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GOE 410 AIRFOIL (goe410-il) Xfoil prediction polar at RE=500,000 Ncrit=9


Details Polar file
Airfoil: GOE 410 AIRFOIL (goe410-il)
Reynolds number: 500,000
Max Cl/Cd: 62.4 at α=9.25°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe410-il-500000.txt
Download as CSV file: xf-goe410-il-500000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 410 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
  ------ -------- --------- --------- -------- -------- --------
 -19.000  -1.2681   0.08888   0.08426  -0.0157   1.0000   0.0451
 -18.750  -1.2754   0.08446   0.07982  -0.0177   1.0000   0.0459
 -18.500  -1.2823   0.08009   0.07541  -0.0197   1.0000   0.0467
 -18.250  -1.2887   0.07584   0.07111  -0.0216   1.0000   0.0477
 -18.000  -1.2928   0.07197   0.06715  -0.0232   1.0000   0.0487
 -17.750  -1.2956   0.06836   0.06344  -0.0246   1.0000   0.0499
 -17.500  -1.3002   0.06464   0.05966  -0.0260   1.0000   0.0511
 -17.250  -1.3054   0.06089   0.05589  -0.0275   1.0000   0.0523
 -17.000  -1.3082   0.05751   0.05246  -0.0287   1.0000   0.0537
 -16.750  -1.3081   0.05455   0.04941  -0.0296   1.0000   0.0553
 -16.500  -1.3088   0.05159   0.04637  -0.0304   1.0000   0.0569
 -16.250  -1.3119   0.04847   0.04324  -0.0313   1.0000   0.0585
 -16.000  -1.3099   0.04590   0.04062  -0.0319   1.0000   0.0604
 -15.750  -1.3043   0.04373   0.03834  -0.0324   1.0000   0.0627
 -15.500  -1.3051   0.04100   0.03560  -0.0329   1.0000   0.0645
 -15.250  -1.3009   0.03877   0.03334  -0.0333   1.0000   0.0665
 -15.000  -1.2933   0.03691   0.03139  -0.0336   1.0000   0.0687
 -14.750  -1.2862   0.03506   0.02945  -0.0337   1.0000   0.0707
 -14.500  -1.2826   0.03298   0.02738  -0.0338   1.0000   0.0726
 -14.250  -1.2741   0.03138   0.02574  -0.0337   1.0000   0.0746
 -14.000  -1.2633   0.03002   0.02429  -0.0336   1.0000   0.0766
 -13.750  -1.2527   0.02872   0.02289  -0.0332   1.0000   0.0783
 -13.500  -1.2475   0.02709   0.02128  -0.0326   1.0000   0.0802
 -13.250  -1.2380   0.02587   0.02003  -0.0319   1.0000   0.0819
 -13.000  -1.2264   0.02486   0.01897  -0.0312   1.0000   0.0837
 -12.750  -1.2141   0.02395   0.01799  -0.0303   1.0000   0.0853
 -12.500  -1.2002   0.02322   0.01716  -0.0293   1.0000   0.0866
 -12.250  -1.1944   0.02204   0.01600  -0.0275   1.0000   0.0885
 -12.000  -1.1842   0.02126   0.01521  -0.0258   1.0000   0.0902
 -11.750  -1.1715   0.02067   0.01460  -0.0241   1.0000   0.0919
 -11.500  -1.1582   0.02015   0.01403  -0.0223   1.0000   0.0935
 -11.250  -1.1440   0.01970   0.01353  -0.0204   1.0000   0.0950
 -11.000  -1.1278   0.01930   0.01306  -0.0187   1.0000   0.0962
 -10.750  -1.1150   0.01854   0.01232  -0.0168   1.0000   0.0983
 -10.500  -1.0974   0.01803   0.01182  -0.0154   1.0000   0.1001
 -10.250  -1.0775   0.01763   0.01142  -0.0143   1.0000   0.1020
 -10.000  -1.0566   0.01727   0.01103  -0.0132   1.0000   0.1039
  -9.750  -1.0350   0.01693   0.01064  -0.0123   1.0000   0.1056
  -9.500  -1.0143   0.01650   0.01017  -0.0112   1.0000   0.1073
  -9.250  -0.9953   0.01595   0.00967  -0.0099   1.0000   0.1098
  -9.000  -0.9733   0.01561   0.00934  -0.0090   1.0000   0.1124
  -8.750  -0.9503   0.01533   0.00905  -0.0082   1.0000   0.1150
  -8.500  -0.9265   0.01511   0.00880  -0.0075   1.0000   0.1174
  -8.250  -0.9064   0.01462   0.00834  -0.0062   1.0000   0.1204
  -8.000  -0.8852   0.01423   0.00799  -0.0051   1.0000   0.1233
  -7.750  -0.8633   0.01394   0.00770  -0.0041   1.0000   0.1261
  -7.500  -0.8414   0.01368   0.00743  -0.0029   1.0000   0.1289
  -7.250  -0.8123   0.01330   0.00704  -0.0034   0.9930   0.1325
  -7.000  -0.7717   0.01281   0.00662  -0.0063   0.9757   0.1377
  -6.750  -0.7281   0.01252   0.00629  -0.0095   0.9527   0.1428
  -6.500  -0.6926   0.01211   0.00586  -0.0110   0.9177   0.1485
  -6.250  -0.6676   0.01186   0.00553  -0.0103   0.8798   0.1538
