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EPPLER 604 AIRFOIL (e604-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: EPPLER 604 AIRFOIL (e604-il)
Reynolds number: 1,000,000
Max Cl/Cd: 136.28 at α=6.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-e604-il-1000000.txt
Download as CSV file: xf-e604-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: EPPLER 604 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
  ------ -------- --------- --------- -------- -------- --------
 -16.250  -0.5821   0.09543   0.09324  -0.0770   1.0000   0.0060
 -16.000  -0.6278   0.08266   0.08026  -0.0837   1.0000   0.0059
 -15.750  -0.6526   0.07492   0.07238  -0.0876   1.0000   0.0059
 -15.500  -0.6672   0.06698   0.06426  -0.0939   0.9992   0.0058
 -15.250  -0.6763   0.06005   0.05715  -0.1000   0.9979   0.0058
 -15.000  -0.6813   0.05413   0.05103  -0.1053   0.9959   0.0057
 -14.750  -0.6882   0.04851   0.04518  -0.1098   0.9930   0.0057
 -14.500  -0.6864   0.04460   0.04111  -0.1127   0.9888   0.0057
 -14.250  -0.6826   0.04085   0.03719  -0.1158   0.9841   0.0057
 -14.000  -0.6770   0.03830   0.03452  -0.1170   0.9726   0.0057
 -13.750  -0.6671   0.03537   0.03142  -0.1196   0.9593   0.0057
 -13.500  -0.6427   0.03257   0.02844  -0.1245   0.9487   0.0057
 -13.250  -0.6055   0.03010   0.02580  -0.1314   0.9409   0.0057
 -13.000  -0.5640   0.02793   0.02344  -0.1386   0.9288   0.0057
 -12.750  -0.5331   0.02607   0.02134  -0.1432   0.9064   0.0058
 -12.500  -0.5201   0.02487   0.01993  -0.1432   0.8823   0.0059
 -12.250  -0.5108   0.02394   0.01884  -0.1420   0.8643   0.0061
 -12.000  -0.5025   0.02301   0.01778  -0.1405   0.8495   0.0060
 -11.750  -0.4933   0.02215   0.01681  -0.1391   0.8375   0.0060
 -11.500  -0.4834   0.02134   0.01589  -0.1376   0.8268   0.0060
 -11.250  -0.4731   0.02054   0.01500  -0.1361   0.8171   0.0061
 -11.000  -0.4611   0.01984   0.01420  -0.1347   0.8088   0.0063
 -10.750  -0.4535   0.01890   0.01316  -0.1329   0.8003   0.0065
 -10.500  -0.4424   0.01818   0.01236  -0.1313   0.7931   0.0066
 -10.250  -0.4313   0.01746   0.01157  -0.1297   0.7857   0.0067
 -10.000  -0.4206   0.01676   0.01080  -0.1279   0.7788   0.0070
  -9.750  -0.4064   0.01620   0.01020  -0.1266   0.7727   0.0073
  -9.500  -0.3922   0.01570   0.00964  -0.1251   0.7665   0.0075
  -9.250  -0.3773   0.01522   0.00911  -0.1237   0.7613   0.0082
  -9.000  -0.3637   0.01469   0.00853  -0.1221   0.7560   0.0082
  -8.750  -0.3533   0.01411   0.00790  -0.1200   0.7506   0.0092
  -8.500  -0.3428   0.01368   0.00742  -0.1177   0.7455   0.0098
  -8.250  -0.3303   0.01334   0.00705  -0.1157   0.7409   0.0108
  -8.000  -0.3149   0.01289   0.00658  -0.1142   0.7361   0.0126
  -7.750  -0.2966   0.01256   0.00620  -0.1131   0.7318   0.0147
  -7.500  -0.2757   0.01226   0.00589  -0.1124   0.7281   0.0170
  -7.250  -0.2547   0.01193   0.00557  -0.1117   0.7244   0.0207
  -7.000  -0.2327   0.01164   0.00527  -0.1111   0.7206   0.0245
  -6.750  -0.2102   0.01138   0.00500  -0.1106   0.7167   0.0293
  -6.500  -0.1868   0.01112   0.00474  -0.1102   0.7131   0.0353
  -6.250  -0.1630   0.01083   0.00450  -0.1100   0.7100   0.0435
  -6.000  -0.1389   0.01053   0.00425  -0.1098   0.7068   0.0557
