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GOE 358 AIRFOIL (goe358-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 358 AIRFOIL (goe358-il)
Reynolds number: 1,000,000
Max Cl/Cd: 119.22 at α=6°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe358-il-1000000.txt
Download as CSV file: xf-goe358-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 358 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
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.7512   0.08063   0.07840  -0.0548   1.0000   0.0167
 -13.750  -0.7917   0.07007   0.06772  -0.0620   1.0000   0.0167
 -13.500  -0.8260   0.06136   0.05890  -0.0679   1.0000   0.0166
 -13.250  -0.8650   0.05506   0.05255  -0.0696   1.0000   0.0165
 -13.000  -0.9001   0.04867   0.04609  -0.0731   1.0000   0.0164
 -12.750  -0.9185   0.04196   0.03925  -0.0797   1.0000   0.0165
 -12.500  -0.9117   0.03551   0.03263  -0.0892   0.9998   0.0167
 -12.250  -0.8751   0.02995   0.02684  -0.1015   0.9985   0.0171
 -12.000  -0.8342   0.02431   0.02093  -0.1139   0.9974   0.0178
 -11.750  -0.7954   0.02081   0.01726  -0.1215   0.9965   0.0186
 -11.500  -0.7606   0.01939   0.01573  -0.1250   0.9956   0.0194
 -11.250  -0.7266   0.01837   0.01461  -0.1275   0.9949   0.0202
 -11.000  -0.6925   0.01759   0.01371  -0.1297   0.9942   0.0209
 -10.750  -0.6583   0.01624   0.01228  -0.1326   0.9935   0.0222
 -10.500  -0.6269   0.01560   0.01159  -0.1340   0.9920   0.0233
 -10.250  -0.5949   0.01505   0.01096  -0.1353   0.9906   0.0243
 -10.000  -0.5621   0.01437   0.01019  -0.1368   0.9893   0.0255
  -9.750  -0.5288   0.01386   0.00968  -0.1384   0.9881   0.0270
  -9.500  -0.4950   0.01357   0.00935  -0.1397   0.9870   0.0284
  -9.250  -0.4609   0.01329   0.00900  -0.1411   0.9860   0.0296
  -9.000  -0.4264   0.01281   0.00853  -0.1427   0.9852   0.0315
  -8.750  -0.3915   0.01265   0.00835  -0.1442   0.9844   0.0329
  -8.500  -0.3562   0.01246   0.00812  -0.1457   0.9838   0.0343
  -8.250  -0.3205   0.01204   0.00765  -0.1475   0.9832   0.0358
  -8.000  -0.2888   0.01187   0.00750  -0.1482   0.9807   0.0372
  -7.750  -0.2555   0.01171   0.00734  -0.1492   0.9780   0.0385
  -7.500  -0.2216   0.01152   0.00710  -0.1503   0.9754   0.0398
  -7.250  -0.1875   0.01141   0.00696  -0.1514   0.9729   0.0408
  -7.000  -0.1549   0.01076   0.00625  -0.1525   0.9698   0.0426
  -6.750  -0.1278   0.01051   0.00599  -0.1522   0.9633   0.0437
  -6.500  -0.0984   0.01030   0.00577  -0.1523   0.9580   0.0450
  -6.250  -0.0707   0.01012   0.00556  -0.1520   0.9508   0.0463
  -6.000  -0.0428   0.00992   0.00530  -0.1518   0.9431   0.0474
  -5.750  -0.0152   0.00981   0.00515  -0.1514   0.9339   0.0482
  -5.500   0.0129   0.00946   0.00473  -0.1513   0.9250   0.0492
  -5.250   0.0414   0.00893   0.00415  -0.1514   0.9147   0.0511
  -5.000   0.0697   0.00870   0.00389  -0.1513   0.9037   0.0524
  -4.750   0.0981   0.00851   0.00363  -0.1512   0.8913   0.0536
  -4.500   0.1264   0.00836   0.00341  -0.1511   0.8770   0.0549
