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GOE 288 AIRFOIL (goe288-il) Xfoil prediction polar at RE=200,000 Ncrit=9


Details Polar file
Airfoil: GOE 288 AIRFOIL (goe288-il)
Reynolds number: 200,000
Max Cl/Cd: 70.21 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe288-il-200000.txt
Download as CSV file: xf-goe288-il-200000.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 =     0.200 e 6     Ncrit =   9.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -10.500  -0.1973   0.11458   0.11114  -0.0507   0.9938   0.0905
 -10.250  -0.4305   0.05609   0.05225  -0.0985   0.9728   0.0617
 -10.000  -0.4439   0.04185   0.03726  -0.1220   0.9549   0.0608
  -9.750  -0.4295   0.03673   0.03159  -0.1276   0.9426   0.0610
  -9.500  -0.4055   0.03315   0.02754  -0.1312   0.9330   0.0615
  -9.250  -0.3808   0.03050   0.02449  -0.1330   0.9211   0.0618
  -9.000  -0.3568   0.02851   0.02214  -0.1337   0.9068   0.0622
  -8.750  -0.3320   0.02662   0.02002  -0.1341   0.8925   0.0628
  -8.500  -0.3065   0.02518   0.01849  -0.1340   0.8778   0.0636
  -8.250  -0.2809   0.02408   0.01728  -0.1338   0.8626   0.0645
  -8.000  -0.2556   0.02313   0.01618  -0.1335   0.8465   0.0656
  -7.750  -0.2303   0.02229   0.01517  -0.1331   0.8297   0.0671
  -7.500  -0.2044   0.02151   0.01418  -0.1329   0.8137   0.0687
  -7.250  -0.1783   0.02066   0.01315  -0.1326   0.7988   0.0702
  -7.000  -0.1523   0.01991   0.01237  -0.1324   0.7855   0.0720
  -6.750  -0.1255   0.01934   0.01171  -0.1322   0.7726   0.0741
  -6.500  -0.0983   0.01879   0.01104  -0.1321   0.7603   0.0768
  -6.250  -0.0711   0.01819   0.01034  -0.1321   0.7506   0.0798
  -6.000  -0.0435   0.01777   0.00991  -0.1321   0.7399   0.0843
  -5.750  -0.0155   0.01733   0.00939  -0.1323   0.7317   0.0904
  -5.500   0.0126   0.01689   0.00895  -0.1324   0.7223   0.0998
  -5.250   0.0412   0.01648   0.00850  -0.1327   0.7148   0.1161
  -5.000   0.0697   0.01608   0.00815  -0.1330   0.7067   0.1379
  -4.750   0.0984   0.01585   0.00790  -0.1333   0.6997   0.1563
  -4.500   0.1274   0.01570   0.00768  -0.1335   0.6934   0.1722
  -4.250   0.1559   0.01551   0.00751  -0.1337   0.6855   0.1869
  -4.000   0.1847   0.01537   0.00732  -0.1339   0.6783   0.2019
  -3.750   0.2134   0.01526   0.00721  -0.1340   0.6709   0.2186
  -3.500   0.2421   0.01516   0.00714  -0.1341   0.6635   0.2381
  -3.250   0.2714   0.01522   0.00712  -0.1342   0.6572   0.2641
  -3.000   0.2997   0.01529   0.00731  -0.1343   0.6499   0.2893
  -2.750   0.3287   0.01544   0.00744  -0.1343   0.6436   0.3123
  -2.500   0.3581   0.01564   0.00755  -0.1344   0.6385   0.3315
  -2.250   0.3867   0.01578   0.00771  -0.1344   0.6327   0.3472
  -2.000   0.4156   0.01589   0.00776  -0.1344   0.6269   0.3614
  -1.750   0.4448   0.01604   0.00783  -0.1345   0.6219   0.3746
  -1.500   0.4737   0.01617   0.00793  -0.1345   0.6172   0.3854
  -1.250   0.5022   0.01627   0.00797  -0.1346   0.6113   0.3968
  -1.000   0.5306   0.01627   0.00801  -0.1345   0.6057   0.4059
  -0.750   0.5601   0.01638   0.00796  -0.1347   0.6007   0.4165
  -0.500   0.5879   0.01640   0.00806  -0.1346   0.5952   0.4251
  -0.250   0.6165   0.01648   0.00807  -0.1347   0.5894   0.4349
   0.000   0.6450   0.01645   0.00806  -0.1347   0.5842   0.4433
   0.250   0.6741   0.01659   0.00809  -0.1348   0.5793   0.4534
   0.500   0.7012   0.01655   0.00816  -0.1346   0.5728   0.4627
   0.750   0.7296   0.01658   0.00814  -0.1346   0.5667   0.4746
   1.000   0.7584   0.01664   0.00815  -0.1346   0.5614   0.4850
   1.250   0.7854   0.01663   0.00820  -0.1345   0.5544   0.4936
   1.500   0.8133   0.01658   0.00817  -0.1344   0.5481   0.5018
   1.750   0.8424   0.01667   0.00814  -0.1345   0.5425   0.5111
   2.000   0.8685   0.01661   0.00822  -0.1342   0.5349   0.5193
   2.250   0.8965   0.01662   0.00818  -0.1341   0.5280   0.5302
   2.500   0.9235   0.01661   0.00823  -0.1339   0.5209   0.5407
   2.750   0.9500   0.01658   0.00824  -0.1336   0.5123   0.5527
   3.000   0.9776   0.01660   0.00822  -0.1335   0.5051   0.5671
   3.250   1.0026   0.01656   0.00833  -0.1329   0.4954   0.5843
   3.500   1.0295   0.01656   0.00831  -0.1327   0.4878   0.6077
