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GOE 647 AIRFOIL (goe647-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 647 AIRFOIL (goe647-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.34 at α=7°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe647-il-1000000-n5.txt
Download as CSV file: xf-goe647-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 647 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.7154   0.09961   0.09703  -0.0638   1.0000   0.0207
 -17.500  -0.7438   0.09144   0.08877  -0.0685   1.0000   0.0208
 -17.250  -0.7727   0.08350   0.08072  -0.0732   1.0000   0.0209
 -17.000  -0.7969   0.07662   0.07377  -0.0772   1.0000   0.0211
 -16.750  -0.8244   0.06972   0.06677  -0.0813   1.0000   0.0211
 -16.500  -0.8539   0.06299   0.05994  -0.0852   1.0000   0.0211
 -16.250  -0.8864   0.05608   0.05293  -0.0891   1.0000   0.0212
 -16.000  -0.9175   0.04955   0.04630  -0.0927   1.0000   0.0212
 -15.750  -0.9434   0.04371   0.04036  -0.0957   1.0000   0.0213
 -15.250  -0.9603   0.03080   0.02714  -0.1110   0.9967   0.0214
 -15.000  -0.9503   0.02776   0.02398  -0.1155   0.9892   0.0216
 -14.500  -0.9191   0.02486   0.02091  -0.1175   0.9745   0.0220
 -14.250  -0.8956   0.02376   0.01974  -0.1187   0.9688   0.0222
 -14.000  -0.8700   0.02274   0.01865  -0.1199   0.9609   0.0224
 -13.750  -0.8355   0.02174   0.01756  -0.1227   0.9562   0.0227
 -13.500  -0.8018   0.02093   0.01667  -0.1249   0.9487   0.0231
 -13.000  -0.7348   0.01934   0.01488  -0.1291   0.9265   0.0236
 -12.750  -0.7088   0.01873   0.01416  -0.1295   0.9110   0.0237
 -12.500  -0.6875   0.01820   0.01350  -0.1287   0.8947   0.0239
 -12.250  -0.6677   0.01774   0.01293  -0.1276   0.8804   0.0240
 -12.000  -0.6517   0.01711   0.01219  -0.1259   0.8660   0.0243
 -11.750  -0.6334   0.01662   0.01161  -0.1244   0.8529   0.0246
 -11.500  -0.6134   0.01619   0.01112  -0.1232   0.8414   0.0248
 -11.250  -0.5931   0.01579   0.01063  -0.1219   0.8304   0.0250
 -11.000  -0.5717   0.01543   0.01020  -0.1207   0.8197   0.0252
 -10.750  -0.5500   0.01508   0.00977  -0.1196   0.8098   0.0255
 -10.500  -0.5279   0.01475   0.00937  -0.1185   0.7991   0.0257
 -10.250  -0.5052   0.01443   0.00898  -0.1175   0.7893   0.0260
 -10.000  -0.4822   0.01416   0.00863  -0.1165   0.7786   0.0263
  -9.750  -0.4589   0.01385   0.00826  -0.1156   0.7682   0.0266
  -9.500  -0.4359   0.01356   0.00788  -0.1146   0.7574   0.0268
  -9.250  -0.4123   0.01328   0.00752  -0.1137   0.7454   0.0270
  -9.000  -0.3886   0.01303   0.00719  -0.1127   0.7329   0.0273
  -8.750  -0.3650   0.01280   0.00687  -0.1118   0.7177   0.0275
  -8.500  -0.3415   0.01262   0.00657  -0.1108   0.6992   0.0276
  -8.250  -0.3188   0.01240   0.00624  -0.1096   0.6772   0.0279
  -8.000  -0.2962   0.01213   0.00587  -0.1085   0.6573   0.0282
  -7.750  -0.2722   0.01191   0.00557  -0.1076   0.6433   0.0286
  -7.500  -0.2477   0.01173   0.00532  -0.1068   0.6314   0.0290
  -7.250  -0.2222   0.01154   0.00509  -0.1061   0.6214   0.0295
  -7.000  -0.1970   0.01139   0.00487  -0.1054   0.6115   0.0299
  -6.750  -0.1712   0.01122   0.00464  -0.1048   0.6024   0.0303
  -6.500  -0.1456   0.01107   0.00444  -0.1042   0.5938   0.0306
  -6.250  -0.1196   0.01092   0.00424  -0.1036   0.5844   0.0311