  -5.750  -0.1147   0.01023   0.00401  -0.1096   0.7034   0.0729
  -5.500  -0.0900   0.00994   0.00379  -0.1095   0.6999   0.0949
  -5.250  -0.0655   0.00956   0.00355  -0.1096   0.6968   0.1301
  -5.000  -0.0410   0.00907   0.00328  -0.1097   0.6941   0.1845
  -4.750  -0.0162   0.00846   0.00297  -0.1100   0.6911   0.2607
  -4.500   0.0091   0.00776   0.00262  -0.1105   0.6881   0.3617
  -4.250   0.0354   0.00691   0.00227  -0.1114   0.6851   0.5059
  -4.000   0.0646   0.00682   0.00225  -0.1119   0.6818   0.5529
  -3.750   0.0941   0.00680   0.00224  -0.1124   0.6796   0.5761
  -3.500   0.1235   0.00680   0.00224  -0.1129   0.6769   0.5906
  -3.250   0.1529   0.00681   0.00225  -0.1133   0.6742   0.5997
  -3.000   0.1824   0.00686   0.00224  -0.1138   0.6715   0.6072
  -2.750   0.2116   0.00689   0.00223  -0.1142   0.6687   0.6126
  -2.500   0.2412   0.00699   0.00228  -0.1147   0.6655   0.6187
  -2.250   0.2707   0.00703   0.00229  -0.1152   0.6635   0.6243
  -2.000   0.2997   0.00705   0.00234  -0.1155   0.6610   0.6312
  -1.750   0.3289   0.00713   0.00240  -0.1159   0.6583   0.6376
  -1.500   0.3581   0.00720   0.00244  -0.1163   0.6557   0.6435
  -1.250   0.3869   0.00727   0.00251  -0.1166   0.6530   0.6482
  -1.000   0.4163   0.00736   0.00255  -0.1171   0.6498   0.6508
  -0.750   0.4454   0.00737   0.00255  -0.1175   0.6476   0.6527
  -0.500   0.4744   0.00737   0.00255  -0.1180   0.6450   0.6545
  -0.250   0.5035   0.00739   0.00254  -0.1184   0.6423   0.6560
   0.000   0.5326   0.00742   0.00254  -0.1189   0.6395   0.6573
   0.250   0.5614   0.00743   0.00253  -0.1193   0.6366   0.6591
   0.500   0.5904   0.00749   0.00256  -0.1198   0.6333   0.6610
   0.750   0.6189   0.00748   0.00258  -0.1201   0.6310   0.6627
   1.000   0.6475   0.00750   0.00261  -0.1204   0.6281   0.6643
   1.250   0.6760   0.00752   0.00264  -0.1208   0.6251   0.6659
   1.500   0.7044   0.00756   0.00267  -0.1211   0.6220   0.6676
   1.750   0.7328   0.00763   0.00271  -0.1215   0.6185   0.6693
   2.000   0.7612   0.00767   0.00276  -0.1218   0.6154   0.6711
   2.250   0.7892   0.00769   0.00279  -0.1220   0.6117   0.6728
   2.500   0.8171   0.00773   0.00282  -0.1223   0.6078   0.6742
   2.750   0.8445   0.00776   0.00285  -0.1224   0.6038   0.6762
   3.000   0.8720   0.00780   0.00291  -0.1226   0.5998   0.6781
   3.250   0.8993   0.00781   0.00296  -0.1227   0.5955   0.6798
   3.500   0.9263   0.00786   0.00302  -0.1228   0.5908   0.6816
   3.750   0.9527   0.00796   0.00309  -0.1227   0.5859   0.6834
   4.000   0.9799   0.00798   0.00316  -0.1228   0.5815   0.6853
   4.250   1.0065   0.00803   0.00323  -0.1228   0.5762   0.6873
   4.500   1.0319   0.00814   0.00331  -0.1226   0.5707   0.6892
   4.750   1.0585   0.00820   0.00340  -0.1226   0.5651   0.6908
   5.000   1.0837   0.00825   0.00347  -0.1223   0.5584   0.6931
   5.250   1.1081   0.00833   0.00357  -0.1219   0.5520   0.6952
   5.500   1.1329   0.00841   0.00368  -0.1215   0.5444   0.6971
   5.750   1.1558   0.00854   0.00380  -0.1208   0.5365   0.6992
   6.000   1.1787   0.00866   0.00393  -0.1201   0.5270   0.7013
   6.250   1.1993   0.00880   0.00407  -0.1189   0.5172   0.7035
   6.500   1.2166   0.00898   0.00422  -0.1171   0.5058   0.7056
   6.750   1.2347   0.00918   0.00440  -0.1154   0.4940   0.7075
