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GOE 679 AIRFOIL (goe679-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 679 AIRFOIL (goe679-il)
Reynolds number: 1,000,000
Max Cl/Cd: 95.94 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe679-il-1000000.txt
Download as CSV file: xf-goe679-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 679 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -19.250  -0.7987   0.11539   0.11258  -0.0619   1.0000   0.0300
 -19.000  -0.8198   0.10871   0.10579  -0.0653   1.0000   0.0300
 -18.750  -0.8370   0.10281   0.09980  -0.0682   1.0000   0.0301
 -18.500  -0.8516   0.09746   0.09436  -0.0707   1.0000   0.0302
 -18.250  -0.8661   0.09231   0.08913  -0.0731   1.0000   0.0303
 -18.000  -0.8791   0.08747   0.08421  -0.0752   1.0000   0.0304
 -17.750  -0.8928   0.08262   0.07928  -0.0774   1.0000   0.0305
 -17.500  -0.9049   0.07831   0.07490  -0.0791   1.0000   0.0305
 -17.250  -0.9188   0.07388   0.07039  -0.0809   1.0000   0.0305
 -17.000  -0.9344   0.06940   0.06584  -0.0826   1.0000   0.0306
 -16.750  -0.9502   0.06502   0.06138  -0.0841   1.0000   0.0307
 -16.500  -0.9563   0.06037   0.05665  -0.0877   0.9994   0.0307
 -16.250  -0.9594   0.05556   0.05174  -0.0922   0.9982   0.0308
 -16.000  -0.9594   0.05106   0.04714  -0.0966   0.9967   0.0308
 -15.750  -0.9557   0.04662   0.04259  -0.1016   0.9951   0.0310
 -15.500  -0.9490   0.04264   0.03850  -0.1064   0.9938   0.0311
 -15.250  -0.9435   0.03862   0.03436  -0.1114   0.9928   0.0312
 -15.000  -0.9496   0.03467   0.03031  -0.1139   0.9893   0.0314
 -14.750  -0.9504   0.03124   0.02679  -0.1168   0.9863   0.0316
 -14.500  -0.9399   0.02907   0.02453  -0.1188   0.9842   0.0317
 -14.250  -0.9253   0.02731   0.02270  -0.1207   0.9826   0.0320
 -14.000  -0.9060   0.02592   0.02126  -0.1223   0.9814   0.0322
 -13.750  -0.9044   0.02482   0.02010  -0.1196   0.9760   0.0323
 -13.500  -0.8890   0.02387   0.01910  -0.1191   0.9729   0.0326
 -13.250  -0.8686   0.02301   0.01819  -0.1192   0.9710   0.0328
 -13.000  -0.8456   0.02221   0.01734  -0.1195   0.9695   0.0331
 -12.750  -0.8199   0.02147   0.01656  -0.1200   0.9684   0.0334
 -12.500  -0.8188   0.02089   0.01594  -0.1155   0.9611   0.0336
 -12.250  -0.7939   0.02012   0.01511  -0.1156   0.9587   0.0339
 -12.000  -0.7650   0.01942   0.01437  -0.1163   0.9572   0.0342
 -11.750  -0.7347   0.01876   0.01367  -0.1173   0.9562   0.0345
 -11.500  -0.7032   0.01809   0.01296  -0.1185   0.9553   0.0348
 -11.250  -0.6936   0.01763   0.01246  -0.1150   0.9483   0.0349
 -11.000  -0.6677   0.01696   0.01174  -0.1149   0.9455   0.0352
 -10.750  -0.6413   0.01608   0.01082  -0.1152   0.9436   0.0358
 -10.500  -0.6093   0.01536   0.01009  -0.1163   0.9422   0.0364
 -10.250  -0.5714   0.01469   0.00940  -0.1184   0.9408   0.0370
 -10.000  -0.5622   0.01425   0.00893  -0.1145   0.9300   0.0374
  -9.750  -0.5264   0.01368   0.00832  -0.1161   0.9264   0.0379
  -9.500  -0.5114   0.01334   0.00794  -0.1134   0.9157   0.0384
  -9.250  -0.4736   0.01288   0.00745  -0.1154   0.9110   0.0390
  -9.000  -0.4457   0.01253   0.00705  -0.1154   0.9005   0.0394
  -8.750  -0.4057   0.01194   0.00641  -0.1181   0.8914   0.0407
  -8.500  -0.3662   0.01156   0.00598  -0.1205   0.8783   0.0417
  -8.250  -0.3234   0.01125   0.00561  -0.1236   0.8640   0.0430
  -8.000  -0.2884   0.01103   0.00528  -0.1250   0.8465   0.0442
  -7.750  -0.2627   0.01078   0.00495  -0.1245   0.8286   0.0460
