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GOE 288 AIRFOIL (goe288-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 288 AIRFOIL (goe288-il)
Reynolds number: 200,000
Max Cl/Cd: 69.44 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe288-il-200000-n5.txt
Download as CSV file: xf-goe288-il-200000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 288 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.5216   0.07535   0.07082  -0.0763   1.0000   0.0388
 -12.750  -0.5858   0.06366   0.05889  -0.0840   1.0000   0.0386
 -12.500  -0.6240   0.05737   0.05249  -0.0869   0.9997   0.0386
 -12.250  -0.6354   0.04926   0.04408  -0.0982   0.9874   0.0387
 -12.000  -0.6363   0.04296   0.03747  -0.1083   0.9713   0.0388
 -11.750  -0.6243   0.03835   0.03253  -0.1166   0.9567   0.0390
 -11.500  -0.6066   0.03579   0.02977  -0.1199   0.9451   0.0392
 -11.250  -0.5833   0.03392   0.02782  -0.1220   0.9356   0.0395
 -11.000  -0.5614   0.03231   0.02611  -0.1234   0.9234   0.0399
 -10.750  -0.5390   0.03085   0.02454  -0.1245   0.9107   0.0402
 -10.500  -0.5156   0.02949   0.02307  -0.1255   0.8977   0.0406
 -10.250  -0.4920   0.02824   0.02168  -0.1262   0.8839   0.0410
 -10.000  -0.4694   0.02711   0.02042  -0.1265   0.8683   0.0415
  -9.750  -0.4462   0.02606   0.01922  -0.1268   0.8529   0.0420
  -9.500  -0.4225   0.02509   0.01810  -0.1269   0.8371   0.0426
  -9.250  -0.3983   0.02421   0.01704  -0.1270   0.8210   0.0433
  -9.000  -0.3738   0.02342   0.01604  -0.1270   0.8043   0.0440
  -8.750  -0.3495   0.02262   0.01514  -0.1269   0.7872   0.0446
  -8.500  -0.3248   0.02191   0.01434  -0.1269   0.7706   0.0453
  -8.250  -0.2995   0.02127   0.01358  -0.1269   0.7543   0.0460
  -8.000  -0.2737   0.02067   0.01286  -0.1269   0.7395   0.0468
  -7.750  -0.2475   0.02011   0.01217  -0.1270   0.7262   0.0476
  -7.250  -0.1940   0.01912   0.01089  -0.1271   0.7026   0.0497
  -7.000  -0.1671   0.01859   0.01028  -0.1273   0.6925   0.0509
  -6.750  -0.1397   0.01814   0.00974  -0.1276   0.6823   0.0525
  -6.500  -0.1120   0.01777   0.00924  -0.1277   0.6735   0.0546
  -6.250  -0.0840   0.01735   0.00876  -0.1280   0.6648   0.0571
  -6.000  -0.0560   0.01699   0.00830  -0.1282   0.6576   0.0605
  -5.750  -0.0274   0.01661   0.00789  -0.1285   0.6508   0.0650
  -5.500   0.0011   0.01627   0.00753  -0.1288   0.6443   0.0721
  -5.250   0.0297   0.01599   0.00721  -0.1290   0.6387   0.0837
  -5.000   0.0586   0.01575   0.00697  -0.1293   0.6329   0.0979
  -4.750   0.0875   0.01555   0.00676  -0.1296   0.6269   0.1114
  -4.500   0.1162   0.01541   0.00655  -0.1298   0.6209   0.1236
  -4.250   0.1452   0.01528   0.00637  -0.1299   0.6149   0.1347
  -4.000   0.1741   0.01511   0.00620  -0.1302   0.6084   0.1455
  -3.750   0.2028   0.01500   0.00603  -0.1303   0.6023   0.1560
  -3.500   0.2317   0.01488   0.00588  -0.1305   0.5965   0.1687
  -3.250   0.2605   0.01469   0.00577  -0.1308   0.5899   0.1897
