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GOE 255 (MVA CA.6) AIRFOIL (goe255-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 255 (MVA CA.6) AIRFOIL (goe255-il)
Reynolds number: 500,000
Max Cl/Cd: 90.51 at α=5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe255-il-500000-n5.txt
Download as CSV file: xf-goe255-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 255 (MVA CA.6) 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -0.6573   0.08941   0.08572  -0.0753   1.0000   0.0087
 -16.250  -0.6657   0.08453   0.08077  -0.0777   1.0000   0.0088
 -16.000  -0.6740   0.07979   0.07597  -0.0800   1.0000   0.0089
 -15.750  -0.6816   0.07509   0.07119  -0.0826   0.9984   0.0089
 -15.500  -0.6849   0.07012   0.06613  -0.0865   0.9937   0.0090
 -15.250  -0.6885   0.06533   0.06125  -0.0901   0.9878   0.0091
 -15.000  -0.6928   0.06071   0.05653  -0.0937   0.9823   0.0092
 -14.750  -0.6978   0.05636   0.05208  -0.0968   0.9755   0.0092
 -14.500  -0.7030   0.05225   0.04787  -0.0995   0.9672   0.0093
 -14.250  -0.7080   0.04843   0.04395  -0.1016   0.9588   0.0094
 -14.000  -0.7138   0.04477   0.04018  -0.1034   0.9484   0.0095
 -13.750  -0.7184   0.04120   0.03651  -0.1051   0.9363   0.0096
 -13.500  -0.7208   0.03779   0.03298  -0.1069   0.9203   0.0098
 -13.250  -0.7220   0.03452   0.02954  -0.1085   0.8881   0.0099
 -13.000  -0.7221   0.03151   0.02623  -0.1099   0.8431   0.0100
 -12.750  -0.7170   0.02874   0.02319  -0.1124   0.8178   0.0102
 -12.500  -0.7101   0.02660   0.02084  -0.1140   0.8027   0.0103
 -12.250  -0.7052   0.02519   0.01924  -0.1133   0.7917   0.0105
 -12.000  -0.6972   0.02377   0.01770  -0.1127   0.7822   0.0108
 -11.750  -0.6832   0.02271   0.01652  -0.1121   0.7741   0.0110
 -11.500  -0.6660   0.02182   0.01553  -0.1117   0.7671   0.0113
 -11.250  -0.6470   0.02104   0.01464  -0.1113   0.7613   0.0117
 -11.000  -0.6268   0.02031   0.01382  -0.1110   0.7564   0.0120
 -10.750  -0.6054   0.01964   0.01306  -0.1107   0.7512   0.0124
 -10.500  -0.5833   0.01902   0.01234  -0.1104   0.7461   0.0128
 -10.250  -0.5603   0.01847   0.01168  -0.1101   0.7415   0.0132
 -10.000  -0.5373   0.01783   0.01097  -0.1099   0.7367   0.0138
  -9.750  -0.5140   0.01723   0.01030  -0.1097   0.7317   0.0145
  -9.500  -0.4897   0.01675   0.00974  -0.1096   0.7271   0.0153
  -9.250  -0.4644   0.01630   0.00921  -0.1095   0.7228   0.0162
  -9.000  -0.4388   0.01587   0.00871  -0.1094   0.7184   0.0172
  -8.750  -0.4136   0.01539   0.00818  -0.1093   0.7139   0.0185
  -8.500  -0.3878   0.01501   0.00772  -0.1093   0.7097   0.0202
  -8.250  -0.3616   0.01459   0.00727  -0.1093   0.7055   0.0228
  -8.000  -0.3354   0.01415   0.00683  -0.1093   0.7008   0.0280
  -7.750  -0.3097   0.01368   0.00638  -0.1093   0.6962   0.0389
  -7.500  -0.2835   0.01327   0.00600  -0.1093   0.6919   0.0537
  -7.250  -0.2564   0.01291   0.00568  -0.1095   0.6872   0.0658
