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GOE 627 AIRFOIL (goe627-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 627 AIRFOIL (goe627-il)
Reynolds number: 1,000,000
Max Cl/Cd: 90.53 at α=7.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe627-il-1000000-n5.txt
Download as CSV file: xf-goe627-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 627 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
  ------ -------- --------- --------- -------- -------- --------
 -18.250  -0.9957   0.06578   0.06273  -0.0874   1.0000   0.0135
 -18.000  -1.0261   0.05689   0.05367  -0.0938   0.9996   0.0137
 -17.750  -1.0442   0.04945   0.04604  -0.1002   0.9989   0.0137
 -17.500  -1.0511   0.04421   0.04065  -0.1048   0.9980   0.0138
 -17.250  -1.0539   0.03995   0.03624  -0.1084   0.9968   0.0140
 -17.000  -1.0510   0.03671   0.03288  -0.1110   0.9953   0.0141
 -16.750  -1.0453   0.03400   0.03004  -0.1130   0.9937   0.0143
 -16.500  -1.0404   0.03185   0.02781  -0.1136   0.9919   0.0144
 -16.250  -1.0309   0.03017   0.02607  -0.1140   0.9901   0.0146
 -16.000  -1.0188   0.02869   0.02452  -0.1145   0.9882   0.0148
 -15.750  -1.0028   0.02753   0.02331  -0.1148   0.9867   0.0150
 -15.500  -0.9857   0.02649   0.02222  -0.1151   0.9855   0.0153
 -15.250  -0.9678   0.02544   0.02112  -0.1155   0.9844   0.0155
 -15.000  -0.9476   0.02455   0.02016  -0.1159   0.9834   0.0157
 -14.750  -0.9327   0.02375   0.01931  -0.1150   0.9812   0.0160
 -14.500  -0.9183   0.02292   0.01841  -0.1140   0.9784   0.0162
 -14.250  -0.8997   0.02215   0.01757  -0.1136   0.9764   0.0165
 -14.000  -0.8793   0.02143   0.01677  -0.1134   0.9749   0.0168
 -13.750  -0.8566   0.02076   0.01603  -0.1134   0.9736   0.0170
 -13.500  -0.8338   0.02005   0.01525  -0.1134   0.9725   0.0172
 -13.250  -0.8084   0.01950   0.01468  -0.1137   0.9715   0.0176
 -13.000  -0.7873   0.01906   0.01422  -0.1130   0.9692   0.0178
 -12.750  -0.7682   0.01863   0.01376  -0.1118   0.9660   0.0180
 -12.500  -0.7425   0.01829   0.01339  -0.1118   0.9640   0.0183
 -12.250  -0.7160   0.01781   0.01287  -0.1120   0.9623   0.0186
 -12.000  -0.6883   0.01733   0.01235  -0.1124   0.9606   0.0189
 -11.750  -0.6574   0.01680   0.01177  -0.1135   0.9588   0.0192
 -11.500  -0.6332   0.01638   0.01129  -0.1131   0.9546   0.0196
 -11.250  -0.6146   0.01598   0.01083  -0.1114   0.9487   0.0198
 -11.000  -0.5881   0.01557   0.01036  -0.1114   0.9457   0.0201
 -10.750  -0.5596   0.01516   0.00990  -0.1118   0.9434   0.0204
 -10.500  -0.5406   0.01479   0.00950  -0.1102   0.9395   0.0207
 -10.250  -0.5230   0.01447   0.00917  -0.1083   0.9346   0.0210
 -10.000  -0.4984   0.01422   0.00890  -0.1077   0.9309   0.0213
  -9.750  -0.4716   0.01391   0.00855  -0.1076   0.9278   0.0216
  -9.500  -0.4494   0.01363   0.00825  -0.1065   0.9238   0.0219
  -9.250  -0.4305   0.01337   0.00796  -0.1046   0.9185   0.0223
  -9.000  -0.4065   0.01309   0.00765  -0.1039   0.9139   0.0226
  -8.750  -0.3799   0.01278   0.00728  -0.1036   0.9100   0.0230
  -8.500  -0.3608   0.01255   0.00702  -0.1018   0.9038   0.0233
  -8.250  -0.3375   0.01227   0.00670  -0.1008   0.8974   0.0235
  -8.000  -0.3133   0.01206   0.00644  -0.0999   0.8894   0.0238
  -7.750  -0.2914   0.01169   0.00600  -0.0987   0.8787   0.0241
  -7.500  -0.2706   0.01137   0.00565  -0.0972   0.8663   0.0245
  -7.250  -0.2480   0.01113   0.00535  -0.0960   0.8545   0.0248
