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Glenn Martin 3 (glennmartin3-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: Glenn Martin 3 (glennmartin3-il)
Reynolds number: 500,000
Max Cl/Cd: 62.62 at α=6.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-glennmartin3-il-500000-n5.txt
Download as CSV file: xf-glennmartin3-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: Glenn Martin 3                                  
  
 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
  ------ -------- --------- --------- -------- -------- --------
 -12.500  -0.6591   0.04266   0.03960  -0.1107   0.9622   0.0143
 -12.250  -0.5942   0.04758   0.04482  -0.1107   0.9627   0.0146
 -12.000  -0.7216   0.03448   0.03069  -0.0988   0.9508   0.0146
 -11.750  -0.7054   0.03379   0.02991  -0.0972   0.9491   0.0152
 -11.500  -0.7248   0.03165   0.02751  -0.0896   0.9415   0.0153
 -11.250  -0.7211   0.02948   0.02502  -0.0862   0.9384   0.0157
 -10.750  -0.7142   0.02644   0.02152  -0.0778   0.9286   0.0164
 -10.500  -0.6921   0.02600   0.02106  -0.0767   0.9266   0.0167
 -10.250  -0.6677   0.02563   0.02065  -0.0759   0.9252   0.0170
 -10.000  -0.6567   0.02502   0.01995  -0.0726   0.9204   0.0172
  -9.750  -0.6397   0.02473   0.01962  -0.0702   0.9162   0.0177
  -9.500  -0.6219   0.02371   0.01844  -0.0683   0.9138   0.0180
  -9.250  -0.5994   0.02300   0.01759  -0.0672   0.9122   0.0187
  -9.000  -0.5788   0.02174   0.01605  -0.0657   0.9109   0.0195
  -8.750  -0.5680   0.02141   0.01565  -0.0621   0.9049   0.0198
  -8.500  -0.5487   0.02085   0.01504  -0.0602   0.9015   0.0201
  -8.250  -0.5249   0.02055   0.01472  -0.0592   0.8995   0.0206
  -8.000  -0.5011   0.01989   0.01397  -0.0581   0.8980   0.0209
  -7.750  -0.4722   0.01949   0.01351  -0.0581   0.8962   0.0217
  -7.500  -0.4567   0.01897   0.01286  -0.0553   0.8910   0.0222
  -7.250  -0.4351   0.01847   0.01222  -0.0536   0.8860   0.0231
  -7.000  -0.4083   0.01778   0.01140  -0.0532   0.8833   0.0236
  -6.750  -0.3782   0.01724   0.01084  -0.0535   0.8812   0.0241
  -6.500  -0.3446   0.01665   0.01022  -0.0545   0.8794   0.0248
  -6.250  -0.3304   0.01642   0.00994  -0.0513   0.8714   0.0253
  -6.000  -0.3003   0.01592   0.00937  -0.0515   0.8680   0.0260
  -5.750  -0.2676   0.01549   0.00886  -0.0523   0.8658   0.0271
  -5.500  -0.2318   0.01500   0.00827  -0.0538   0.8637   0.0277
  -5.250  -0.2056   0.01449   0.00772  -0.0533   0.8589   0.0281
  -5.000  -0.1787   0.01411   0.00733  -0.0529   0.8535   0.0290
  -4.750  -0.1455   0.01375   0.00696  -0.0539   0.8499   0.0300
  -4.500  -0.1082   0.01329   0.00646  -0.0558   0.8470   0.0308
  -4.250  -0.0764   0.01297   0.00611  -0.0565   0.8430   0.0316
  -4.000  -0.0504   0.01269   0.00578  -0.0559   0.8357   0.0321
  -3.750  -0.0062   0.01226   0.00527  -0.0593   0.8283   0.0333
  -3.500   0.0181   0.01199   0.00500  -0.0583   0.8194   0.0343
  -3.250   0.0561   0.01169   0.00463  -0.0604   0.8083   0.0351
  -3.000   0.0832   0.01150   0.00439  -0.0601   0.7944   0.0359
  -2.750   0.1083   0.01137   0.00419  -0.0593   0.7765   0.0368
  -2.500   0.1319   0.01126   0.00400  -0.0582   0.7587   0.0383
  -2.250   0.1542   0.01116   0.00383  -0.0568   0.7388   0.0397
  -2.000   0.1722   0.01113   0.00368  -0.0544   0.7036   0.0413
  -1.750   0.1826   0.01127   0.00360  -0.0504   0.6589   0.0425
  -1.500   0.1885   0.01154   0.00362  -0.0455   0.6120   0.0438
  -1.250   0.2023   0.01170   0.00363  -0.0424   0.5777   0.0467
  -1.000   0.2164   0.01188   0.00367  -0.0394   0.5409   0.0490
  -0.750   0.2250   0.01219   0.00376  -0.0354   0.4828   0.0592
  -0.500   0.2411   0.01239   0.00382  -0.0329   0.4495   0.0699
  -0.250   0.2646   0.01236   0.00387  -0.0323   0.4278   0.1206
   0.250   0.3085   0.01252   0.00400  -0.0300   0.4004   0.1651
   0.500   0.3310   0.01259   0.00406  -0.0290   0.3895   0.1808
   0.750   0.3548   0.01262   0.00412  -0.0283   0.3797   0.2031
   1.000   0.3927   0.01200   0.00426  -0.0313   0.3672   0.4646
   1.250   0.6295   0.01325   0.00662  -0.0788   0.3191   0.9832
   1.500   0.6656   0.01354   0.00677  -0.0809   0.3010   0.9869
   1.750   0.7130   0.01374   0.00683  -0.0856   0.2832   0.9921