  -6.000  -0.0939   0.01080   0.00405  -0.1030   0.5753   0.0314
  -5.750  -0.0675   0.01067   0.00388  -0.1024   0.5665   0.0317
  -5.500  -0.0419   0.01053   0.00368  -0.1018   0.5582   0.0323
  -5.250  -0.0157   0.01037   0.00350  -0.1013   0.5496   0.0330
  -5.000   0.0101   0.01028   0.00335  -0.1006   0.5396   0.0337
  -4.750   0.0365   0.01018   0.00322  -0.1001   0.5295   0.0345
  -4.500   0.0626   0.01011   0.00309  -0.0995   0.5200   0.0354
  -4.250   0.0891   0.01004   0.00298  -0.0990   0.5099   0.0363
  -4.000   0.1150   0.00996   0.00286  -0.0984   0.4997   0.0378
  -3.750   0.1408   0.00992   0.00277  -0.0978   0.4876   0.0394
  -3.500   0.1669   0.00988   0.00268  -0.0973   0.4744   0.0413
  -3.250   0.1927   0.00983   0.00260  -0.0967   0.4632   0.0445
  -3.000   0.2183   0.00980   0.00253  -0.0960   0.4512   0.0489
  -2.750   0.2439   0.00976   0.00246  -0.0954   0.4381   0.0562
  -2.500   0.2691   0.00973   0.00242  -0.0947   0.4244   0.0669
  -2.250   0.2941   0.00970   0.00238  -0.0940   0.4110   0.0809
  -2.000   0.3193   0.00970   0.00236  -0.0933   0.3987   0.0924
  -1.750   0.3449   0.00970   0.00234  -0.0927   0.3877   0.1023
  -1.500   0.3702   0.00970   0.00232  -0.0921   0.3773   0.1130
  -1.250   0.3948   0.00968   0.00230  -0.0913   0.3660   0.1337
  -1.000   0.4191   0.00956   0.00232  -0.0905   0.3566   0.1845
  -0.750   0.4441   0.00961   0.00235  -0.0898   0.3472   0.2001
  -0.500   0.4700   0.00963   0.00238  -0.0893   0.3405   0.2116
  -0.250   0.4951   0.00966   0.00242  -0.0886   0.3336   0.2288
   0.000   0.5205   0.00969   0.00246  -0.0880   0.3281   0.2456
   0.250   0.5463   0.00972   0.00250  -0.0875   0.3230   0.2570
   0.500   0.5715   0.00976   0.00255  -0.0868   0.3177   0.2705
   0.750   0.5966   0.00983   0.00261  -0.0861   0.3125   0.2820
   1.000   0.6221   0.00986   0.00266  -0.0856   0.3087   0.2947
   1.250   0.6472   0.00991   0.00273  -0.0849   0.3041   0.3086
   1.500   0.6717   0.00998   0.00280  -0.0842   0.2995   0.3264
   1.750   0.6961   0.01002   0.00289  -0.0834   0.2956   0.3510
   2.000   0.7209   0.01003   0.00296  -0.0827   0.2930   0.3768
   2.250   0.7455   0.01007   0.00305  -0.0820   0.2900   0.4002
   2.500   0.7697   0.01012   0.00315  -0.0812   0.2868   0.4244
   2.750   0.7934   0.01019   0.00325  -0.0803   0.2835   0.4503
   3.000   0.8168   0.01028   0.00336  -0.0794   0.2800   0.4702
   3.250   0.8408   0.01034   0.00346  -0.0786   0.2778   0.4879
   3.500   0.8645   0.01039   0.00356  -0.0777   0.2753   0.5066
   3.750   0.8873   0.01044   0.00367  -0.0767   0.2725   0.5304
   4.000   0.9079   0.01046   0.00379  -0.0753   0.2694   0.5713
   4.250   0.9195   0.01019   0.00395  -0.0720   0.2665   0.7376
   4.750   1.0613   0.01039   0.00460  -0.0908   0.2595   1.0000
   5.000   1.0832   0.01053   0.00473  -0.0896   0.2574   1.0000
   5.250   1.1048   0.01069   0.00487  -0.0884   0.2551   1.0000
   5.500   1.1254   0.01086   0.00503  -0.0870   0.2527   1.0000
   5.750   1.1442   0.01104   0.00519  -0.0852   0.2502   1.0000
   6.000   1.1623   0.01123   0.00536  -0.0834   0.2477   1.0000
   6.250   1.1820   0.01139   0.00552  -0.0818   0.2462   1.0000
   6.500   1.2022   0.01155   0.00569  -0.0804   0.2448   1.0000
