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GOE 612 AIRFOIL (goe612-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 612 AIRFOIL (goe612-il)
Reynolds number: 500,000
Max Cl/Cd: 85.11 at α=3.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe612-il-500000-n5.txt
Download as CSV file: xf-goe612-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 612 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
  ------ -------- --------- --------- -------- -------- --------
 -14.750  -0.6358   0.07125   0.06796  -0.0878   0.9916   0.0283
 -14.500  -0.6800   0.05916   0.05563  -0.0989   0.9856   0.0283
 -14.250  -0.7005   0.05048   0.04672  -0.1084   0.9807   0.0284
 -14.000  -0.7069   0.04382   0.03986  -0.1168   0.9751   0.0284
 -13.750  -0.7007   0.03765   0.03345  -0.1268   0.9709   0.0285
 -13.500  -0.6887   0.03272   0.02829  -0.1360   0.9645   0.0287
 -13.250  -0.6759   0.02959   0.02502  -0.1412   0.9574   0.0290
 -13.000  -0.6674   0.02790   0.02322  -0.1419   0.9486   0.0292
 -12.500  -0.6552   0.02566   0.02078  -0.1387   0.9314   0.0295
 -12.250  -0.6434   0.02473   0.01974  -0.1374   0.9246   0.0297
 -12.000  -0.6329   0.02390   0.01883  -0.1355   0.9166   0.0299
 -11.750  -0.6184   0.02308   0.01792  -0.1342   0.9102   0.0301
 -11.500  -0.6039   0.02234   0.01709  -0.1327   0.9032   0.0303
 -11.250  -0.5876   0.02160   0.01625  -0.1313   0.8960   0.0305
 -11.000  -0.5700   0.02090   0.01546  -0.1301   0.8893   0.0308
 -10.750  -0.5520   0.02023   0.01469  -0.1288   0.8812   0.0311
 -10.500  -0.5324   0.01959   0.01394  -0.1278   0.8743   0.0314
 -10.250  -0.5128   0.01897   0.01323  -0.1266   0.8661   0.0316
 -10.000  -0.4918   0.01839   0.01253  -0.1257   0.8585   0.0319
  -9.750  -0.4708   0.01784   0.01189  -0.1247   0.8495   0.0322
  -9.500  -0.4487   0.01734   0.01127  -0.1238   0.8405   0.0325
  -9.250  -0.4262   0.01690   0.01072  -0.1229   0.8302   0.0328
  -9.000  -0.4047   0.01634   0.01008  -0.1219   0.8202   0.0333
  -8.750  -0.3825   0.01584   0.00952  -0.1210   0.8096   0.0336
  -8.500  -0.3595   0.01543   0.00903  -0.1202   0.7996   0.0340
  -8.250  -0.3360   0.01506   0.00858  -0.1194   0.7896   0.0344
  -8.000  -0.3121   0.01471   0.00815  -0.1187   0.7796   0.0349
  -7.750  -0.2881   0.01439   0.00774  -0.1179   0.7702   0.0353
  -7.500  -0.2638   0.01407   0.00735  -0.1172   0.7607   0.0358
  -7.250  -0.2394   0.01378   0.00697  -0.1166   0.7526   0.0363
  -7.000  -0.2144   0.01350   0.00662  -0.1160   0.7451   0.0368
  -6.750  -0.1894   0.01325   0.00628  -0.1153   0.7381   0.0373
  -6.500  -0.1642   0.01296   0.00594  -0.1148   0.7319   0.0379
  -6.250  -0.1393   0.01267   0.00561  -0.1142   0.7252   0.0386
  -5.750  -0.0878   0.01224   0.00509  -0.1132   0.7137   0.0405
  -5.500  -0.0616   0.01205   0.00485  -0.1127   0.7084   0.0416
  -5.250  -0.0354   0.01188   0.00463  -0.1123   0.7034   0.0426
  -5.000  -0.0094   0.01167   0.00438  -0.1118   0.6988   0.0439
  -4.750   0.0169   0.01147   0.00417  -0.1114   0.6938   0.0455
