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GOE 288 AIRFOIL (goe288-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 288 AIRFOIL (goe288-il)
Reynolds number: 500,000
Max Cl/Cd: 96.46 at α=5.5°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe288-il-500000.txt
Download as CSV file: xf-goe288-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 288 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 =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -13.250  -0.6391   0.05939   0.05616  -0.0882   1.0000   0.0369
 -13.000  -0.6945   0.05164   0.04824  -0.0919   1.0000   0.0366
 -12.750  -0.7202   0.04472   0.04111  -0.0995   0.9959   0.0366
 -12.500  -0.7086   0.03775   0.03384  -0.1141   0.9862   0.0368
 -12.250  -0.6837   0.03429   0.03014  -0.1212   0.9816   0.0372
 -12.000  -0.6620   0.03176   0.02740  -0.1249   0.9743   0.0375
 -11.750  -0.6366   0.02958   0.02502  -0.1279   0.9684   0.0377
 -11.500  -0.6145   0.02787   0.02314  -0.1293   0.9591   0.0380
 -11.250  -0.5893   0.02636   0.02145  -0.1307   0.9513   0.0383
 -11.000  -0.5675   0.02513   0.02006  -0.1309   0.9395   0.0385
 -10.750  -0.5448   0.02407   0.01885  -0.1310   0.9274   0.0388
 -10.500  -0.5214   0.02317   0.01778  -0.1309   0.9148   0.0390
 -10.250  -0.4998   0.02179   0.01628  -0.1305   0.9013   0.0393
 -10.000  -0.4774   0.02070   0.01513  -0.1302   0.8861   0.0398
  -9.750  -0.4535   0.01989   0.01425  -0.1299   0.8706   0.0402
  -9.500  -0.4289   0.01922   0.01350  -0.1297   0.8540   0.0407
  -9.250  -0.4037   0.01863   0.01281  -0.1294   0.8362   0.0413
  -9.000  -0.3783   0.01807   0.01212  -0.1292   0.8172   0.0419
  -8.750  -0.3526   0.01753   0.01144  -0.1291   0.7971   0.0424
  -8.500  -0.3266   0.01703   0.01079  -0.1289   0.7765   0.0429
  -8.250  -0.3003   0.01658   0.01019  -0.1287   0.7563   0.0434
  -8.000  -0.2735   0.01620   0.00965  -0.1286   0.7374   0.0439
  -7.750  -0.2471   0.01562   0.00896  -0.1286   0.7207   0.0445
  -7.500  -0.2203   0.01507   0.00834  -0.1287   0.7063   0.0454
  -7.250  -0.1929   0.01470   0.00787  -0.1288   0.6936   0.0463
  -7.000  -0.1647   0.01436   0.00745  -0.1290   0.6821   0.0473
  -6.750  -0.1364   0.01406   0.00706  -0.1291   0.6724   0.0484
  -6.500  -0.1077   0.01382   0.00671  -0.1293   0.6632   0.0496
  -6.250  -0.0795   0.01338   0.00622  -0.1296   0.6551   0.0514
  -6.000  -0.0504   0.01308   0.00588  -0.1298   0.6470   0.0535
  -5.750  -0.0216   0.01289   0.00558  -0.1300   0.6393   0.0557
  -5.500   0.0076   0.01252   0.00521  -0.1303   0.6321   0.0596
  -5.250   0.0367   0.01222   0.00489  -0.1306   0.6249   0.0663
  -5.000   0.0656   0.01192   0.00462  -0.1309   0.6185   0.0861
  -4.750   0.0952   0.01165   0.00446  -0.1313   0.6131   0.1101
  -4.500   0.1246   0.01151   0.00433  -0.1315   0.6071   0.1243
  -4.250   0.1538   0.01146   0.00422  -0.1317   0.6013   0.1352
  -4.000   0.1833   0.01134   0.00411  -0.1320   0.5961   0.1458
