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GOE 796 AIRFOIL (goe796-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 796 AIRFOIL (goe796-il)
Reynolds number: 1,000,000
Max Cl/Cd: 122.7 at α=3.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe796-il-1000000.txt
Download as CSV file: xf-goe796-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 796 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
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.6267   0.08376   0.08185  -0.0504   1.0000   0.0186
 -12.500  -0.8443   0.03850   0.03596  -0.0870   1.0000   0.0172
 -12.250  -0.8665   0.03582   0.03313  -0.0838   0.9983   0.0172
 -12.000  -0.8542   0.03237   0.02942  -0.0865   0.9953   0.0172
 -11.750  -0.8358   0.02965   0.02647  -0.0887   0.9935   0.0173
 -11.500  -0.8170   0.02754   0.02415  -0.0897   0.9902   0.0173
 -11.250  -0.7938   0.02575   0.02218  -0.0909   0.9879   0.0174
 -11.000  -0.7681   0.02427   0.02054  -0.0922   0.9859   0.0176
 -10.750  -0.7413   0.02302   0.01914  -0.0933   0.9839   0.0178
 -10.500  -0.7165   0.02201   0.01800  -0.0937   0.9804   0.0180
 -10.250  -0.6920   0.02119   0.01707  -0.0937   0.9760   0.0182
 -10.000  -0.6670   0.02041   0.01618  -0.0938   0.9723   0.0183
  -9.750  -0.6444   0.01965   0.01530  -0.0932   0.9672   0.0184
  -9.500  -0.6274   0.01797   0.01341  -0.0920   0.9611   0.0186
  -9.250  -0.6067   0.01688   0.01218  -0.0911   0.9560   0.0187
  -9.000  -0.5856   0.01593   0.01111  -0.0902   0.9500   0.0188
  -8.750  -0.5635   0.01511   0.01018  -0.0893   0.9446   0.0190
  -8.500  -0.5403   0.01439   0.00936  -0.0886   0.9389   0.0191
  -8.250  -0.5165   0.01376   0.00866  -0.0879   0.9327   0.0193
  -8.000  -0.4922   0.01322   0.00802  -0.0873   0.9273   0.0194
  -7.750  -0.4669   0.01270   0.00744  -0.0868   0.9208   0.0196
  -7.500  -0.4416   0.01224   0.00691  -0.0863   0.9144   0.0197
  -7.250  -0.4156   0.01183   0.00642  -0.0860   0.9077   0.0198
  -7.000  -0.3895   0.01144   0.00596  -0.0856   0.9003   0.0200
  -6.750  -0.3630   0.01108   0.00554  -0.0853   0.8931   0.0201
  -6.500  -0.3362   0.01075   0.00515  -0.0851   0.8848   0.0203
  -6.250  -0.3093   0.01045   0.00478  -0.0848   0.8761   0.0204
  -6.000  -0.2823   0.01018   0.00443  -0.0846   0.8668   0.0206
  -5.750  -0.2549   0.00992   0.00412  -0.0844   0.8565   0.0208
  -5.500  -0.2275   0.00969   0.00382  -0.0843   0.8461   0.0210
  -5.250  -0.2002   0.00949   0.00355  -0.0841   0.8348   0.0212
  -5.000  -0.1726   0.00931   0.00329  -0.0839   0.8225   0.0214
  -4.750  -0.1449   0.00914   0.00306  -0.0838   0.8098   0.0219
  -4.500  -0.1172   0.00900   0.00284  -0.0837   0.7971   0.0224
  -4.250  -0.0895   0.00888   0.00265  -0.0836   0.7845   0.0231
  -4.000  -0.0618   0.00874   0.00248  -0.0835   0.7733   0.0255
  -3.750  -0.0343   0.00851   0.00230  -0.0834   0.7634   0.0401
  -3.500  -0.0063   0.00839   0.00218  -0.0834   0.7545   0.0480