   3.750   1.0532   0.01648   0.00847  -0.1319   0.4775   0.6431
   4.000   1.0727   0.01606   0.00847  -0.1299   0.4698   0.7962
   4.250   1.0975   0.01600   0.00854  -0.1292   0.4590   1.0000
   4.500   1.1236   0.01625   0.00863  -0.1289   0.4502   1.0000
   4.750   1.1482   0.01648   0.00881  -0.1283   0.4402   1.0000
   5.000   1.1731   0.01677   0.00900  -0.1279   0.4316   1.0000
   5.250   1.1975   0.01706   0.00923  -0.1273   0.4229   1.0000
   5.500   1.2223   0.01741   0.00947  -0.1269   0.4158   1.0000
   5.750   1.2462   0.01775   0.00980  -0.1263   0.4083   1.0000
   6.000   1.2713   0.01813   0.01005  -0.1259   0.4024   1.0000
   6.250   1.2950   0.01854   0.01047  -0.1254   0.3962   1.0000
   6.500   1.3188   0.01892   0.01083  -0.1248   0.3905   1.0000
   6.750   1.3440   0.01936   0.01115  -0.1245   0.3856   1.0000
   7.000   1.3672   0.01982   0.01163  -0.1239   0.3806   1.0000
   7.250   1.3902   0.02025   0.01208  -0.1232   0.3758   1.0000
   7.500   1.4143   0.02070   0.01249  -0.1228   0.3717   1.0000
   7.750   1.4419   0.02126   0.01292  -0.1230   0.3679   1.0000
   8.000   1.4632   0.02176   0.01352  -0.1221   0.3644   1.0000
   8.250   1.4853   0.02227   0.01409  -0.1214   0.3608   1.0000
   8.500   1.5086   0.02277   0.01462  -0.1209   0.3575   1.0000
   8.750   1.5332   0.02330   0.01512  -0.1206   0.3544   1.0000
   9.000   1.5627   0.02395   0.01567  -0.1212   0.3512   1.0000
   9.250   1.5815   0.02455   0.01639  -0.1200   0.3484   1.0000
   9.500   1.6007   0.02514   0.01709  -0.1189   0.3454   1.0000
   9.750   1.6218   0.02575   0.01777  -0.1181   0.3426   1.0000
  10.000   1.6445   0.02635   0.01841  -0.1176   0.3401   1.0000
  10.250   1.6693   0.02695   0.01901  -0.1174   0.3376   1.0000
  10.500   1.6997   0.02768   0.01966  -0.1183   0.3347   1.0000
  10.750   1.7152   0.02843   0.02056  -0.1167   0.3321   1.0000
  11.000   1.7273   0.02916   0.02144  -0.1146   0.3293   1.0000
  11.250   1.7420   0.02987   0.02226  -0.1129   0.3265   1.0000
  11.500   1.7592   0.03051   0.02297  -0.1116   0.3237   1.0000
  11.750   1.7822   0.03108   0.02353  -0.1112   0.3208   1.0000
  12.000   1.8170   0.03182   0.02420  -0.1129   0.3177   1.0000
  12.250   1.8259   0.03276   0.02530  -0.1104   0.3157   1.0000
  12.500   1.8271   0.03373   0.02646  -0.1068   0.3136   1.0000
  12.750   1.8313   0.03476   0.02765  -0.1039   0.3113   1.0000
  13.000   1.8386   0.03572   0.02873  -0.1016   0.3086   1.0000
  13.250   1.8534   0.03634   0.02938  -0.1002   0.3053   1.0000
  13.500   1.8963   0.03651   0.02936  -0.1025   0.3003   1.0000
  13.750   1.8803   0.03798   0.03109  -0.0974   0.2981   1.0000
  14.000   1.8684   0.03965   0.03297  -0.0933   0.2951   1.0000
  14.250   1.8664   0.04108   0.03453  -0.0907   0.2918   1.0000
  14.500   1.8784   0.04179   0.03526  -0.0894   0.2881   1.0000
  14.750   1.9102   0.04175   0.03510  -0.0898   0.2834   1.0000
  15.000   1.8874   0.04442   0.03804  -0.0859   0.2810   1.0000
  15.250   1.8704   0.04713   0.04097  -0.0831   0.2777   1.0000
  15.500   1.8660   0.04905   0.04299  -0.0813   0.2736   1.0000
  15.750   1.8920   0.04863   0.04241  -0.0810   0.2681   1.0000
  16.000   1.8690   0.05234   0.04637  -0.0789   0.2650   1.0000
  16.250   1.8463   0.05639   0.05065  -0.0773   0.2615   1.0000
  16.500   1.8394   0.05921   0.05359  -0.0765   0.2575   1.0000
  16.750   1.8521   0.06008   0.05444  -0.0760   0.2535   1.0000
  17.000   1.8426   0.06347   0.05797  -0.0755   0.2499   1.0000
  17.250   1.8123   0.06946   0.06423  -0.0753   0.2463   1.0000
  17.500   1.7989   0.07371   0.06861  -0.0754   0.2420   1.0000
  17.750   1.8181   0.07387   0.06870  -0.0751   0.2371   1.0000
  18.000   1.7803   0.08155   0.07666  -0.0760   0.2332   1.0000
  18.250   1.7447   0.08926   0.08460  -0.0773   0.2285   1.0000
  18.500   1.7594   0.09014   0.08543  -0.0773   0.2228   1.0000
  18.750   1.7121   0.09993   0.09549  -0.0795   0.2181   1.0000
  19.000   1.6606   0.11075   0.10653  -0.0825   0.2122   1.0000
  19.250   1.6652   0.11327   0.10906  -0.0832   0.2055   1.0000
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