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GOE 480 AIRFOIL (goe480-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 480 AIRFOIL (goe480-il)
Reynolds number: 1,000,000
Max Cl/Cd: 127.76 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe480-il-1000000-n5.txt
Download as CSV file: xf-goe480-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 480 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
  ------ -------- --------- --------- -------- -------- --------
 -17.000  -0.4278   0.16864   0.16673  -0.0258   1.0000   0.0112
 -16.750  -0.4200   0.16609   0.16418  -0.0270   1.0000   0.0114
 -14.750  -0.9786   0.03067   0.02823  -0.1185   0.9881   0.0285
 -14.500  -0.9620   0.02746   0.02478  -0.1217   0.9840   0.0291
 -14.250  -0.9326   0.02754   0.02491  -0.1218   0.9806   0.0296
 -14.000  -0.8995   0.02808   0.02552  -0.1220   0.9773   0.0302
 -13.750  -0.8685   0.02756   0.02497  -0.1233   0.9742   0.0308
 -13.500  -0.8421   0.02607   0.02334  -0.1253   0.9695   0.0315
 -13.250  -0.8153   0.02432   0.02140  -0.1275   0.9641   0.0322
 -13.000  -0.7885   0.02260   0.01947  -0.1296   0.9576   0.0328
 -12.750  -0.7600   0.02124   0.01790  -0.1313   0.9492   0.0332
 -12.500  -0.7306   0.02059   0.01716  -0.1324   0.9381   0.0336
 -12.250  -0.6999   0.02048   0.01703  -0.1330   0.9257   0.0340
 -12.000  -0.6715   0.02039   0.01689  -0.1331   0.9114   0.0343
 -11.750  -0.6443   0.02041   0.01685  -0.1329   0.8961   0.0345
 -11.500  -0.6175   0.02054   0.01694  -0.1325   0.8799   0.0348
 -11.250  -0.5923   0.02055   0.01688  -0.1319   0.8635   0.0351
 -11.000  -0.5693   0.02027   0.01649  -0.1311   0.8480   0.0354
 -10.750  -0.5449   0.02020   0.01633  -0.1305   0.8334   0.0358
 -10.500  -0.5227   0.01973   0.01573  -0.1298   0.8194   0.0362
 -10.250  -0.5008   0.01916   0.01501  -0.1290   0.8074   0.0367
 -10.000  -0.4791   0.01852   0.01420  -0.1283   0.7959   0.0372
  -9.750  -0.4572   0.01783   0.01334  -0.1276   0.7852   0.0376
  -9.500  -0.4338   0.01733   0.01270  -0.1269   0.7760   0.0379
  -9.250  -0.4104   0.01680   0.01203  -0.1263   0.7672   0.0381
  -9.000  -0.3865   0.01629   0.01139  -0.1258   0.7599   0.0383
  -8.750  -0.3639   0.01549   0.01043  -0.1251   0.7527   0.0386
  -8.250  -0.3144   0.01462   0.00940  -0.1241   0.7403   0.0392
  -8.000  -0.2888   0.01430   0.00901  -0.1237   0.7342   0.0395
  -7.750  -0.2634   0.01400   0.00862  -0.1232   0.7283   0.0397
  -7.500  -0.2371   0.01369   0.00827  -0.1229   0.7236   0.0399
  -7.250  -0.2110   0.01340   0.00791  -0.1225   0.7181   0.0401
  -7.000  -0.1850   0.01311   0.00755  -0.1221   0.7128   0.0404
  -6.750  -0.1587   0.01282   0.00719  -0.1218   0.7083   0.0406
  -6.500  -0.1320   0.01258   0.00690  -0.1215   0.7033   0.0410
  -6.250  -0.1055   0.01232   0.00658  -0.1211   0.6983   0.0413
  -5.750  -0.0526   0.01170   0.00583  -0.1204   0.6888   0.0419
  -5.500  -0.0259   0.01142   0.00549  -0.1201   0.6838   0.0422
  -5.250   0.0006   0.01115   0.00516  -0.1197   0.6786   0.0425
  -5.000   0.0274   0.01090   0.00484  -0.1194   0.6740   0.0428
