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GOE 797 AIRFOIL (goe797-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 797 AIRFOIL (goe797-il)
Reynolds number: 1,000,000
Max Cl/Cd: 106.55 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe797-il-1000000-n5.txt
Download as CSV file: xf-goe797-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 797 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
  ------ -------- --------- --------- -------- -------- --------
 -17.250  -0.7973   0.09378   0.09110  -0.0765   1.0000   0.0269
 -17.000  -0.8665   0.07999   0.07714  -0.0852   1.0000   0.0270
 -16.750  -1.0933   0.04117   0.03770  -0.1135   1.0000   0.0265
 -16.500  -1.1080   0.03317   0.02944  -0.1236   0.9907   0.0266
 -16.250  -1.1045   0.03009   0.02621  -0.1265   0.9815   0.0267
 -16.000  -1.0999   0.02811   0.02410  -0.1269   0.9714   0.0269
 -15.750  -1.0957   0.02667   0.02255  -0.1256   0.9614   0.0270
 -15.500  -1.0908   0.02558   0.02135  -0.1236   0.9527   0.0272
 -15.250  -1.0793   0.02462   0.02029  -0.1222   0.9458   0.0274
 -15.000  -1.0645   0.02375   0.01932  -0.1212   0.9397   0.0275
 -14.750  -1.0480   0.02298   0.01845  -0.1202   0.9333   0.0277
 -14.500  -1.0297   0.02228   0.01766  -0.1194   0.9278   0.0278
 -14.250  -1.0125   0.02142   0.01672  -0.1185   0.9217   0.0282
 -14.000  -0.9941   0.02065   0.01586  -0.1177   0.9162   0.0285
 -13.750  -0.9735   0.01997   0.01511  -0.1171   0.9111   0.0288
 -13.500  -0.9520   0.01935   0.01443  -0.1165   0.9053   0.0291
 -13.250  -0.9299   0.01879   0.01380  -0.1160   0.8994   0.0294
 -13.000  -0.9067   0.01826   0.01321  -0.1156   0.8939   0.0297
 -12.750  -0.8831   0.01777   0.01265  -0.1152   0.8877   0.0300
 -12.500  -0.8592   0.01731   0.01211  -0.1148   0.8818   0.0303
 -12.250  -0.8345   0.01686   0.01160  -0.1146   0.8756   0.0306
 -12.000  -0.8097   0.01644   0.01110  -0.1143   0.8680   0.0309
 -11.750  -0.7845   0.01604   0.01063  -0.1140   0.8607   0.0313
 -11.500  -0.7590   0.01567   0.01018  -0.1138   0.8518   0.0316
 -11.250  -0.7331   0.01533   0.00976  -0.1136   0.8436   0.0319
 -11.000  -0.7076   0.01493   0.00928  -0.1133   0.8335   0.0323
 -10.750  -0.6820   0.01454   0.00883  -0.1131   0.8229   0.0329
 -10.500  -0.6560   0.01421   0.00842  -0.1129   0.8105   0.0334
 -10.000  -0.6031   0.01365   0.00770  -0.1126   0.7840   0.0344
  -9.750  -0.5762   0.01340   0.00738  -0.1125   0.7731   0.0350
  -9.250  -0.5217   0.01294   0.00676  -0.1124   0.7541   0.0360
  -8.750  -0.4669   0.01246   0.00616  -0.1123   0.7383   0.0373
  -8.500  -0.4393   0.01223   0.00588  -0.1124   0.7311   0.0381
  -8.250  -0.4114   0.01202   0.00564  -0.1124   0.7255   0.0390
  -8.000  -0.3831   0.01182   0.00540  -0.1125   0.7204   0.0400
  -7.750  -0.3549   0.01164   0.00519  -0.1126   0.7153   0.0409
  -7.250  -0.2982   0.01126   0.00473  -0.1128   0.7062   0.0429
  -7.000  -0.2697   0.01107   0.00453  -0.1130   0.7016   0.0442
  -6.750  -0.2412   0.01091   0.00435  -0.1131   0.6972   0.0455
  -6.500  -0.2126   0.01078   0.00417  -0.1133   0.6932   0.0467
  -6.250  -0.1836   0.01063   0.00400  -0.1135   0.6900   0.0478
  -6.000  -0.1548   0.01045   0.00382  -0.1137   0.6864   0.0495
