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GOE 798 AIRFOIL (goe798-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 798 AIRFOIL (goe798-il)
Reynolds number: 1,000,000
Max Cl/Cd: 84.65 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe798-il-1000000-n5.txt
Download as CSV file: xf-goe798-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 798 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
  ------ -------- --------- --------- -------- -------- --------
 -17.750  -0.6705   0.08750   0.08437  -0.1114   0.9345   0.0350
 -17.500  -0.7448   0.07418   0.07086  -0.1194   0.9287   0.0352
 -17.250  -0.9686   0.03930   0.03524  -0.1440   0.9165   0.0348
 -17.000  -0.9874   0.03295   0.02867  -0.1500   0.9083   0.0350
 -16.750  -0.9915   0.02978   0.02534  -0.1519   0.9003   0.0351
 -16.500  -0.9893   0.02765   0.02310  -0.1526   0.8931   0.0353
 -16.250  -0.9839   0.02610   0.02143  -0.1523   0.8849   0.0356
 -16.000  -0.9756   0.02490   0.02013  -0.1515   0.8778   0.0358
 -15.750  -0.9655   0.02389   0.01902  -0.1505   0.8698   0.0361
 -15.500  -0.9541   0.02304   0.01807  -0.1493   0.8619   0.0363
 -15.250  -0.9415   0.02229   0.01724  -0.1479   0.8533   0.0366
 -15.000  -0.9299   0.02167   0.01651  -0.1460   0.8431   0.0368
 -14.750  -0.9155   0.02112   0.01587  -0.1444   0.8313   0.0369
 -14.500  -0.8997   0.02049   0.01514  -0.1432   0.8184   0.0372
 -14.250  -0.8830   0.01990   0.01443  -0.1420   0.8036   0.0376
 -14.000  -0.8645   0.01938   0.01381  -0.1409   0.7889   0.0379
 -13.750  -0.8445   0.01890   0.01325  -0.1401   0.7761   0.0383
 -13.500  -0.8237   0.01848   0.01274  -0.1392   0.7649   0.0386
 -13.250  -0.8020   0.01807   0.01225  -0.1385   0.7548   0.0390
 -13.000  -0.7797   0.01770   0.01180  -0.1379   0.7463   0.0394
 -12.750  -0.7566   0.01733   0.01137  -0.1373   0.7387   0.0397
 -12.250  -0.7092   0.01667   0.01056  -0.1363   0.7255   0.0405
 -12.000  -0.6846   0.01635   0.01019  -0.1359   0.7205   0.0409
 -11.750  -0.6596   0.01607   0.00984  -0.1356   0.7156   0.0412
 -11.500  -0.6355   0.01572   0.00943  -0.1351   0.7109   0.0417
 -11.250  -0.6108   0.01537   0.00904  -0.1347   0.7071   0.0423
 -11.000  -0.5854   0.01504   0.00869  -0.1344   0.7038   0.0428
 -10.750  -0.5596   0.01475   0.00837  -0.1342   0.7000   0.0434
 -10.500  -0.5336   0.01449   0.00806  -0.1339   0.6959   0.0439
 -10.250  -0.5076   0.01425   0.00777  -0.1337   0.6918   0.0445
 -10.000  -0.4813   0.01403   0.00750  -0.1334   0.6880   0.0450
  -9.750  -0.4542   0.01379   0.00723  -0.1334   0.6857   0.0455
  -9.500  -0.4270   0.01358   0.00699  -0.1333   0.6830   0.0459
  -9.250  -0.4005   0.01329   0.00668  -0.1331   0.6800   0.0467
  -9.000  -0.3737   0.01304   0.00641  -0.1330   0.6770   0.0475
  -8.750  -0.3468   0.01282   0.00616  -0.1328   0.6739   0.0483
  -8.500  -0.3197   0.01264   0.00594  -0.1327   0.6706   0.0492
  -8.250  -0.2924   0.01246   0.00573  -0.1326   0.6674   0.0500
  -8.000  -0.2644   0.01228   0.00552  -0.1327   0.6652   0.0507
  -7.750  -0.2367   0.01207   0.00530  -0.1326   0.6627   0.0517
  -7.500  -0.2091   0.01186   0.00509  -0.1326   0.6602   0.0528
  -7.250  -0.1813   0.01167   0.00489  -0.1326   0.6575   0.0540
  -7.000  -0.1535   0.01152   0.00471  -0.1326   0.6547   0.0553
  -6.750  -0.1259   0.01136   0.00454  -0.1326   0.6517   0.0570
