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GOE 797 AIRFOIL (goe797-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 797 AIRFOIL (goe797-il)
Reynolds number: 500,000
Max Cl/Cd: 96.67 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe797-il-500000-n5.txt
Download as CSV file: xf-goe797-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -15.750  -0.7790   0.07476   0.07124  -0.0886   1.0000   0.0319
 -15.500  -0.8411   0.06248   0.05877  -0.0962   1.0000   0.0319
 -15.000  -0.9087   0.04118   0.03696  -0.1164   0.9931   0.0319
 -14.750  -0.9121   0.03566   0.03126  -0.1235   0.9849   0.0321
 -14.500  -0.9094   0.03253   0.02798  -0.1264   0.9769   0.0324
 -14.250  -0.9025   0.03043   0.02577  -0.1274   0.9699   0.0326
 -14.000  -0.8970   0.02896   0.02420  -0.1263   0.9612   0.0328
 -13.750  -0.8866   0.02776   0.02289  -0.1254   0.9541   0.0331
 -13.500  -0.8730   0.02668   0.02172  -0.1245   0.9473   0.0333
 -13.250  -0.8578   0.02572   0.02066  -0.1236   0.9409   0.0336
 -13.000  -0.8413   0.02484   0.01968  -0.1228   0.9343   0.0340
 -12.750  -0.8234   0.02400   0.01874  -0.1220   0.9288   0.0343
 -12.500  -0.8049   0.02321   0.01785  -0.1212   0.9222   0.0347
 -12.250  -0.7851   0.02247   0.01699  -0.1204   0.9160   0.0351
 -12.000  -0.7645   0.02178   0.01619  -0.1198   0.9096   0.0355
 -11.750  -0.7429   0.02114   0.01543  -0.1192   0.9029   0.0360
 -11.500  -0.7206   0.02053   0.01470  -0.1186   0.8971   0.0364
 -11.250  -0.6989   0.01984   0.01394  -0.1181   0.8900   0.0369
 -11.000  -0.6765   0.01921   0.01324  -0.1175   0.8830   0.0374
 -10.750  -0.6529   0.01867   0.01264  -0.1171   0.8754   0.0378
 -10.500  -0.6288   0.01818   0.01207  -0.1167   0.8673   0.0384
 -10.250  -0.6040   0.01772   0.01153  -0.1164   0.8595   0.0389
 -10.000  -0.5791   0.01728   0.01100  -0.1161   0.8509   0.0396
  -9.750  -0.5537   0.01685   0.01049  -0.1158   0.8422   0.0402
  -9.500  -0.5282   0.01645   0.00998  -0.1155   0.8323   0.0409
  -9.250  -0.5023   0.01608   0.00951  -0.1153   0.8219   0.0415
  -9.000  -0.4770   0.01565   0.00900  -0.1150   0.8114   0.0423
  -8.750  -0.4509   0.01528   0.00857  -0.1148   0.8008   0.0432
  -8.500  -0.4244   0.01498   0.00819  -0.1147   0.7914   0.0442
  -8.250  -0.3977   0.01469   0.00782  -0.1145   0.7819   0.0452
  -8.000  -0.3708   0.01442   0.00746  -0.1144   0.7732   0.0462
  -7.750  -0.3437   0.01417   0.00711  -0.1143   0.7646   0.0471
  -7.500  -0.3168   0.01386   0.00674  -0.1142   0.7571   0.0483
  -7.250  -0.2896   0.01359   0.00642  -0.1142   0.7499   0.0496
  -7.000  -0.2621   0.01337   0.00614  -0.1142   0.7441   0.0510
  -6.750  -0.2342   0.01315   0.00588  -0.1142   0.7384   0.0525
  -6.500  -0.2062   0.01297   0.00563  -0.1143   0.7327   0.0540
  -6.250  -0.1787   0.01274   0.00535  -0.1143   0.7275   0.0560
  -6.000  -0.1505   0.01253   0.00513  -0.1144   0.7226   0.0581
  -5.750  -0.1223   0.01235   0.00492  -0.1145   0.7177   0.0602
  -5.500  -0.0939   0.01221   0.00472  -0.1146   0.7134   0.0620
  -5.250  -0.0658   0.01202   0.00452  -0.1147   0.7095   0.0649
  -5.000  -0.0372   0.01185   0.00435  -0.1148   0.7054   0.0682