   2.000   0.7583   0.01387   0.00682  -0.0898   0.2656   0.9967
   2.250   0.7969   0.01394   0.00677  -0.0926   0.2530   0.9996
   2.500   0.8184   0.01412   0.00688  -0.0916   0.2441   1.0000
   2.750   0.8365   0.01433   0.00702  -0.0898   0.2369   1.0000
   3.000   0.8548   0.01454   0.00718  -0.0880   0.2296   1.0000
   3.250   0.8732   0.01475   0.00734  -0.0863   0.2249   1.0000
   3.500   0.8922   0.01494   0.00750  -0.0847   0.2205   1.0000
   3.750   0.9113   0.01514   0.00767  -0.0831   0.2161   1.0000
   4.000   0.9301   0.01535   0.00786  -0.0816   0.2124   1.0000
   4.250   0.9484   0.01560   0.00807  -0.0799   0.2085   1.0000
   4.500   0.9674   0.01582   0.00828  -0.0784   0.2057   1.0000
   4.750   0.9865   0.01603   0.00849  -0.0769   0.2034   1.0000
   5.000   1.0053   0.01625   0.00871  -0.0754   0.2005   1.0000
   5.250   1.0240   0.01650   0.00894  -0.0739   0.1980   1.0000
   5.500   1.0422   0.01678   0.00920  -0.0723   0.1950   1.0000
   5.750   1.0604   0.01706   0.00948  -0.0708   0.1925   1.0000
   6.000   1.0785   0.01735   0.00976  -0.0692   0.1909   1.0000
   6.250   1.0975   0.01759   0.01003  -0.0678   0.1892   1.0000
   6.500   1.1161   0.01785   0.01032  -0.0664   0.1879   1.0000
   6.750   1.1347   0.01812   0.01060  -0.0651   0.1855   1.0000
   7.000   1.1531   0.01842   0.01091  -0.0637   0.1837   1.0000
   7.250   1.1708   0.01874   0.01124  -0.0622   0.1818   1.0000
   7.500   1.1881   0.01908   0.01160  -0.0606   0.1803   1.0000
   7.750   1.2051   0.01944   0.01197  -0.0591   0.1787   1.0000
   8.000   1.2218   0.01983   0.01238  -0.0575   0.1772   1.0000
   8.250   1.2379   0.02026   0.01282  -0.0559   0.1755   1.0000
   8.500   1.2558   0.02059   0.01320  -0.0546   0.1745   1.0000
   8.750   1.2731   0.02095   0.01360  -0.0532   0.1736   1.0000
   9.000   1.2903   0.02133   0.01404  -0.0518   0.1728   1.0000
   9.250   1.3075   0.02172   0.01448  -0.0505   0.1716   1.0000
   9.500   1.3239   0.02215   0.01495  -0.0491   0.1706   1.0000
   9.750   1.3402   0.02258   0.01544  -0.0477   0.1694   1.0000
  10.000   1.3566   0.02302   0.01593  -0.0463   0.1685   1.0000
  10.250   1.3721   0.02352   0.01646  -0.0449   0.1672   1.0000
  10.500   1.3873   0.02403   0.01701  -0.0434   0.1658   1.0000
  10.750   1.4011   0.02461   0.01758  -0.0419   0.1624   1.0000
  11.000   1.4153   0.02519   0.01820  -0.0404   0.1600   1.0000
  11.250   1.4310   0.02569   0.01878  -0.0391   0.1591   1.0000
  11.500   1.4479   0.02612   0.01927  -0.0381   0.1557   1.0000
  11.750   1.4627   0.02668   0.01989  -0.0369   0.1538   1.0000
  12.000   1.4768   0.02729   0.02056  -0.0355   0.1519   1.0000
  12.250   1.4894   0.02800   0.02128  -0.0341   0.1490   1.0000
  12.500   1.5008   0.02880   0.02210  -0.0325   0.1461   1.0000
  12.750   1.5157   0.02940   0.02280  -0.0315   0.1448   1.0000
  13.000   1.5296   0.03008   0.02356  -0.0303   0.1431   1.0000
  13.250   1.5430   0.03079   0.02435  -0.0291   0.1412   1.0000
  13.500   1.5546   0.03163   0.02523  -0.0278   0.1374   1.0000
  13.750   1.5649   0.03257   0.02621  -0.0265   0.1349   1.0000
  14.000   1.5764   0.03345   0.02716  -0.0253   0.1317   1.0000
  14.250   1.5866   0.03445   0.02817  -0.0241   0.1234   1.0000
  14.750   1.6029   0.03680   0.03061  -0.0214   0.1130   1.0000
  15.000   1.6072   0.03833   0.03214  -0.0199   0.1044   1.0000
  15.250   1.5921   0.04153   0.03518  -0.0170   0.0823   1.0000
  15.500   1.5866   0.04403   0.03770  -0.0152   0.0737   1.0000
  15.750   1.5787   0.04689   0.04059  -0.0135   0.0649   1.0000
  16.000   1.5328   0.05382   0.04741  -0.0107   0.0387   1.0000
  16.250   1.5248   0.05719   0.05086  -0.0100   0.0347   1.0000
  16.500   1.5014   0.06261   0.05636  -0.0095   0.0270   1.0000
  16.750   1.4770   0.06849   0.06234  -0.0097   0.0218   1.0000
  17.000   1.4527   0.07474   0.06872  -0.0105   0.0189   1.0000
  17.250   1.4375   0.07999   0.07412  -0.0115   0.0184   1.0000
  17.500   1.4180   0.08607   0.08034  -0.0130   0.0177   1.0000
  17.750   1.3911   0.09336   0.08778  -0.0149   0.0165   1.0000
  18.000   1.3715   0.09959   0.09417  -0.0166   0.0168   1.0000
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