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GOE 493 AIRFOIL (goe493-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 493 AIRFOIL (goe493-il)
Reynolds number: 1,000,000
Max Cl/Cd: 98.85 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe493-il-1000000-n5.txt
Download as CSV file: xf-goe493-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 493 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
  ------ -------- --------- --------- -------- -------- --------
 -17.500  -0.8436   0.08694   0.08389  -0.0737   1.0000   0.0074
 -17.250  -0.8800   0.07791   0.07473  -0.0782   1.0000   0.0073
 -17.000  -0.9182   0.06895   0.06562  -0.0827   1.0000   0.0073
 -16.750  -0.9487   0.06151   0.05805  -0.0863   1.0000   0.0073
 -16.500  -0.9707   0.05556   0.05199  -0.0891   1.0000   0.0074
 -16.250  -0.9965   0.04943   0.04572  -0.0918   1.0000   0.0073
 -16.000  -1.0156   0.04456   0.04074  -0.0936   1.0000   0.0073
 -15.500  -1.0244   0.03628   0.03223  -0.0998   0.9986   0.0075
 -15.250  -1.0148   0.03300   0.02883  -0.1038   0.9962   0.0076
 -15.000  -1.0064   0.03010   0.02582  -0.1068   0.9916   0.0076
 -14.750  -0.9937   0.02776   0.02339  -0.1096   0.9873   0.0078
 -14.500  -0.9781   0.02576   0.02128  -0.1122   0.9836   0.0079
 -14.250  -0.9645   0.02419   0.01962  -0.1134   0.9770   0.0080
 -14.000  -0.9440   0.02271   0.01805  -0.1156   0.9731   0.0081
 -13.750  -0.9271   0.02125   0.01649  -0.1170   0.9662   0.0084
 -13.500  -0.9004   0.02011   0.01526  -0.1193   0.9624   0.0087
 -13.250  -0.8728   0.01916   0.01425  -0.1212   0.9579   0.0090
 -13.000  -0.8466   0.01837   0.01339  -0.1224   0.9514   0.0094
 -12.750  -0.8192   0.01763   0.01257  -0.1238   0.9454   0.0097
 -12.500  -0.7976   0.01707   0.01193  -0.1236   0.9366   0.0100
 -12.250  -0.7743   0.01652   0.01129  -0.1237   0.9293   0.0103
 -12.000  -0.7549   0.01605   0.01076  -0.1228   0.9208   0.0106
 -11.750  -0.7359   0.01551   0.01013  -0.1219   0.9133   0.0111
 -11.500  -0.7179   0.01505   0.00962  -0.1206   0.9056   0.0115
 -11.000  -0.6782   0.01425   0.00869  -0.1186   0.8924   0.0125
 -10.750  -0.6573   0.01390   0.00827  -0.1176   0.8861   0.0130
 -10.500  -0.6358   0.01357   0.00788  -0.1168   0.8806   0.0135
 -10.250  -0.6153   0.01318   0.00744  -0.1157   0.8746   0.0144
 -10.000  -0.5936   0.01284   0.00705  -0.1149   0.8689   0.0154
  -9.750  -0.5712   0.01253   0.00670  -0.1141   0.8638   0.0165
  -9.500  -0.5490   0.01220   0.00634  -0.1133   0.8581   0.0181
  -9.250  -0.5263   0.01190   0.00600  -0.1125   0.8527   0.0198
  -9.000  -0.5032   0.01159   0.00567  -0.1119   0.8477   0.0222
  -8.750  -0.4799   0.01131   0.00536  -0.1112   0.8420   0.0253
  -8.500  -0.4567   0.01101   0.00505  -0.1105   0.8366   0.0292
  -8.250  -0.4332   0.01072   0.00476  -0.1099   0.8314   0.0336
  -8.000  -0.4093   0.01045   0.00448  -0.1093   0.8259   0.0386
  -7.750  -0.3853   0.01021   0.00422  -0.1087   0.8205   0.0444
  -7.500  -0.3609   0.00995   0.00397  -0.1082   0.8154   0.0513
  -7.250  -0.3366   0.00970   0.00375  -0.1076   0.8097   0.0597
  -7.000  -0.3121   0.00948   0.00353  -0.1071   0.8042   0.0681
  -6.750  -0.2867   0.00929   0.00335  -0.1068   0.7989   0.0752
