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GOE 796 AIRFOIL (goe796-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 796 AIRFOIL (goe796-il)
Reynolds number: 1,000,000
Max Cl/Cd: 105.19 at α=4.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe796-il-1000000-n5.txt
Download as CSV file: xf-goe796-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 796 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
  ------ -------- --------- --------- -------- -------- --------
 -14.500  -0.7184   0.09505   0.09285  -0.0435   1.0000   0.0126
 -14.250  -0.7933   0.07833   0.07598  -0.0538   1.0000   0.0125
 -14.000  -0.9955   0.03555   0.03243  -0.0901   1.0000   0.0118
 -13.750  -1.0103   0.03312   0.02988  -0.0876   0.9999   0.0118
 -13.500  -0.9952   0.03086   0.02748  -0.0893   0.9950   0.0120
 -13.250  -0.9776   0.02911   0.02561  -0.0903   0.9899   0.0121
 -13.000  -0.9582   0.02761   0.02400  -0.0910   0.9853   0.0122
 -12.750  -0.9381   0.02629   0.02257  -0.0915   0.9810   0.0123
 -12.500  -0.9188   0.02509   0.02127  -0.0914   0.9755   0.0124
 -12.000  -0.8789   0.02298   0.01894  -0.0909   0.9651   0.0127
 -11.750  -0.8587   0.02205   0.01790  -0.0904   0.9598   0.0128
 -11.500  -0.8380   0.02120   0.01694  -0.0899   0.9547   0.0129
 -11.250  -0.8166   0.02044   0.01609  -0.0893   0.9491   0.0131
 -11.000  -0.7947   0.01974   0.01529  -0.0887   0.9440   0.0133
 -10.750  -0.7721   0.01905   0.01451  -0.0882   0.9390   0.0134
 -10.500  -0.7492   0.01841   0.01377  -0.0878   0.9332   0.0136
 -10.250  -0.7259   0.01782   0.01309  -0.0872   0.9279   0.0138
 -10.000  -0.7018   0.01723   0.01241  -0.0869   0.9227   0.0139
  -9.750  -0.6775   0.01670   0.01180  -0.0865   0.9166   0.0141
  -9.500  -0.6529   0.01622   0.01123  -0.0861   0.9109   0.0142
  -9.250  -0.6282   0.01566   0.01058  -0.0858   0.9043   0.0143
  -9.000  -0.6034   0.01514   0.00997  -0.0854   0.8977   0.0143
  -8.750  -0.5780   0.01465   0.00940  -0.0851   0.8909   0.0144
  -8.500  -0.5526   0.01419   0.00885  -0.0848   0.8830   0.0144
  -8.250  -0.5268   0.01375   0.00833  -0.0845   0.8749   0.0144
  -8.000  -0.5009   0.01335   0.00783  -0.0842   0.8664   0.0145
  -7.750  -0.4746   0.01295   0.00736  -0.0840   0.8571   0.0145
  -7.500  -0.4483   0.01259   0.00692  -0.0838   0.8471   0.0145
  -7.250  -0.4223   0.01217   0.00640  -0.0835   0.8357   0.0146
  -7.000  -0.3959   0.01178   0.00592  -0.0833   0.8236   0.0147
  -6.750  -0.3692   0.01144   0.00549  -0.0831   0.8118   0.0148
  -6.500  -0.3423   0.01114   0.00510  -0.0829   0.7998   0.0149
  -6.250  -0.3154   0.01087   0.00474  -0.0828   0.7876   0.0150
  -6.000  -0.2882   0.01062   0.00441  -0.0826   0.7757   0.0151
  -5.750  -0.2607   0.01039   0.00411  -0.0825   0.7654   0.0153
  -5.500  -0.2332   0.01018   0.00383  -0.0825   0.7565   0.0154
  -5.250  -0.2055   0.00997   0.00357  -0.0824   0.7476   0.0156
  -5.000  -0.1777   0.00979   0.00333  -0.0824   0.7395   0.0159
  -4.750  -0.1499   0.00963   0.00312  -0.0824   0.7308   0.0162