  -7.000  -0.2256   0.01093   0.00509  -0.0947   0.8394   0.0251
  -6.750  -0.2034   0.01079   0.00488  -0.0934   0.8235   0.0255
  -6.500  -0.1824   0.01065   0.00466  -0.0918   0.8043   0.0259
  -6.250  -0.1620   0.01052   0.00443  -0.0901   0.7854   0.0263
  -6.000  -0.1416   0.01041   0.00424  -0.0884   0.7669   0.0266
  -5.750  -0.1218   0.01033   0.00406  -0.0866   0.7466   0.0269
  -5.500  -0.1030   0.01027   0.00389  -0.0845   0.7238   0.0272
  -5.250  -0.0833   0.01022   0.00374  -0.0826   0.7021   0.0275
  -5.000  -0.0645   0.01021   0.00361  -0.0806   0.6771   0.0277
  -4.750  -0.0463   0.01015   0.00343  -0.0784   0.6534   0.0282
  -4.500  -0.0272   0.01008   0.00327  -0.0765   0.6307   0.0288
  -4.250  -0.0064   0.01001   0.00314  -0.0748   0.6139   0.0293
  -4.000   0.0148   0.00996   0.00302  -0.0733   0.5985   0.0297
  -3.750   0.0360   0.00992   0.00291  -0.0718   0.5816   0.0302
  -3.500   0.0574   0.00989   0.00282  -0.0703   0.5650   0.0308
  -3.250   0.0794   0.00986   0.00272  -0.0689   0.5493   0.0314
  -3.000   0.1012   0.00984   0.00264  -0.0675   0.5332   0.0319
  -2.750   0.1226   0.00984   0.00256  -0.0661   0.5153   0.0325
  -2.500   0.1432   0.00984   0.00249  -0.0644   0.4957   0.0336
  -2.250   0.1639   0.00987   0.00244  -0.0628   0.4752   0.0349
  -2.000   0.1849   0.00990   0.00239  -0.0613   0.4556   0.0364
  -1.750   0.2060   0.00992   0.00235  -0.0598   0.4390   0.0392
  -1.500   0.2271   0.00993   0.00232  -0.0583   0.4241   0.0452
  -1.250   0.2474   0.00985   0.00229  -0.0566   0.4102   0.0702
  -1.000   0.2668   0.00973   0.00224  -0.0549   0.3983   0.1077
  -0.750   0.2849   0.00961   0.00221  -0.0528   0.3869   0.1550
  -0.500   0.3031   0.00951   0.00219  -0.0508   0.3753   0.1912
  -0.250   0.3206   0.00937   0.00219  -0.0486   0.3656   0.2483
   0.000   0.3383   0.00929   0.00220  -0.0465   0.3542   0.2980
   0.250   0.3568   0.00920   0.00222  -0.0445   0.3433   0.3477
   0.500   0.3739   0.00908   0.00225  -0.0423   0.3336   0.4097
   0.750   0.3904   0.00893   0.00229  -0.0400   0.3252   0.4854
   1.000   0.4058   0.00878   0.00236  -0.0374   0.3176   0.5675
   1.250   0.4208   0.00863   0.00243  -0.0346   0.3107   0.6475
   1.500   0.4370   0.00860   0.00252  -0.0321   0.3034   0.7010
   1.750   0.4487   0.00843   0.00262  -0.0285   0.2981   0.7837
   2.000   0.4656   0.00842   0.00273  -0.0261   0.2916   0.8329
   2.250   0.4897   0.00842   0.00289  -0.0252   0.2848   0.8928
   2.500   0.5253   0.00855   0.00303  -0.0269   0.2779   0.9160
   2.750   0.5770   0.00880   0.00324  -0.0323   0.2685   0.9383
   3.000   0.6327   0.00905   0.00345  -0.0385   0.2608   0.9503
   3.250   0.6784   0.00930   0.00364  -0.0425   0.2542   0.9586
   3.500   0.7157   0.00950   0.00380  -0.0447   0.2499   0.9643
   3.750   0.7463   0.00968   0.00395  -0.0454   0.2458   0.9710
   4.000   0.7799   0.00990   0.00413  -0.0468   0.2410   0.9753
   4.250   0.8080   0.01013   0.00432  -0.0470   0.2363   0.9810
   4.500   0.8403   0.01030   0.00448  -0.0481   0.2331   0.9842
   4.750   0.8720   0.01048   0.00463  -0.0492   0.2296   0.9864
   5.000   0.9022   0.01069   0.00480  -0.0500   0.2253   0.9891
   5.250   0.9310   0.01092   0.00499  -0.0505   0.2214   0.9919
   5.500   0.9605   0.01110   0.00517  -0.0511   0.2189   0.9944
   5.750   0.9920   0.01128   0.00534  -0.0521   0.2164   0.9965