  -7.000  -0.2289   0.01265   0.00540  -0.1096   0.6821   0.0754
  -6.750  -0.2016   0.01237   0.00511  -0.1097   0.6772   0.0857
  -6.500  -0.1740   0.01208   0.00484  -0.1099   0.6722   0.0978
  -6.250  -0.1466   0.01175   0.00459  -0.1100   0.6665   0.1179
  -6.000  -0.1192   0.01149   0.00437  -0.1102   0.6609   0.1423
  -5.750  -0.0911   0.01126   0.00419  -0.1104   0.6550   0.1605
  -5.500  -0.0630   0.01109   0.00402  -0.1106   0.6481   0.1759
  -5.250  -0.0348   0.01094   0.00386  -0.1108   0.6416   0.1900
  -5.000  -0.0066   0.01078   0.00369  -0.1110   0.6336   0.2026
  -4.750   0.0214   0.01066   0.00354  -0.1111   0.6248   0.2128
  -4.500   0.0494   0.01055   0.00339  -0.1112   0.6146   0.2247
  -4.250   0.0774   0.01044   0.00326  -0.1114   0.6047   0.2383
  -4.000   0.1051   0.01032   0.00314  -0.1115   0.5961   0.2562
  -3.750   0.1331   0.01019   0.00307  -0.1117   0.5880   0.2842
  -3.500   0.1609   0.01014   0.00305  -0.1118   0.5801   0.3143
  -3.250   0.1893   0.01016   0.00305  -0.1120   0.5718   0.3326
  -3.000   0.2174   0.01021   0.00304  -0.1121   0.5645   0.3449
  -2.750   0.2461   0.01023   0.00304  -0.1123   0.5587   0.3540
  -2.500   0.2747   0.01029   0.00303  -0.1125   0.5538   0.3628
  -2.000   0.3318   0.01036   0.00304  -0.1129   0.5458   0.3750
  -1.750   0.3606   0.01041   0.00303  -0.1131   0.5418   0.3792
  -1.500   0.3889   0.01044   0.00304  -0.1133   0.5377   0.3829
  -1.000   0.4456   0.01054   0.00308  -0.1137   0.5309   0.3912
  -0.750   0.4744   0.01059   0.00309  -0.1139   0.5279   0.3950
  -0.500   0.5028   0.01062   0.00311  -0.1141   0.5244   0.3982
  -0.250   0.5308   0.01067   0.00315  -0.1143   0.5210   0.4021
   0.000   0.5589   0.01074   0.00320  -0.1144   0.5181   0.4072
   0.250   0.5871   0.01081   0.00324  -0.1146   0.5154   0.4113
   0.500   0.6156   0.01083   0.00328  -0.1148   0.5130   0.4153
   0.750   0.6439   0.01085   0.00334  -0.1151   0.5105   0.4200
   1.000   0.6721   0.01091   0.00340  -0.1152   0.5078   0.4249
   1.250   0.7000   0.01098   0.00346  -0.1154   0.5049   0.4292
   1.500   0.7274   0.01105   0.00353  -0.1155   0.5018   0.4329
   1.750   0.7550   0.01111   0.00361  -0.1156   0.4985   0.4362
   2.000   0.7831   0.01115   0.00368  -0.1158   0.4955   0.4400
   2.250   0.8109   0.01121   0.00376  -0.1159   0.4926   0.4441
   2.500   0.8384   0.01128   0.00385  -0.1160   0.4895   0.4482
   2.750   0.8654   0.01135   0.00394  -0.1160   0.4864   0.4529
   3.000   0.8921   0.01145   0.00405  -0.1160   0.4833   0.4583
   3.500   0.9463   0.01155   0.00426  -0.1161   0.4737   0.4718
   3.750   0.9718   0.01166   0.00439  -0.1158   0.4680   0.4810
   4.000   0.9984   0.01171   0.00451  -0.1158   0.4626   0.4934
   4.250   1.0242   0.01178   0.00466  -0.1157   0.4561   0.5105
   4.500   1.0489   0.01186   0.00481  -0.1153   0.4480   0.5362
   4.750   1.0723   0.01194   0.00499  -0.1147   0.4356   0.5741
