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GOE 704 AIRFOIL (goe704-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 704 AIRFOIL (goe704-il)
Reynolds number: 1,000,000
Max Cl/Cd: 90.11 at α=8.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe704-il-1000000.txt
Download as CSV file: xf-goe704-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 704 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
  ------ -------- --------- --------- -------- -------- --------
 -16.500  -1.0772   0.08830   0.08555  -0.0151   1.0000   0.0102
 -16.250  -1.1384   0.07459   0.07168  -0.0227   1.0000   0.0100
 -16.000  -1.2316   0.05018   0.04685  -0.0413   1.0000   0.0096
 -15.750  -1.2590   0.04184   0.03825  -0.0474   1.0000   0.0096
 -15.500  -1.2702   0.03817   0.03442  -0.0475   1.0000   0.0097
 -15.250  -1.2764   0.03550   0.03163  -0.0463   1.0000   0.0098
 -15.000  -1.2788   0.03340   0.02941  -0.0445   1.0000   0.0099
 -14.750  -1.2787   0.03163   0.02754  -0.0423   1.0000   0.0100
 -14.500  -1.2761   0.03013   0.02593  -0.0399   1.0000   0.0102
 -14.250  -1.2721   0.02880   0.02449  -0.0373   1.0000   0.0103
 -14.000  -1.2664   0.02764   0.02323  -0.0346   1.0000   0.0105
 -13.750  -1.2588   0.02662   0.02211  -0.0319   1.0000   0.0107
 -13.500  -1.2464   0.02565   0.02105  -0.0300   1.0000   0.0109
 -13.250  -1.2315   0.02478   0.02009  -0.0284   1.0000   0.0110
 -13.000  -1.2145   0.02401   0.01923  -0.0270   1.0000   0.0112
 -12.750  -1.2065   0.02246   0.01754  -0.0245   1.0000   0.0116
 -12.500  -1.1913   0.02141   0.01641  -0.0228   1.0000   0.0120
 -12.250  -1.1727   0.02061   0.01554  -0.0216   1.0000   0.0123
 -12.000  -1.1525   0.01992   0.01479  -0.0206   1.0000   0.0127
 -11.750  -1.1316   0.01927   0.01408  -0.0196   1.0000   0.0131
 -11.500  -1.1101   0.01865   0.01340  -0.0187   1.0000   0.0135
 -11.250  -1.0876   0.01811   0.01280  -0.0179   1.0000   0.0139
 -11.000  -1.0668   0.01738   0.01198  -0.0169   1.0000   0.0145
 -10.750  -1.0458   0.01664   0.01119  -0.0159   1.0000   0.0153
 -10.500  -1.0228   0.01612   0.01065  -0.0152   1.0000   0.0160
 -10.250  -0.9997   0.01566   0.01014  -0.0145   1.0000   0.0167
 -10.000  -0.9675   0.01521   0.00963  -0.0156   0.9902   0.0174
  -9.750  -0.9382   0.01447   0.00885  -0.0163   0.9763   0.0191
  -9.500  -0.9115   0.01405   0.00838  -0.0161   0.9581   0.0204
  -9.250  -0.8893   0.01368   0.00794  -0.0149   0.9373   0.0219
  -9.000  -0.8674   0.01326   0.00747  -0.0136   0.9166   0.0244
  -8.750  -0.8442   0.01291   0.00703  -0.0126   0.8975   0.0273
  -8.500  -0.8200   0.01257   0.00665  -0.0118   0.8800   0.0310
  -8.250  -0.7955   0.01220   0.00623  -0.0112   0.8639   0.0357
  -8.000  -0.7701   0.01189   0.00587  -0.0107   0.8493   0.0404
  -7.750  -0.7442   0.01163   0.00557  -0.0103   0.8365   0.0449
  -7.500  -0.7184   0.01131   0.00522  -0.0099   0.8252   0.0509
  -7.250  -0.6920   0.01104   0.00493  -0.0096   0.8147   0.0571
  -7.000  -0.6654   0.01079   0.00467  -0.0093   0.8056   0.0640
  -6.750  -0.6388   0.01054   0.00442  -0.0091   0.7972   0.0729
  -6.500  -0.6117   0.01032   0.00423  -0.0090   0.7899   0.0819