   6.750   1.2224   0.01172   0.00587  -0.0790   0.2432   1.0000
   7.000   1.2427   0.01191   0.00606  -0.0777   0.2412   1.0000
   7.250   1.2626   0.01212   0.00627  -0.0763   0.2389   1.0000
   7.500   1.2825   0.01235   0.00649  -0.0750   0.2369   1.0000
   7.750   1.3019   0.01261   0.00674  -0.0737   0.2346   1.0000
   8.000   1.3210   0.01289   0.00702  -0.0723   0.2323   1.0000
   8.250   1.3412   0.01314   0.00728  -0.0711   0.2309   1.0000
   8.500   1.3618   0.01338   0.00755  -0.0701   0.2299   1.0000
   8.750   1.3822   0.01363   0.00782  -0.0690   0.2286   1.0000
   9.000   1.4023   0.01391   0.00812  -0.0680   0.2272   1.0000
   9.250   1.4220   0.01420   0.00844  -0.0669   0.2258   1.0000
   9.500   1.4415   0.01453   0.00877  -0.0658   0.2241   1.0000
   9.750   1.4602   0.01489   0.00915  -0.0647   0.2224   1.0000
  10.000   1.4786   0.01528   0.00955  -0.0636   0.2206   1.0000
  10.250   1.4959   0.01573   0.01001  -0.0623   0.2183   1.0000
  10.500   1.5131   0.01620   0.01050  -0.0612   0.2163   1.0000
  10.750   1.5327   0.01657   0.01090  -0.0603   0.2149   1.0000
  11.000   1.5516   0.01698   0.01134  -0.0594   0.2126   1.0000
  11.250   1.5695   0.01745   0.01184  -0.0585   0.2106   1.0000
  11.500   1.5862   0.01800   0.01240  -0.0574   0.2080   1.0000
  11.750   1.6023   0.01859   0.01301  -0.0563   0.2059   1.0000
  12.000   1.6158   0.01935   0.01377  -0.0551   0.2020   1.0000
  12.250   1.6336   0.01988   0.01435  -0.0543   0.2001   1.0000
  12.500   1.6497   0.02053   0.01501  -0.0534   0.1960   1.0000
  12.750   1.6632   0.02134   0.01584  -0.0523   0.1923   1.0000
  13.000   1.6750   0.02229   0.01679  -0.0511   0.1886   1.0000
  13.250   1.6903   0.02303   0.01758  -0.0503   0.1867   1.0000
  13.500   1.7045   0.02386   0.01844  -0.0494   0.1834   1.0000
  13.750   1.7152   0.02494   0.01953  -0.0484   0.1787   1.0000
  14.000   1.7242   0.02617   0.02077  -0.0473   0.1744   1.0000
  14.250   1.7347   0.02733   0.02196  -0.0463   0.1688   1.0000
  14.500   1.7392   0.02898   0.02358  -0.0451   0.1617   1.0000
  14.750   1.7465   0.03045   0.02508  -0.0441   0.1559   1.0000
  15.000   1.7451   0.03267   0.02728  -0.0429   0.1458   1.0000
  15.250   1.7353   0.03574   0.03029  -0.0414   0.1320   1.0000
  15.500   1.7247   0.03900   0.03353  -0.0402   0.1206   1.0000
  15.750   1.7119   0.04266   0.03717  -0.0393   0.1101   1.0000
  16.000   1.7013   0.04622   0.04075  -0.0386   0.1029   1.0000
  16.250   1.6893   0.05006   0.04462  -0.0381   0.0958   1.0000
  16.500   1.6761   0.05416   0.04875  -0.0379   0.0887   1.0000
  16.750   1.6571   0.05903   0.05365  -0.0378   0.0817   1.0000
  17.000   1.6396   0.06390   0.05857  -0.0380   0.0763   1.0000
  17.250   1.6248   0.06856   0.06330  -0.0383   0.0716   1.0000
  17.500   1.5994   0.07466   0.06946  -0.0390   0.0657   1.0000
  17.750   1.5809   0.08007   0.07495  -0.0398   0.0617   1.0000
  18.000   1.5567   0.08629   0.08125  -0.0409   0.0574   1.0000
  18.250   1.5327   0.09267   0.08771  -0.0421   0.0535   1.0000
  18.500   1.5092   0.09911   0.09423  -0.0436   0.0502   1.0000
  18.750   1.4777   0.10674   0.10194  -0.0455   0.0447   1.0000
  19.000   1.4514   0.11381   0.10908  -0.0474   0.0404   1.0000
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