  -4.750   0.0544   0.01066   0.00456  -0.1191   0.6689   0.0431
  -4.500   0.0813   0.01044   0.00429  -0.1188   0.6632   0.0434
  -4.250   0.1080   0.01026   0.00405  -0.1184   0.6580   0.0436
  -4.000   0.1354   0.01008   0.00384  -0.1182   0.6526   0.0438
  -3.750   0.1624   0.00992   0.00364  -0.1179   0.6462   0.0440
  -3.500   0.1893   0.00979   0.00346  -0.1176   0.6404   0.0442
  -3.250   0.2166   0.00964   0.00329  -0.1173   0.6340   0.0443
  -3.000   0.2426   0.00933   0.00293  -0.1169   0.6268   0.0451
  -2.750   0.2695   0.00918   0.00276  -0.1165   0.6203   0.0456
  -2.500   0.2964   0.00906   0.00262  -0.1162   0.6121   0.0460
  -2.250   0.3232   0.00897   0.00249  -0.1158   0.6044   0.0463
  -2.000   0.3502   0.00889   0.00239  -0.1155   0.5957   0.0467
  -1.750   0.3769   0.00882   0.00229  -0.1152   0.5873   0.0471
  -1.500   0.4038   0.00877   0.00220  -0.1148   0.5782   0.0476
  -1.250   0.4305   0.00872   0.00212  -0.1144   0.5697   0.0480
  -1.000   0.4570   0.00869   0.00205  -0.1140   0.5598   0.0485
  -0.750   0.4838   0.00865   0.00198  -0.1137   0.5511   0.0490
  -0.500   0.5101   0.00865   0.00194  -0.1133   0.5415   0.0496
  -0.250   0.5369   0.00863   0.00189  -0.1129   0.5330   0.0501
   0.000   0.5632   0.00865   0.00187  -0.1125   0.5238   0.0506
   0.250   0.5900   0.00865   0.00185  -0.1121   0.5154   0.0510
   0.500   0.6161   0.00870   0.00186  -0.1117   0.5057   0.0514
   0.750   0.6425   0.00868   0.00183  -0.1113   0.4959   0.0523
   1.000   0.6685   0.00870   0.00181  -0.1108   0.4866   0.0533
   1.250   0.6947   0.00873   0.00181  -0.1104   0.4771   0.0544
   1.500   0.7209   0.00876   0.00184  -0.1100   0.4692   0.0553
   1.750   0.7472   0.00880   0.00186  -0.1096   0.4613   0.0564
   2.000   0.7731   0.00886   0.00190  -0.1091   0.4534   0.0576
   2.250   0.7994   0.00891   0.00194  -0.1087   0.4454   0.0587
   2.500   0.8250   0.00899   0.00200  -0.1082   0.4373   0.0599
   2.750   0.8513   0.00904   0.00206  -0.1078   0.4303   0.0624
   3.250   0.9022   0.00915   0.00221  -0.1068   0.4144   0.0886
   3.500   0.9264   0.00914   0.00235  -0.1061   0.4057   0.1749
   3.750   0.9517   0.00917   0.00245  -0.1056   0.3987   0.2100
   4.000   0.9747   0.00901   0.00263  -0.1048   0.3910   0.3768
   4.250   0.9943   0.00860   0.00284  -0.1033   0.3847   0.6526
   4.750   1.0783   0.00844   0.00328  -0.1098   0.3598   1.0000
   5.000   1.1009   0.00865   0.00343  -0.1088   0.3478   1.0000
   5.250   1.1232   0.00888   0.00360  -0.1077   0.3369   1.0000
   5.500   1.1464   0.00905   0.00375  -0.1068   0.3286   1.0000
   5.750   1.1687   0.00927   0.00392  -0.1057   0.3198   1.0000
   6.000   1.1909   0.00949   0.00410  -0.1046   0.3099   1.0000
   6.250   1.2126   0.00972   0.00430  -0.1035   0.2996   1.0000
   6.500   1.2334   0.01000   0.00452  -0.1022   0.2889   1.0000
   6.750   1.2549   0.01023   0.00472  -0.1010   0.2796   1.0000
   7.000   1.2755   0.01049   0.00495  -0.0997   0.2707   1.0000
   7.500   1.3134   0.01113   0.00548  -0.0965   0.2464   1.0000
