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GOE 655 AIRFOIL (goe655-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 655 AIRFOIL (goe655-il)
Reynolds number: 500,000
Max Cl/Cd: 89.48 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe655-il-500000-n5.txt
Download as CSV file: xf-goe655-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 655 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.8617   0.04040   0.03696  -0.0907   1.0000   0.0185
 -13.750  -0.8944   0.03515   0.03153  -0.0932   1.0000   0.0185
 -13.500  -0.9089   0.03307   0.02934  -0.0915   0.9988   0.0186
 -13.250  -0.8916   0.03130   0.02744  -0.0933   0.9942   0.0190
 -13.000  -0.8727   0.02973   0.02573  -0.0945   0.9898   0.0194
 -12.750  -0.8504   0.02836   0.02422  -0.0958   0.9862   0.0200
 -12.500  -0.8264   0.02690   0.02257  -0.0973   0.9835   0.0206
 -12.250  -0.8076   0.02559   0.02105  -0.0973   0.9783   0.0211
 -12.000  -0.7821   0.02465   0.02007  -0.0982   0.9751   0.0216
 -11.750  -0.7535   0.02394   0.01930  -0.0993   0.9729   0.0220
 -11.500  -0.7283   0.02320   0.01850  -0.0997   0.9692   0.0224
 -11.250  -0.7027   0.02248   0.01769  -0.1000   0.9648   0.0230
 -11.000  -0.6734   0.02173   0.01683  -0.1010   0.9619   0.0236
 -10.750  -0.6431   0.02090   0.01585  -0.1023   0.9595   0.0243
 -10.500  -0.6183   0.02022   0.01501  -0.1022   0.9539   0.0249
 -10.250  -0.5919   0.01938   0.01408  -0.1025   0.9487   0.0254
 -10.000  -0.5611   0.01872   0.01338  -0.1036   0.9450   0.0260
  -9.750  -0.5354   0.01825   0.01287  -0.1034   0.9380   0.0265
  -9.500  -0.5066   0.01775   0.01230  -0.1039   0.9316   0.0272
  -9.250  -0.4787   0.01721   0.01167  -0.1041   0.9247   0.0278
  -9.000  -0.4526   0.01671   0.01106  -0.1039   0.9160   0.0285
  -8.750  -0.4258   0.01621   0.01044  -0.1038   0.9078   0.0291
  -8.500  -0.3996   0.01579   0.00990  -0.1035   0.8982   0.0296
  -8.250  -0.3759   0.01514   0.00919  -0.1028   0.8881   0.0302
  -8.000  -0.3503   0.01468   0.00868  -0.1024   0.8773   0.0308
  -7.750  -0.3251   0.01435   0.00827  -0.1019   0.8641   0.0315
  -7.500  -0.3001   0.01401   0.00785  -0.1012   0.8486   0.0322
  -7.250  -0.2754   0.01368   0.00740  -0.1005   0.8303   0.0327
  -7.000  -0.2512   0.01336   0.00696  -0.0997   0.8105   0.0334
  -6.750  -0.2271   0.01308   0.00654  -0.0988   0.7900   0.0340
  -6.500  -0.2032   0.01287   0.00617  -0.0978   0.7689   0.0346
  -6.250  -0.1794   0.01262   0.00579  -0.0969   0.7514   0.0352
  -6.000  -0.1555   0.01231   0.00541  -0.0960   0.7375   0.0361
  -5.750  -0.1308   0.01208   0.00511  -0.0953   0.7260   0.0369
  -5.500  -0.1057   0.01189   0.00484  -0.0946   0.7154   0.0377
  -5.250  -0.0801   0.01168   0.00458  -0.0940   0.7061   0.0387
  -5.000  -0.0548   0.01152   0.00433  -0.0934   0.6969   0.0397
  -4.750  -0.0288   0.01135   0.00410  -0.0928   0.6871   0.0407
  -4.500  -0.0035   0.01116   0.00386  -0.0922   0.6770   0.0420