  -5.750  -0.1260   0.01030   0.00366  -0.1139   0.6824   0.0514
  -5.500  -0.0971   0.01018   0.00352  -0.1140   0.6785   0.0532
  -5.000  -0.0393   0.00991   0.00324  -0.1145   0.6712   0.0576
  -4.750  -0.0102   0.00979   0.00311  -0.1147   0.6661   0.0601
  -4.500   0.0187   0.00970   0.00299  -0.1149   0.6610   0.0622
  -4.250   0.0474   0.00959   0.00288  -0.1150   0.6566   0.0660
  -4.000   0.0767   0.00948   0.00278  -0.1153   0.6531   0.0700
  -3.750   0.1058   0.00937   0.00268  -0.1156   0.6483   0.0749
  -3.500   0.1347   0.00928   0.00260  -0.1158   0.6433   0.0803
  -3.250   0.1637   0.00922   0.00253  -0.1160   0.6395   0.0854
  -3.000   0.1930   0.00912   0.00247  -0.1163   0.6360   0.0922
  -2.750   0.2223   0.00906   0.00241  -0.1165   0.6311   0.0966
  -2.500   0.2513   0.00900   0.00236  -0.1167   0.6257   0.1032
  -2.250   0.2802   0.00897   0.00232  -0.1169   0.6208   0.1086
  -2.000   0.3096   0.00893   0.00228  -0.1172   0.6155   0.1121
  -1.750   0.3386   0.00889   0.00225  -0.1174   0.6095   0.1174
  -1.500   0.3673   0.00888   0.00222  -0.1176   0.6039   0.1224
  -1.250   0.3967   0.00885   0.00220  -0.1179   0.5993   0.1264
  -1.000   0.4259   0.00884   0.00218  -0.1181   0.5946   0.1294
  -0.750   0.4546   0.00882   0.00216  -0.1183   0.5895   0.1347
  -0.500   0.4836   0.00880   0.00215  -0.1186   0.5846   0.1394
  -0.250   0.5126   0.00880   0.00215  -0.1188   0.5784   0.1439
   0.000   0.5411   0.00881   0.00215  -0.1189   0.5721   0.1504
   0.250   0.5700   0.00879   0.00215  -0.1192   0.5668   0.1566
   0.750   0.6269   0.00882   0.00218  -0.1194   0.5536   0.1697
   1.000   0.6556   0.00882   0.00220  -0.1196   0.5465   0.1789
   1.250   0.6833   0.00883   0.00224  -0.1197   0.5381   0.1982
   1.500   0.7114   0.00879   0.00228  -0.1198   0.5294   0.2322
   1.750   0.7387   0.00880   0.00235  -0.1198   0.5193   0.2687
   2.250   0.7927   0.00883   0.00250  -0.1197   0.4934   0.3466
   2.500   0.8183   0.00881   0.00262  -0.1195   0.4763   0.4307
   2.750   0.8431   0.00878   0.00278  -0.1192   0.4571   0.5335
   3.000   0.8668   0.00883   0.00297  -0.1186   0.4340   0.6281
   3.250   0.8896   0.00893   0.00318  -0.1178   0.4097   0.7181
   3.500   0.9107   0.00901   0.00343  -0.1165   0.3879   0.8165
   3.750   0.9280   0.00904   0.00367  -0.1141   0.3723   0.9207
   4.000   0.9576   0.00923   0.00385  -0.1145   0.3589   0.9880
   4.250   0.9866   0.00945   0.00401  -0.1150   0.3490   1.0000
   4.500   1.0103   0.00968   0.00418  -0.1143   0.3399   1.0000
   4.750   1.0348   0.00987   0.00434  -0.1138   0.3334   1.0000
   5.000   1.0592   0.01006   0.00450  -0.1132   0.3276   1.0000
   5.250   1.0831   0.01027   0.00468  -0.1126   0.3227   1.0000
   5.500   1.1074   0.01045   0.00484  -0.1120   0.3190   1.0000
   5.750   1.1316   0.01062   0.00501  -0.1114   0.3150   1.0000
   6.000   1.1542   0.01085   0.00521  -0.1106   0.3092   1.0000
   6.250   1.1753   0.01111   0.00543  -0.1094   0.3033   1.0000
   6.500   1.1976   0.01129   0.00562  -0.1084   0.3006   1.0000
   6.750   1.2192   0.01149   0.00583  -0.1074   0.2975   1.0000
   7.000   1.2405   0.01172   0.00606  -0.1063   0.2941   1.0000
