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GOE 797 AIRFOIL (goe797-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 797 AIRFOIL (goe797-il)
Reynolds number: 1,000,000
Max Cl/Cd: 128.68 at α=3.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe797-il-1000000.txt
Download as CSV file: xf-goe797-il-1000000.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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.7316   0.10747   0.10509  -0.0683   1.0000   0.0298
 -17.250  -0.8013   0.09197   0.08940  -0.0777   1.0000   0.0301
 -17.000  -0.8542   0.08035   0.07762  -0.0851   1.0000   0.0302
 -16.750  -0.9104   0.06857   0.06568  -0.0928   1.0000   0.0302
 -16.500  -0.9616   0.05747   0.05440  -0.1003   1.0000   0.0302
 -16.250  -1.0017   0.04723   0.04397  -0.1082   1.0000   0.0302
 -16.000  -1.0314   0.03947   0.03604  -0.1144   1.0000   0.0302
 -15.750  -1.0526   0.03481   0.03123  -0.1171   0.9987   0.0303
 -15.500  -1.0427   0.03166   0.02797  -0.1213   0.9956   0.0306
 -15.250  -1.0280   0.02950   0.02571  -0.1240   0.9934   0.0308
 -15.000  -1.0135   0.02789   0.02401  -0.1251   0.9898   0.0311
 -14.750  -0.9973   0.02658   0.02262  -0.1255   0.9853   0.0313
 -14.500  -0.9778   0.02543   0.02139  -0.1260   0.9818   0.0316
 -14.250  -0.9620   0.02448   0.02035  -0.1254   0.9757   0.0320
 -14.000  -0.9447   0.02358   0.01937  -0.1247   0.9703   0.0323
 -13.750  -0.9270   0.02282   0.01851  -0.1239   0.9650   0.0326
 -13.500  -0.9093   0.02213   0.01773  -0.1228   0.9589   0.0329
 -13.250  -0.8901   0.02152   0.01703  -0.1218   0.9537   0.0332
 -13.000  -0.8700   0.02095   0.01637  -0.1210   0.9480   0.0334
 -12.750  -0.8543   0.01991   0.01522  -0.1197   0.9419   0.0338
 -12.500  -0.8363   0.01903   0.01427  -0.1186   0.9366   0.0343
 -12.250  -0.8147   0.01840   0.01360  -0.1180   0.9312   0.0347
 -12.000  -0.7922   0.01788   0.01303  -0.1173   0.9255   0.0351
 -11.750  -0.7689   0.01742   0.01250  -0.1168   0.9201   0.0356
 -11.500  -0.7447   0.01695   0.01198  -0.1164   0.9143   0.0360
 -11.250  -0.7204   0.01651   0.01147  -0.1159   0.9083   0.0365
 -11.000  -0.6956   0.01611   0.01099  -0.1155   0.9027   0.0371
 -10.750  -0.6697   0.01574   0.01056  -0.1153   0.8964   0.0375
 -10.500  -0.6438   0.01544   0.01017  -0.1150   0.8897   0.0379
 -10.250  -0.6206   0.01472   0.00938  -0.1145   0.8828   0.0387
 -10.000  -0.5953   0.01425   0.00888  -0.1142   0.8748   0.0394
  -9.750  -0.5691   0.01391   0.00848  -0.1140   0.8672   0.0401
  -9.500  -0.5423   0.01360   0.00812  -0.1139   0.8583   0.0408
  -9.250  -0.5156   0.01331   0.00776  -0.1137   0.8495   0.0415
  -9.000  -0.4884   0.01304   0.00742  -0.1136   0.8391   0.0422
  -8.750  -0.4610   0.01282   0.00712  -0.1135   0.8284   0.0428
  -8.500  -0.4354   0.01237   0.00658  -0.1132   0.8164   0.0440
  -8.250  -0.4082   0.01209   0.00627  -0.1132   0.8041   0.0451
  -8.000  -0.3805   0.01190   0.00601  -0.1131   0.7931   0.0462
  -7.500  -0.3247   0.01157   0.00553  -0.1131   0.7732   0.0482
  -7.000  -0.2696   0.01103   0.00491  -0.1131   0.7569   0.0515
  -6.750  -0.2414   0.01089   0.00470  -0.1132   0.7495   0.0530
  -6.500  -0.2127   0.01077   0.00453  -0.1133   0.7435   0.0542
