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GOE 503 AIRFOIL (goe503-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 503 AIRFOIL (goe503-il)
Reynolds number: 500,000
Max Cl/Cd: 96.38 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe503-il-500000.txt
Download as CSV file: xf-goe503-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 503 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
  ------ -------- --------- --------- -------- -------- --------
 -13.000  -0.4052   0.06808   0.06539  -0.1056   0.9790   0.0175
 -12.750  -0.4432   0.05597   0.05312  -0.1183   0.9733   0.0174
 -12.500  -0.4883   0.04280   0.03974  -0.1345   0.9619   0.0171
 -12.250  -0.4879   0.03410   0.03064  -0.1442   0.9576   0.0172
 -12.000  -0.4900   0.03102   0.02730  -0.1434   0.9474   0.0173
 -11.750  -0.4672   0.02836   0.02434  -0.1461   0.9441   0.0175
 -11.500  -0.4629   0.02587   0.02164  -0.1446   0.9345   0.0178
 -11.250  -0.4403   0.02381   0.01941  -0.1458   0.9294   0.0182
 -11.000  -0.4239   0.02256   0.01805  -0.1448   0.9196   0.0186
 -10.750  -0.3952   0.02126   0.01661  -0.1461   0.9133   0.0190
 -10.500  -0.3770   0.02030   0.01551  -0.1449   0.9015   0.0196
 -10.250  -0.3543   0.01933   0.01437  -0.1446   0.8903   0.0203
 -10.000  -0.3290   0.01848   0.01332  -0.1446   0.8792   0.0209
  -9.750  -0.3106   0.01748   0.01218  -0.1433   0.8655   0.0218
  -9.500  -0.2912   0.01680   0.01139  -0.1419   0.8510   0.0227
  -9.250  -0.2703   0.01626   0.01070  -0.1407   0.8366   0.0237
  -9.000  -0.2495   0.01574   0.01002  -0.1394   0.8226   0.0247
  -8.750  -0.2305   0.01512   0.00926  -0.1379   0.8098   0.0261
  -8.500  -0.2087   0.01469   0.00872  -0.1367   0.7986   0.0277
  -8.250  -0.1871   0.01428   0.00818  -0.1355   0.7878   0.0301
  -8.000  -0.1653   0.01391   0.00775  -0.1343   0.7779   0.0332
  -7.750  -0.1416   0.01363   0.00739  -0.1335   0.7688   0.0382
  -7.500  -0.1184   0.01343   0.00715  -0.1325   0.7600   0.0442
  -7.250  -0.0930   0.01333   0.00693  -0.1320   0.7523   0.0498
  -7.000  -0.0694   0.01321   0.00678  -0.1311   0.7445   0.0539
  -6.750  -0.0441   0.01313   0.00655  -0.1305   0.7373   0.0572
  -6.500  -0.0219   0.01286   0.00629  -0.1294   0.7299   0.0607
  -6.250   0.0029   0.01280   0.00613  -0.1287   0.7227   0.0640
  -6.000   0.0275   0.01270   0.00594  -0.1280   0.7161   0.0664
  -5.750   0.0500   0.01241   0.00564  -0.1269   0.7092   0.0700
  -5.500   0.0754   0.01234   0.00548  -0.1263   0.7028   0.0731
  -5.250   0.0989   0.01224   0.00533  -0.1253   0.6958   0.0760
  -5.000   0.1224   0.01203   0.00508  -0.1244   0.6891   0.0802
  -4.750   0.1465   0.01194   0.00498  -0.1236   0.6826   0.0841
  -4.500   0.1705   0.01189   0.00485  -0.1227   0.6756   0.0879
  -4.250   0.1941   0.01167   0.00458  -0.1218   0.6692   0.0924
  -4.000   0.2168   0.01153   0.00446  -0.1206   0.6621   0.0976
  -3.750   0.2407   0.01144   0.00428  -0.1197   0.6555   0.1027
  -3.500   0.2632   0.01125   0.00412  -0.1186   0.6487   0.1107
  -3.250   0.2860   0.01115   0.00396  -0.1174   0.6416   0.1181
  -3.000   0.3092   0.01106   0.00386  -0.1164   0.6351   0.1270
  -2.750   0.3316   0.01096   0.00377  -0.1153   0.6280   0.1352
  -2.500   0.3550   0.01095   0.00370  -0.1143   0.6215   0.1437
  -2.250   0.3773   0.01087   0.00364  -0.1131   0.6146   0.1521
  -2.000   0.4003   0.01087   0.00359  -0.1120   0.6080   0.1605
  -1.750   0.4230   0.01083   0.00357  -0.1109   0.6018   0.1698
  -1.500   0.4455   0.01083   0.00353  -0.1098   0.5951   0.1789
  -1.250   0.4685   0.01085   0.00353  -0.1088   0.5892   0.1893
  -1.000   0.4907   0.01083   0.00352  -0.1076   0.5830   0.1989
  -0.750   0.5132   0.01085   0.00351  -0.1064   0.5771   0.2082
  -0.500   0.5361   0.01088   0.00351  -0.1054   0.5718   0.2177
  -0.250   0.5585   0.01090   0.00353  -0.1043   0.5661   0.2272
   0.000   0.5799   0.01090   0.00354  -0.1030   0.5606   0.2379
   0.250   0.6033   0.01097   0.00356  -0.1021   0.5556   0.2469
   0.500   0.6237   0.01094   0.00358  -0.1006   0.5506   0.2554
   0.750   0.6445   0.01097   0.00358  -0.0991   0.5454   0.2635
   1.000   0.6671   0.01103   0.00361  -0.0981   0.5408   0.2735