  -3.000   0.2891   0.01455   0.00569  -0.1310   0.5838   0.2182
  -2.750   0.3179   0.01449   0.00566  -0.1312   0.5783   0.2459
  -2.500   0.3469   0.01445   0.00566  -0.1313   0.5722   0.2683
  -2.250   0.3758   0.01447   0.00565  -0.1314   0.5670   0.2859
  -2.000   0.4046   0.01452   0.00565  -0.1315   0.5624   0.3009
  -1.750   0.4336   0.01456   0.00568  -0.1316   0.5577   0.3141
  -1.500   0.4626   0.01460   0.00570  -0.1317   0.5526   0.3259
  -1.250   0.4914   0.01466   0.00571  -0.1318   0.5480   0.3367
  -1.000   0.5201   0.01473   0.00572  -0.1318   0.5437   0.3455
  -0.750   0.5488   0.01480   0.00575  -0.1319   0.5390   0.3551
  -0.500   0.5774   0.01483   0.00580  -0.1319   0.5335   0.3633
  -0.250   0.6058   0.01490   0.00582  -0.1319   0.5282   0.3716
   0.000   0.6341   0.01499   0.00582  -0.1319   0.5235   0.3795
   0.250   0.6625   0.01502   0.00591  -0.1319   0.5182   0.3876
   0.500   0.6908   0.01510   0.00596  -0.1319   0.5127   0.3978
   0.750   0.7186   0.01517   0.00603  -0.1319   0.5075   0.4083
   1.000   0.7466   0.01524   0.00609  -0.1318   0.5021   0.4171
   1.250   0.7743   0.01527   0.00616  -0.1318   0.4956   0.4235
   1.500   0.8018   0.01534   0.00619  -0.1316   0.4892   0.4301
   1.750   0.8293   0.01541   0.00625  -0.1315   0.4827   0.4360
   2.000   0.8565   0.01546   0.00634  -0.1314   0.4754   0.4424
   2.250   0.8833   0.01556   0.00640  -0.1312   0.4689   0.4498
   2.500   0.9105   0.01563   0.00652  -0.1311   0.4611   0.4568
   2.750   0.9368   0.01572   0.00662  -0.1308   0.4533   0.4640
   3.000   0.9634   0.01584   0.00674  -0.1305   0.4447   0.4728
   3.250   0.9889   0.01595   0.00687  -0.1301   0.4355   0.4822
   3.500   1.0146   0.01608   0.00702  -0.1298   0.4254   0.4931
   3.750   1.0392   0.01624   0.00718  -0.1292   0.4153   0.5049
   4.000   1.0639   0.01640   0.00737  -0.1287   0.4046   0.5193
   4.250   1.0880   0.01659   0.00759  -0.1281   0.3951   0.5387
   4.500   1.1113   0.01679   0.00783  -0.1274   0.3859   0.5656
   4.750   1.1344   0.01696   0.00811  -0.1266   0.3777   0.6062
   5.000   1.1559   0.01705   0.00840  -0.1255   0.3702   0.6933
   5.250   1.1729   0.01689   0.00858  -0.1231   0.3640   1.0000
   5.500   1.1959   0.01726   0.00890  -0.1224   0.3575   1.0000
   5.750   1.2174   0.01768   0.00924  -0.1215   0.3517   1.0000
   6.000   1.2397   0.01807   0.00959  -0.1207   0.3466   1.0000
   6.250   1.2617   0.01846   0.00997  -0.1198   0.3417   1.0000
   6.500   1.2827   0.01890   0.01036  -0.1188   0.3375   1.0000
   6.750   1.3028   0.01938   0.01078  -0.1177   0.3339   1.0000
   7.000   1.3239   0.01979   0.01120  -0.1168   0.3306   1.0000
   7.250   1.3442   0.02020   0.01164  -0.1157   0.3273   1.0000
   7.500   1.3631   0.02065   0.01209  -0.1143   0.3242   1.0000
   7.750   1.3817   0.02114   0.01258  -0.1130   0.3212   1.0000
   8.000   1.3999   0.02168   0.01309  -0.1117   0.3184   1.0000
