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GOE 796 AIRFOIL (goe796-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 796 AIRFOIL (goe796-il)
Reynolds number: 500,000
Max Cl/Cd: 90.49 at α=5.25°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe796-il-500000-n5.txt
Download as CSV file: xf-goe796-il-500000-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 =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.750  -0.7554   0.06086   0.05793  -0.0665   1.0000   0.0165
 -12.500  -0.8514   0.03908   0.03562  -0.0854   1.0000   0.0159
 -12.250  -0.8592   0.03624   0.03260  -0.0847   0.9968   0.0160
 -12.000  -0.8443   0.03353   0.02968  -0.0870   0.9930   0.0162
 -11.750  -0.8283   0.03126   0.02719  -0.0883   0.9883   0.0164
 -11.500  -0.8086   0.02926   0.02500  -0.0895   0.9846   0.0165
 -11.250  -0.7882   0.02750   0.02304  -0.0903   0.9807   0.0166
 -11.000  -0.7678   0.02597   0.02133  -0.0906   0.9758   0.0167
 -10.750  -0.7446   0.02457   0.01975  -0.0912   0.9722   0.0168
 -10.500  -0.7226   0.02336   0.01839  -0.0913   0.9674   0.0169
 -10.250  -0.7003   0.02227   0.01713  -0.0911   0.9621   0.0170
 -10.000  -0.6761   0.02125   0.01596  -0.0912   0.9580   0.0171
  -9.750  -0.6542   0.02036   0.01495  -0.0907   0.9522   0.0172
  -9.500  -0.6310   0.01953   0.01400  -0.0903   0.9466   0.0173
  -9.250  -0.6071   0.01875   0.01310  -0.0900   0.9416   0.0174
  -9.000  -0.5841   0.01805   0.01229  -0.0894   0.9352   0.0175
  -8.750  -0.5600   0.01738   0.01151  -0.0889   0.9296   0.0176
  -8.500  -0.5359   0.01676   0.01079  -0.0885   0.9234   0.0177
  -8.250  -0.5115   0.01618   0.01012  -0.0880   0.9166   0.0178
  -8.000  -0.4866   0.01564   0.00947  -0.0875   0.9106   0.0179
  -7.750  -0.4615   0.01513   0.00888  -0.0871   0.9032   0.0180
  -7.500  -0.4361   0.01465   0.00831  -0.0867   0.8965   0.0181
  -7.250  -0.4104   0.01421   0.00779  -0.0864   0.8881   0.0182
  -7.000  -0.3845   0.01379   0.00728  -0.0860   0.8806   0.0182
  -6.750  -0.3582   0.01341   0.00682  -0.0857   0.8718   0.0183
  -6.500  -0.3320   0.01300   0.00633  -0.0854   0.8631   0.0186
  -6.250  -0.3057   0.01262   0.00586  -0.0851   0.8532   0.0190
  -6.000  -0.2790   0.01228   0.00544  -0.0849   0.8432   0.0194
  -5.750  -0.2521   0.01198   0.00507  -0.0847   0.8335   0.0198
  -5.500  -0.2251   0.01172   0.00472  -0.0845   0.8228   0.0201
  -5.250  -0.1979   0.01148   0.00440  -0.0843   0.8121   0.0206
  -5.000  -0.1707   0.01126   0.00411  -0.0841   0.8016   0.0211
  -4.750  -0.1434   0.01106   0.00384  -0.0839   0.7916   0.0220
  -4.500  -0.1159   0.01085   0.00358  -0.0838   0.7822   0.0239
  -4.250  -0.0889   0.01058   0.00335  -0.0837   0.7733   0.0338
  -4.000  -0.0613   0.01042   0.00317  -0.0836   0.7642   0.0426
  -3.750  -0.0336   0.01030   0.00301  -0.0835   0.7557   0.0486
  -3.500  -0.0059   0.01019   0.00285  -0.0834   0.7465   0.0522
  -3.250   0.0218   0.01007   0.00271  -0.0834   0.7373   0.0568