   1.250   0.6868   0.01102   0.00365  -0.0965   0.5364   0.2835
   1.750   0.7278   0.01107   0.00373  -0.0936   0.5271   0.3129
   2.000   0.7492   0.01110   0.00382  -0.0923   0.5227   0.3347
   2.250   0.7676   0.01108   0.00390  -0.0905   0.5183   0.3650
   2.500   0.7856   0.01102   0.00398  -0.0886   0.5140   0.4167
   2.750   0.9118   0.01064   0.00490  -0.1102   0.5071   0.9731
   3.000   0.9653   0.01093   0.00518  -0.1159   0.5018   0.9856
   3.250   1.0149   0.01118   0.00537  -0.1208   0.4966   0.9925
   3.500   1.0637   0.01143   0.00553  -0.1256   0.4913   0.9968
   3.750   1.1063   0.01153   0.00565  -0.1291   0.4864   1.0000
   4.000   1.1176   0.01161   0.00572  -0.1259   0.4821   1.0000
   4.250   1.1283   0.01173   0.00580  -0.1226   0.4781   1.0000
   4.500   1.1379   0.01183   0.00589  -0.1190   0.4736   1.0000
   4.750   1.1460   0.01189   0.00597  -0.1151   0.4687   1.0000
   5.000   1.1554   0.01200   0.00605  -0.1115   0.4637   1.0000
   5.250   1.1672   0.01216   0.00618  -0.1084   0.4585   1.0000
   5.500   1.1784   0.01226   0.00631  -0.1053   0.4534   1.0000
   5.750   1.1904   0.01241   0.00645  -0.1023   0.4480   1.0000
   6.000   1.2040   0.01263   0.00662  -0.0997   0.4431   1.0000
   6.250   1.2181   0.01277   0.00680  -0.0973   0.4380   1.0000
   6.500   1.2328   0.01296   0.00700  -0.0950   0.4331   1.0000
   6.750   1.2466   0.01324   0.00722  -0.0926   0.4281   1.0000
   7.000   1.2628   0.01342   0.00746  -0.0906   0.4234   1.0000
   7.250   1.2783   0.01366   0.00771  -0.0886   0.4183   1.0000
   7.500   1.2925   0.01397   0.00800  -0.0864   0.4134   1.0000
   7.750   1.3090   0.01423   0.00829  -0.0846   0.4085   1.0000
   8.000   1.3247   0.01452   0.00861  -0.0828   0.4031   1.0000
   8.250   1.3382   0.01491   0.00896  -0.0806   0.3977   1.0000
   8.500   1.3537   0.01524   0.00934  -0.0788   0.3914   1.0000
   8.750   1.3656   0.01569   0.00977  -0.0765   0.3838   1.0000
   9.000   1.3792   0.01613   0.01023  -0.0746   0.3766   1.0000
   9.250   1.3925   0.01661   0.01072  -0.0727   0.3701   1.0000
   9.500   1.4044   0.01717   0.01128  -0.0706   0.3625   1.0000
   9.750   1.4162   0.01776   0.01188  -0.0686   0.3543   1.0000
  10.000   1.4276   0.01842   0.01254  -0.0666   0.3469   1.0000
  10.250   1.4393   0.01909   0.01323  -0.0648   0.3393   1.0000
  10.500   1.4498   0.01986   0.01400  -0.0629   0.3323   1.0000
  10.750   1.4609   0.02063   0.01480  -0.0611   0.3245   1.0000
  11.000   1.4697   0.02156   0.01574  -0.0592   0.3163   1.0000
  11.250   1.4783   0.02256   0.01674  -0.0573   0.3078   1.0000
  11.500   1.4862   0.02364   0.01783  -0.0555   0.2986   1.0000
  11.750   1.4899   0.02504   0.01921  -0.0534   0.2884   1.0000
  12.000   1.4966   0.02631   0.02050  -0.0518   0.2782   1.0000
  12.250   1.5014   0.02777   0.02196  -0.0501   0.2679   1.0000
  12.500   1.5027   0.02955   0.02373  -0.0482   0.2563   1.0000
  12.750   1.5016   0.03159   0.02574  -0.0463   0.2439   1.0000
  13.000   1.4996   0.03377   0.02790  -0.0445   0.2306   1.0000
  13.250   1.4925   0.03645   0.03053  -0.0425   0.2141   1.0000
  13.500   1.4844   0.03933   0.03335  -0.0407   0.1981   1.0000
  13.750   1.4761   0.04230   0.03628  -0.0390   0.1843   1.0000
  14.000   1.4637   0.04576   0.03968  -0.0374   0.1680   1.0000
  14.250   1.4532   0.04918   0.04306  -0.0360   0.1541   1.0000
  14.500   1.4371   0.05325   0.04706  -0.0347   0.1364   1.0000
  14.750   1.4157   0.05803   0.05172  -0.0334   0.1117   1.0000
  15.000   1.3810   0.06441   0.05792  -0.0321   0.0775   1.0000
  15.250   1.3585   0.06967   0.06312  -0.0314   0.0581   1.0000
  15.500   1.3314   0.07566   0.06906  -0.0309   0.0356   1.0000
  15.750   1.3147   0.08059   0.07396  -0.0307   0.0239   1.0000
  16.000   1.3073   0.08446   0.07788  -0.0307   0.0213   1.0000
  16.250   1.3006   0.08837   0.08186  -0.0308   0.0195   1.0000
  16.500   1.2969   0.09189   0.08548  -0.0310   0.0186   1.0000
  16.750   1.2926   0.09551   0.08919  -0.0312   0.0180   1.0000
  17.000   1.2857   0.09955   0.09332  -0.0316   0.0172   1.0000
  17.250   1.2787   0.10366   0.09752  -0.0321   0.0168   1.0000
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