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GOE 446 AIRFOIL (goe446-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 446 AIRFOIL (goe446-il)
Reynolds number: 1,000,000
Max Cl/Cd: 148.66 at α=2.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe446-il-1000000.txt
Download as CSV file: xf-goe446-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 446 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
  ------ -------- --------- --------- -------- -------- --------
 -11.000  -0.0295   0.09254   0.09062  -0.0966   0.9118   0.0250
 -10.750  -0.0212   0.09027   0.08832  -0.0966   0.9008   0.0252
 -10.500  -0.1080   0.09689   0.09495  -0.0944   0.9365   0.0250
 -10.250  -0.0992   0.09481   0.09285  -0.0945   0.9283   0.0252
 -10.000  -0.0900   0.09270   0.09073  -0.0949   0.9192   0.0253
  -9.750  -0.0817   0.09055   0.08854  -0.0954   0.9079   0.0255
  -9.500  -0.0737   0.08829   0.08622  -0.0960   0.8936   0.0258
  -9.250  -0.0661   0.08590   0.08376  -0.0969   0.8767   0.0262
  -9.000  -0.0588   0.08336   0.08115  -0.0981   0.8591   0.0268
  -8.750  -0.0032   0.06271   0.06029  -0.1050   0.8012   0.0293
  -8.500   0.0046   0.06032   0.05788  -0.1057   0.7930   0.0295
  -8.250   0.0122   0.05797   0.05549  -0.1063   0.7847   0.0297
  -8.000  -0.1375   0.02342   0.01980  -0.1541   0.7968   0.0276
  -7.750  -0.1192   0.02010   0.01603  -0.1550   0.7896   0.0275
  -7.500  -0.0966   0.01836   0.01395  -0.1553   0.7829   0.0276
  -7.250  -0.0720   0.01704   0.01241  -0.1554   0.7770   0.0277
  -7.000  -0.0467   0.01601   0.01116  -0.1555   0.7705   0.0279
  -6.750  -0.0207   0.01521   0.01016  -0.1555   0.7643   0.0281
  -6.500   0.0063   0.01459   0.00940  -0.1556   0.7587   0.0284
  -6.250   0.0338   0.01423   0.00892  -0.1557   0.7534   0.0287
  -6.000   0.0612   0.01390   0.00844  -0.1557   0.7483   0.0289
  -5.750   0.0880   0.01294   0.00735  -0.1558   0.7436   0.0291
  -5.500   0.1146   0.01207   0.00636  -0.1559   0.7385   0.0295
  -5.250   0.1417   0.01154   0.00574  -0.1559   0.7334   0.0298
  -5.000   0.1696   0.01111   0.00526  -0.1560   0.7290   0.0301
  -4.750   0.1977   0.01075   0.00487  -0.1561   0.7246   0.0304
  -4.500   0.2257   0.01046   0.00453  -0.1562   0.7203   0.0307
  -4.250   0.2537   0.01022   0.00422  -0.1563   0.7160   0.0311
  -4.000   0.2822   0.00995   0.00393  -0.1565   0.7125   0.0315
  -3.750   0.3107   0.00971   0.00367  -0.1566   0.7089   0.0320
  -3.500   0.3391   0.00951   0.00342  -0.1567   0.7051   0.0325
  -3.250   0.3674   0.00936   0.00323  -0.1568   0.7013   0.0331
  -3.000   0.3959   0.00925   0.00308  -0.1570   0.6976   0.0336
  -2.750   0.4245   0.00896   0.00278  -0.1571   0.6941   0.0345
  -2.500   0.4530   0.00877   0.00258  -0.1573   0.6900   0.0355
  -2.250   0.4814   0.00866   0.00243  -0.1574   0.6858   0.0365
  -2.000   0.5097   0.00858   0.00232  -0.1575   0.6817   0.0377
  -1.750   0.5386   0.00847   0.00221  -0.1577   0.6782   0.0389
  -1.500   0.5672   0.00834   0.00209  -0.1578   0.6741   0.0421
  -1.250   0.5955   0.00822   0.00201  -0.1580   0.6699   0.0529
  -1.000   0.6235   0.00816   0.00203  -0.1581   0.6655   0.0816
  -0.750   0.6523   0.00814   0.00205  -0.1583   0.6616   0.0903
  -0.500   0.6808   0.00810   0.00205  -0.1584   0.6568   0.0973
  -0.250   0.7087   0.00813   0.00205  -0.1584   0.6518   0.1020
   0.000   0.7369   0.00814   0.00205  -0.1585   0.6469   0.1054
   0.250   0.7653   0.00809   0.00204  -0.1587   0.6415   0.1114
   0.500   0.7931   0.00810   0.00204  -0.1587   0.6360   0.1162
   0.750   0.8211   0.00812   0.00205  -0.1588   0.6306   0.1214
   1.000   0.8492   0.00809   0.00206  -0.1589   0.6244   0.1306
   1.250   0.8764   0.00812   0.00208  -0.1588   0.6178   0.1409
   1.500   0.9043   0.00808   0.00211  -0.1589   0.6111   0.1621
   1.750   0.9314   0.00800   0.00218  -0.1589   0.6031   0.2308
   2.000   0.9581   0.00740   0.00237  -0.1593   0.5949   0.5833
   2.250   0.9787   0.00669   0.00252  -0.1576   0.5856   1.0000
   2.500   1.0057   0.00680   0.00258  -0.1575   0.5757   1.0000
   2.750   1.0317   0.00694   0.00265  -0.1572   0.5652   1.0000
