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GOE 550 AIRFOIL (goe550-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 550 AIRFOIL (goe550-il)
Reynolds number: 1,000,000
Max Cl/Cd: 114.84 at α=6.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe550-il-1000000-n5.txt
Download as CSV file: xf-goe550-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 550 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.8487   0.08435   0.08149  -0.0638   1.0000   0.0175
 -16.000  -0.8667   0.07858   0.07566  -0.0668   1.0000   0.0176
 -15.750  -0.8891   0.07242   0.06942  -0.0701   1.0000   0.0177
 -15.500  -0.9192   0.06566   0.06258  -0.0738   1.0000   0.0178
 -15.250  -0.9707   0.05695   0.05376  -0.0786   1.0000   0.0174
 -15.000  -1.1435   0.02997   0.02625  -0.1004   0.9976   0.0148
 -14.750  -1.1264   0.02632   0.02242  -0.1054   0.9950   0.0155
 -14.500  -1.1046   0.02433   0.02032  -0.1079   0.9931   0.0165
 -14.250  -1.0835   0.02293   0.01882  -0.1090   0.9906   0.0174
 -14.000  -1.0595   0.02170   0.01750  -0.1102   0.9883   0.0183
 -13.750  -1.0334   0.02059   0.01634  -0.1115   0.9863   0.0196
 -13.500  -1.0052   0.01968   0.01537  -0.1129   0.9848   0.0208
 -13.250  -0.9759   0.01887   0.01448  -0.1143   0.9836   0.0219
 -13.000  -0.9534   0.01810   0.01367  -0.1141   0.9801   0.0231
 -12.750  -0.9270   0.01744   0.01296  -0.1146   0.9772   0.0243
 -12.500  -0.8981   0.01685   0.01231  -0.1154   0.9750   0.0253
 -12.250  -0.8682   0.01624   0.01164  -0.1165   0.9733   0.0262
 -12.000  -0.8375   0.01561   0.01098  -0.1177   0.9718   0.0274
 -11.750  -0.8154   0.01513   0.01046  -0.1169   0.9660   0.0284
 -11.500  -0.7863   0.01466   0.00993  -0.1175   0.9626   0.0295
 -11.250  -0.7534   0.01424   0.00946  -0.1188   0.9602   0.0304
 -11.000  -0.7241   0.01372   0.00890  -0.1195   0.9557   0.0316
 -10.750  -0.6937   0.01326   0.00840  -0.1204   0.9500   0.0329
 -10.500  -0.6588   0.01283   0.00794  -0.1221   0.9456   0.0342
 -10.250  -0.6266   0.01247   0.00752  -0.1231   0.9371   0.0353
 -10.000  -0.5910   0.01211   0.00708  -0.1249   0.9262   0.0364
  -9.750  -0.5585   0.01170   0.00660  -0.1260   0.9099   0.0381
  -9.500  -0.5294   0.01141   0.00623  -0.1264   0.8912   0.0398
  -9.250  -0.5023   0.01119   0.00592  -0.1262   0.8744   0.0413
  -9.000  -0.4760   0.01102   0.00563  -0.1259   0.8589   0.0422
  -8.750  -0.4506   0.01077   0.00529  -0.1254   0.8454   0.0437
  -8.250  -0.3993   0.01032   0.00472  -0.1245   0.8218   0.0475
  -8.000  -0.3732   0.01015   0.00447  -0.1241   0.8121   0.0490
  -7.750  -0.3468   0.00998   0.00424  -0.1237   0.8025   0.0504
  -7.500  -0.3207   0.00976   0.00397  -0.1233   0.7939   0.0532
  -7.250  -0.2943   0.00957   0.00375  -0.1230   0.7854   0.0559
  -7.000  -0.2675   0.00942   0.00354  -0.1227   0.7779   0.0584
  -6.750  -0.2411   0.00921   0.00332  -0.1223   0.7697   0.0636
  -6.500  -0.2144   0.00904   0.00313  -0.1220   0.7622   0.0691
  -6.250  -0.1876   0.00885   0.00294  -0.1217   0.7548   0.0766
  -6.000  -0.1609   0.00870   0.00278  -0.1214   0.7479   0.0834
  -5.750  -0.1335   0.00858   0.00265  -0.1212   0.7408   0.0889