  -3.250   0.0217   0.00831   0.00207  -0.0834   0.7455   0.0543
  -3.000   0.0500   0.00821   0.00196  -0.0834   0.7374   0.0595
  -2.750   0.0780   0.00811   0.00187  -0.0834   0.7301   0.0695
  -2.500   0.1062   0.00799   0.00183  -0.0835   0.7233   0.0873
  -2.250   0.1347   0.00796   0.00179  -0.0836   0.7163   0.0961
  -2.000   0.1631   0.00790   0.00174  -0.0837   0.7097   0.1044
  -1.750   0.1916   0.00787   0.00169  -0.0838   0.7023   0.1097
  -1.500   0.2200   0.00786   0.00165  -0.0838   0.6954   0.1139
  -1.250   0.2486   0.00778   0.00160  -0.0840   0.6889   0.1206
  -1.000   0.2770   0.00776   0.00156  -0.0840   0.6833   0.1256
  -0.750   0.3057   0.00771   0.00153  -0.0842   0.6782   0.1327
  -0.500   0.3342   0.00764   0.00150  -0.0843   0.6726   0.1454
  -0.250   0.3621   0.00751   0.00148  -0.0844   0.6669   0.1816
   0.000   0.3901   0.00732   0.00147  -0.0845   0.6599   0.2423
   0.250   0.4175   0.00715   0.00146  -0.0845   0.6516   0.3091
   0.500   0.4448   0.00685   0.00147  -0.0845   0.6443   0.4155
   0.750   0.4710   0.00646   0.00150  -0.0844   0.6375   0.5639
   1.000   0.4960   0.00604   0.00155  -0.0839   0.6314   0.7257
   1.250   0.5173   0.00563   0.00163  -0.0822   0.6245   0.8835
   1.500   0.5497   0.00563   0.00173  -0.0827   0.6168   0.9725
   1.750   0.5899   0.00571   0.00178  -0.0854   0.6070   0.9884
   2.000   0.6300   0.00581   0.00182  -0.0881   0.5970   0.9946
   2.250   0.6736   0.00592   0.00187  -0.0917   0.5848   0.9994
   2.750   0.7272   0.00610   0.00195  -0.0913   0.5591   1.0000
   3.000   0.7522   0.00622   0.00201  -0.0907   0.5433   1.0000
   3.250   0.7768   0.00636   0.00207  -0.0900   0.5252   1.0000
   3.500   0.8012   0.00653   0.00215  -0.0893   0.5033   1.0000
   3.750   0.8246   0.00677   0.00227  -0.0885   0.4769   1.0000
   4.000   0.8473   0.00706   0.00241  -0.0875   0.4449   1.0000
   4.250   0.8697   0.00739   0.00259  -0.0865   0.4131   1.0000
   4.500   0.8927   0.00767   0.00276  -0.0856   0.3902   1.0000
   4.750   0.9160   0.00796   0.00294  -0.0848   0.3682   1.0000
   5.000   0.9393   0.00826   0.00313  -0.0840   0.3473   1.0000
   5.250   0.9634   0.00851   0.00331  -0.0833   0.3317   1.0000
   5.500   0.9879   0.00874   0.00349  -0.0828   0.3187   1.0000
   5.750   1.0125   0.00897   0.00366  -0.0822   0.3070   1.0000
   6.000   1.0370   0.00922   0.00385  -0.0817   0.2947   1.0000
   6.250   1.0620   0.00942   0.00402  -0.0812   0.2828   1.0000
   6.500   1.0867   0.00965   0.00422  -0.0807   0.2697   1.0000
   6.750   1.1104   0.00994   0.00443  -0.0801   0.2523   1.0000
   7.000   1.1319   0.01039   0.00472  -0.0791   0.2212   1.0000
   7.250   1.1498   0.01106   0.00516  -0.0776   0.1813   1.0000
   7.500   1.1712   0.01150   0.00552  -0.0766   0.1666   1.0000
   7.750   1.1939   0.01182   0.00582  -0.0758   0.1578   1.0000
   8.000   1.2157   0.01220   0.00616  -0.0749   0.1487   1.0000