  -6.250  -0.1847   0.01049   0.00424  -0.1134   0.7379   0.0567
  -6.000  -0.1563   0.01035   0.00407  -0.1135   0.7324   0.0589
  -5.750  -0.1275   0.01026   0.00393  -0.1137   0.7272   0.0607
  -5.500  -0.0989   0.01002   0.00370  -0.1138   0.7227   0.0639
  -5.250  -0.0700   0.00989   0.00356  -0.1140   0.7180   0.0667
  -5.000  -0.0414   0.00977   0.00340  -0.1142   0.7132   0.0699
  -4.750  -0.0126   0.00963   0.00327  -0.1144   0.7083   0.0739
  -4.500   0.0165   0.00950   0.00314  -0.1146   0.7036   0.0783
  -4.250   0.0454   0.00939   0.00304  -0.1148   0.6985   0.0835
  -4.000   0.0741   0.00931   0.00294  -0.1149   0.6935   0.0892
  -3.750   0.1034   0.00923   0.00287  -0.1152   0.6898   0.0947
  -3.500   0.1327   0.00911   0.00280  -0.1155   0.6858   0.1015
  -3.250   0.1620   0.00907   0.00274  -0.1157   0.6811   0.1064
  -3.000   0.1908   0.00901   0.00269  -0.1159   0.6764   0.1130
  -2.750   0.2202   0.00899   0.00265  -0.1162   0.6726   0.1177
  -2.500   0.2496   0.00889   0.00259  -0.1165   0.6689   0.1233
  -2.250   0.2789   0.00884   0.00255  -0.1167   0.6644   0.1285
  -2.000   0.3080   0.00885   0.00252  -0.1169   0.6596   0.1320
  -1.750   0.3370   0.00878   0.00246  -0.1172   0.6547   0.1377
  -1.500   0.3664   0.00871   0.00242  -0.1175   0.6503   0.1430
  -1.250   0.3958   0.00870   0.00239  -0.1177   0.6461   0.1466
  -1.000   0.4247   0.00865   0.00234  -0.1179   0.6421   0.1524
  -0.750   0.4536   0.00863   0.00232  -0.1182   0.6380   0.1585
  -0.500   0.4832   0.00858   0.00230  -0.1185   0.6346   0.1633
  -0.250   0.5124   0.00851   0.00227  -0.1188   0.6305   0.1725
   0.000   0.5414   0.00848   0.00225  -0.1190   0.6262   0.1814
   0.250   0.5698   0.00845   0.00225  -0.1192   0.6215   0.1987
   0.500   0.5988   0.00831   0.00225  -0.1195   0.6175   0.2358
   0.750   0.6274   0.00815   0.00227  -0.1198   0.6125   0.2962
   1.000   0.6555   0.00798   0.00229  -0.1200   0.6073   0.3669
   1.250   0.6828   0.00769   0.00234  -0.1201   0.6024   0.4931
   1.500   0.7098   0.00728   0.00241  -0.1202   0.5975   0.6567
   1.750   0.7350   0.00697   0.00250  -0.1196   0.5919   0.7960
   2.000   0.7576   0.00685   0.00261  -0.1182   0.5861   0.8889
   2.250   0.7818   0.00681   0.00268  -0.1171   0.5806   0.9467
   2.500   0.8142   0.00688   0.00273  -0.1179   0.5736   0.9788
   2.750   0.8513   0.00698   0.00279  -0.1200   0.5663   0.9930
   3.000   0.8911   0.00708   0.00285  -0.1227   0.5569   0.9992
   3.250   0.9175   0.00719   0.00291  -0.1225   0.5466   1.0000
   3.500   0.9412   0.00733   0.00297  -0.1217   0.5335   1.0000
   3.750   0.9651   0.00750   0.00306  -0.1209   0.5179   1.0000
   4.000   0.9890   0.00769   0.00317  -0.1202   0.5003   1.0000
   4.250   1.0126   0.00792   0.00330  -0.1195   0.4801   1.0000
   4.500   1.0354   0.00820   0.00347  -0.1186   0.4582   1.0000
   5.000   1.0782   0.00891   0.00392  -0.1163   0.4102   1.0000
   5.250   1.1000   0.00924   0.00415  -0.1153   0.3920   1.0000
   5.500   1.1223   0.00954   0.00437  -0.1144   0.3785   1.0000
   6.000   1.1674   0.01008   0.00481  -0.1126   0.3579   1.0000
   6.250   1.1888   0.01038   0.00505  -0.1115   0.3496   1.0000
