   0.1200   1.0000
  17.250   1.3877   0.08146   0.07459  -0.0322   0.1134   1.0000
  17.500   1.3808   0.08542   0.07857  -0.0328   0.1070   1.0000
  17.750   1.3744   0.08936   0.08256  -0.0334   0.1018   1.0000
  18.000   1.3664   0.09357   0.08680  -0.0343   0.0975   1.0000
  18.250   1.3597   0.09766   0.09093  -0.0351   0.0941   1.0000
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