  -6.500  -0.0985   0.01120   0.00436  -0.1325   0.6485   0.0594
  -6.250  -0.0703   0.01104   0.00421  -0.1326   0.6464   0.0621
  -6.000  -0.0421   0.01087   0.00407  -0.1327   0.6443   0.0664
  -5.750  -0.0136   0.01073   0.00398  -0.1328   0.6418   0.0722
  -5.500   0.0150   0.01066   0.00393  -0.1329   0.6385   0.0780
  -5.250   0.0434   0.01060   0.00386  -0.1330   0.6345   0.0816
  -5.000   0.0715   0.01058   0.00382  -0.1330   0.6303   0.0848
  -4.750   0.1001   0.01055   0.00377  -0.1331   0.6272   0.0872
  -4.500   0.1292   0.01048   0.00370  -0.1333   0.6247   0.0887
  -4.250   0.1579   0.01041   0.00364  -0.1334   0.6216   0.0904
  -4.000   0.1864   0.01036   0.00359  -0.1335   0.6178   0.0919
  -3.750   0.2147   0.01034   0.00354  -0.1336   0.6140   0.0933
  -3.500   0.2426   0.01033   0.00350  -0.1335   0.6102   0.0947
  -3.250   0.2713   0.01030   0.00346  -0.1337   0.6073   0.0957
  -3.000   0.3001   0.01026   0.00341  -0.1339   0.6041   0.0964
  -2.750   0.3282   0.01017   0.00333  -0.1339   0.6004   0.0976
  -2.500   0.3561   0.01012   0.00328  -0.1339   0.5966   0.0991
  -2.250   0.3834   0.01010   0.00324  -0.1338   0.5924   0.1004
  -2.000   0.4112   0.01008   0.00321  -0.1338   0.5880   0.1014
  -1.750   0.4394   0.01004   0.00317  -0.1339   0.5831   0.1024
  -1.500   0.4668   0.01003   0.00314  -0.1338   0.5777   0.1034
  -1.250   0.4937   0.01004   0.00312  -0.1336   0.5732   0.1042
  -1.000   0.5214   0.01003   0.00310  -0.1336   0.5699   0.1049
  -0.750   0.5495   0.01002   0.00309  -0.1336   0.5664   0.1056
  -0.500   0.5768   0.00998   0.00306  -0.1336   0.5621   0.1074
  -0.250   0.6034   0.00997   0.00304  -0.1333   0.5575   0.1085
   0.000   0.6294   0.00999   0.00304  -0.1330   0.5529   0.1094
   0.250   0.6569   0.00998   0.00304  -0.1330   0.5489   0.1102
   0.500   0.6835   0.00998   0.00305  -0.1328   0.5436   0.1111
   0.750   0.7088   0.01003   0.00307  -0.1323   0.5377   0.1121
   1.000   0.7343   0.01007   0.00310  -0.1319   0.5321   0.1131
   1.250   0.7597   0.01011   0.00313  -0.1314   0.5248   0.1141
   1.500   0.7824   0.01021   0.00319  -0.1305   0.5164   0.1150
   2.000   0.8249   0.01038   0.00332  -0.1279   0.4979   0.1181
   2.250   0.8448   0.01047   0.00340  -0.1264   0.4875   0.1206
   2.500   0.8632   0.01063   0.00352  -0.1246   0.4765   0.1235
   2.750   0.8816   0.01085   0.00369  -0.1229   0.4632   0.1270
   3.000   0.9017   0.01107   0.00389  -0.1215   0.4491   0.1360
   3.250   0.9211   0.01129   0.00415  -0.1201   0.4343   0.1695
   3.500   0.9395   0.01155   0.00445  -0.1186   0.4192   0.2081
   3.750   0.9577   0.01186   0.00477  -0.1171   0.4045   0.2381
   4.000   0.9755   0.01218   0.00512  -0.1156   0.3908   0.2778
   4.500   1.0132   0.01271   0.00584  -0.1130   0.3671   0.3942
   4.750   1.0318   0.01284   0.00628  -0.1119   0.3569   0.5381
   5.000   1.0501   0.01250   0.00677  -0.1106   0.3498   0.8369
   5.250   1.0725   0.01267   0.00720  -0.1097   0.3425   1.0000
   5.500   1.0893   0.01314   0.00762  -0.1081   0.3353   1.0000
   5.750   1.1099   0.01348   0.00794  -0.1072   0.3310   1.0000
   6.000   1.1298   0.01386   0.00830  -0.1062   0.3271   1.0000
   6.250   1.1486   0.01430   0.00871  -0.1050   0.3231   1.0000
   6.500   1.1670   0.01478   0.00916  -0.1038   0.3187   1.0000