  -4.250   0.0220   0.01099   0.00365  -0.0916   0.6658   0.0439
  -4.000   0.0479   0.01085   0.00347  -0.0910   0.6549   0.0457
  -3.750   0.0737   0.01075   0.00329  -0.0904   0.6441   0.0477
  -3.500   0.0994   0.01061   0.00311  -0.0899   0.6323   0.0503
  -3.250   0.1252   0.01049   0.00296  -0.0893   0.6199   0.0539
  -3.000   0.1508   0.01041   0.00282  -0.0887   0.6067   0.0584
  -2.750   0.1761   0.01032   0.00269  -0.0880   0.5921   0.0654
  -2.500   0.2010   0.01023   0.00258  -0.0873   0.5763   0.0763
  -2.250   0.2255   0.01012   0.00247  -0.0866   0.5594   0.0965
  -2.000   0.2497   0.00999   0.00240  -0.0858   0.5428   0.1326
  -1.750   0.2742   0.00992   0.00235  -0.0851   0.5272   0.1637
  -1.500   0.2989   0.00987   0.00232  -0.0844   0.5120   0.1919
  -1.250   0.3235   0.00984   0.00231  -0.0837   0.4971   0.2223
  -1.000   0.3484   0.00982   0.00231  -0.0830   0.4822   0.2510
  -0.750   0.3732   0.00980   0.00232  -0.0823   0.4677   0.2840
  -0.500   0.3977   0.00977   0.00235  -0.0816   0.4538   0.3227
  -0.250   0.4220   0.00975   0.00239  -0.0809   0.4397   0.3628
   0.000   0.4458   0.00974   0.00244  -0.0801   0.4246   0.4084
   0.250   0.4696   0.00975   0.00250  -0.0792   0.4104   0.4525
   0.500   0.4936   0.00980   0.00256  -0.0784   0.3960   0.4839
   0.750   0.5173   0.00984   0.00262  -0.0775   0.3838   0.5198
   1.000   0.5408   0.00980   0.00269  -0.0766   0.3740   0.5712
   1.250   0.5622   0.00970   0.00279  -0.0753   0.3658   0.6507
   1.500   0.5823   0.00952   0.00289  -0.0735   0.3587   0.7519
   1.750   0.6052   0.00935   0.00303  -0.0721   0.3520   0.8716
   2.000   0.6857   0.00955   0.00326  -0.0834   0.3438   0.9714
   2.250   0.7285   0.00973   0.00338  -0.0867   0.3379   0.9913
   2.500   0.7596   0.00993   0.00351  -0.0874   0.3332   1.0000
   2.750   0.7826   0.01005   0.00360  -0.0864   0.3290   1.0000
   3.000   0.8052   0.01019   0.00369  -0.0853   0.3241   1.0000
   3.250   0.8272   0.01036   0.00381  -0.0841   0.3193   1.0000
   3.500   0.8496   0.01052   0.00393  -0.0830   0.3154   1.0000
   3.750   0.8727   0.01064   0.00405  -0.0820   0.3117   1.0000
   4.000   0.8955   0.01079   0.00417  -0.0810   0.3080   1.0000
   4.250   0.9177   0.01096   0.00431  -0.0798   0.3038   1.0000
   4.500   0.9395   0.01115   0.00446  -0.0786   0.3000   1.0000
   4.750   0.9629   0.01128   0.00460  -0.0777   0.2968   1.0000
   5.000   0.9858   0.01143   0.00475  -0.0768   0.2932   1.0000
   5.250   1.0082   0.01160   0.00491  -0.0757   0.2894   1.0000
   5.500   1.0299   0.01180   0.00509  -0.0746   0.2856   1.0000
   5.750   1.0523   0.01197   0.00526  -0.0735   0.2823   1.0000
   6.000   1.0750   0.01213   0.00543  -0.0726   0.2782   1.0000
   6.250   1.0966   0.01233   0.00562  -0.0714   0.2729   1.0000
   6.500   1.1173   0.01256   0.00583  -0.0701   0.2680   1.0000
   6.750   1.1391   0.01273   0.00602  -0.0690   0.2623   1.0000