  -3.000   0.0494   0.00999   0.00257  -0.0833   0.7289   0.0615
  -2.500   0.1051   0.00976   0.00241  -0.0833   0.7142   0.0843
  -2.250   0.1332   0.00970   0.00234  -0.0833   0.7072   0.0934
  -2.000   0.1613   0.00965   0.00226  -0.0833   0.6999   0.0987
  -1.750   0.1893   0.00959   0.00220  -0.0833   0.6930   0.1062
  -1.500   0.2175   0.00954   0.00214  -0.0833   0.6861   0.1136
  -1.250   0.2453   0.00948   0.00209  -0.0833   0.6795   0.1237
  -1.000   0.2735   0.00942   0.00204  -0.0834   0.6718   0.1309
  -0.750   0.3013   0.00938   0.00199  -0.0833   0.6641   0.1387
  -0.500   0.3294   0.00930   0.00196  -0.0834   0.6568   0.1531
  -0.250   0.3571   0.00921   0.00193  -0.0834   0.6506   0.1781
   0.000   0.3851   0.00910   0.00192  -0.0835   0.6446   0.2107
   0.250   0.4129   0.00900   0.00192  -0.0835   0.6383   0.2489
   0.500   0.4404   0.00886   0.00193  -0.0835   0.6323   0.3024
   0.750   0.4672   0.00858   0.00195  -0.0835   0.6247   0.3993
   1.000   0.4926   0.00821   0.00198  -0.0832   0.6155   0.5438
   1.250   0.5172   0.00790   0.00203  -0.0826   0.6042   0.6704
   1.500   0.5405   0.00759   0.00209  -0.0815   0.5933   0.7904
   1.750   0.5667   0.00742   0.00223  -0.0805   0.5830   0.9249
   2.000   0.6070   0.00752   0.00230  -0.0831   0.5711   0.9730
   2.250   0.6462   0.00764   0.00236  -0.0857   0.5578   0.9911
   2.500   0.6866   0.00779   0.00243  -0.0885   0.5402   1.0000
   2.750   0.7106   0.00795   0.00250  -0.0877   0.5187   1.0000
   3.000   0.7339   0.00817   0.00259  -0.0868   0.4951   1.0000
   3.250   0.7573   0.00838   0.00269  -0.0860   0.4722   1.0000
   3.500   0.7802   0.00864   0.00283  -0.0850   0.4477   1.0000
   3.750   0.8029   0.00892   0.00299  -0.0841   0.4225   1.0000
   4.000   0.8260   0.00921   0.00317  -0.0832   0.4010   1.0000
   4.250   0.8495   0.00947   0.00334  -0.0824   0.3841   1.0000
   4.500   0.8732   0.00973   0.00353  -0.0817   0.3687   1.0000
   4.750   0.8970   0.00999   0.00373  -0.0810   0.3557   1.0000
   5.000   0.9211   0.01023   0.00393  -0.0804   0.3445   1.0000
   5.250   0.9456   0.01045   0.00412  -0.0798   0.3351   1.0000
   5.500   0.9691   0.01074   0.00435  -0.0790   0.3216   1.0000
   5.750   0.9924   0.01104   0.00459  -0.0783   0.3070   1.0000
   6.000   1.0158   0.01134   0.00483  -0.0776   0.2941   1.0000
   6.250   1.0396   0.01159   0.00506  -0.0769   0.2816   1.0000
   6.500   1.0632   0.01187   0.00531  -0.0763   0.2679   1.0000
   6.750   1.0854   0.01222   0.00558  -0.0754   0.2478   1.0000
   7.000   1.1038   0.01283   0.00596  -0.0740   0.2055   1.0000
   7.250   1.1210   0.01350   0.00644  -0.0723   0.1752   1.0000
   7.500   1.1407   0.01400   0.00687  -0.0711   0.1614   1.0000
   7.750   1.1610   0.01443   0.00728  -0.0699   0.1519   1.0000
   8.000   1.1819   0.01481   0.00765  -0.0689   0.1438   1.0000
   8.250   1.2015   0.01525   0.00806  -0.0676   0.1356   1.0000
