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GOE 497 AIRFOIL (goe497-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 497 AIRFOIL (goe497-il)
Reynolds number: 1,000,000
Max Cl/Cd: 135.19 at α=5.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe497-il-1000000.txt
Download as CSV file: xf-goe497-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 497 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.6675   0.10838   0.10614  -0.0612   1.0000   0.0198
 -16.500  -0.6823   0.10226   0.10000  -0.0645   1.0000   0.0203
 -16.250  -0.6988   0.09597   0.09367  -0.0678   1.0000   0.0206
 -16.000  -0.7189   0.08922   0.08686  -0.0715   1.0000   0.0208
 -15.750  -0.7407   0.08252   0.08009  -0.0752   1.0000   0.0210
 -15.500  -0.7609   0.07633   0.07383  -0.0785   1.0000   0.0212
 -15.250  -0.7836   0.07013   0.06756  -0.0818   1.0000   0.0213
 -15.000  -0.8093   0.06405   0.06141  -0.0848   1.0000   0.0214
 -14.750  -0.8427   0.05799   0.05529  -0.0873   1.0000   0.0214
 -14.500  -0.8855   0.05243   0.04967  -0.0878   1.0000   0.0213
 -14.250  -0.9033   0.04504   0.04217  -0.0962   0.9971   0.0215
 -14.000  -0.9058   0.03623   0.03318  -0.1105   0.9893   0.0217
 -13.750  -0.8826   0.02849   0.02522  -0.1262   0.9846   0.0222
 -13.500  -0.8474   0.02496   0.02148  -0.1350   0.9828   0.0228
 -13.250  -0.8197   0.02359   0.01998  -0.1376   0.9784   0.0232
 -13.000  -0.7920   0.02125   0.01753  -0.1421   0.9745   0.0242
 -12.750  -0.7592   0.02023   0.01646  -0.1448   0.9725   0.0248
 -12.500  -0.7260   0.01941   0.01558  -0.1471   0.9706   0.0256
 -12.250  -0.6968   0.01865   0.01473  -0.1485   0.9666   0.0262
 -12.000  -0.6693   0.01802   0.01401  -0.1493   0.9613   0.0268
 -11.750  -0.6376   0.01758   0.01348  -0.1506   0.9577   0.0273
 -11.500  -0.6138   0.01631   0.01213  -0.1515   0.9513   0.0284
 -11.250  -0.5878   0.01574   0.01150  -0.1517   0.9447   0.0291
 -11.000  -0.5591   0.01526   0.01096  -0.1524   0.9396   0.0298
 -10.750  -0.5349   0.01483   0.01047  -0.1520   0.9323   0.0306
 -10.500  -0.5079   0.01445   0.01000  -0.1522   0.9264   0.0313
 -10.250  -0.4811   0.01416   0.00963  -0.1521   0.9206   0.0319
 -10.000  -0.4574   0.01341   0.00880  -0.1519   0.9137   0.0328
  -9.750  -0.4312   0.01291   0.00823  -0.1520   0.9079   0.0337
  -9.500  -0.4051   0.01259   0.00788  -0.1518   0.9018   0.0347
  -9.250  -0.3784   0.01229   0.00752  -0.1516   0.8957   0.0356
  -9.000  -0.3512   0.01201   0.00715  -0.1516   0.8902   0.0365
  -8.750  -0.3245   0.01174   0.00683  -0.1514   0.8843   0.0371
  -8.500  -0.2984   0.01124   0.00625  -0.1513   0.8781   0.0383
  -8.250  -0.2717   0.01088   0.00584  -0.1512   0.8720   0.0396
  -8.000  -0.2447   0.01061   0.00553  -0.1510   0.8655   0.0407
  -7.750  -0.2173   0.01038   0.00523  -0.1509   0.8594   0.0419
  -7.500  -0.1897   0.01019   0.00499  -0.1508   0.8538   0.0430
  -7.250  -0.1626   0.00985   0.00459  -0.1506   0.8474   0.0445
  -7.000  -0.1353   0.00957   0.00425  -0.1505   0.8412   0.0464
  -6.750  -0.1076   0.00934   0.00401  -0.1504   0.8354   0.0482