   7.000   1.1584   0.01296   0.00623  -0.0675   0.2561   1.0000
   7.250   1.1777   0.01318   0.00646  -0.0659   0.2503   1.0000
   7.500   1.1963   0.01343   0.00669  -0.0643   0.2422   1.0000
   7.750   1.2146   0.01371   0.00695  -0.0627   0.2335   1.0000
   8.000   1.2318   0.01405   0.00725  -0.0609   0.2232   1.0000
   8.250   1.2479   0.01444   0.00760  -0.0590   0.2106   1.0000
   8.750   1.2777   0.01540   0.00844  -0.0550   0.1877   1.0000
   9.000   1.2925   0.01591   0.00892  -0.0531   0.1802   1.0000
   9.250   1.3065   0.01646   0.00945  -0.0511   0.1731   1.0000
   9.500   1.3211   0.01700   0.00998  -0.0493   0.1671   1.0000
   9.750   1.3368   0.01749   0.01049  -0.0477   0.1634   1.0000
  10.000   1.3506   0.01810   0.01109  -0.0459   0.1589   1.0000
  10.250   1.3643   0.01871   0.01173  -0.0441   0.1559   1.0000
  10.500   1.3807   0.01921   0.01227  -0.0428   0.1534   1.0000
  10.750   1.3964   0.01975   0.01286  -0.0414   0.1506   1.0000
  11.000   1.4108   0.02038   0.01353  -0.0399   0.1476   1.0000
  11.250   1.4233   0.02114   0.01431  -0.0383   0.1441   1.0000
  11.500   1.4351   0.02197   0.01516  -0.0367   0.1405   1.0000
  11.750   1.4504   0.02260   0.01586  -0.0355   0.1376   1.0000
  12.000   1.4639   0.02338   0.01668  -0.0343   0.1341   1.0000
  12.250   1.4745   0.02436   0.01769  -0.0329   0.1295   1.0000
  12.500   1.4857   0.02534   0.01870  -0.0316   0.1254   1.0000
  12.750   1.4960   0.02642   0.01980  -0.0303   0.1180   1.0000
  13.000   1.5038   0.02773   0.02111  -0.0290   0.1102   1.0000
  13.250   1.5049   0.02961   0.02292  -0.0275   0.0950   1.0000
  13.500   1.4916   0.03280   0.02596  -0.0255   0.0710   1.0000
  13.750   1.4591   0.03799   0.03100  -0.0234   0.0409   1.0000
  14.000   1.4370   0.04266   0.03564  -0.0224   0.0238   1.0000
  14.250   1.4293   0.04611   0.03915  -0.0220   0.0195   1.0000
  14.500   1.4250   0.04934   0.04247  -0.0219   0.0177   1.0000
  14.750   1.4214   0.05260   0.04582  -0.0220   0.0166   1.0000
  15.000   1.4166   0.05609   0.04941  -0.0222   0.0156   1.0000
  15.250   1.4116   0.05974   0.05316  -0.0226   0.0150   1.0000
  15.500   1.4042   0.06378   0.05730  -0.0232   0.0144   1.0000
  15.750   1.3963   0.06797   0.06160  -0.0240   0.0140   1.0000
  16.000   1.3895   0.07211   0.06585  -0.0248   0.0134   1.0000
  16.250   1.3819   0.07645   0.07030  -0.0258   0.0132   1.0000
  16.500   1.3731   0.08099   0.07495  -0.0269   0.0130   1.0000
  16.750   1.3642   0.08561   0.07969  -0.0281   0.0126   1.0000
  17.000   1.3535   0.09059   0.08479  -0.0295   0.0123   1.0000
  17.250   1.3425   0.09568   0.08998  -0.0310   0.0121   1.0000
  17.500   1.3313   0.10085   0.09526  -0.0326   0.0119   1.0000
  17.750   1.3201   0.10609   0.10060  -0.0344   0.0117   1.0000
  18.000   1.3068   0.11178   0.10640  -0.0364   0.0115   1.0000
  18.250   1.2958   0.11715   0.11187  -0.0384   0.0113   1.0000
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