   8.500   1.2220   0.01560   0.00844  -0.0665   0.1288   1.0000
   8.750   1.2394   0.01606   0.00887  -0.0648   0.1194   1.0000
   9.000   1.2556   0.01657   0.00934  -0.0630   0.1069   1.0000
   9.250   1.2704   0.01718   0.00987  -0.0611   0.0926   1.0000
   9.500   1.2847   0.01784   0.01047  -0.0592   0.0816   1.0000
   9.750   1.3006   0.01842   0.01107  -0.0575   0.0748   1.0000
  10.000   1.3157   0.01907   0.01172  -0.0558   0.0686   1.0000
  10.250   1.3309   0.01973   0.01238  -0.0542   0.0632   1.0000
  10.500   1.3453   0.02044   0.01311  -0.0525   0.0585   1.0000
  10.750   1.3602   0.02115   0.01384  -0.0510   0.0539   1.0000
  11.000   1.3732   0.02199   0.01470  -0.0493   0.0490   1.0000
  11.250   1.3867   0.02282   0.01555  -0.0477   0.0436   1.0000
  11.500   1.3975   0.02386   0.01658  -0.0460   0.0366   1.0000
  11.750   1.4060   0.02509   0.01777  -0.0441   0.0287   1.0000
  12.000   1.4140   0.02639   0.01907  -0.0423   0.0237   1.0000
  12.250   1.4229   0.02768   0.02039  -0.0407   0.0208   1.0000
  12.500   1.4312   0.02905   0.02181  -0.0391   0.0187   1.0000
  12.750   1.4399   0.03043   0.02325  -0.0378   0.0173   1.0000
  13.000   1.4489   0.03183   0.02472  -0.0365   0.0162   1.0000
  13.250   1.4561   0.03341   0.02636  -0.0352   0.0151   1.0000
  13.500   1.4618   0.03517   0.02819  -0.0340   0.0142   1.0000
  13.750   1.4697   0.03679   0.02989  -0.0330   0.0135   1.0000
  14.000   1.4766   0.03853   0.03173  -0.0321   0.0128   1.0000
  14.250   1.4820   0.04044   0.03373  -0.0312   0.0122   1.0000
  14.500   1.4859   0.04255   0.03592  -0.0304   0.0116   1.0000
  14.750   1.4884   0.04487   0.03831  -0.0296   0.0111   1.0000
  15.000   1.4925   0.04708   0.04061  -0.0291   0.0106   1.0000
  15.250   1.4955   0.04946   0.04309  -0.0286   0.0101   1.0000
  15.500   1.4974   0.05202   0.04575  -0.0282   0.0097   1.0000
  15.750   1.4981   0.05479   0.04860  -0.0280   0.0093   1.0000
  16.000   1.4974   0.05779   0.05168  -0.0278   0.0089   1.0000
  16.250   1.4953   0.06104   0.05502  -0.0279   0.0086   1.0000
  16.500   1.4928   0.06443   0.05853  -0.0280   0.0084   1.0000
  16.750   1.4893   0.06805   0.06226  -0.0284   0.0082   1.0000
  17.000   1.4847   0.07189   0.06621  -0.0289   0.0080   1.0000
  17.250   1.4786   0.07605   0.07047  -0.0296   0.0078   1.0000
  17.500   1.4713   0.08049   0.07503  -0.0306   0.0076   1.0000
  17.750   1.4630   0.08519   0.07984  -0.0318   0.0075   1.0000
  18.000   1.4530   0.09024   0.08501  -0.0332   0.0074   1.0000
  18.250   1.4423   0.09549   0.09037  -0.0348   0.0073   1.0000
  18.500   1.4303   0.10107   0.09608  -0.0367   0.0072   1.0000
  18.750   1.4175   0.10688   0.10201  -0.0388   0.0070   1.0000
  19.000   1.4039   0.11290   0.10815  -0.0411   0.0070   1.0000
  19.250   1.3895   0.11913   0.11450  -0.0437   0.0069   1.0000
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