   6.000   1.0234   0.01147   0.00552  -0.0532   0.2135   0.9982
   6.250   1.0546   0.01169   0.00571  -0.0543   0.2104   0.9995
   6.500   1.0759   0.01189   0.00590  -0.0533   0.2072   1.0000
   6.750   1.0889   0.01208   0.00607  -0.0505   0.2042   1.0000
   7.000   1.1047   0.01222   0.00623  -0.0483   0.2029   1.0000
   7.250   1.1207   0.01238   0.00640  -0.0462   0.2014   1.0000
   7.500   1.1371   0.01256   0.00660  -0.0441   0.1998   1.0000
   7.750   1.1539   0.01276   0.00680  -0.0422   0.1977   1.0000
   8.000   1.1703   0.01299   0.00702  -0.0403   0.1948   1.0000
   8.250   1.1864   0.01326   0.00728  -0.0383   0.1920   1.0000
   8.500   1.2031   0.01352   0.00754  -0.0365   0.1895   1.0000
   8.750   1.2217   0.01374   0.00778  -0.0350   0.1882   1.0000
   9.000   1.2400   0.01398   0.00804  -0.0336   0.1866   1.0000
   9.250   1.2581   0.01424   0.00833  -0.0321   0.1846   1.0000
   9.500   1.2762   0.01452   0.00862  -0.0307   0.1824   1.0000
   9.750   1.2940   0.01483   0.00894  -0.0293   0.1802   1.0000
  10.000   1.3111   0.01518   0.00929  -0.0278   0.1777   1.0000
  10.250   1.3282   0.01555   0.00967  -0.0263   0.1752   1.0000
  10.500   1.3470   0.01585   0.01001  -0.0252   0.1737   1.0000
  10.750   1.3650   0.01620   0.01038  -0.0240   0.1708   1.0000
  11.000   1.3810   0.01665   0.01082  -0.0225   0.1653   1.0000
  11.250   1.3975   0.01710   0.01128  -0.0212   0.1625   1.0000
  11.500   1.4141   0.01755   0.01174  -0.0199   0.1580   1.0000
  11.750   1.4291   0.01810   0.01228  -0.0185   0.1522   1.0000
  12.000   1.4429   0.01873   0.01289  -0.0170   0.1454   1.0000
  12.250   1.4571   0.01934   0.01350  -0.0155   0.1404   1.0000
  12.500   1.4676   0.02018   0.01430  -0.0138   0.1310   1.0000
  12.750   1.4757   0.02119   0.01526  -0.0118   0.1206   1.0000
  13.000   1.4851   0.02215   0.01620  -0.0101   0.1141   1.0000
  13.250   1.4913   0.02333   0.01735  -0.0081   0.1048   1.0000
  13.500   1.5012   0.02434   0.01836  -0.0067   0.1007   1.0000
  13.750   1.5081   0.02556   0.01958  -0.0051   0.0950   1.0000
  14.000   1.5163   0.02674   0.02079  -0.0037   0.0914   1.0000
  14.250   1.5263   0.02784   0.02193  -0.0025   0.0890   1.0000
  14.500   1.5339   0.02916   0.02327  -0.0013   0.0862   1.0000
  14.750   1.5402   0.03062   0.02475  -0.0002   0.0834   1.0000
  15.000   1.5467   0.03211   0.02629   0.0009   0.0805   1.0000
  15.250   1.5541   0.03358   0.02781   0.0017   0.0784   1.0000
  15.500   1.5592   0.03529   0.02955   0.0026   0.0760   1.0000
  15.750   1.5626   0.03721   0.03151   0.0034   0.0738   1.0000
  16.000   1.5665   0.03914   0.03349   0.0040   0.0713   1.0000
  16.250   1.5709   0.04108   0.03550   0.0045   0.0693   1.0000
  16.500   1.5686   0.04372   0.03816   0.0051   0.0652   1.0000
  16.750   1.5683   0.04625   0.04075   0.0054   0.0629   1.0000
  17.000   1.5615   0.04953   0.04406   0.0056   0.0573   1.0000
  17.250   1.5492   0.05350   0.04806   0.0057   0.0509   1.0000
  17.500   1.5267   0.05884   0.05341   0.0053   0.0431   1.0000
  17.750   1.5023   0.06462   0.05926   0.0046   0.0364   1.0000
  18.000   1.4688   0.07181   0.06653   0.0033   0.0289   1.0000
  18.250   1.4351   0.07935   0.07416   0.0016   0.0231   1.0000
  18.500   1.4073   0.08632   0.08124  -0.0002   0.0202   1.0000
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