   8.250   1.2386   0.01249   0.00644  -0.0741   0.1414   1.0000
   8.500   1.2603   0.01285   0.00678  -0.0732   0.1335   1.0000
   8.750   1.2819   0.01319   0.00709  -0.0723   0.1241   1.0000
   9.000   1.3022   0.01361   0.00746  -0.0711   0.1118   1.0000
   9.250   1.3202   0.01412   0.00788  -0.0696   0.0974   1.0000
   9.500   1.3364   0.01465   0.00835  -0.0678   0.0852   1.0000
   9.750   1.3525   0.01514   0.00881  -0.0659   0.0772   1.0000
  10.000   1.3678   0.01569   0.00932  -0.0640   0.0695   1.0000
  10.250   1.3833   0.01624   0.00986  -0.0622   0.0628   1.0000
  10.500   1.3990   0.01681   0.01042  -0.0604   0.0564   1.0000
  10.750   1.4128   0.01750   0.01108  -0.0585   0.0494   1.0000
  11.000   1.4271   0.01818   0.01174  -0.0567   0.0426   1.0000
  11.250   1.4377   0.01910   0.01260  -0.0545   0.0327   1.0000
  11.500   1.4474   0.02012   0.01357  -0.0523   0.0248   1.0000
  11.750   1.4585   0.02106   0.01452  -0.0504   0.0212   1.0000
  12.000   1.4695   0.02205   0.01553  -0.0485   0.0191   1.0000
  12.250   1.4809   0.02304   0.01657  -0.0468   0.0174   1.0000
  12.500   1.4927   0.02402   0.01759  -0.0453   0.0163   1.0000
  12.750   1.5023   0.02518   0.01880  -0.0436   0.0151   1.0000
  13.000   1.5107   0.02650   0.02016  -0.0419   0.0140   1.0000
  13.250   1.5226   0.02755   0.02128  -0.0407   0.0134   1.0000
  13.500   1.5330   0.02876   0.02255  -0.0394   0.0128   1.0000
  13.750   1.5419   0.03013   0.02397  -0.0381   0.0122   1.0000
  14.000   1.5490   0.03169   0.02558  -0.0368   0.0116   1.0000
  14.250   1.5544   0.03344   0.02739  -0.0355   0.0110   1.0000
  14.500   1.5633   0.03493   0.02895  -0.0345   0.0107   1.0000
  14.750   1.5708   0.03657   0.03066  -0.0336   0.0102   1.0000
  15.000   1.5772   0.03835   0.03250  -0.0327   0.0098   1.0000
  15.250   1.5819   0.04033   0.03453  -0.0319   0.0093   1.0000
  15.500   1.5840   0.04265   0.03692  -0.0310   0.0089   1.0000
  15.750   1.5842   0.04523   0.03959  -0.0303   0.0085   1.0000
  16.000   1.5856   0.04774   0.04218  -0.0297   0.0083   1.0000
  16.250   1.5859   0.05045   0.04498  -0.0293   0.0080   1.0000
  16.500   1.5846   0.05342   0.04804  -0.0290   0.0078   1.0000
  16.750   1.5812   0.05672   0.05143  -0.0288   0.0076   1.0000
  17.000   1.5758   0.06034   0.05514  -0.0288   0.0074   1.0000
  17.250   1.5672   0.06450   0.05940  -0.0291   0.0071   1.0000
  17.500   1.5546   0.06936   0.06438  -0.0296   0.0069   1.0000
  17.750   1.5388   0.07479   0.06995  -0.0305   0.0068   1.0000
  18.000   1.5274   0.07978   0.07506  -0.0316   0.0067   1.0000
  18.250   1.5191   0.08444   0.07983  -0.0327   0.0066   1.0000
  18.500   1.5091   0.08945   0.08496  -0.0340   0.0065   1.0000
  18.750   1.4979   0.09469   0.09031  -0.0356   0.0064   1.0000
  19.000   1.4854   0.10027   0.09601  -0.0374   0.0064   1.0000
  19.250   1.4721   0.10605   0.10191  -0.0394   0.0063   1.0000
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