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GOE 484 AIRFOIL (goe484-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 484 AIRFOIL (goe484-il)
Reynolds number: 500,000
Max Cl/Cd: 93.42 at α=2.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe484-il-500000-n5.txt
Download as CSV file: xf-goe484-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 484 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
  ------ -------- --------- --------- -------- -------- --------
 -11.750  -0.3831   0.13139   0.12888  -0.0290   1.0000   0.0099
 -11.500  -0.3821   0.12770   0.12520  -0.0295   1.0000   0.0105
 -11.250  -0.3839   0.12331   0.12084  -0.0303   1.0000   0.0109
 -11.000  -0.3788   0.12150   0.11904  -0.0301   1.0000   0.0110
 -10.750  -0.3764   0.11896   0.11651  -0.0301   1.0000   0.0111
 -10.500  -0.3739   0.11664   0.11421  -0.0299   1.0000   0.0112
 -10.250  -0.3714   0.11451   0.11210  -0.0295   1.0000   0.0116
 -10.000  -0.3632   0.11114   0.10873  -0.0315   0.9993   0.0117
  -9.750  -0.3508   0.10765   0.10525  -0.0345   0.9981   0.0123
  -9.500  -0.3394   0.10367   0.10126  -0.0379   0.9965   0.0131
  -9.250  -0.3334   0.09745   0.09504  -0.0430   0.9942   0.0139
  -9.000  -0.3202   0.09470   0.09228  -0.0454   0.9920   0.0141
  -8.750  -0.3052   0.09219   0.08977  -0.0479   0.9898   0.0144
  -8.500  -0.2906   0.08883   0.08640  -0.0515   0.9875   0.0146
  -8.250  -0.2742   0.08586   0.08343  -0.0550   0.9850   0.0153
  -8.000  -0.2614   0.08229   0.07986  -0.0586   0.9801   0.0161
  -7.750  -0.2473   0.07760   0.07516  -0.0643   0.9757   0.0169
  -7.500  -0.2332   0.07062   0.06817  -0.0740   0.9682   0.0177
  -7.250  -0.2123   0.06854   0.06608  -0.0768   0.9644   0.0180
  -7.000  -0.1908   0.06564   0.06316  -0.0811   0.9595   0.0184
  -6.750  -0.1632   0.06278   0.06028  -0.0866   0.9569   0.0194
  -6.500  -0.1385   0.05846   0.05592  -0.0936   0.9504   0.0202
  -6.250  -0.1055   0.05274   0.05012  -0.1039   0.9456   0.0208
  -6.000  -0.0661   0.04189   0.03906  -0.1205   0.9362   0.0223
  -5.750  -0.0369   0.03977   0.03687  -0.1242   0.9325   0.0229
  -5.500  -0.0110   0.03718   0.03420  -0.1272   0.9250   0.0233
  -5.250   0.0236   0.03163   0.02840  -0.1338   0.9193   0.0236
  -5.000   0.0523   0.02564   0.02206  -0.1381   0.9115   0.0239
  -4.750   0.0819   0.02030   0.01620  -0.1413   0.9059   0.0247
  -4.500   0.1081   0.01742   0.01286  -0.1421   0.8992   0.0251
  -4.250   0.1357   0.01570   0.01080  -0.1427   0.8933   0.0254
  -4.000   0.1631   0.01452   0.00936  -0.1429   0.8875   0.0258
  -3.750   0.1902   0.01359   0.00820  -0.1429   0.8807   0.0261
  -3.250   0.2450   0.01216   0.00642  -0.1429   0.8691   0.0265
  -3.000   0.2725   0.01161   0.00573  -0.1428   0.8635   0.0268
  -2.750   0.3003   0.01123   0.00524  -0.1427   0.8585   0.0273
  -2.500   0.3272   0.01085   0.00477  -0.1425   0.8526   0.0275
  -2.250   0.3546   0.01042   0.00425  -0.1423   0.8469   0.0277
  -2.000   0.3818   0.01005   0.00381  -0.1421   0.8411   0.0278
  -1.750   0.4088   0.00974   0.00345  -0.1418   0.8345   0.0279
  -1.500   0.4361   0.00944   0.00310  -0.1416   0.8284   0.0281
  -1.250   0.4625   0.00898   0.00261  -0.1413   0.8217   0.0287
  -1.000   0.4895   0.00869   0.00229  -0.1410   0.8152   0.0294
  -0.750   0.5163   0.00849   0.00209  -0.1407   0.8082   0.0300
  -0.500   0.5432   0.00835   0.00193  -0.1404   0.8006   0.0306
  -0.250   0.5699   0.00823   0.00182  -0.1401   0.7924   0.0312
   0.000   0.5967   0.00816   0.00171  -0.1397   0.7829   0.0318
   0.250   0.6227   0.00810   0.00163  -0.1392   0.7683   0.0330
   0.500   0.6473   0.00810   0.00154  -0.1383   0.7399   0.0341
   0.750   0.6696   0.00823   0.00146  -0.1369   0.6903   0.0348
   1.000   0.6909   0.00849   0.00145  -0.1353   0.6443   0.0354
   1.500   0.7374   0.00890   0.00158  -0.1332   0.5872   0.0401
   1.750   0.7616   0.00895   0.00169  -0.1324   0.5642   0.0913
   2.000   0.7861   0.00903   0.00183  -0.1317   0.5437   0.1411
   2.250   0.8102   0.00916   0.00196  -0.1310   0.5207   0.1788
   2.500   0.8324   0.00891   0.00222  -0.1302   0.4875   0.4623