  -5.500  -0.1064   0.00848   0.00251  -0.1209   0.7331   0.0933
  -5.250  -0.0791   0.00835   0.00238  -0.1207   0.7262   0.0984
  -5.000  -0.0517   0.00828   0.00226  -0.1204   0.7189   0.1022
  -4.750  -0.0244   0.00820   0.00215  -0.1202   0.7121   0.1060
  -4.500   0.0030   0.00809   0.00203  -0.1199   0.7044   0.1106
  -4.250   0.0301   0.00802   0.00193  -0.1196   0.6965   0.1153
  -4.000   0.0573   0.00795   0.00183  -0.1193   0.6867   0.1204
  -3.750   0.0842   0.00787   0.00174  -0.1190   0.6756   0.1273
  -3.500   0.1106   0.00781   0.00165  -0.1186   0.6622   0.1365
  -3.000   0.1639   0.00770   0.00154  -0.1178   0.6356   0.1624
  -2.750   0.1912   0.00768   0.00151  -0.1175   0.6258   0.1733
  -2.500   0.2181   0.00767   0.00149  -0.1172   0.6153   0.1815
  -2.250   0.2455   0.00768   0.00146  -0.1169   0.6042   0.1874
  -2.000   0.2727   0.00769   0.00144  -0.1166   0.5943   0.1912
  -1.750   0.2998   0.00770   0.00143  -0.1163   0.5843   0.1964
  -1.500   0.3272   0.00772   0.00142  -0.1160   0.5749   0.2006
  -1.250   0.3542   0.00776   0.00141  -0.1157   0.5648   0.2034
  -1.000   0.3814   0.00780   0.00141  -0.1154   0.5542   0.2058
  -0.750   0.4086   0.00782   0.00142  -0.1151   0.5458   0.2096
  -0.500   0.4358   0.00785   0.00143  -0.1148   0.5373   0.2129
  -0.250   0.4629   0.00789   0.00144  -0.1145   0.5294   0.2161
   0.000   0.4900   0.00793   0.00146  -0.1141   0.5204   0.2190
   0.250   0.5171   0.00799   0.00149  -0.1138   0.5116   0.2213
   0.500   0.5440   0.00803   0.00152  -0.1135   0.5032   0.2259
   0.750   0.5711   0.00806   0.00156  -0.1132   0.4957   0.2313
   1.000   0.5977   0.00814   0.00160  -0.1128   0.4856   0.2351
   1.250   0.6243   0.00821   0.00165  -0.1124   0.4737   0.2377
   1.500   0.6507   0.00829   0.00170  -0.1120   0.4622   0.2417
   1.750   0.6768   0.00838   0.00177  -0.1115   0.4508   0.2471
   2.000   0.7034   0.00845   0.00183  -0.1111   0.4399   0.2516
   2.500   0.7555   0.00865   0.00198  -0.1102   0.4181   0.2600
   2.750   0.7811   0.00877   0.00207  -0.1097   0.4042   0.2656
   3.000   0.8061   0.00893   0.00218  -0.1090   0.3880   0.2702
   3.500   0.8560   0.00924   0.00242  -0.1077   0.3586   0.2814
   3.750   0.8814   0.00937   0.00254  -0.1071   0.3489   0.2869
   4.000   0.9065   0.00950   0.00266  -0.1065   0.3402   0.2942
   4.250   0.9320   0.00961   0.00278  -0.1060   0.3333   0.3020
   4.500   0.9571   0.00973   0.00292  -0.1054   0.3259   0.3115
   4.750   0.9822   0.00984   0.00306  -0.1048   0.3197   0.3239
   5.000   1.0071   0.00992   0.00320  -0.1041   0.3131   0.3473
   5.250   1.0307   0.00997   0.00341  -0.1034   0.3057   0.4222
   5.500   1.0552   0.01002   0.00358  -0.1027   0.2993   0.4751
   5.750   1.0789   0.01012   0.00376  -0.1019   0.2926   0.5156
   6.000   1.0989   0.00993   0.00402  -0.1004   0.2820   0.7170
   6.500   1.1553   0.01006   0.00454  -0.1008   0.2500   1.0000
   6.750   1.1769   0.01036   0.00478  -0.0996   0.2353   1.0000
   7.000   1.1958   0.01078   0.00507  -0.0980   0.2131   1.0000
   7.250   1.2114   0.01136   0.00547  -0.0958   0.1803   1.0000