  -3.750   0.2129   0.01120   0.00398  -0.1322   0.5906   0.1559
  -3.500   0.2423   0.01112   0.00387  -0.1325   0.5851   0.1669
  -3.250   0.2715   0.01106   0.00378  -0.1327   0.5802   0.1807
  -3.000   0.3012   0.01087   0.00370  -0.1330   0.5762   0.2008
  -2.750   0.3308   0.01073   0.00364  -0.1333   0.5716   0.2301
  -2.500   0.3602   0.01065   0.00363  -0.1336   0.5671   0.2634
  -2.250   0.3894   0.01068   0.00367  -0.1338   0.5626   0.2876
  -2.000   0.4191   0.01069   0.00371  -0.1340   0.5588   0.3058
  -1.750   0.4487   0.01073   0.00375  -0.1342   0.5548   0.3211
  -1.500   0.4782   0.01077   0.00380  -0.1344   0.5506   0.3334
  -1.250   0.5074   0.01083   0.00381  -0.1345   0.5463   0.3422
  -1.000   0.5366   0.01092   0.00386  -0.1346   0.5420   0.3504
  -0.750   0.5662   0.01096   0.00388  -0.1348   0.5377   0.3579
  -0.500   0.5954   0.01094   0.00390  -0.1350   0.5331   0.3656
  -0.250   0.6244   0.01101   0.00392  -0.1351   0.5286   0.3726
   0.000   0.6534   0.01112   0.00395  -0.1352   0.5241   0.3785
   0.250   0.6826   0.01108   0.00399  -0.1353   0.5200   0.3850
   0.500   0.7117   0.01112   0.00402  -0.1355   0.5151   0.3918
   0.750   0.7404   0.01118   0.00403  -0.1355   0.5101   0.3977
   1.000   0.7688   0.01123   0.00408  -0.1356   0.5049   0.4044
   1.250   0.7978   0.01126   0.00413  -0.1357   0.4994   0.4131
   1.500   0.8262   0.01128   0.00417  -0.1357   0.4933   0.4220
   1.750   0.8541   0.01138   0.00423  -0.1357   0.4875   0.4294
   2.000   0.8830   0.01140   0.00427  -0.1358   0.4812   0.4354
   2.250   0.9109   0.01141   0.00431  -0.1358   0.4742   0.4419
   2.500   0.9388   0.01148   0.00437  -0.1358   0.4672   0.4485
   2.750   0.9668   0.01154   0.00442  -0.1358   0.4586   0.4553
   3.000   0.9940   0.01161   0.00450  -0.1356   0.4498   0.4634
   3.250   1.0211   0.01171   0.00458  -0.1355   0.4386   0.4719
   3.500   1.0480   0.01180   0.00469  -0.1353   0.4263   0.4809
   3.750   1.0740   0.01197   0.00482  -0.1350   0.4129   0.4918
   4.000   1.0993   0.01216   0.00499  -0.1346   0.3991   0.5055
   4.250   1.1243   0.01238   0.00519  -0.1342   0.3859   0.5234
   4.500   1.1496   0.01257   0.00542  -0.1338   0.3749   0.5495
   4.750   1.1739   0.01276   0.00570  -0.1334   0.3657   0.5963
   5.000   1.1921   0.01236   0.00600  -0.1314   0.3585   0.8711
   5.250   1.2151   0.01260   0.00622  -0.1305   0.3515   1.0000
   5.500   1.2405   0.01286   0.00645  -0.1301   0.3461   1.0000
   5.750   1.2648   0.01317   0.00672  -0.1296   0.3407   1.0000
   6.000   1.2876   0.01356   0.00704  -0.1288   0.3356   1.0000
   6.250   1.3118   0.01386   0.00733  -0.1282   0.3318   1.0000
   6.500   1.3362   0.01413   0.00760  -0.1277   0.3283   1.0000
   6.750   1.3595   0.01445   0.00791  -0.1270   0.3248   1.0000
   7.000   1.3815   0.01482   0.00825  -0.1262   0.3215   1.0000
   7.250   1.4021   0.01528   0.00866  -0.1250   0.3180   1.0000