  -4.250   0.1547   0.00821   0.00318  -0.1509   0.8604   0.0559
  -4.000   0.1830   0.00810   0.00297  -0.1508   0.8409   0.0568
  -3.750   0.2111   0.00805   0.00281  -0.1505   0.8192   0.0575
  -3.500   0.2394   0.00790   0.00252  -0.1504   0.7974   0.0589
  -3.250   0.2679   0.00776   0.00226  -0.1504   0.7769   0.0609
  -3.000   0.2963   0.00770   0.00210  -0.1503   0.7584   0.0627
  -2.750   0.3248   0.00765   0.00197  -0.1502   0.7431   0.0644
  -2.500   0.3534   0.00762   0.00186  -0.1502   0.7298   0.0662
  -2.000   0.4109   0.00753   0.00165  -0.1501   0.7056   0.0721
  -1.750   0.4397   0.00746   0.00156  -0.1501   0.6941   0.0795
  -1.500   0.4689   0.00717   0.00144  -0.1504   0.6822   0.1493
  -1.250   0.4978   0.00687   0.00138  -0.1507   0.6694   0.2375
  -1.000   0.5264   0.00686   0.00140  -0.1507   0.6558   0.2708
  -0.750   0.5546   0.00691   0.00143  -0.1506   0.6389   0.2902
  -0.500   0.5825   0.00701   0.00146  -0.1504   0.6188   0.3013
  -0.250   0.6104   0.00713   0.00149  -0.1501   0.5949   0.3087
   0.000   0.6378   0.00727   0.00154  -0.1499   0.5692   0.3163
   0.250   0.6653   0.00745   0.00160  -0.1496   0.5432   0.3234
   0.500   0.6928   0.00761   0.00168  -0.1494   0.5205   0.3297
   0.750   0.7204   0.00776   0.00175  -0.1492   0.5005   0.3353
   1.000   0.7480   0.00792   0.00183  -0.1490   0.4803   0.3404
   1.250   0.7755   0.00808   0.00193  -0.1487   0.4602   0.3471
   1.500   0.8028   0.00826   0.00203  -0.1485   0.4413   0.3533
   1.750   0.8303   0.00843   0.00212  -0.1483   0.4249   0.3574
   2.000   0.8579   0.00856   0.00222  -0.1481   0.4106   0.3631
   2.250   0.8855   0.00870   0.00234  -0.1479   0.3982   0.3691
   2.500   0.9129   0.00887   0.00245  -0.1477   0.3862   0.3739
   2.750   0.9401   0.00902   0.00257  -0.1474   0.3745   0.3788
   3.000   0.9677   0.00913   0.00268  -0.1472   0.3654   0.3831
   3.250   0.9950   0.00929   0.00280  -0.1470   0.3573   0.3873
   3.500   1.0227   0.00940   0.00292  -0.1468   0.3513   0.3909
   3.750   1.0498   0.00954   0.00305  -0.1466   0.3443   0.3964
   4.000   1.0774   0.00964   0.00318  -0.1464   0.3392   0.4016
   4.250   1.1047   0.00977   0.00331  -0.1462   0.3340   0.4062
   4.750   1.1591   0.01002   0.00361  -0.1457   0.3219   0.4171
   5.000   1.1861   0.01016   0.00376  -0.1454   0.3163   0.4225
   5.250   1.2129   0.01031   0.00392  -0.1451   0.3085   0.4285
   5.500   1.2395   0.01048   0.00408  -0.1448   0.2984   0.4352
   5.750   1.2662   0.01063   0.00425  -0.1445   0.2893   0.4421
   6.000   1.2923   0.01084   0.00445  -0.1442   0.2771   0.4499
   6.250   1.3180   0.01108   0.00465  -0.1437   0.2581   0.4575
   6.500   1.3370   0.01204   0.00520  -0.1423   0.1839   0.4656
   6.750   1.3589   0.01268   0.00571  -0.1413   0.1575   0.4746
   7.000   1.3826   0.01309   0.00609  -0.1406   0.1433   0.4857
   7.250   1.4060   0.01353   0.00649  -0.1398   0.1253   0.4998
   7.750   1.4467   0.01495   0.00766  -0.1375   0.0678   0.5523