   3.000   0.8677   0.00976   0.00304  -0.1268   0.2639   1.0000
   3.250   0.8875   0.01048   0.00340  -0.1254   0.1926   1.0000
   3.500   0.9018   0.01177   0.00403  -0.1231   0.0580   1.0000
   3.750   0.9257   0.01210   0.00430  -0.1224   0.0486   1.0000
   4.000   0.9502   0.01235   0.00455  -0.1217   0.0457   1.0000
   4.250   0.9743   0.01264   0.00483  -0.1209   0.0433   1.0000
   4.500   0.9980   0.01296   0.00514  -0.1201   0.0412   1.0000
   4.750   1.0212   0.01332   0.00551  -0.1192   0.0392   1.0000
   5.000   1.0438   0.01374   0.00595  -0.1182   0.0372   1.0000
   5.250   1.0671   0.01405   0.00629  -0.1173   0.0366   1.0000
   5.500   1.0900   0.01441   0.00669  -0.1164   0.0358   1.0000
   5.750   1.1125   0.01479   0.00710  -0.1154   0.0349   1.0000
   6.000   1.1347   0.01517   0.00751  -0.1143   0.0338   1.0000
   6.250   1.1565   0.01558   0.00795  -0.1133   0.0327   1.0000
   6.500   1.1780   0.01600   0.00840  -0.1121   0.0315   1.0000
   6.750   1.1987   0.01647   0.00888  -0.1109   0.0303   1.0000
   7.000   1.2171   0.01713   0.00957  -0.1093   0.0289   1.0000
   7.250   1.2357   0.01775   0.01024  -0.1077   0.0279   1.0000
   7.500   1.2572   0.01808   0.01062  -0.1066   0.0271   1.0000
   7.750   1.2775   0.01850   0.01110  -0.1053   0.0260   1.0000
   8.000   1.2975   0.01892   0.01156  -0.1040   0.0248   1.0000
   8.250   1.3171   0.01929   0.01195  -0.1027   0.0235   1.0000
   8.500   1.3358   0.01968   0.01235  -0.1012   0.0223   1.0000
   8.750   1.3500   0.02039   0.01308  -0.0989   0.0211   1.0000
   9.000   1.3679   0.02082   0.01360  -0.0972   0.0203   1.0000
   9.250   1.3852   0.02128   0.01413  -0.0956   0.0191   1.0000
   9.500   1.4027   0.02173   0.01462  -0.0939   0.0179   1.0000
   9.750   1.4206   0.02213   0.01504  -0.0925   0.0167   1.0000
  10.000   1.4353   0.02279   0.01571  -0.0905   0.0157   1.0000
  10.250   1.4492   0.02351   0.01654  -0.0884   0.0149   1.0000
  10.500   1.4630   0.02426   0.01736  -0.0864   0.0140   1.0000
  10.750   1.4772   0.02496   0.01813  -0.0846   0.0132   1.0000
  11.000   1.4910   0.02571   0.01890  -0.0828   0.0124   1.0000
  11.250   1.5015   0.02674   0.01998  -0.0806   0.0116   1.0000
  11.500   1.5127   0.02772   0.02108  -0.0785   0.0111   1.0000
  11.750   1.5230   0.02882   0.02230  -0.0764   0.0106   1.0000
  12.000   1.5327   0.02997   0.02356  -0.0744   0.0102   1.0000
  12.250   1.5422   0.03116   0.02484  -0.0724   0.0097   1.0000
  12.500   1.5508   0.03246   0.02624  -0.0705   0.0094   1.0000
  12.750   1.5580   0.03391   0.02778  -0.0686   0.0090   1.0000
  13.000   1.5626   0.03564   0.02962  -0.0666   0.0087   1.0000
  13.250   1.5664   0.03752   0.03162  -0.0646   0.0084   1.0000
  13.500   1.5710   0.03937   0.03364  -0.0629   0.0082   1.0000
  13.750   1.5749   0.04134   0.03576  -0.0613   0.0080   1.0000
  14.000   1.5776   0.04350   0.03807  -0.0598   0.0078   1.0000
  14.250   1.5795   0.04578   0.04050  -0.0585   0.0076   1.0000
  14.500   1.5812   0.04817   0.04302  -0.0574   0.0074   1.0000
  14.750   1.5813   0.05080   0.04580  -0.0564   0.0072   1.0000
  15.000   1.5801   0.05368   0.04882  -0.0557   0.0070   1.0000
  15.250   1.5794   0.05660   0.05187  -0.0553   0.0068   1.0000
  15.500   1.5755   0.06010   0.05552  -0.0551   0.0067   1.0000
  15.750   1.5707   0.06387   0.05943  -0.0553   0.0066   1.0000
  16.000   1.5641   0.06809   0.06380  -0.0559   0.0065   1.0000
  16.250   1.5551   0.07291   0.06878  -0.0570   0.0063   1.0000
  16.500   1.5440   0.07828   0.07433  -0.0585   0.0063   1.0000
  16.750   1.5301   0.08438   0.08060  -0.0607   0.0062   1.0000
  17.000   1.5145   0.09109   0.08749  -0.0634   0.0062   1.0000
  17.250   1.4976   0.09838   0.09496  -0.0667   0.0061   1.0000
  17.500   1.4784   0.10652   0.10328  -0.0709   0.0061   1.0000
  17.750   1.4591   0.11518   0.11212  -0.0756   0.0061   1.0000
  18.000   1.4376   0.12487   0.12201  -0.0814   0.0061   1.0000
  18.250   1.4146   0.13546   0.13279  -0.0879   0.0061   1.0000
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