  -7.500  -0.2396   0.01061   0.00471  -0.1234   0.8142   0.0480
  -7.250  -0.2178   0.01042   0.00446  -0.1221   0.8018   0.0510
  -7.000  -0.1974   0.01022   0.00424  -0.1204   0.7911   0.0551
  -6.750  -0.1776   0.00996   0.00399  -0.1187   0.7808   0.0642
  -6.500  -0.1588   0.00966   0.00375  -0.1168   0.7714   0.0802
  -6.250  -0.1384   0.00948   0.00359  -0.1151   0.7618   0.0949
  -6.000  -0.1167   0.00933   0.00347  -0.1137   0.7539   0.1049
  -5.750  -0.0950   0.00923   0.00336  -0.1122   0.7453   0.1129
  -5.500  -0.0729   0.00913   0.00327  -0.1108   0.7373   0.1191
  -5.250  -0.0510   0.00906   0.00318  -0.1093   0.7285   0.1247
  -5.000  -0.0293   0.00900   0.00309  -0.1078   0.7202   0.1297
  -4.750  -0.0080   0.00891   0.00301  -0.1062   0.7120   0.1348
  -4.500   0.0126   0.00890   0.00293  -0.1044   0.7032   0.1380
  -4.250   0.0330   0.00879   0.00284  -0.1026   0.6951   0.1436
  -4.000   0.0525   0.00875   0.00277  -0.1006   0.6849   0.1480
  -3.750   0.0738   0.00872   0.00270  -0.0990   0.6751   0.1515
  -3.500   0.0927   0.00866   0.00262  -0.0969   0.6640   0.1567
  -3.250   0.1139   0.00861   0.00256  -0.0953   0.6529   0.1613
  -3.000   0.1337   0.00862   0.00251  -0.0933   0.6401   0.1649
  -2.750   0.1523   0.00859   0.00245  -0.0911   0.6246   0.1716
  -2.500   0.1723   0.00859   0.00242  -0.0893   0.6091   0.1776
  -2.250   0.1911   0.00862   0.00239  -0.0872   0.5919   0.1823
  -2.000   0.2092   0.00864   0.00237  -0.0850   0.5735   0.1896
  -1.750   0.2283   0.00872   0.00237  -0.0829   0.5553   0.1951
  -1.500   0.2476   0.00878   0.00238  -0.0810   0.5382   0.2028
  -1.250   0.2672   0.00885   0.00241  -0.0791   0.5224   0.2107
  -1.000   0.2875   0.00893   0.00243  -0.0774   0.5075   0.2183
  -0.750   0.3088   0.00898   0.00247  -0.0759   0.4945   0.2279
  -0.500   0.3295   0.00905   0.00250  -0.0743   0.4824   0.2368
  -0.250   0.3506   0.00910   0.00255  -0.0727   0.4719   0.2478
   0.000   0.3717   0.00916   0.00259  -0.0712   0.4627   0.2583
   0.250   0.3936   0.00920   0.00264  -0.0698   0.4546   0.2694
   0.500   0.4140   0.00927   0.00270  -0.0681   0.4461   0.2816
   1.000   0.4580   0.00936   0.00281  -0.0655   0.4322   0.3083
   1.250   0.4793   0.00941   0.00287  -0.0640   0.4253   0.3227
   1.500   0.5019   0.00943   0.00293  -0.0628   0.4200   0.3391
   1.750   0.5224   0.00947   0.00300  -0.0612   0.4138   0.3615
   2.000   0.5417   0.00951   0.00310  -0.0594   0.4076   0.3895
   2.250   0.5627   0.00946   0.00317  -0.0579   0.4033   0.4293
   2.500   0.5814   0.00940   0.00327  -0.0560   0.3978   0.4881
   2.750   0.5958   0.00928   0.00340  -0.0533   0.3922   0.5830
   3.000   0.6082   0.00907   0.00353  -0.0500   0.3877   0.6960
   3.250   0.6187   0.00876   0.00368  -0.0461   0.3841   0.8359
   3.500   0.7990   0.00919   0.00424  -0.0791   0.3697   0.9703
   3.750   0.8374   0.00937   0.00441  -0.0813   0.3648   0.9840
   4.000   0.8724   0.00961   0.00460  -0.0828   0.3588   0.9920
   4.500   0.9566   0.01006   0.00494  -0.0890   0.3465   1.0000
   4.750   0.9717   0.01018   0.00504  -0.0865   0.3410   1.0000
   5.000   0.9850   0.01037   0.00518  -0.0836   0.3347   1.0000
   5.250   1.0026   0.01048   0.00528  -0.0816   0.3302   1.0000
   5.500   1.0198   0.01063   0.00541  -0.0795   0.3247   1.0000
   5.750   1.0356   0.01085   0.00557  -0.0771   0.3184   1.0000
   6.000   1.0538   0.01101   0.00572  -0.0753   0.3134   1.0000