  -4.500  -0.1219   0.00948   0.00292  -0.0824   0.7226   0.0164
  -4.250  -0.0940   0.00936   0.00274  -0.0823   0.7136   0.0166
  -4.000  -0.0658   0.00923   0.00257  -0.0824   0.7061   0.0169
  -3.750  -0.0377   0.00912   0.00241  -0.0824   0.6992   0.0174
  -3.500  -0.0093   0.00901   0.00228  -0.0824   0.6933   0.0178
  -3.250   0.0190   0.00890   0.00214  -0.0825   0.6860   0.0192
  -3.000   0.0467   0.00869   0.00198  -0.0825   0.6794   0.0313
  -2.750   0.0750   0.00854   0.00187  -0.0826   0.6736   0.0427
  -2.500   0.1033   0.00846   0.00178  -0.0826   0.6672   0.0481
  -2.250   0.1318   0.00838   0.00170  -0.0827   0.6613   0.0529
  -2.000   0.1601   0.00830   0.00163  -0.0828   0.6542   0.0580
  -1.750   0.1883   0.00822   0.00156  -0.0829   0.6468   0.0684
  -1.500   0.2165   0.00811   0.00153  -0.0829   0.6383   0.0873
  -1.250   0.2449   0.00809   0.00150  -0.0830   0.6311   0.0948
  -1.000   0.2736   0.00806   0.00146  -0.0832   0.6248   0.0989
  -0.500   0.3306   0.00799   0.00141  -0.0834   0.6132   0.1106
  -0.250   0.3590   0.00795   0.00139  -0.0835   0.6063   0.1202
   0.000   0.3872   0.00794   0.00138  -0.0835   0.5963   0.1273
   0.250   0.4151   0.00794   0.00137  -0.0836   0.5828   0.1391
   0.500   0.4428   0.00791   0.00138  -0.0836   0.5701   0.1624
   0.750   0.4706   0.00786   0.00139  -0.0836   0.5590   0.1962
   1.000   0.4985   0.00782   0.00141  -0.0837   0.5481   0.2299
   1.250   0.5260   0.00778   0.00145  -0.0837   0.5355   0.2714
   1.750   0.5788   0.00755   0.00157  -0.0834   0.4970   0.4509
   2.000   0.6045   0.00750   0.00167  -0.0832   0.4719   0.5421
   2.250   0.6288   0.00739   0.00179  -0.0827   0.4441   0.6663
   2.500   0.6521   0.00734   0.00194  -0.0818   0.4149   0.7780
   2.750   0.6711   0.00719   0.00213  -0.0797   0.3927   0.9270
   3.000   0.7055   0.00741   0.00229  -0.0811   0.3718   0.9783
   3.250   0.7464   0.00765   0.00244  -0.0841   0.3551   0.9956
   3.750   0.8076   0.00797   0.00267  -0.0856   0.3354   1.0000
   4.250   0.8568   0.00829   0.00291  -0.0843   0.3178   1.0000
   4.500   0.8816   0.00847   0.00304  -0.0838   0.3105   1.0000
   4.750   0.9067   0.00862   0.00317  -0.0833   0.3014   1.0000
   5.000   0.9310   0.00886   0.00333  -0.0826   0.2858   1.0000
   5.250   0.9548   0.00913   0.00351  -0.0820   0.2673   1.0000
   5.500   0.9781   0.00945   0.00371  -0.0812   0.2422   1.0000
   5.750   0.9971   0.01009   0.00406  -0.0798   0.1915   1.0000
   6.250   1.0416   0.01088   0.00465  -0.0780   0.1550   1.0000
   6.500   1.0656   0.01115   0.00490  -0.0774   0.1477   1.0000
   6.750   1.0900   0.01138   0.00512  -0.0769   0.1422   1.0000
   7.000   1.1135   0.01167   0.00537  -0.0762   0.1350   1.0000
   7.250   1.1374   0.01192   0.00561  -0.0756   0.1278   1.0000
   7.500   1.1600   0.01226   0.00590  -0.0748   0.1180   1.0000
   7.750   1.1817   0.01264   0.00621  -0.0739   0.1048   1.0000
   8.000   1.2018   0.01313   0.00659  -0.0727   0.0880   1.0000