   6.750   1.1870   0.01519   0.00957  -0.1029   0.3158   1.0000
   7.000   1.2074   0.01560   0.00998  -0.1021   0.3132   1.0000
   7.250   1.2275   0.01603   0.01041  -0.1013   0.3106   1.0000
   7.500   1.2469   0.01651   0.01088  -0.1004   0.3081   1.0000
   7.750   1.2652   0.01704   0.01142  -0.0994   0.3057   1.0000
   8.000   1.2830   0.01762   0.01198  -0.0983   0.3027   1.0000
   8.250   1.2996   0.01828   0.01263  -0.0972   0.2993   1.0000
   8.500   1.3194   0.01878   0.01315  -0.0965   0.2978   1.0000
   8.750   1.3392   0.01929   0.01367  -0.0958   0.2959   1.0000
   9.000   1.3577   0.01987   0.01427  -0.0950   0.2937   1.0000
   9.250   1.3754   0.02051   0.01493  -0.0941   0.2914   1.0000
   9.500   1.3930   0.02117   0.01559  -0.0932   0.2892   1.0000
   9.750   1.4091   0.02195   0.01638  -0.0922   0.2870   1.0000
  10.000   1.4248   0.02276   0.01720  -0.0912   0.2845   1.0000
  10.250   1.4397   0.02365   0.01809  -0.0902   0.2815   1.0000
  10.500   1.4578   0.02434   0.01881  -0.0895   0.2794   1.0000
  10.750   1.4754   0.02508   0.01957  -0.0889   0.2768   1.0000
  11.000   1.4911   0.02596   0.02047  -0.0880   0.2740   1.0000
  11.250   1.5059   0.02690   0.02143  -0.0871   0.2710   1.0000
  11.500   1.5190   0.02799   0.02251  -0.0861   0.2677   1.0000
  11.750   1.5322   0.02909   0.02363  -0.0851   0.2646   1.0000
  12.000   1.5489   0.02993   0.02450  -0.0845   0.2625   1.0000
  12.250   1.5636   0.03095   0.02555  -0.0838   0.2594   1.0000
  12.500   1.5768   0.03207   0.02668  -0.0829   0.2551   1.0000
  12.750   1.5863   0.03349   0.02809  -0.0818   0.2504   1.0000
  13.000   1.5993   0.03464   0.02927  -0.0809   0.2466   1.0000
  13.250   1.6121   0.03581   0.03045  -0.0801   0.2414   1.0000
  13.500   1.6187   0.03751   0.03213  -0.0789   0.2348   1.0000
  13.750   1.6289   0.03890   0.03352  -0.0779   0.2276   1.0000
  14.000   1.6311   0.04097   0.03556  -0.0764   0.2165   1.0000
  14.250   1.6297   0.04332   0.03782  -0.0746   0.2008   1.0000
  14.500   1.6254   0.04598   0.04043  -0.0728   0.1874   1.0000
  14.750   1.6253   0.04832   0.04272  -0.0713   0.1780   1.0000
  15.000   1.6293   0.05038   0.04479  -0.0702   0.1725   1.0000
  15.250   1.6319   0.05250   0.04691  -0.0691   0.1668   1.0000
  15.500   1.6351   0.05468   0.04910  -0.0680   0.1620   1.0000
  15.750   1.6389   0.05679   0.05121  -0.0671   0.1574   1.0000
  16.000   1.6394   0.05926   0.05369  -0.0661   0.1526   1.0000
  16.250   1.6457   0.06120   0.05566  -0.0654   0.1493   1.0000
  16.500   1.6521   0.06311   0.05760  -0.0648   0.1461   1.0000
  16.750   1.6546   0.06546   0.05997  -0.0640   0.1434   1.0000
  17.000   1.6578   0.06773   0.06227  -0.0634   0.1406   1.0000
  17.250   1.6632   0.06981   0.06439  -0.0628   0.1384   1.0000
  17.500   1.6687   0.07193   0.06656  -0.0624   0.1364   1.0000
  17.750   1.6744   0.07399   0.06865  -0.0620   0.1342   1.0000
  18.000   1.6762   0.07649   0.07120  -0.0615   0.1318   1.0000
  18.250   1.6774   0.07906   0.07379  -0.0610   0.1294   1.0000
  18.500   1.6796   0.08153   0.07631  -0.0606   0.1271   1.0000
  18.750   1.6829   0.08394   0.07877  -0.0604   0.1252   1.0000
  19.000   1.6868   0.08625   0.08113  -0.0601   0.1231   1.0000
  19.250   1.6868   0.08905   0.08397  -0.0599   0.1210   1.0000
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