   3.250   1.0824   0.00730   0.00285  -0.1563   0.5381   1.0000
   3.500   1.1069   0.00751   0.00298  -0.1558   0.5221   1.0000
   3.750   1.1310   0.00775   0.00313  -0.1551   0.5059   1.0000
   4.000   1.1553   0.00798   0.00329  -0.1545   0.4916   1.0000
   4.250   1.1800   0.00819   0.00344  -0.1540   0.4807   1.0000
   4.500   1.2038   0.00843   0.00361  -0.1534   0.4701   1.0000
   4.750   1.2275   0.00867   0.00380  -0.1527   0.4587   1.0000
   5.000   1.2511   0.00891   0.00398  -0.1520   0.4472   1.0000
   5.250   1.2739   0.00917   0.00419  -0.1512   0.4362   1.0000
   5.500   1.2976   0.00939   0.00438  -0.1506   0.4283   1.0000
   5.750   1.3206   0.00962   0.00458  -0.1498   0.4226   1.0000
   6.000   1.3451   0.00978   0.00475  -0.1493   0.4173   1.0000
   6.250   1.3657   0.01005   0.00498  -0.1481   0.4090   1.0000
   6.500   1.3878   0.01026   0.00518  -0.1471   0.4010   1.0000
   6.750   1.4083   0.01053   0.00543  -0.1459   0.3935   1.0000
   7.000   1.4303   0.01076   0.00566  -0.1449   0.3867   1.0000
   7.250   1.4513   0.01103   0.00592  -0.1439   0.3788   1.0000
   7.500   1.4719   0.01132   0.00619  -0.1427   0.3693   1.0000
   7.750   1.4906   0.01170   0.00652  -0.1413   0.3581   1.0000
   8.000   1.5103   0.01204   0.00684  -0.1400   0.3458   1.0000
   8.250   1.5272   0.01251   0.00725  -0.1383   0.3290   1.0000
   8.500   1.5395   0.01320   0.00781  -0.1359   0.3014   1.0000
   8.750   1.5430   0.01436   0.00872  -0.1322   0.2604   1.0000
   9.000   1.5432   0.01574   0.00986  -0.1280   0.2206   1.0000
   9.250   1.5467   0.01701   0.01096  -0.1246   0.1899   1.0000
   9.500   1.5506   0.01831   0.01210  -0.1214   0.1631   1.0000
   9.750   1.5574   0.01950   0.01318  -0.1187   0.1427   1.0000
  10.000   1.5653   0.02065   0.01426  -0.1163   0.1279   1.0000
  10.250   1.5740   0.02179   0.01535  -0.1141   0.1157   1.0000
  10.500   1.5826   0.02299   0.01651  -0.1120   0.1046   1.0000
  10.750   1.5893   0.02434   0.01780  -0.1098   0.0921   1.0000
  11.000   1.5894   0.02623   0.01956  -0.1070   0.0723   1.0000
  11.250   1.5708   0.02962   0.02272  -0.1025   0.0342   1.0000
  11.500   1.5730   0.03157   0.02468  -0.1003   0.0280   1.0000
  11.750   1.5784   0.03332   0.02647  -0.0986   0.0253   1.0000
  12.000   1.5862   0.03491   0.02811  -0.0972   0.0238   1.0000
  12.250   1.5915   0.03674   0.02998  -0.0956   0.0224   1.0000
  12.500   1.5969   0.03862   0.03191  -0.0941   0.0213   1.0000
  12.750   1.6048   0.04030   0.03365  -0.0930   0.0205   1.0000
  13.000   1.6114   0.04214   0.03553  -0.0918   0.0197   1.0000
  13.250   1.6163   0.04414   0.03759  -0.0905   0.0189   1.0000
  13.500   1.6178   0.04652   0.04003  -0.0891   0.0182   1.0000
  13.750   1.6209   0.04881   0.04239  -0.0880   0.0177   1.0000
  14.000   1.6267   0.05085   0.04448  -0.0870   0.0173   1.0000
  14.250   1.6312   0.05305   0.04675  -0.0861   0.0168   1.0000
  14.500   1.6346   0.05540   0.04917  -0.0852   0.0164   1.0000
  14.750   1.6375   0.05782   0.05165  -0.0843   0.0160   1.0000
  15.000   1.6388   0.06048   0.05437  -0.0835   0.0156   1.0000
  15.250   1.6373   0.06351   0.05746  -0.0827   0.0152   1.0000
  15.500   1.6309   0.06718   0.06123  -0.0818   0.0148   1.0000
  15.750   1.6309   0.07012   0.06424  -0.0812   0.0146   1.0000
  16.000   1.6333   0.07280   0.06700  -0.0808   0.0143   1.0000
  16.250   1.6339   0.07576   0.07004  -0.0805   0.0140   1.0000
  16.500   1.6333   0.07890   0.07325  -0.0802   0.0138   1.0000
  16.750   1.6325   0.08210   0.07653  -0.0799   0.0135   1.0000
  17.000   1.6304   0.08548   0.07999  -0.0798   0.0133   1.0000
  17.250   1.6277   0.08899   0.08357  -0.0797   0.0131   1.0000
  17.500   1.6247   0.09256   0.08721  -0.0798   0.0129   1.0000
  17.750   1.6207   0.09631   0.09104  -0.0799   0.0127   1.0000
  18.000   1.6145   0.10042   0.09523  -0.0803   0.0125   1.0000
  18.250   1.6057   0.10493   0.09983  -0.0807   0.0123   1.0000
  18.500   1.5935   0.10996   0.10496  -0.0814   0.0121   1.0000
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