  -6.500  -0.2612   0.00913   0.00318  -0.1064   0.7931   0.0821
  -6.250  -0.2360   0.00897   0.00302  -0.1059   0.7874   0.0890
  -6.000  -0.2099   0.00883   0.00287  -0.1057   0.7819   0.0960
  -5.750  -0.1845   0.00867   0.00272  -0.1053   0.7756   0.1039
  -5.500  -0.1584   0.00856   0.00259  -0.1049   0.7697   0.1091
  -5.250  -0.1323   0.00844   0.00246  -0.1046   0.7633   0.1153
  -5.000  -0.1066   0.00833   0.00234  -0.1043   0.7572   0.1221
  -4.750  -0.0805   0.00820   0.00222  -0.1040   0.7511   0.1315
  -4.250  -0.0289   0.00798   0.00200  -0.1032   0.7375   0.1518
  -4.000  -0.0029   0.00787   0.00190  -0.1029   0.7303   0.1633
  -3.750   0.0229   0.00778   0.00182  -0.1025   0.7238   0.1742
  -3.500   0.0490   0.00767   0.00174  -0.1022   0.7167   0.1887
  -3.000   0.1005   0.00749   0.00159  -0.1015   0.7017   0.2192
  -2.750   0.1259   0.00742   0.00153  -0.1010   0.6941   0.2356
  -2.500   0.1518   0.00731   0.00147  -0.1006   0.6866   0.2554
  -2.000   0.2019   0.00716   0.00138  -0.0996   0.6673   0.3019
  -1.750   0.2268   0.00711   0.00135  -0.0990   0.6572   0.3227
  -1.500   0.2519   0.00707   0.00134  -0.0985   0.6477   0.3431
  -1.250   0.2774   0.00703   0.00132  -0.0980   0.6386   0.3651
  -1.000   0.3021   0.00701   0.00133  -0.0974   0.6295   0.3857
  -0.750   0.3281   0.00699   0.00133  -0.0971   0.6211   0.4026
  -0.500   0.3530   0.00700   0.00134  -0.0965   0.6115   0.4191
  -0.250   0.3781   0.00701   0.00136  -0.0960   0.6011   0.4365
   0.000   0.4032   0.00701   0.00139  -0.0954   0.5918   0.4574
   0.250   0.4282   0.00702   0.00142  -0.0949   0.5838   0.4766
   0.500   0.4541   0.00703   0.00146  -0.0945   0.5778   0.4913
   0.750   0.4799   0.00705   0.00149  -0.0941   0.5711   0.5037
   1.000   0.5051   0.00708   0.00154  -0.0935   0.5649   0.5162
   1.250   0.5311   0.00711   0.00158  -0.0932   0.5584   0.5286
   1.500   0.5556   0.00715   0.00164  -0.0925   0.5507   0.5426
   1.750   0.5811   0.00717   0.00169  -0.0920   0.5442   0.5583
   2.000   0.6058   0.00721   0.00176  -0.0914   0.5370   0.5727
   2.250   0.6306   0.00725   0.00182  -0.0908   0.5306   0.5859
   2.500   0.6554   0.00729   0.00189  -0.0902   0.5232   0.5987
   2.750   0.6776   0.00741   0.00198  -0.0891   0.5075   0.6119
   3.000   0.7007   0.00748   0.00207  -0.0882   0.4978   0.6274
   3.250   0.7233   0.00755   0.00217  -0.0871   0.4875   0.6439
   3.750   0.7651   0.00774   0.00240  -0.0844   0.4583   0.6869
   4.000   0.7799   0.00795   0.00255  -0.0818   0.4300   0.7110
   4.250   0.7947   0.00815   0.00272  -0.0792   0.4049   0.7389
   4.750   0.8247   0.00863   0.00315  -0.0741   0.3582   0.7911
   5.000   0.8404   0.00883   0.00337  -0.0717   0.3404   0.8195
   5.250   0.8554   0.00900   0.00359  -0.0692   0.3245   0.8576
   5.500   0.8979   0.00928   0.00398  -0.0728   0.3003   0.9419
   5.750   0.9542   0.00981   0.00439  -0.0798   0.2721   1.0000
   6.000   0.9682   0.01017   0.00465  -0.0772   0.2513   1.0000
   6.250   0.9800   0.01065   0.00497  -0.0743   0.2198   1.0000
   6.500   0.9798   0.01163   0.00562  -0.0695   0.1583   1.0000
   6.750   0.9898   0.01226   0.00611  -0.0665   0.1296   1.0000
   7.000   0.9967   0.01307   0.00671  -0.0631   0.0906   1.0000