   6.250   1.0715   0.01120   0.00589  -0.0733   0.3077   1.0000
   6.500   1.0874   0.01147   0.00611  -0.0711   0.3006   1.0000
   6.750   1.1063   0.01167   0.00629  -0.0695   0.2942   1.0000
   7.000   1.1243   0.01192   0.00651  -0.0677   0.2879   1.0000
   7.250   1.1410   0.01222   0.00677  -0.0658   0.2806   1.0000
   7.500   1.1595   0.01248   0.00701  -0.0642   0.2744   1.0000
   7.750   1.1755   0.01285   0.00732  -0.0622   0.2666   1.0000
   8.000   1.1948   0.01312   0.00759  -0.0608   0.2612   1.0000
   8.250   1.2118   0.01347   0.00791  -0.0591   0.2550   1.0000
   8.500   1.2281   0.01387   0.00827  -0.0573   0.2490   1.0000
   8.750   1.2471   0.01418   0.00857  -0.0560   0.2441   1.0000
   9.000   1.2638   0.01458   0.00896  -0.0543   0.2388   1.0000
   9.250   1.2793   0.01505   0.00940  -0.0525   0.2335   1.0000
   9.500   1.2984   0.01539   0.00975  -0.0513   0.2301   1.0000
   9.750   1.3158   0.01580   0.01016  -0.0499   0.2264   1.0000
  10.000   1.3308   0.01633   0.01066  -0.0482   0.2219   1.0000
  10.250   1.3464   0.01685   0.01118  -0.0466   0.2179   1.0000
  10.500   1.3645   0.01727   0.01162  -0.0454   0.2155   1.0000
  10.750   1.3810   0.01777   0.01212  -0.0441   0.2117   1.0000
  11.000   1.3959   0.01837   0.01271  -0.0426   0.2083   1.0000
  11.250   1.4078   0.01913   0.01345  -0.0408   0.2038   1.0000
  11.500   1.4258   0.01960   0.01397  -0.0398   0.2021   1.0000
  11.750   1.4422   0.02016   0.01456  -0.0386   0.1998   1.0000
  12.000   1.4578   0.02079   0.01520  -0.0374   0.1974   1.0000
  12.250   1.4714   0.02155   0.01597  -0.0360   0.1948   1.0000
  12.500   1.4841   0.02238   0.01681  -0.0347   0.1920   1.0000
  12.750   1.4946   0.02336   0.01780  -0.0331   0.1891   1.0000
  13.000   1.5117   0.02397   0.01845  -0.0323   0.1875   1.0000
  13.250   1.5265   0.02473   0.01925  -0.0313   0.1855   1.0000
  13.500   1.5404   0.02557   0.02012  -0.0303   0.1834   1.0000
  13.750   1.5521   0.02658   0.02114  -0.0291   0.1811   1.0000
  14.000   1.5626   0.02767   0.02226  -0.0279   0.1787   1.0000
  14.250   1.5691   0.02907   0.02367  -0.0265   0.1759   1.0000
  14.500   1.5836   0.02994   0.02459  -0.0257   0.1746   1.0000
  14.750   1.5966   0.03094   0.02564  -0.0249   0.1731   1.0000
  15.000   1.6091   0.03198   0.02672  -0.0241   0.1710   1.0000
  15.250   1.6189   0.03325   0.02803  -0.0232   0.1690   1.0000
  15.500   1.6270   0.03466   0.02946  -0.0223   0.1664   1.0000
  15.750   1.6308   0.03645   0.03127  -0.0212   0.1635   1.0000
  16.000   1.6405   0.03780   0.03266  -0.0204   0.1614   1.0000
  16.250   1.6509   0.03911   0.03403  -0.0198   0.1595   1.0000
  16.500   1.6597   0.04057   0.03553  -0.0192   0.1568   1.0000
  16.750   1.6640   0.04245   0.03744  -0.0185   0.1540   1.0000
  17.000   1.6627   0.04488   0.03988  -0.0176   0.1504   1.0000
  17.250   1.6716   0.04641   0.04147  -0.0172   0.1485   1.0000
  17.500   1.6775   0.04826   0.04338  -0.0167   0.1469   1.0000
  17.750   1.6803   0.05043   0.04558  -0.0163   0.1432   1.0000
  18.000   1.6795   0.05298   0.04817  -0.0159   0.1404   1.0000
  18.250   1.6775   0.05572   0.05095  -0.0155   0.1376   1.0000
  18.500   1.6808   0.05794   0.05324  -0.0153   0.1348   1.0000
  18.750   1.6796   0.06066   0.05600  -0.0152   0.1314   1.0000
  19.000   1.6689   0.06448   0.05985  -0.0151   0.1272   1.0000
  19.250   1.6675   0.06731   0.06274  -0.0152   0.1233   1.0000
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