   8.250   1.4184   0.02227   0.01363  -0.1105   0.3156   1.0000
   8.500   1.4375   0.02276   0.01419  -0.1093   0.3131   1.0000
   8.750   1.4562   0.02329   0.01478  -0.1082   0.3104   1.0000
   9.000   1.4745   0.02385   0.01539  -0.1071   0.3080   1.0000
   9.250   1.4926   0.02445   0.01602  -0.1059   0.3057   1.0000
   9.500   1.5104   0.02508   0.01667  -0.1048   0.3035   1.0000
   9.750   1.5283   0.02572   0.01733  -0.1037   0.3014   1.0000
  10.000   1.5471   0.02638   0.01797  -0.1027   0.2995   1.0000
  10.250   1.5658   0.02704   0.01866  -0.1018   0.2977   1.0000
  10.500   1.5816   0.02776   0.01950  -0.1006   0.2957   1.0000
  10.750   1.5963   0.02854   0.02038  -0.0993   0.2933   1.0000
  11.000   1.6104   0.02937   0.02129  -0.0980   0.2907   1.0000
  11.250   1.6241   0.03023   0.02222  -0.0967   0.2881   1.0000
  11.500   1.6379   0.03111   0.02315  -0.0955   0.2855   1.0000
  11.750   1.6530   0.03197   0.02401  -0.0944   0.2832   1.0000
  12.000   1.6696   0.03280   0.02483  -0.0935   0.2809   1.0000
  12.250   1.6800   0.03392   0.02612  -0.0921   0.2789   1.0000
  12.500   1.6911   0.03506   0.02738  -0.0909   0.2769   1.0000
  12.750   1.7023   0.03621   0.02866  -0.0898   0.2750   1.0000
  13.000   1.7130   0.03743   0.02998  -0.0887   0.2729   1.0000
  13.250   1.7223   0.03873   0.03138  -0.0875   0.2706   1.0000
  13.500   1.7315   0.04004   0.03274  -0.0864   0.2679   1.0000
  13.750   1.7438   0.04113   0.03381  -0.0855   0.2650   1.0000
  14.000   1.7465   0.04303   0.03588  -0.0843   0.2622   1.0000
  14.250   1.7484   0.04509   0.03811  -0.0832   0.2593   1.0000
  14.500   1.7505   0.04716   0.04032  -0.0823   0.2561   1.0000
  14.750   1.7532   0.04923   0.04248  -0.0815   0.2529   1.0000
  15.000   1.7591   0.05098   0.04424  -0.0807   0.2495   1.0000
  15.250   1.7580   0.05362   0.04702  -0.0801   0.2460   1.0000
  15.500   1.7534   0.05675   0.05033  -0.0796   0.2420   1.0000
  15.750   1.7510   0.05969   0.05339  -0.0793   0.2380   1.0000
  16.000   1.7520   0.06222   0.05595  -0.0790   0.2340   1.0000
  16.250   1.7453   0.06587   0.05977  -0.0789   0.2296   1.0000
  16.500   1.7360   0.06993   0.06399  -0.0790   0.2244   1.0000
  16.750   1.7305   0.07348   0.06757  -0.0791   0.2190   1.0000
  17.000   1.7170   0.07829   0.07255  -0.0795   0.2132   1.0000
  17.250   1.7046   0.08299   0.07737  -0.0800   0.2070   1.0000
  17.500   1.6922   0.08777   0.08225  -0.0806   0.2011   1.0000
  17.750   1.6751   0.09331   0.08793  -0.0814   0.1946   1.0000
  18.000   1.6589   0.09877   0.09349  -0.0824   0.1881   1.0000
  18.250   1.6371   0.10522   0.10007  -0.0838   0.1809   1.0000
  18.500   1.6146   0.11184   0.10679  -0.0854   0.1733   1.0000
  18.750   1.5901   0.11890   0.11392  -0.0874   0.1643   1.0000
  19.000   1.5610   0.12690   0.12201  -0.0900   0.1540   1.0000
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