   7.500   1.2200   0.01222   0.00607  -0.0924   0.1358   1.0000
   7.750   1.2343   0.01271   0.00647  -0.0899   0.1202   1.0000
   8.000   1.2504   0.01311   0.00683  -0.0877   0.1102   1.0000
   8.250   1.2668   0.01350   0.00719  -0.0857   0.1028   1.0000
   8.500   1.2848   0.01384   0.00751  -0.0839   0.0979   1.0000
   8.750   1.3022   0.01419   0.00786  -0.0821   0.0914   1.0000
   9.000   1.3181   0.01463   0.00826  -0.0800   0.0835   1.0000
   9.250   1.3319   0.01516   0.00873  -0.0777   0.0718   1.0000
   9.500   1.3445   0.01576   0.00926  -0.0753   0.0604   1.0000
   9.750   1.3577   0.01634   0.00980  -0.0731   0.0531   1.0000
  10.250   1.3845   0.01752   0.01096  -0.0688   0.0427   1.0000
  10.500   1.3966   0.01820   0.01163  -0.0666   0.0382   1.0000
  10.750   1.4098   0.01884   0.01227  -0.0646   0.0350   1.0000
  11.000   1.4218   0.01956   0.01300  -0.0626   0.0320   1.0000
  11.250   1.4334   0.02033   0.01378  -0.0606   0.0289   1.0000
  11.500   1.4447   0.02116   0.01462  -0.0587   0.0266   1.0000
  11.750   1.4560   0.02200   0.01549  -0.0569   0.0243   1.0000
  12.000   1.4659   0.02298   0.01648  -0.0550   0.0223   1.0000
  12.250   1.4764   0.02396   0.01749  -0.0533   0.0203   1.0000
  12.500   1.4851   0.02511   0.01865  -0.0516   0.0186   1.0000
  12.750   1.4947   0.02623   0.01982  -0.0501   0.0174   1.0000
  13.000   1.5033   0.02748   0.02110  -0.0486   0.0162   1.0000
  13.250   1.5104   0.02889   0.02254  -0.0471   0.0150   1.0000
  13.500   1.5186   0.03025   0.02395  -0.0458   0.0144   1.0000
  13.750   1.5261   0.03173   0.02548  -0.0446   0.0138   1.0000
  14.000   1.5318   0.03340   0.02719  -0.0434   0.0130   1.0000
  14.250   1.5370   0.03516   0.02900  -0.0422   0.0125   1.0000
  14.500   1.5415   0.03705   0.03094  -0.0412   0.0119   1.0000
  14.750   1.5470   0.03891   0.03287  -0.0404   0.0117   1.0000
  15.000   1.5516   0.04090   0.03493  -0.0396   0.0113   1.0000
  15.250   1.5552   0.04305   0.03714  -0.0389   0.0109   1.0000
  15.500   1.5577   0.04537   0.03953  -0.0384   0.0105   1.0000
  15.750   1.5596   0.04784   0.04206  -0.0379   0.0103   1.0000
  16.000   1.5605   0.05048   0.04476  -0.0376   0.0100   1.0000
  16.250   1.5597   0.05337   0.04773  -0.0373   0.0097   1.0000
  16.500   1.5584   0.05642   0.05085  -0.0373   0.0095   1.0000
  16.750   1.5586   0.05936   0.05387  -0.0373   0.0093   1.0000
  17.000   1.5581   0.06244   0.05703  -0.0375   0.0091   1.0000
  17.250   1.5563   0.06576   0.06043  -0.0378   0.0090   1.0000
  17.500   1.5548   0.06909   0.06384  -0.0382   0.0087   1.0000
  17.750   1.5516   0.07274   0.06757  -0.0388   0.0085   1.0000
  18.000   1.5477   0.07653   0.07145  -0.0395   0.0085   1.0000
  18.250   1.5439   0.08036   0.07535  -0.0403   0.0082   1.0000
  18.500   1.5388   0.08447   0.07955  -0.0413   0.0080   1.0000
  18.750   1.5337   0.08867   0.08384  -0.0424   0.0079   1.0000
  19.000   1.5278   0.09304   0.08830  -0.0437   0.0078   1.0000
  19.250   1.5208   0.09766   0.09300  -0.0452   0.0077   1.0000
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