   7.500   1.4246   0.01559   0.00900  -0.1242   0.3156   1.0000
   7.750   1.4469   0.01588   0.00933  -0.1234   0.3133   1.0000
   8.000   1.4672   0.01620   0.00967  -0.1222   0.3108   1.0000
   8.250   1.4868   0.01657   0.01005  -0.1209   0.3083   1.0000
   8.500   1.5057   0.01699   0.01047  -0.1196   0.3057   1.0000
   8.750   1.5240   0.01750   0.01096  -0.1182   0.3031   1.0000
   9.000   1.5430   0.01805   0.01149  -0.1170   0.3000   1.0000
   9.250   1.5625   0.01840   0.01192  -0.1158   0.2981   1.0000
   9.500   1.5816   0.01880   0.01237  -0.1147   0.2957   1.0000
   9.750   1.6004   0.01925   0.01286  -0.1135   0.2935   1.0000
  10.000   1.6190   0.01974   0.01339  -0.1123   0.2915   1.0000
  10.250   1.6368   0.02028   0.01395  -0.1111   0.2895   1.0000
  10.500   1.6539   0.02088   0.01455  -0.1099   0.2872   1.0000
  10.750   1.6716   0.02158   0.01523  -0.1087   0.2842   1.0000
  11.000   1.6886   0.02214   0.01586  -0.1075   0.2825   1.0000
  11.250   1.7049   0.02273   0.01654  -0.1063   0.2805   1.0000
  11.500   1.7206   0.02337   0.01724  -0.1051   0.2779   1.0000
  11.750   1.7355   0.02407   0.01800  -0.1039   0.2752   1.0000
  12.000   1.7495   0.02486   0.01883  -0.1026   0.2725   1.0000
  12.250   1.7630   0.02576   0.01971  -0.1013   0.2696   1.0000
  12.500   1.7775   0.02662   0.02060  -0.1001   0.2669   1.0000
  12.750   1.7909   0.02750   0.02160  -0.0990   0.2650   1.0000
  13.000   1.8034   0.02848   0.02267  -0.0979   0.2622   1.0000
  13.250   1.8155   0.02954   0.02380  -0.0969   0.2594   1.0000
  13.500   1.8266   0.03069   0.02500  -0.0958   0.2566   1.0000
  13.750   1.8361   0.03198   0.02630  -0.0946   0.2537   1.0000
  14.000   1.8461   0.03327   0.02765  -0.0935   0.2508   1.0000
  14.250   1.8559   0.03468   0.02918  -0.0927   0.2478   1.0000
  14.500   1.8641   0.03625   0.03084  -0.0920   0.2438   1.0000
  14.750   1.8690   0.03815   0.03276  -0.0910   0.2395   1.0000
  15.000   1.8737   0.04008   0.03474  -0.0901   0.2358   1.0000
  15.250   1.8829   0.04173   0.03651  -0.0896   0.2325   1.0000
  15.500   1.8888   0.04371   0.03857  -0.0890   0.2283   1.0000
  15.750   1.8898   0.04621   0.04110  -0.0883   0.2238   1.0000
  16.000   1.8929   0.04854   0.04351  -0.0878   0.2194   1.0000
  16.250   1.8957   0.05097   0.04603  -0.0873   0.2139   1.0000
  16.500   1.8917   0.05413   0.04922  -0.0868   0.2086   1.0000
  16.750   1.8929   0.05678   0.05195  -0.0864   0.2023   1.0000
  17.000   1.8848   0.06051   0.05571  -0.0860   0.1950   1.0000
  17.250   1.8785   0.06405   0.05931  -0.0856   0.1861   1.0000
  17.500   1.8638   0.06865   0.06392  -0.0854   0.1758   1.0000
  17.750   1.8434   0.07402   0.06929  -0.0853   0.1634   1.0000
  18.000   1.8152   0.08042   0.07568  -0.0853   0.1486   1.0000
  18.250   1.7811   0.08777   0.08300  -0.0857   0.1336   1.0000
  18.500   1.7462   0.09540   0.09063  -0.0864   0.1208   1.0000
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