   5.000   1.0934   0.01208   0.00521  -0.1137   0.4118   0.6222
   5.500   1.1091   0.01314   0.00620  -0.1070   0.3390   0.7400
   5.750   1.1177   0.01324   0.00669  -0.1032   0.3284   0.9029
   6.000   1.1386   0.01357   0.00704  -0.1023   0.3212   1.0000
   6.250   1.1562   0.01402   0.00746  -0.1009   0.3154   1.0000
   6.500   1.1756   0.01441   0.00785  -0.0997   0.3112   1.0000
   6.750   1.1953   0.01479   0.00825  -0.0987   0.3075   1.0000
   7.000   1.2135   0.01525   0.00870  -0.0975   0.3030   1.0000
   7.500   1.2481   0.01629   0.00973  -0.0949   0.2917   1.0000
   7.750   1.2652   0.01684   0.01029  -0.0937   0.2861   1.0000
   8.000   1.2792   0.01757   0.01098  -0.0921   0.2801   1.0000
   8.250   1.2985   0.01804   0.01149  -0.0912   0.2737   1.0000
   8.500   1.3121   0.01883   0.01224  -0.0897   0.2654   1.0000
   8.750   1.3294   0.01945   0.01289  -0.0887   0.2585   1.0000
   9.000   1.3432   0.02029   0.01371  -0.0874   0.2501   1.0000
   9.250   1.3582   0.02109   0.01452  -0.0863   0.2408   1.0000
   9.500   1.3702   0.02213   0.01552  -0.0849   0.2292   1.0000
   9.750   1.3781   0.02349   0.01680  -0.0833   0.2098   1.0000
  10.000   1.3755   0.02566   0.01881  -0.0809   0.1804   1.0000
  10.250   1.3726   0.02796   0.02100  -0.0786   0.1600   1.0000
  10.500   1.3740   0.03000   0.02299  -0.0769   0.1469   1.0000
  10.750   1.3746   0.03215   0.02508  -0.0751   0.1331   1.0000
  11.000   1.3744   0.03442   0.02729  -0.0735   0.1165   1.0000
  11.250   1.3604   0.03790   0.03057  -0.0711   0.0854   1.0000
  11.500   1.3523   0.04101   0.03359  -0.0692   0.0669   1.0000
  11.750   1.3326   0.04532   0.03773  -0.0669   0.0322   1.0000
  12.000   1.3243   0.04872   0.04112  -0.0655   0.0163   1.0000
  12.250   1.3289   0.05097   0.04343  -0.0648   0.0144   1.0000
  12.500   1.3335   0.05325   0.04577  -0.0641   0.0132   1.0000
  12.750   1.3393   0.05544   0.04803  -0.0636   0.0124   1.0000
  13.000   1.3449   0.05767   0.05034  -0.0632   0.0118   1.0000
  13.250   1.3498   0.06000   0.05274  -0.0628   0.0113   1.0000
  13.500   1.3535   0.06252   0.05533  -0.0624   0.0109   1.0000
  13.750   1.3562   0.06518   0.05806  -0.0620   0.0104   1.0000
  14.000   1.3580   0.06796   0.06094  -0.0617   0.0100   1.0000
  14.250   1.3618   0.07054   0.06359  -0.0615   0.0097   1.0000
  14.500   1.3650   0.07320   0.06632  -0.0613   0.0094   1.0000
  14.750   1.3674   0.07599   0.06920  -0.0612   0.0090   1.0000
  15.000   1.3689   0.07892   0.07220  -0.0611   0.0087   1.0000
  15.250   1.3698   0.08195   0.07531  -0.0611   0.0084   1.0000
  15.500   1.3692   0.08519   0.07863  -0.0611   0.0082   1.0000
  15.750   1.3679   0.08853   0.08205  -0.0612   0.0080   1.0000
  16.000   1.3643   0.09223   0.08585  -0.0614   0.0079   1.0000
  16.250   1.3586   0.09627   0.08999  -0.0617   0.0077   1.0000
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