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GOE 407 AIRFOIL (goe407-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 407 AIRFOIL (goe407-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.09 at α=5.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe407-il-1000000-n5.txt
Download as CSV file: xf-goe407-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 407 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
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.2790   0.10334   0.10154  -0.0495   0.9890   0.0118
 -10.250  -0.2708   0.09968   0.09788  -0.0520   0.9876   0.0120
 -10.000  -0.2718   0.09318   0.09138  -0.0563   0.9860   0.0132
  -9.750  -0.2560   0.09105   0.08925  -0.0587   0.9848   0.0133
  -9.500  -0.2482   0.08812   0.08633  -0.0605   0.9819   0.0134
  -9.250  -0.2376   0.08588   0.08410  -0.0619   0.9788   0.0137
  -9.000  -0.2272   0.08287   0.08109  -0.0645   0.9760   0.0139
  -8.750  -0.2157   0.07957   0.07779  -0.0677   0.9735   0.0142
  -8.500  -0.2120   0.07641   0.07464  -0.0696   0.9676   0.0143
  -8.250  -0.2024   0.07252   0.07074  -0.0740   0.9618   0.0148
  -8.000  -0.2073   0.06411   0.06229  -0.0834   0.9497   0.0160
  -7.750  -0.1822   0.06118   0.05932  -0.0885   0.9409   0.0162
  -7.500  -0.1425   0.05686   0.05492  -0.0983   0.9245   0.0164
  -7.250  -0.0880   0.05200   0.04968  -0.1114   0.8515   0.0167
  -7.000  -0.0819   0.04995   0.04738  -0.1109   0.8100   0.0170
  -6.750  -0.0769   0.04691   0.04419  -0.1107   0.7906   0.0172
  -6.500  -0.0683   0.04417   0.04132  -0.1104   0.7753   0.0177
  -5.750  -0.0679   0.02670   0.02296  -0.1043   0.7377   0.0195
  -5.500  -0.0515   0.02522   0.02132  -0.1027   0.7257   0.0197
  -5.250  -0.0360   0.02348   0.01939  -0.1008   0.7125   0.0199
  -5.000  -0.0230   0.02110   0.01676  -0.0983   0.6978   0.0202
  -4.750  -0.0152   0.01754   0.01273  -0.0946   0.6835   0.0206
  -4.500   0.0006   0.01584   0.01069  -0.0923   0.6695   0.0210
  -4.250   0.0191   0.01461   0.00918  -0.0904   0.6566   0.0212
  -4.000   0.0396   0.01369   0.00802  -0.0888   0.6459   0.0214
  -3.750   0.0619   0.01294   0.00707  -0.0876   0.6367   0.0216
  -3.500   0.0849   0.01233   0.00631  -0.0865   0.6292   0.0218
  -3.250   0.1093   0.01188   0.00573  -0.0857   0.6228   0.0221
  -3.000   0.1337   0.01151   0.00525  -0.0848   0.6173   0.0224
  -2.750   0.1586   0.01112   0.00477  -0.0841   0.6121   0.0225
  -2.500   0.1839   0.01081   0.00439  -0.0834   0.6069   0.0227
  -2.250   0.2089   0.01052   0.00402  -0.0827   0.6017   0.0228
  -2.000   0.2343   0.01036   0.00381  -0.0821   0.5966   0.0230
  -1.750   0.2591   0.00992   0.00332  -0.0813   0.5910   0.0233
  -1.500   0.2834   0.00964   0.00299  -0.0805   0.5843   0.0235
  -1.250   0.3083   0.00943   0.00276  -0.0798   0.5785   0.0238
  -1.000   0.3334   0.00925   0.00257  -0.0791   0.5723   0.0241
  -0.750   0.3580   0.00913   0.00242  -0.0783   0.5652   0.0243
  -0.500   0.3833   0.00900   0.00228  -0.0776   0.5589   0.0246
  -0.250   0.4080   0.00889   0.00214  -0.0768   0.5516   0.0249
   0.000   0.4329   0.00879   0.00202  -0.0761   0.5439   0.0251
   0.250   0.4570   0.00872   0.00192  -0.0752   0.5323   0.0255
   0.500   0.4812   0.00869   0.00184  -0.0743   0.5186   0.0259
   0.750   0.5048   0.00869   0.00178  -0.0734   0.4997   0.0264
   1.000   0.5279   0.00873   0.00174  -0.0723   0.4776   0.0268
   1.250   0.5503   0.00882   0.00173  -0.0711   0.4546   0.0272
   1.500   0.5719   0.00898   0.00176  -0.0697   0.4252   0.0275
   1.750   0.5944   0.00909   0.00178  -0.0686   0.4048   0.0278
   2.000   0.6175   0.00914   0.00177  -0.0675   0.3909   0.0289
   2.250   0.6410   0.00921   0.00180  -0.0666   0.3777   0.0296
   2.500   0.6645   0.00929   0.00184  -0.0656   0.3650   0.0304
   2.750   0.6879   0.00938   0.00189  -0.0647   0.3530   0.0317
   3.000   0.7113   0.00948   0.00195  -0.0637   0.3430   0.0329
   3.250   0.7350   0.00954   0.00201  -0.0628   0.3339   0.0376
   3.500   0.7575   0.00960   0.00212  -0.0617   0.3233   0.0754