   8.250   1.2218   0.01359   0.00699  -0.0716   0.0761   1.0000
   8.500   1.2422   0.01401   0.00738  -0.0704   0.0685   1.0000
   8.750   1.2625   0.01440   0.00775  -0.0693   0.0626   1.0000
   9.000   1.2818   0.01482   0.00815  -0.0680   0.0568   1.0000
   9.250   1.2992   0.01525   0.00856  -0.0663   0.0515   1.0000
   9.500   1.3167   0.01567   0.00899  -0.0647   0.0476   1.0000
   9.750   1.3326   0.01620   0.00949  -0.0629   0.0414   1.0000
  10.000   1.3472   0.01682   0.01007  -0.0609   0.0335   1.0000
  10.250   1.3592   0.01761   0.01080  -0.0587   0.0236   1.0000
  10.500   1.3730   0.01833   0.01150  -0.0568   0.0193   1.0000
  10.750   1.3881   0.01898   0.01217  -0.0552   0.0171   1.0000
  11.000   1.4035   0.01962   0.01284  -0.0536   0.0158   1.0000
  11.250   1.4179   0.02034   0.01359  -0.0520   0.0146   1.0000
  11.500   1.4330   0.02104   0.01432  -0.0506   0.0138   1.0000
  11.750   1.4479   0.02175   0.01507  -0.0492   0.0129   1.0000
  12.000   1.4615   0.02257   0.01593  -0.0477   0.0119   1.0000
  12.250   1.4742   0.02348   0.01687  -0.0462   0.0109   1.0000
  12.500   1.4872   0.02438   0.01781  -0.0448   0.0099   1.0000
  12.750   1.4988   0.02541   0.01887  -0.0434   0.0088   1.0000
  13.000   1.5096   0.02654   0.02002  -0.0420   0.0083   1.0000
  13.250   1.5198   0.02773   0.02125  -0.0406   0.0079   1.0000
  13.500   1.5295   0.02899   0.02256  -0.0393   0.0077   1.0000
  13.750   1.5386   0.03036   0.02398  -0.0380   0.0074   1.0000
  14.000   1.5468   0.03182   0.02550  -0.0368   0.0071   1.0000
  14.250   1.5543   0.03338   0.02713  -0.0357   0.0069   1.0000
  14.500   1.5611   0.03505   0.02886  -0.0346   0.0067   1.0000
  14.750   1.5686   0.03671   0.03059  -0.0337   0.0066   1.0000
  15.000   1.5750   0.03848   0.03244  -0.0328   0.0065   1.0000
  15.250   1.5805   0.04039   0.03442  -0.0320   0.0063   1.0000
  15.500   1.5852   0.04244   0.03656  -0.0312   0.0062   1.0000
  15.750   1.5889   0.04465   0.03885  -0.0306   0.0060   1.0000
  16.000   1.5915   0.04701   0.04129  -0.0300   0.0058   1.0000
  16.250   1.5931   0.04954   0.04391  -0.0296   0.0057   1.0000
  16.500   1.5934   0.05229   0.04674  -0.0292   0.0055   1.0000
  16.750   1.5924   0.05527   0.04981  -0.0290   0.0054   1.0000
  17.000   1.5899   0.05847   0.05310  -0.0289   0.0052   1.0000
  17.250   1.5853   0.06202   0.05674  -0.0290   0.0051   1.0000
  17.500   1.5790   0.06593   0.06075  -0.0293   0.0050   1.0000
  17.750   1.5765   0.06941   0.06433  -0.0297   0.0049   1.0000
  18.000   1.5732   0.07306   0.06808  -0.0302   0.0048   1.0000
  18.250   1.5679   0.07706   0.07219  -0.0309   0.0048   1.0000
  18.500   1.5617   0.08128   0.07650  -0.0318   0.0047   1.0000
  18.750   1.5542   0.08577   0.08111  -0.0329   0.0046   1.0000
  19.000   1.5451   0.09058   0.08603  -0.0342   0.0045   1.0000
  19.250   1.5352   0.09557   0.09112  -0.0356   0.0044   1.0000
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