  -6.500  -0.0798   0.00918   0.00379  -0.1503   0.8295   0.0499
  -6.250  -0.0522   0.00893   0.00348  -0.1502   0.8239   0.0528
  -6.000  -0.0243   0.00870   0.00326  -0.1502   0.8179   0.0558
  -5.750   0.0036   0.00857   0.00307  -0.1500   0.8115   0.0583
  -5.500   0.0313   0.00833   0.00282  -0.1500   0.8055   0.0637
  -5.250   0.0594   0.00817   0.00265  -0.1499   0.7991   0.0688
  -5.000   0.0872   0.00801   0.00249  -0.1498   0.7929   0.0769
  -4.750   0.1153   0.00785   0.00236  -0.1497   0.7867   0.0871
  -4.500   0.1433   0.00772   0.00224  -0.1496   0.7798   0.0962
  -4.250   0.1713   0.00767   0.00214  -0.1495   0.7732   0.1026
  -4.000   0.1994   0.00753   0.00203  -0.1494   0.7658   0.1112
  -3.750   0.2271   0.00749   0.00193  -0.1493   0.7581   0.1174
  -3.500   0.2553   0.00736   0.00183  -0.1492   0.7500   0.1263
  -3.250   0.2830   0.00731   0.00174  -0.1490   0.7425   0.1344
  -3.000   0.3112   0.00721   0.00167  -0.1490   0.7353   0.1451
  -2.750   0.3390   0.00713   0.00160  -0.1488   0.7274   0.1601
  -2.500   0.3669   0.00704   0.00155  -0.1487   0.7192   0.1783
  -2.250   0.3944   0.00699   0.00151  -0.1485   0.7103   0.1966
  -2.000   0.4223   0.00693   0.00148  -0.1484   0.7018   0.2139
  -1.500   0.4778   0.00689   0.00145  -0.1481   0.6851   0.2440
  -1.000   0.5332   0.00688   0.00146  -0.1477   0.6688   0.2735
  -0.500   0.5884   0.00691   0.00148  -0.1473   0.6521   0.2974
   0.000   0.6435   0.00695   0.00153  -0.1469   0.6358   0.3214
   0.250   0.6707   0.00700   0.00156  -0.1467   0.6279   0.3333
   0.750   0.7256   0.00706   0.00164  -0.1462   0.6120   0.3598
   1.000   0.7531   0.00708   0.00169  -0.1460   0.6029   0.3747
   1.250   0.7797   0.00715   0.00175  -0.1457   0.5922   0.3913
   1.500   0.8067   0.00719   0.00181  -0.1454   0.5807   0.4094
   1.750   0.8335   0.00725   0.00188  -0.1451   0.5690   0.4278
   2.000   0.8597   0.00734   0.00196  -0.1446   0.5542   0.4463
   2.250   0.8853   0.00745   0.00205  -0.1441   0.5350   0.4649
   2.500   0.9097   0.00763   0.00217  -0.1434   0.5116   0.4809
   2.750   0.9342   0.00782   0.00230  -0.1426   0.4883   0.4974
   3.000   0.9588   0.00800   0.00244  -0.1420   0.4710   0.5166
   3.250   0.9838   0.00814   0.00258  -0.1414   0.4585   0.5395
   4.250   1.0823   0.00803   0.00328  -0.1386   0.4191   1.0000
   4.500   1.1072   0.00823   0.00342  -0.1380   0.4088   1.0000
   4.750   1.1322   0.00842   0.00357  -0.1374   0.4002   1.0000
   5.000   1.1577   0.00858   0.00372  -0.1369   0.3935   1.0000
   5.250   1.1829   0.00875   0.00387  -0.1364   0.3853   1.0000
   5.500   1.2076   0.00894   0.00403  -0.1357   0.3763   1.0000
   5.750   1.2316   0.00916   0.00420  -0.1350   0.3650   1.0000
   6.000   1.2558   0.00936   0.00437  -0.1343   0.3520   1.0000
   6.250   1.2788   0.00962   0.00456  -0.1334   0.3364   1.0000
   6.500   1.2994   0.00998   0.00481  -0.1321   0.3122   1.0000
   6.750   1.3172   0.01048   0.00514  -0.1303   0.2818   1.0000
   7.000   1.3344   0.01099   0.00551  -0.1284   0.2580   1.0000
   7.250   1.3524   0.01139   0.00584  -0.1266   0.2438   1.0000