   4.000   0.8025   0.00971   0.00234  -0.0595   0.3042   0.1663
   4.500   1.0285   0.00923   0.00349  -0.0994   0.2730   0.9984
   4.750   1.0651   0.00941   0.00360  -0.1016   0.2628   1.0000
   5.000   1.0875   0.00957   0.00374  -0.1005   0.2546   1.0000
   5.250   1.1094   0.00976   0.00390  -0.0993   0.2475   1.0000
   5.500   1.1318   0.00992   0.00404  -0.0982   0.2407   1.0000
   5.750   1.1529   0.01014   0.00422  -0.0969   0.2316   1.0000
   6.000   1.1744   0.01033   0.00440  -0.0957   0.2234   1.0000
   6.250   1.1937   0.01064   0.00462  -0.0940   0.2073   1.0000
   6.500   1.2128   0.01095   0.00486  -0.0924   0.1916   1.0000
   6.750   1.2259   0.01156   0.00526  -0.0896   0.1525   1.0000
   7.000   1.2361   0.01232   0.00580  -0.0864   0.1165   1.0000
   7.250   1.2538   0.01266   0.00611  -0.0844   0.1091   1.0000
   7.500   1.2718   0.01297   0.00640  -0.0826   0.1026   1.0000
   7.750   1.2900   0.01325   0.00668  -0.0808   0.0982   1.0000
   8.000   1.3069   0.01358   0.00700  -0.0788   0.0932   1.0000
   8.250   1.3244   0.01386   0.00729  -0.0768   0.0890   1.0000
   8.500   1.3418   0.01412   0.00757  -0.0749   0.0862   1.0000
   8.750   1.3544   0.01446   0.00789  -0.0720   0.0801   1.0000
   9.000   1.3666   0.01476   0.00819  -0.0691   0.0752   1.0000
   9.250   1.3775   0.01513   0.00853  -0.0659   0.0684   1.0000
   9.500   1.3887   0.01553   0.00890  -0.0629   0.0612   1.0000
   9.750   1.3984   0.01602   0.00935  -0.0597   0.0527   1.0000
  10.000   1.4047   0.01670   0.00995  -0.0560   0.0400   1.0000
  10.250   1.4029   0.01780   0.01092  -0.0511   0.0200   1.0000
  10.500   1.4116   0.01845   0.01159  -0.0481   0.0162   1.0000
  10.750   1.4220   0.01905   0.01221  -0.0454   0.0147   1.0000
  11.000   1.4323   0.01968   0.01288  -0.0428   0.0133   1.0000
  11.250   1.4431   0.02030   0.01354  -0.0404   0.0125   1.0000
  11.500   1.4534   0.02098   0.01426  -0.0380   0.0120   1.0000
  11.750   1.4621   0.02177   0.01510  -0.0355   0.0111   1.0000
  12.000   1.4699   0.02266   0.01603  -0.0330   0.0104   1.0000
  12.250   1.4797   0.02347   0.01689  -0.0310   0.0102   1.0000
  12.500   1.4886   0.02439   0.01787  -0.0289   0.0098   1.0000
  12.750   1.4969   0.02538   0.01892  -0.0269   0.0095   1.0000
  13.000   1.5039   0.02653   0.02013  -0.0250   0.0090   1.0000
  13.250   1.5106   0.02778   0.02144  -0.0232   0.0088   1.0000
  13.500   1.5165   0.02914   0.02285  -0.0216   0.0084   1.0000
  13.750   1.5212   0.03067   0.02444  -0.0199   0.0081   1.0000
  14.000   1.5241   0.03242   0.02627  -0.0184   0.0078   1.0000
  14.250   1.5298   0.03399   0.02791  -0.0172   0.0076   1.0000
  14.500   1.5332   0.03581   0.02981  -0.0160   0.0076   1.0000
  14.750   1.5373   0.03764   0.03171  -0.0150   0.0073   1.0000
  15.000   1.5403   0.03965   0.03379  -0.0141   0.0071   1.0000
  15.250   1.5416   0.04189   0.03612  -0.0133   0.0070   1.0000
  15.500   1.5431   0.04416   0.03846  -0.0126   0.0067   1.0000
  15.750   1.5434   0.04662   0.04100  -0.0121   0.0066   1.0000
  16.000   1.5421   0.04933   0.04379  -0.0116   0.0064   1.0000
  16.250   1.5392   0.05229   0.04682  -0.0113   0.0063   1.0000
  16.500   1.5358   0.05537   0.04999  -0.0111   0.0062   1.0000
  16.750   1.5312   0.05869   0.05340  -0.0111   0.0060   1.0000
  17.000   1.5242   0.06244   0.05725  -0.0113   0.0060   1.0000
  17.250   1.5147   0.06659   0.06150  -0.0118   0.0057   1.0000
  17.500   1.5063   0.07076   0.06577  -0.0124   0.0057   1.0000
  17.750   1.5003   0.07469   0.06980  -0.0130   0.0057   1.0000
  18.000   1.4919   0.07907   0.07428  -0.0140   0.0056   1.0000
  18.250   1.4832   0.08354   0.07886  -0.0150   0.0056   1.0000
  18.500   1.4752   0.08800   0.08342  -0.0162   0.0055   1.0000
  18.750   1.4623   0.09331   0.08883  -0.0177   0.0055   1.0000
  19.000   1.4489   0.09874   0.09438  -0.0193   0.0055   1.0000
  19.250   1.4408   0.10335   0.09908  -0.0208   0.0054   1.0000
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