  -6.250  -0.5842   0.01016   0.00406  -0.0089   0.7828   0.0892
  -6.000  -0.5566   0.01004   0.00393  -0.0088   0.7765   0.0959
  -5.750  -0.5285   0.00991   0.00378  -0.0088   0.7705   0.1005
  -5.500  -0.5008   0.00979   0.00365  -0.0087   0.7648   0.1064
  -5.250  -0.4723   0.00974   0.00357  -0.0088   0.7596   0.1108
  -5.000  -0.4445   0.00959   0.00341  -0.0088   0.7544   0.1159
  -4.750  -0.4165   0.00948   0.00329  -0.0087   0.7494   0.1200
  -4.500  -0.3882   0.00940   0.00318  -0.0088   0.7446   0.1232
  -4.250  -0.3595   0.00934   0.00309  -0.0089   0.7400   0.1254
  -4.000  -0.3318   0.00917   0.00291  -0.0088   0.7351   0.1301
  -3.750  -0.3038   0.00908   0.00281  -0.0088   0.7301   0.1343
  -3.500  -0.2753   0.00898   0.00270  -0.0088   0.7243   0.1379
  -3.250  -0.2468   0.00893   0.00260  -0.0089   0.7168   0.1403
  -3.000  -0.2190   0.00877   0.00245  -0.0088   0.7101   0.1464
  -2.750  -0.1907   0.00866   0.00236  -0.0089   0.7047   0.1518
  -2.500  -0.1622   0.00861   0.00227  -0.0089   0.6999   0.1555
  -2.250  -0.1341   0.00848   0.00216  -0.0089   0.6952   0.1629
  -2.000  -0.1056   0.00836   0.00207  -0.0090   0.6903   0.1694
  -1.750  -0.0775   0.00825   0.00198  -0.0090   0.6852   0.1797
  -1.500  -0.0494   0.00814   0.00191  -0.0090   0.6803   0.1945
  -1.250  -0.0214   0.00796   0.00184  -0.0091   0.6749   0.2195
  -1.000   0.0061   0.00778   0.00178  -0.0090   0.6693   0.2557
  -0.750   0.0337   0.00763   0.00173  -0.0090   0.6627   0.2907
  -0.500   0.0615   0.00747   0.00168  -0.0089   0.6542   0.3246
  -0.250   0.0890   0.00732   0.00163  -0.0089   0.6456   0.3637
   0.000   0.1157   0.00708   0.00158  -0.0087   0.6374   0.4221
   0.250   0.1400   0.00664   0.00152  -0.0081   0.6305   0.5378
   0.500   0.1511   0.00548   0.00152  -0.0044   0.6233   0.8667
   0.750   0.1783   0.00552   0.00160  -0.0040   0.6151   0.8968
   1.000   0.2059   0.00558   0.00165  -0.0037   0.6053   0.9120
   1.250   0.2334   0.00566   0.00170  -0.0034   0.5946   0.9232
   1.500   0.2611   0.00576   0.00177  -0.0032   0.5802   0.9307
   1.750   0.2877   0.00589   0.00182  -0.0028   0.5602   0.9382
   2.000   0.3147   0.00605   0.00191  -0.0024   0.5369   0.9441
   2.250   0.3412   0.00624   0.00201  -0.0019   0.5130   0.9503
   2.500   0.3668   0.00644   0.00210  -0.0014   0.4867   0.9555
   2.750   0.3949   0.00670   0.00226  -0.0013   0.4576   0.9598
   3.000   0.4227   0.00700   0.00243  -0.0013   0.4289   0.9651
   3.250   0.4483   0.00725   0.00258  -0.0007   0.4030   0.9700
   3.500   0.4842   0.00755   0.00277  -0.0025   0.3782   0.9722
   4.000   0.5637   0.00822   0.00322  -0.0080   0.3313   0.9756
   4.250   0.5988   0.00847   0.00340  -0.0097   0.3133   0.9773
   4.500   0.6300   0.00868   0.00354  -0.0106   0.2989   0.9794
   4.750   0.6551   0.00888   0.00369  -0.0101   0.2868   0.9825
   5.000   0.6922   0.00909   0.00384  -0.0123   0.2730   0.9832
   5.250   0.7261   0.00929   0.00398  -0.0138   0.2595   0.9839
   5.500   0.7568   0.00946   0.00411  -0.0147   0.2473   0.9844
   5.750   0.7871   0.00962   0.00424  -0.0154   0.2369   0.9850