   7.250   1.0103   0.01362   0.00717  -0.0609   0.0735   1.0000
   7.500   1.0243   0.01418   0.00765  -0.0589   0.0589   1.0000
   7.750   1.0379   0.01478   0.00817  -0.0568   0.0441   1.0000
   8.000   1.0531   0.01532   0.00868  -0.0550   0.0372   1.0000
   8.250   1.0702   0.01579   0.00914  -0.0536   0.0344   1.0000
   8.500   1.0876   0.01625   0.00961  -0.0522   0.0329   1.0000
   8.750   1.1047   0.01674   0.01011  -0.0509   0.0315   1.0000
   9.000   1.1210   0.01729   0.01067  -0.0494   0.0303   1.0000
   9.250   1.1372   0.01786   0.01126  -0.0480   0.0292   1.0000
   9.500   1.1533   0.01846   0.01187  -0.0467   0.0282   1.0000
   9.750   1.1703   0.01902   0.01246  -0.0455   0.0276   1.0000
  10.000   1.1866   0.01962   0.01310  -0.0443   0.0270   1.0000
  10.250   1.2025   0.02027   0.01377  -0.0431   0.0263   1.0000
  10.500   1.2177   0.02098   0.01451  -0.0418   0.0256   1.0000
  10.750   1.2323   0.02173   0.01528  -0.0406   0.0249   1.0000
  11.000   1.2458   0.02257   0.01615  -0.0393   0.0241   1.0000
  11.250   1.2584   0.02350   0.01711  -0.0379   0.0234   1.0000
  11.500   1.2718   0.02439   0.01804  -0.0367   0.0229   1.0000
  11.750   1.2867   0.02520   0.01888  -0.0357   0.0224   1.0000
  12.000   1.3012   0.02604   0.01976  -0.0347   0.0217   1.0000
  12.250   1.3138   0.02704   0.02080  -0.0336   0.0213   1.0000
  12.500   1.3269   0.02802   0.02181  -0.0326   0.0205   1.0000
  12.750   1.3388   0.02912   0.02295  -0.0315   0.0199   1.0000
  13.000   1.3500   0.03028   0.02415  -0.0305   0.0194   1.0000
  13.250   1.3594   0.03162   0.02551  -0.0294   0.0188   1.0000
  13.500   1.3707   0.03283   0.02677  -0.0285   0.0182   1.0000
  13.750   1.3823   0.03404   0.02803  -0.0277   0.0177   1.0000
  14.000   1.3923   0.03543   0.02948  -0.0268   0.0172   1.0000
  14.250   1.4019   0.03686   0.03095  -0.0260   0.0165   1.0000
  14.500   1.4111   0.03835   0.03248  -0.0252   0.0160   1.0000
  14.750   1.4192   0.03997   0.03412  -0.0245   0.0151   1.0000
  15.000   1.4268   0.04168   0.03588  -0.0238   0.0146   1.0000
  15.250   1.4342   0.04343   0.03769  -0.0232   0.0141   1.0000
  15.500   1.4411   0.04526   0.03958  -0.0226   0.0136   1.0000
  15.750   1.4472   0.04720   0.04157  -0.0220   0.0130   1.0000
  16.000   1.4524   0.04926   0.04366  -0.0216   0.0124   1.0000
  16.250   1.4569   0.05142   0.04587  -0.0211   0.0118   1.0000
  16.500   1.4611   0.05367   0.04818  -0.0208   0.0114   1.0000
  16.750   1.4643   0.05606   0.05064  -0.0205   0.0110   1.0000
  17.000   1.4671   0.05850   0.05314  -0.0202   0.0107   1.0000
  17.250   1.4691   0.06106   0.05576  -0.0201   0.0102   1.0000
  17.500   1.4700   0.06379   0.05855  -0.0200   0.0098   1.0000
  17.750   1.4700   0.06668   0.06150  -0.0200   0.0094   1.0000
  18.000   1.4696   0.06965   0.06454  -0.0200   0.0091   1.0000
  18.250   1.4692   0.07263   0.06760  -0.0202   0.0089   1.0000
  18.500   1.4682   0.07573   0.07078  -0.0204   0.0087   1.0000
  18.750   1.4662   0.07900   0.07412  -0.0207   0.0084   1.0000
  19.000   1.4633   0.08242   0.07763  -0.0211   0.0082   1.0000
  19.250   1.4598   0.08596   0.08125  -0.0217   0.0080   1.0000
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