  -4.500   0.0433   0.01132   0.00398  -0.1110   0.6883   0.0473
  -4.000   0.0959   0.01101   0.00362  -0.1101   0.6769   0.0522
  -3.750   0.1223   0.01088   0.00346  -0.1097   0.6708   0.0558
  -3.500   0.1485   0.01074   0.00330  -0.1092   0.6655   0.0615
  -3.250   0.1749   0.01057   0.00317  -0.1088   0.6607   0.0710
  -3.000   0.2012   0.01041   0.00308  -0.1084   0.6551   0.0866
  -2.750   0.2277   0.01032   0.00299  -0.1080   0.6496   0.0988
  -2.500   0.2543   0.01024   0.00291  -0.1076   0.6448   0.1077
  -2.250   0.2812   0.01016   0.00284  -0.1073   0.6394   0.1159
  -2.000   0.3075   0.01007   0.00277  -0.1068   0.6333   0.1259
  -1.750   0.3336   0.01000   0.00270  -0.1064   0.6273   0.1373
  -1.500   0.3600   0.00990   0.00265  -0.1060   0.6211   0.1521
  -1.250   0.3858   0.00980   0.00260  -0.1054   0.6148   0.1765
  -1.000   0.4115   0.00968   0.00258  -0.1049   0.6096   0.2107
  -0.750   0.4377   0.00957   0.00258  -0.1045   0.6040   0.2427
  -0.500   0.4635   0.00951   0.00259  -0.1040   0.5978   0.2707
  -0.250   0.4892   0.00948   0.00260  -0.1035   0.5922   0.2952
   0.000   0.5158   0.00945   0.00261  -0.1031   0.5865   0.3121
   0.250   0.5417   0.00946   0.00263  -0.1025   0.5798   0.3262
   0.500   0.5674   0.00948   0.00265  -0.1020   0.5728   0.3405
   0.750   0.5929   0.00949   0.00268  -0.1014   0.5644   0.3546
   1.000   0.6179   0.00952   0.00271  -0.1007   0.5563   0.3682
   1.250   0.6431   0.00954   0.00275  -0.1000   0.5473   0.3835
   1.500   0.6673   0.00958   0.00280  -0.0992   0.5375   0.4028
   1.750   0.6905   0.00963   0.00286  -0.0982   0.5248   0.4232
   2.000   0.7133   0.00970   0.00293  -0.0971   0.5098   0.4429
   2.250   0.7346   0.00980   0.00302  -0.0957   0.4919   0.4632
   2.500   0.7545   0.00995   0.00313  -0.0941   0.4714   0.4852
   2.750   0.7720   0.01012   0.00328  -0.0921   0.4461   0.5168
   3.000   0.7871   0.01030   0.00346  -0.0896   0.4206   0.5614
   3.250   0.7966   0.01021   0.00368  -0.0860   0.3978   0.6952
   3.500   0.8920   0.01048   0.00431  -0.1008   0.3629   1.0000
   3.750   0.9086   0.01078   0.00451  -0.0986   0.3496   1.0000
   4.250   0.9407   0.01134   0.00492  -0.0940   0.3277   1.0000
   4.500   0.9539   0.01164   0.00514  -0.0912   0.3177   1.0000
   4.750   0.9695   0.01190   0.00535  -0.0888   0.3084   1.0000
   5.000   0.9845   0.01220   0.00559  -0.0864   0.3010   1.0000
   5.250   1.0033   0.01242   0.00579  -0.0847   0.2960   1.0000
   5.500   1.0215   0.01267   0.00602  -0.0830   0.2910   1.0000
   5.750   1.0386   0.01298   0.00629  -0.0811   0.2860   1.0000
   6.000   1.0574   0.01324   0.00655  -0.0795   0.2816   1.0000
   6.250   1.0766   0.01351   0.00681  -0.0781   0.2766   1.0000
   6.500   1.0943   0.01384   0.00712  -0.0764   0.2712   1.0000
   6.750   1.1117   0.01420   0.00745  -0.0748   0.2665   1.0000
   7.000   1.1314   0.01448   0.00774  -0.0735   0.2624   1.0000
   7.250   1.1501   0.01481   0.00807  -0.0721   0.2578   1.0000