   7.000   1.2527   0.00939   0.00461  -0.1138   0.4814   0.7102
   7.250   1.2687   0.00967   0.00488  -0.1118   0.4674   0.7128
   7.500   1.2836   0.01000   0.00518  -0.1097   0.4525   0.7152
   7.750   1.2975   0.01038   0.00552  -0.1074   0.4368   0.7176
   8.000   1.3093   0.01083   0.00592  -0.1049   0.4187   0.7202
   8.250   1.3186   0.01138   0.00639  -0.1019   0.3993   0.7226
   8.500   1.3267   0.01200   0.00693  -0.0989   0.3793   0.7247
   8.750   1.3341   0.01265   0.00753  -0.0959   0.3582   0.7278
   9.000   1.3393   0.01344   0.00825  -0.0926   0.3372   0.7306
   9.250   1.3437   0.01432   0.00906  -0.0894   0.3170   0.7335
   9.500   1.3488   0.01525   0.00993  -0.0865   0.2971   0.7365
   9.750   1.3528   0.01630   0.01090  -0.0835   0.2774   0.7394
  10.000   1.3571   0.01740   0.01192  -0.0808   0.2595   0.7422
  10.250   1.3600   0.01861   0.01308  -0.0780   0.2412   0.7455
  10.500   1.3654   0.01977   0.01421  -0.0757   0.2260   0.7486
  10.750   1.3693   0.02108   0.01546  -0.0733   0.2099   0.7518
  11.000   1.3750   0.02234   0.01669  -0.0713   0.1960   0.7549
  11.250   1.3788   0.02377   0.01806  -0.0692   0.1807   0.7577
  11.500   1.3836   0.02518   0.01944  -0.0673   0.1668   0.7613
  11.750   1.3894   0.02658   0.02083  -0.0656   0.1548   0.7648
  12.000   1.3942   0.02810   0.02232  -0.0639   0.1425   0.7684
  12.250   1.4004   0.02958   0.02379  -0.0624   0.1326   0.7721
  12.500   1.4051   0.03121   0.02539  -0.0609   0.1221   0.7758
  12.750   1.4103   0.03284   0.02702  -0.0596   0.1122   0.7799
  13.000   1.4176   0.03436   0.02855  -0.0585   0.1043   0.7841
  13.250   1.4223   0.03615   0.03032  -0.0573   0.0956   0.7883
  13.500   1.4276   0.03792   0.03209  -0.0562   0.0876   0.7924
  13.750   1.4335   0.03967   0.03386  -0.0552   0.0798   0.7970
  14.000   1.4378   0.04162   0.03581  -0.0542   0.0730   0.8020
  14.250   1.4439   0.04347   0.03766  -0.0535   0.0665   0.8070
  14.500   1.4491   0.04542   0.03964  -0.0527   0.0610   0.8129
  14.750   1.4527   0.04755   0.04177  -0.0520   0.0545   0.8193
  15.000   1.4578   0.04960   0.04386  -0.0514   0.0492   0.8262
  15.250   1.4617   0.05179   0.04608  -0.0508   0.0446   0.8345
  15.500   1.4659   0.05401   0.04834  -0.0503   0.0400   0.8436
  16.000   1.4736   0.05854   0.05299  -0.0494   0.0332   0.8708
  16.250   1.4759   0.06076   0.05534  -0.0487   0.0303   0.9025
  16.500   1.4793   0.06298   0.05770  -0.0484   0.0280   1.0000
  16.750   1.4823   0.06564   0.06039  -0.0484   0.0257   1.0000
  17.000   1.4873   0.06811   0.06290  -0.0485   0.0239   1.0000
  17.250   1.4885   0.07107   0.06589  -0.0487   0.0217   1.0000
  17.500   1.4933   0.07362   0.06849  -0.0489   0.0203   1.0000
  17.750   1.4954   0.07657   0.07149  -0.0492   0.0191   1.0000
  18.000   1.4963   0.07970   0.07466  -0.0496   0.0176   1.0000
  18.250   1.4995   0.08260   0.07763  -0.0501   0.0166   1.0000
  18.500   1.5004   0.08582   0.08089  -0.0507   0.0154   1.0000
  18.750   1.4998   0.08929   0.08441  -0.0514   0.0143   1.0000
  19.000   1.5016   0.09248   0.08767  -0.0522   0.0135   1.0000
  19.250   1.5021   0.09588   0.09114  -0.0531   0.0128   1.0000
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