  -4.750  -0.0086   0.01172   0.00420  -0.1150   0.7011   0.0713
  -4.500   0.0198   0.01157   0.00405  -0.1151   0.6970   0.0758
  -4.250   0.0483   0.01146   0.00392  -0.1153   0.6935   0.0803
  -4.000   0.0771   0.01135   0.00380  -0.1154   0.6894   0.0850
  -3.750   0.1057   0.01123   0.00371  -0.1156   0.6842   0.0911
  -3.500   0.1343   0.01116   0.00361  -0.1157   0.6790   0.0962
  -3.000   0.1917   0.01100   0.00346  -0.1161   0.6704   0.1082
  -2.750   0.2206   0.01095   0.00339  -0.1162   0.6653   0.1123
  -2.500   0.2491   0.01088   0.00332  -0.1164   0.6606   0.1182
  -2.250   0.2777   0.01084   0.00326  -0.1165   0.6565   0.1236
  -2.000   0.3068   0.01079   0.00321  -0.1167   0.6521   0.1278
  -1.750   0.3355   0.01073   0.00316  -0.1169   0.6473   0.1326
  -1.500   0.3640   0.01068   0.00311  -0.1170   0.6422   0.1379
  -1.250   0.3925   0.01066   0.00306  -0.1171   0.6368   0.1425
  -1.000   0.4211   0.01061   0.00302  -0.1173   0.6306   0.1471
  -0.750   0.4494   0.01057   0.00299  -0.1174   0.6250   0.1537
  -0.500   0.4779   0.01056   0.00296  -0.1175   0.6209   0.1598
  -0.250   0.5066   0.01049   0.00294  -0.1177   0.6166   0.1671
   0.000   0.5351   0.01046   0.00293  -0.1179   0.6118   0.1750
   0.250   0.5633   0.01043   0.00292  -0.1180   0.6071   0.1849
   0.500   0.5916   0.01039   0.00293  -0.1181   0.6024   0.1998
   0.750   0.6198   0.01031   0.00295  -0.1183   0.5966   0.2287
   1.000   0.6474   0.01023   0.00298  -0.1183   0.5904   0.2686
   1.250   0.6751   0.01015   0.00301  -0.1184   0.5846   0.3110
   1.500   0.7026   0.01004   0.00306  -0.1185   0.5780   0.3665
   1.750   0.7290   0.00984   0.00312  -0.1184   0.5715   0.4674
   2.000   0.7551   0.00952   0.00322  -0.1183   0.5647   0.6075
   2.250   0.7792   0.00925   0.00334  -0.1175   0.5570   0.7386
   2.500   0.8014   0.00909   0.00347  -0.1161   0.5494   0.8405
   2.750   0.8236   0.00909   0.00359  -0.1145   0.5402   0.9153
   3.000   0.8560   0.00918   0.00368  -0.1154   0.5299   0.9645
   3.250   0.8955   0.00934   0.00378  -0.1181   0.5173   1.0000
   3.500   0.9189   0.00952   0.00388  -0.1173   0.5037   1.0000
   3.750   0.9416   0.00974   0.00401  -0.1163   0.4874   1.0000
   4.000   0.9633   0.01002   0.00417  -0.1152   0.4671   1.0000
   4.250   0.9836   0.01035   0.00438  -0.1139   0.4444   1.0000
   4.500   1.0031   0.01073   0.00462  -0.1124   0.4231   1.0000
   4.750   1.0227   0.01109   0.00487  -0.1109   0.4044   1.0000
   5.000   1.0423   0.01146   0.00514  -0.1095   0.3883   1.0000
   5.250   1.0630   0.01177   0.00539  -0.1083   0.3762   1.0000
   5.500   1.0833   0.01208   0.00565  -0.1070   0.3667   1.0000
   5.750   1.1020   0.01240   0.00592  -0.1054   0.3575   1.0000
   6.000   1.1209   0.01270   0.00619  -0.1038   0.3506   1.0000
   6.250   1.1405   0.01300   0.00647  -0.1024   0.3447   1.0000
   6.500   1.1585   0.01337   0.00681  -0.1008   0.3386   1.0000
   6.750   1.1789   0.01368   0.00712  -0.0996   0.3328   1.0000
   7.000   1.1982   0.01404   0.00746  -0.0983   0.3268   1.0000
   7.250   1.2163   0.01446   0.00786  -0.0968   0.3215   1.0000