   7.500   1.3701   0.01175   0.00615  -0.1247   0.2330   1.0000
   7.750   1.3867   0.01215   0.00650  -0.1227   0.2225   1.0000
   8.000   1.4050   0.01247   0.00681  -0.1210   0.2138   1.0000
   8.250   1.4224   0.01285   0.00716  -0.1191   0.2051   1.0000
   8.500   1.4397   0.01323   0.00751  -0.1173   0.1953   1.0000
   8.750   1.4569   0.01363   0.00788  -0.1155   0.1832   1.0000
   9.000   1.4700   0.01423   0.00836  -0.1131   0.1632   1.0000
   9.250   1.4751   0.01523   0.00913  -0.1096   0.1278   1.0000
   9.500   1.4822   0.01616   0.00993  -0.1065   0.1082   1.0000
   9.750   1.4939   0.01689   0.01062  -0.1042   0.0982   1.0000
  10.000   1.5070   0.01755   0.01127  -0.1021   0.0908   1.0000
  10.250   1.5187   0.01832   0.01200  -0.0999   0.0838   1.0000
  10.500   1.5334   0.01893   0.01263  -0.0982   0.0799   1.0000
  10.750   1.5448   0.01975   0.01343  -0.0961   0.0743   1.0000
  11.000   1.5588   0.02044   0.01415  -0.0944   0.0709   1.0000
  11.250   1.5718   0.02121   0.01492  -0.0927   0.0678   1.0000
  11.500   1.5831   0.02211   0.01582  -0.0908   0.0642   1.0000
  11.750   1.5962   0.02292   0.01667  -0.0892   0.0617   1.0000
  12.000   1.6089   0.02377   0.01755  -0.0876   0.0592   1.0000
  12.250   1.6193   0.02480   0.01858  -0.0859   0.0560   1.0000
  12.500   1.6302   0.02583   0.01964  -0.0842   0.0532   1.0000
  12.750   1.6417   0.02683   0.02067  -0.0828   0.0506   1.0000
  13.000   1.6499   0.02812   0.02195  -0.0811   0.0470   1.0000
  13.250   1.6601   0.02929   0.02316  -0.0797   0.0438   1.0000
  13.500   1.6658   0.03084   0.02469  -0.0780   0.0390   1.0000
  13.750   1.6700   0.03256   0.02641  -0.0763   0.0328   1.0000
  14.000   1.6710   0.03464   0.02846  -0.0746   0.0260   1.0000
  14.250   1.6714   0.03687   0.03069  -0.0730   0.0218   1.0000
  14.500   1.6724   0.03913   0.03298  -0.0717   0.0195   1.0000
  14.750   1.6750   0.04131   0.03522  -0.0705   0.0182   1.0000
  15.000   1.6752   0.04384   0.03780  -0.0695   0.0170   1.0000
  15.250   1.6776   0.04623   0.04026  -0.0686   0.0162   1.0000
  15.500   1.6804   0.04863   0.04274  -0.0679   0.0157   1.0000
  15.750   1.6816   0.05131   0.04549  -0.0674   0.0151   1.0000
  16.000   1.6807   0.05431   0.04856  -0.0669   0.0145   1.0000
  16.250   1.6784   0.05758   0.05191  -0.0667   0.0141   1.0000
  16.500   1.6733   0.06129   0.05572  -0.0666   0.0137   1.0000
  16.750   1.6740   0.06437   0.05888  -0.0666   0.0134   1.0000
  17.000   1.6733   0.06771   0.06231  -0.0668   0.0132   1.0000
  17.250   1.6713   0.07131   0.06601  -0.0672   0.0129   1.0000
  17.500   1.6683   0.07513   0.06993  -0.0678   0.0126   1.0000
  17.750   1.6643   0.07920   0.07409  -0.0685   0.0124   1.0000
  18.000   1.6593   0.08355   0.07853  -0.0695   0.0122   1.0000
  18.250   1.6524   0.08828   0.08337  -0.0708   0.0119   1.0000
  18.500   1.6438   0.09339   0.08857  -0.0723   0.0117   1.0000
  18.750   1.6333   0.09892   0.09421  -0.0741   0.0115   1.0000
  19.000   1.6209   0.10488   0.10028  -0.0763   0.0113   1.0000
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