   7.500   1.1675   0.01522   0.00845  -0.0706   0.2530   1.0000
   7.750   1.1853   0.01561   0.00884  -0.0691   0.2488   1.0000
   8.000   1.2043   0.01597   0.00921  -0.0679   0.2442   1.0000
   8.250   1.2218   0.01640   0.00964  -0.0665   0.2393   1.0000
   8.500   1.2378   0.01692   0.01014  -0.0650   0.2343   1.0000
   8.750   1.2564   0.01733   0.01057  -0.0638   0.2300   1.0000
   9.000   1.2735   0.01782   0.01107  -0.0625   0.2247   1.0000
   9.250   1.2888   0.01842   0.01165  -0.0610   0.2192   1.0000
   9.500   1.3058   0.01895   0.01220  -0.0597   0.2140   1.0000
   9.750   1.3215   0.01957   0.01281  -0.0584   0.2077   1.0000
  10.000   1.3356   0.02029   0.01352  -0.0569   0.2023   1.0000
  10.250   1.3517   0.02092   0.01417  -0.0557   0.1963   1.0000
  10.500   1.3653   0.02172   0.01495  -0.0543   0.1903   1.0000
  10.750   1.3796   0.02249   0.01573  -0.0531   0.1854   1.0000
  11.000   1.3931   0.02333   0.01657  -0.0518   0.1791   1.0000
  11.250   1.4047   0.02432   0.01755  -0.0504   0.1733   1.0000
  11.500   1.4176   0.02524   0.01848  -0.0492   0.1666   1.0000
  11.750   1.4274   0.02641   0.01962  -0.0478   0.1602   1.0000
  12.000   1.4404   0.02738   0.02062  -0.0467   0.1555   1.0000
  12.250   1.4504   0.02858   0.02182  -0.0455   0.1494   1.0000
  12.500   1.4608   0.02979   0.02304  -0.0443   0.1458   1.0000
  12.750   1.4726   0.03091   0.02420  -0.0433   0.1415   1.0000
  13.000   1.4829   0.03218   0.02549  -0.0423   0.1378   1.0000
  13.250   1.4913   0.03363   0.02694  -0.0413   0.1339   1.0000
  13.500   1.5016   0.03494   0.02830  -0.0404   0.1301   1.0000
  13.750   1.5119   0.03627   0.02966  -0.0395   0.1273   1.0000
  14.000   1.5198   0.03783   0.03124  -0.0386   0.1237   1.0000
  14.250   1.5270   0.03947   0.03292  -0.0377   0.1213   1.0000
  14.500   1.5362   0.04097   0.03447  -0.0370   0.1191   1.0000
  14.750   1.5454   0.04248   0.03604  -0.0363   0.1169   1.0000
  15.000   1.5534   0.04411   0.03772  -0.0356   0.1143   1.0000
  15.250   1.5589   0.04601   0.03967  -0.0349   0.1113   1.0000
  15.500   1.5623   0.04815   0.04182  -0.0342   0.1076   1.0000
  15.750   1.5701   0.04988   0.04363  -0.0337   0.1058   1.0000
  16.000   1.5767   0.05175   0.04557  -0.0332   0.1037   1.0000
  16.250   1.5807   0.05392   0.04777  -0.0328   0.1006   1.0000
  16.500   1.5830   0.05629   0.05020  -0.0323   0.0983   1.0000
  16.750   1.5860   0.05862   0.05259  -0.0320   0.0958   1.0000
  17.000   1.5897   0.06093   0.05497  -0.0317   0.0919   1.0000
  17.250   1.5892   0.06373   0.05779  -0.0315   0.0879   1.0000
  17.500   1.5890   0.06652   0.06064  -0.0314   0.0834   1.0000
  17.750   1.5860   0.06971   0.06387  -0.0314   0.0784   1.0000
  18.000   1.5772   0.07366   0.06783  -0.0315   0.0700   1.0000
  18.250   1.5616   0.07855   0.07271  -0.0319   0.0607   1.0000
  18.500   1.5376   0.08465   0.07880  -0.0327   0.0492   1.0000
  18.750   1.5108   0.09138   0.08555  -0.0339   0.0398   1.0000
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