   7.500   1.2371   0.01478   0.00820  -0.0958   0.3174   1.0000
   7.750   1.2574   0.01514   0.00857  -0.0947   0.3130   1.0000
   8.000   1.2762   0.01557   0.00900  -0.0935   0.3083   1.0000
   8.250   1.2936   0.01607   0.00948  -0.0920   0.3036   1.0000
   8.500   1.3145   0.01642   0.00988  -0.0912   0.2995   1.0000
   8.750   1.3338   0.01686   0.01033  -0.0901   0.2945   1.0000
   9.000   1.3514   0.01739   0.01086  -0.0888   0.2900   1.0000
   9.250   1.3692   0.01792   0.01141  -0.0876   0.2859   1.0000
   9.500   1.3887   0.01837   0.01190  -0.0866   0.2808   1.0000
   9.750   1.4058   0.01896   0.01250  -0.0854   0.2746   1.0000
  10.000   1.4219   0.01962   0.01316  -0.0841   0.2687   1.0000
  10.250   1.4392   0.02022   0.01379  -0.0830   0.2610   1.0000
  10.500   1.4532   0.02103   0.01458  -0.0815   0.2522   1.0000
  10.750   1.4669   0.02188   0.01542  -0.0801   0.2409   1.0000
  11.000   1.4783   0.02291   0.01640  -0.0784   0.2265   1.0000
  11.250   1.4847   0.02429   0.01769  -0.0763   0.2061   1.0000
  11.500   1.4876   0.02595   0.01924  -0.0740   0.1863   1.0000
  11.750   1.4924   0.02755   0.02078  -0.0720   0.1733   1.0000
  12.000   1.4989   0.02908   0.02227  -0.0703   0.1643   1.0000
  12.250   1.5056   0.03062   0.02381  -0.0687   0.1569   1.0000
  12.500   1.5150   0.03201   0.02522  -0.0674   0.1514   1.0000
  12.750   1.5237   0.03350   0.02673  -0.0662   0.1459   1.0000
  13.000   1.5306   0.03518   0.02841  -0.0648   0.1410   1.0000
  13.250   1.5415   0.03652   0.02980  -0.0639   0.1367   1.0000
  13.500   1.5498   0.03813   0.03144  -0.0628   0.1318   1.0000
  13.750   1.5557   0.03997   0.03329  -0.0617   0.1271   1.0000
  14.000   1.5656   0.04149   0.03487  -0.0609   0.1234   1.0000
  14.250   1.5736   0.04320   0.03661  -0.0600   0.1189   1.0000
  14.500   1.5790   0.04516   0.03859  -0.0590   0.1143   1.0000
  14.750   1.5851   0.04709   0.04056  -0.0581   0.1103   1.0000
  15.000   1.5923   0.04894   0.04246  -0.0574   0.1061   1.0000
  15.250   1.5962   0.05114   0.04469  -0.0566   0.1013   1.0000
  15.500   1.5991   0.05349   0.04706  -0.0558   0.0970   1.0000
  15.750   1.6040   0.05565   0.04928  -0.0551   0.0925   1.0000
  16.000   1.6048   0.05827   0.05191  -0.0544   0.0874   1.0000
  16.250   1.6056   0.06095   0.05462  -0.0538   0.0829   1.0000
  16.500   1.6067   0.06362   0.05733  -0.0533   0.0783   1.0000
  16.750   1.6037   0.06683   0.06056  -0.0528   0.0735   1.0000
  17.000   1.6035   0.06974   0.06351  -0.0524   0.0695   1.0000
  17.250   1.6006   0.07301   0.06682  -0.0521   0.0654   1.0000
  17.500   1.5973   0.07639   0.07025  -0.0519   0.0618   1.0000
  17.750   1.5933   0.07991   0.07382  -0.0519   0.0578   1.0000
  18.000   1.5872   0.08375   0.07771  -0.0519   0.0543   1.0000
  18.250   1.5817   0.08754   0.08155  -0.0520   0.0504   1.0000
  18.500   1.5742   0.09164   0.08570  -0.0523   0.0466   1.0000
  18.750   1.5660   0.09592   0.09003  -0.0527   0.0426   1.0000
  19.000   1.5567   0.10042   0.09458  -0.0534   0.0382   1.0000
  19.250   1.5462   0.10514   0.09934  -0.0542   0.0337   1.0000
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