   7.750   1.3288   0.01150   0.00579  -0.0942   0.2320   1.0000
   8.000   1.3437   0.01186   0.00609  -0.0918   0.2197   1.0000
   8.250   1.3578   0.01227   0.00644  -0.0894   0.2067   1.0000
   8.500   1.3719   0.01271   0.00681  -0.0870   0.1938   1.0000
   8.750   1.3849   0.01321   0.00724  -0.0846   0.1785   1.0000
   9.000   1.3973   0.01376   0.00771  -0.0821   0.1627   1.0000
   9.250   1.4066   0.01447   0.00831  -0.0792   0.1421   1.0000
   9.500   1.4114   0.01543   0.00912  -0.0758   0.1158   1.0000
   9.750   1.4126   0.01664   0.01016  -0.0721   0.0882   1.0000
  10.000   1.4204   0.01758   0.01103  -0.0695   0.0749   1.0000
  10.250   1.4307   0.01843   0.01185  -0.0674   0.0663   1.0000
  10.500   1.4436   0.01917   0.01260  -0.0657   0.0617   1.0000
  10.750   1.4545   0.02007   0.01348  -0.0639   0.0566   1.0000
  11.000   1.4680   0.02084   0.01428  -0.0624   0.0536   1.0000
  11.250   1.4793   0.02179   0.01523  -0.0608   0.0493   1.0000
  11.500   1.4912   0.02273   0.01619  -0.0594   0.0463   1.0000
  11.750   1.5025   0.02375   0.01722  -0.0580   0.0422   1.0000
  12.000   1.5124   0.02492   0.01839  -0.0566   0.0384   1.0000
  12.250   1.5205   0.02624   0.01971  -0.0552   0.0337   1.0000
  12.500   1.5293   0.02757   0.02105  -0.0539   0.0303   1.0000
  13.000   1.5459   0.03039   0.02392  -0.0515   0.0259   1.0000
  13.250   1.5528   0.03197   0.02552  -0.0504   0.0241   1.0000
  13.500   1.5593   0.03362   0.02721  -0.0493   0.0225   1.0000
  13.750   1.5665   0.03523   0.02887  -0.0483   0.0215   1.0000
  14.000   1.5717   0.03706   0.03074  -0.0473   0.0203   1.0000
  14.250   1.5760   0.03902   0.03275  -0.0464   0.0192   1.0000
  14.500   1.5816   0.04091   0.03469  -0.0456   0.0185   1.0000
  14.750   1.5858   0.04295   0.03679  -0.0449   0.0177   1.0000
  15.000   1.5888   0.04516   0.03905  -0.0442   0.0170   1.0000
  15.250   1.5908   0.04753   0.04148  -0.0436   0.0163   1.0000
  15.500   1.5925   0.05000   0.04400  -0.0430   0.0157   1.0000
  15.750   1.5947   0.05244   0.04651  -0.0426   0.0152   1.0000
  16.000   1.5958   0.05504   0.04919  -0.0422   0.0149   1.0000
  16.250   1.5958   0.05783   0.05204  -0.0419   0.0143   1.0000
  16.500   1.5949   0.06078   0.05505  -0.0418   0.0139   1.0000
  16.750   1.5924   0.06394   0.05827  -0.0416   0.0132   1.0000
  17.000   1.5896   0.06719   0.06160  -0.0416   0.0130   1.0000
  17.250   1.5876   0.07042   0.06490  -0.0417   0.0127   1.0000
  17.500   1.5851   0.07373   0.06830  -0.0419   0.0125   1.0000
  17.750   1.5816   0.07722   0.07187  -0.0421   0.0121   1.0000
  18.000   1.5774   0.08080   0.07553  -0.0424   0.0119   1.0000
  18.250   1.5726   0.08452   0.07933  -0.0429   0.0117   1.0000
  18.500   1.5663   0.08854   0.08343  -0.0435   0.0114   1.0000
  18.750   1.5597   0.09266   0.08762  -0.0442   0.0111   1.0000
  19.000   1.5525   0.09687   0.09191  -0.0451   0.0109   1.0000
  19.250   1.5456   0.10114   0.09625  -0.0461   0.0107   1.0000
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