   8.000   1.4656   0.01481   0.00819  -0.1359   0.0599   1.0000
   8.250   1.4888   0.01521   0.00858  -0.1350   0.0558   1.0000
   8.500   1.5103   0.01574   0.00909  -0.1340   0.0502   1.0000
   8.750   1.5334   0.01609   0.00946  -0.1331   0.0470   1.0000
   9.000   1.5540   0.01665   0.00998  -0.1319   0.0417   1.0000
   9.250   1.5758   0.01706   0.01040  -0.1309   0.0380   1.0000
   9.500   1.5958   0.01761   0.01093  -0.1296   0.0339   1.0000
   9.750   1.6155   0.01814   0.01145  -0.1282   0.0307   1.0000
  10.000   1.6340   0.01873   0.01205  -0.1267   0.0280   1.0000
  10.250   1.6523   0.01929   0.01262  -0.1251   0.0260   1.0000
  10.500   1.6668   0.02006   0.01339  -0.1230   0.0238   1.0000
  10.750   1.6833   0.02057   0.01395  -0.1211   0.0228   1.0000
  11.000   1.6964   0.02119   0.01461  -0.1186   0.0217   1.0000
  11.250   1.7074   0.02196   0.01541  -0.1160   0.0207   1.0000
  11.500   1.7149   0.02297   0.01647  -0.1129   0.0195   1.0000
  11.750   1.7276   0.02369   0.01726  -0.1107   0.0190   1.0000
  12.000   1.7388   0.02454   0.01816  -0.1084   0.0183   1.0000
  12.250   1.7489   0.02548   0.01916  -0.1061   0.0177   1.0000
  12.500   1.7569   0.02661   0.02033  -0.1037   0.0170   1.0000
  12.750   1.7601   0.02815   0.02193  -0.1009   0.0163   1.0000
  13.000   1.7651   0.02962   0.02350  -0.0985   0.0158   1.0000
  13.250   1.7735   0.03091   0.02486  -0.0966   0.0155   1.0000
  13.500   1.7799   0.03242   0.02645  -0.0948   0.0151   1.0000
  13.750   1.7852   0.03410   0.02820  -0.0930   0.0147   1.0000
  14.000   1.7897   0.03595   0.03012  -0.0915   0.0143   1.0000
  14.250   1.7921   0.03809   0.03233  -0.0900   0.0140   1.0000
  14.500   1.7923   0.04057   0.03490  -0.0887   0.0137   1.0000
  14.750   1.7885   0.04364   0.03805  -0.0876   0.0133   1.0000
  15.000   1.7786   0.04752   0.04206  -0.0867   0.0130   1.0000
  15.250   1.7730   0.05109   0.04574  -0.0861   0.0128   1.0000
  15.500   1.7717   0.05424   0.04900  -0.0857   0.0127   1.0000
  15.750   1.7690   0.05764   0.05250  -0.0856   0.0125   1.0000
  16.000   1.7650   0.06132   0.05628  -0.0856   0.0123   1.0000
  16.250   1.7594   0.06532   0.06039  -0.0858   0.0122   1.0000
  16.500   1.7527   0.06958   0.06476  -0.0862   0.0120   1.0000
  16.750   1.7452   0.07401   0.06930  -0.0868   0.0118   1.0000
  17.000   1.7371   0.07861   0.07400  -0.0876   0.0116   1.0000
  17.250   1.7279   0.08349   0.07897  -0.0885   0.0115   1.0000
  17.500   1.7187   0.08842   0.08400  -0.0896   0.0113   1.0000
  17.750   1.7082   0.09356   0.08924  -0.0908   0.0112   1.0000
  18.000   1.6971   0.09887   0.09466  -0.0922   0.0111   1.0000
  18.250   1.6855   0.10436   0.10024  -0.0938   0.0109   1.0000
  18.500   1.6731   0.10998   0.10596  -0.0955   0.0108   1.0000
  18.750   1.6600   0.11575   0.11182  -0.0974   0.0107   1.0000
  19.000   1.6470   0.12160   0.11776  -0.0995   0.0106   1.0000
  19.250   1.6326   0.12772   0.12398  -0.1018   0.0104   1.0000
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