   6.000   0.8169   0.00981   0.00439  -0.0161   0.2269   0.9857
   6.500   0.8757   0.01022   0.00471  -0.0173   0.2052   0.9872
   6.750   0.9047   0.01042   0.00489  -0.0179   0.1965   0.9881
   7.000   0.9332   0.01066   0.00508  -0.0183   0.1872   0.9891
   7.250   0.9620   0.01085   0.00527  -0.0188   0.1800   0.9902
   7.500   0.9896   0.01111   0.00549  -0.0191   0.1713   0.9915
   7.750   1.0167   0.01131   0.00569  -0.0192   0.1638   0.9928
   8.000   1.0432   0.01159   0.00593  -0.0193   0.1546   0.9938
   8.250   1.0723   0.01190   0.00619  -0.0200   0.1418   0.9943
   8.500   1.0997   0.01237   0.00653  -0.0205   0.1176   0.9950
   8.750   1.1248   0.01308   0.00705  -0.0208   0.0904   0.9959
   9.000   1.1514   0.01358   0.00749  -0.0211   0.0817   0.9967
   9.250   1.1789   0.01394   0.00787  -0.0216   0.0757   0.9976
   9.500   1.2050   0.01444   0.00834  -0.0218   0.0668   0.9986
   9.750   1.2227   0.01582   0.00939  -0.0212   0.0266   0.9998
  10.000   1.2356   0.01651   0.01006  -0.0189   0.0204   1.0000
  10.250   1.2454   0.01702   0.01059  -0.0159   0.0183   1.0000
  10.500   1.2545   0.01746   0.01106  -0.0127   0.0172   1.0000
  10.750   1.2596   0.01795   0.01158  -0.0088   0.0163   1.0000
  11.000   1.2599   0.01849   0.01217  -0.0040   0.0154   1.0000
  11.250   1.2536   0.01891   0.01264   0.0021   0.0150   1.0000
  11.500   1.2582   0.01943   0.01321   0.0057   0.0146   1.0000
  11.750   1.2677   0.02011   0.01395   0.0081   0.0141   1.0000
  12.000   1.2786   0.02091   0.01479   0.0099   0.0135   1.0000
  12.250   1.2889   0.02185   0.01578   0.0116   0.0130   1.0000
  12.500   1.2964   0.02309   0.01708   0.0133   0.0124   1.0000
  12.750   1.3022   0.02456   0.01864   0.0149   0.0120   1.0000
  13.000   1.3138   0.02567   0.01981   0.0158   0.0117   1.0000
  13.250   1.3238   0.02695   0.02115   0.0167   0.0114   1.0000
  13.500   1.3326   0.02839   0.02267   0.0176   0.0111   1.0000
  13.750   1.3405   0.02996   0.02431   0.0183   0.0109   1.0000
  14.000   1.3470   0.03169   0.02610   0.0189   0.0106   1.0000
  14.250   1.3525   0.03359   0.02807   0.0195   0.0104   1.0000
  14.500   1.3557   0.03574   0.03030   0.0199   0.0102   1.0000
  14.750   1.3560   0.03824   0.03288   0.0203   0.0100   1.0000
  15.000   1.3519   0.04128   0.03601   0.0205   0.0098   1.0000
  15.250   1.3417   0.04506   0.03992   0.0206   0.0096   1.0000
  15.500   1.3274   0.04955   0.04453   0.0202   0.0094   1.0000
  15.750   1.3268   0.05264   0.04772   0.0197   0.0093   1.0000
  16.000   1.3242   0.05610   0.05127   0.0190   0.0093   1.0000
  16.250   1.3196   0.05995   0.05523   0.0180   0.0092   1.0000
  16.500   1.3134   0.06418   0.05955   0.0168   0.0091   1.0000
  16.750   1.3060   0.06865   0.06413   0.0154   0.0090   1.0000
  17.000   1.2966   0.07356   0.06915   0.0137   0.0089   1.0000
  17.250   1.2861   0.07873   0.07443   0.0118   0.0089   1.0000
  17.500   1.2750   0.08404   0.07984   0.0099   0.0088   1.0000
  17.750   1.2633   0.08952   0.08542   0.0078   0.0087   1.0000
  18.000   1.2514   0.09508   0.09109   0.0056   0.0086   1.0000
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