   6.500   1.2118   0.01059   0.00526  -0.1107   0.3434   1.0000
   6.750   1.2327   0.01086   0.00550  -0.1095   0.3367   1.0000
   7.000   1.2513   0.01116   0.00577  -0.1079   0.3307   1.0000
   7.250   1.2730   0.01137   0.00598  -0.1069   0.3266   1.0000
   7.500   1.2936   0.01163   0.00625  -0.1056   0.3221   1.0000
   7.750   1.3127   0.01197   0.00656  -0.1042   0.3172   1.0000
   8.000   1.3331   0.01227   0.00687  -0.1030   0.3130   1.0000
   8.250   1.3552   0.01251   0.00713  -0.1022   0.3093   1.0000
   8.500   1.3758   0.01282   0.00745  -0.1011   0.3051   1.0000
   8.750   1.3945   0.01322   0.00783  -0.0998   0.3001   1.0000
   9.000   1.4146   0.01356   0.00819  -0.0987   0.2957   1.0000
   9.250   1.4362   0.01385   0.00850  -0.0979   0.2911   1.0000
   9.500   1.4549   0.01428   0.00892  -0.0967   0.2854   1.0000
   9.750   1.4732   0.01473   0.00937  -0.0954   0.2793   1.0000
  10.000   1.4932   0.01512   0.00976  -0.0944   0.2721   1.0000
  10.250   1.5092   0.01571   0.01032  -0.0929   0.2638   1.0000
  10.500   1.5273   0.01621   0.01081  -0.0917   0.2539   1.0000
  10.750   1.5422   0.01688   0.01145  -0.0902   0.2418   1.0000
  11.000   1.5545   0.01772   0.01222  -0.0883   0.2263   1.0000
  11.250   1.5614   0.01890   0.01328  -0.0858   0.2047   1.0000
  11.500   1.5658   0.02027   0.01452  -0.0831   0.1846   1.0000
  11.750   1.5722   0.02157   0.01576  -0.0808   0.1715   1.0000
  12.250   1.5915   0.02388   0.01803  -0.0773   0.1559   1.0000
  12.500   1.6012   0.02508   0.01923  -0.0756   0.1503   1.0000
  12.750   1.6121   0.02623   0.02040  -0.0742   0.1454   1.0000
  13.000   1.6241   0.02733   0.02151  -0.0730   0.1408   1.0000
  13.250   1.6323   0.02874   0.02292  -0.0715   0.1354   1.0000
  13.500   1.6434   0.02996   0.02417  -0.0703   0.1311   1.0000
  13.750   1.6541   0.03124   0.02546  -0.0692   0.1267   1.0000
  14.000   1.6617   0.03280   0.02703  -0.0678   0.1220   1.0000
  14.250   1.6723   0.03415   0.02842  -0.0668   0.1182   1.0000
  14.500   1.6808   0.03570   0.02997  -0.0657   0.1132   1.0000
  14.750   1.6868   0.03748   0.03175  -0.0645   0.1083   1.0000
  15.000   1.6954   0.03905   0.03336  -0.0636   0.1039   1.0000
  15.250   1.6998   0.04103   0.03532  -0.0624   0.0987   1.0000
  15.500   1.7066   0.04284   0.03717  -0.0615   0.0945   1.0000
  15.750   1.7103   0.04494   0.03927  -0.0605   0.0895   1.0000
  16.000   1.7144   0.04702   0.04138  -0.0595   0.0852   1.0000
  16.250   1.7161   0.04938   0.04375  -0.0585   0.0803   1.0000
  16.500   1.7184   0.05172   0.04611  -0.0576   0.0758   1.0000
  16.750   1.7175   0.05444   0.04883  -0.0567   0.0709   1.0000
  17.000   1.7173   0.05712   0.05154  -0.0560   0.0665   1.0000
  17.250   1.7136   0.06019   0.05462  -0.0552   0.0617   1.0000
  17.500   1.7110   0.06322   0.05768  -0.0545   0.0568   1.0000
  17.750   1.7052   0.06669   0.06116  -0.0539   0.0517   1.0000
  18.000   1.6970   0.07048   0.06497  -0.0534   0.0464   1.0000
  18.250   1.6860   0.07465   0.06915  -0.0530   0.0401   1.0000
  18.500   1.6727   0.07921   0.07372  -0.0528   0.0339   1.0000
  18.750   1.6577   0.08410   0.07863  -0.0527   0.0284   1.0000
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