   7.250   1.2607   0.01202   0.00634  -0.1050   0.2895   1.0000
   7.500   1.2817   0.01229   0.00661  -0.1040   0.2851   1.0000
   7.750   1.3034   0.01255   0.00687  -0.1030   0.2806   1.0000
   8.000   1.3241   0.01285   0.00717  -0.1020   0.2761   1.0000
   8.250   1.3437   0.01321   0.00752  -0.1007   0.2716   1.0000
   8.500   1.3649   0.01351   0.00783  -0.0998   0.2672   1.0000
   8.750   1.3848   0.01388   0.00819  -0.0987   0.2609   1.0000
   9.000   1.4030   0.01433   0.00862  -0.0974   0.2542   1.0000
   9.250   1.4218   0.01476   0.00904  -0.0962   0.2454   1.0000
   9.500   1.4375   0.01536   0.00958  -0.0946   0.2328   1.0000
   9.750   1.4480   0.01625   0.01035  -0.0923   0.2116   1.0000
  10.000   1.4533   0.01744   0.01139  -0.0893   0.1860   1.0000
  10.500   1.4722   0.01953   0.01334  -0.0849   0.1592   1.0000
  10.750   1.4847   0.02043   0.01422  -0.0833   0.1519   1.0000
  11.000   1.4982   0.02131   0.01509  -0.0818   0.1458   1.0000
  11.250   1.5112   0.02224   0.01602  -0.0803   0.1404   1.0000
  11.500   1.5263   0.02305   0.01685  -0.0792   0.1367   1.0000
  11.750   1.5396   0.02399   0.01780  -0.0778   0.1320   1.0000
  12.000   1.5506   0.02511   0.01891  -0.0764   0.1265   1.0000
  12.250   1.5644   0.02606   0.01988  -0.0752   0.1223   1.0000
  12.500   1.5756   0.02722   0.02103  -0.0739   0.1170   1.0000
  12.750   1.5859   0.02847   0.02228  -0.0726   0.1121   1.0000
  13.000   1.5989   0.02955   0.02339  -0.0715   0.1090   1.0000
  13.250   1.6094   0.03084   0.02470  -0.0704   0.1044   1.0000
  13.500   1.6173   0.03238   0.02623  -0.0690   0.0988   1.0000
  13.750   1.6271   0.03379   0.02765  -0.0679   0.0940   1.0000
  14.000   1.6331   0.03555   0.02939  -0.0666   0.0877   1.0000
  14.250   1.6401   0.03725   0.03111  -0.0655   0.0828   1.0000
  14.500   1.6469   0.03899   0.03286  -0.0644   0.0782   1.0000
  14.750   1.6508   0.04103   0.03489  -0.0632   0.0731   1.0000
  15.000   1.6565   0.04296   0.03685  -0.0622   0.0688   1.0000
  15.250   1.6574   0.04534   0.03921  -0.0610   0.0634   1.0000
  15.500   1.6596   0.04763   0.04152  -0.0600   0.0582   1.0000
  15.750   1.6594   0.05023   0.04412  -0.0589   0.0535   1.0000
  16.000   1.6589   0.05290   0.04681  -0.0580   0.0489   1.0000
  16.250   1.6590   0.05554   0.04947  -0.0571   0.0444   1.0000
  16.500   1.6561   0.05855   0.05249  -0.0563   0.0398   1.0000
  16.750   1.6514   0.06183   0.05579  -0.0555   0.0346   1.0000
  17.000   1.6442   0.06545   0.05942  -0.0549   0.0288   1.0000
  17.250   1.6356   0.06933   0.06332  -0.0543   0.0236   1.0000
  17.500   1.6288   0.07303   0.06706  -0.0539   0.0204   1.0000
  17.750   1.6240   0.07659   0.07067  -0.0537   0.0184   1.0000
  18.000   1.6196   0.08017   0.07432  -0.0536   0.0172   1.0000
  18.250   1.6158   0.08374   0.07796  -0.0536   0.0163   1.0000
  18.500   1.6110   0.08745   0.08173  -0.0537   0.0155   1.0000
  18.750   1.6068   0.09110   0.08545  -0.0539   0.0148   1.0000
  19.000   1.6027   0.09481   0.08924  -0.0543   0.0144   1.0000
  19.250   1.5977   0.09870   0.09320  -0.0548   0.0139   1.0000
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