  -6.000  -0.6433   0.01175   0.00528  -0.0093   0.8490   0.1584
  -5.750  -0.6205   0.01146   0.00493  -0.0082   0.8239   0.1652
  -5.500  -0.5962   0.01124   0.00465  -0.0073   0.8020   0.1722
  -5.250  -0.5719   0.01097   0.00436  -0.0066   0.7810   0.1816
  -5.000  -0.5476   0.01065   0.00406  -0.0058   0.7601   0.1961
  -4.750  -0.5247   0.01016   0.00372  -0.0050   0.7389   0.2359
  -4.500  -0.5012   0.00973   0.00347  -0.0043   0.7175   0.2900
  -4.250  -0.4756   0.00952   0.00331  -0.0037   0.6958   0.3224
  -4.000  -0.4494   0.00938   0.00317  -0.0032   0.6751   0.3445
  -3.750  -0.4225   0.00930   0.00307  -0.0028   0.6562   0.3623
  -3.500  -0.3951   0.00926   0.00299  -0.0025   0.6395   0.3776
  -3.250  -0.3677   0.00923   0.00292  -0.0022   0.6246   0.3911
  -3.000  -0.3399   0.00919   0.00287  -0.0020   0.6111   0.4023
  -2.750  -0.3116   0.00920   0.00282  -0.0018   0.5998   0.4130
  -2.500  -0.2839   0.00918   0.00279  -0.0016   0.5894   0.4228
  -2.250  -0.2554   0.00919   0.00276  -0.0014   0.5796   0.4331
  -2.000  -0.2275   0.00919   0.00274  -0.0012   0.5694   0.4427
  -1.750  -0.1990   0.00919   0.00273  -0.0010   0.5598   0.4524
  -1.500  -0.1709   0.00920   0.00272  -0.0008   0.5510   0.4616
  -1.250  -0.1422   0.00924   0.00271  -0.0007   0.5434   0.4694
  -1.000  -0.1140   0.00919   0.00271  -0.0006   0.5357   0.4776
  -0.750  -0.0856   0.00927   0.00270  -0.0004   0.5278   0.4858
  -0.500  -0.0570   0.00921   0.00269  -0.0003   0.5205   0.4924
  -0.250  -0.0286   0.00921   0.00268  -0.0001   0.5126   0.4991
   0.000   0.0000   0.00926   0.00268   0.0000   0.5057   0.5057
   0.250   0.0286   0.00921   0.00268   0.0001   0.4991   0.5126
   0.500   0.0570   0.00921   0.00269   0.0003   0.4924   0.5204
   0.750   0.0856   0.00927   0.00270   0.0004   0.4858   0.5278
   1.000   0.1140   0.00919   0.00271   0.0005   0.4775   0.5358
   1.250   0.1422   0.00924   0.00271   0.0007   0.4694   0.5434
   1.500   0.1709   0.00920   0.00272   0.0008   0.4616   0.5509
   1.750   0.1990   0.00920   0.00273   0.0010   0.4524   0.5597
   2.000   0.2275   0.00919   0.00274   0.0012   0.4427   0.5694
   2.250   0.2554   0.00918   0.00276   0.0014   0.4332   0.5797
   2.500   0.2839   0.00918   0.00279   0.0016   0.4228   0.5894
   2.750   0.3117   0.00920   0.00282   0.0018   0.4130   0.5998
   3.000   0.3400   0.00919   0.00287   0.0020   0.4023   0.6111
   3.250   0.3677   0.00923   0.00292   0.0022   0.3911   0.6246
   3.500   0.3951   0.00926   0.00299   0.0025   0.3777   0.6395
   3.750   0.4225   0.00930   0.00307   0.0028   0.3623   0.6562
   4.000   0.4494   0.00938   0.00317   0.0032   0.3445   0.6752
   4.250   0.4757   0.00952   0.00331   0.0037   0.3223   0.6958
   4.500   0.5012   0.00973   0.00347   0.0042   0.2899   0.7174
   4.750   0.5247   0.01016   0.00372   0.0050   0.2359   0.7389
   5.000   0.5477   0.01065   0.00406   0.0058   0.1961   0.7600
   5.250   0.5719   0.01096   0.00436   0.0066   0.1817   0.7810
   5.500   0.5963   0.01124   0.00465   0.0073   0.1722   0.8020
   5.750   0.6205   0.01146   0.00493   0.0082   0.1651   0.8239
   6.000   0.6433   0.01175   0.00528   0.0093   0.1584   0.8488
   6.250   0.6676   0.01186   0.00553   0.0103   0.1538   0.8797
   6.500   0.6927   0.01211   0.00586   0.0110   0.1485   0.9177
   6.750   0.7282   0.01252   0.00629   0.0094   0.1428   0.9528
   7.000   0.7718   0.01281   0.00662   0.0062   0.1378   0.9758
   7.250   0.8123   0.01329   0.00704   0.0034   0.1325   0.9930
   7.500   0.8414   0.01368   0.00743   0.0029   0.1289   1.0000
   7.750   0.8633   0.01394   0.00770   0.0041   0.1261   1.0000
   8.000   0.8852   0.01424   0.00799   0.0051   0.1234   1.0000
   8.250   0.9064   0.01462   0.00834   0.0062   0.1205   1.0000
   8.500   0.9265   0.01511   0.00880   0.0075   0.1174   1.0000
   8.750   0.9503   0.01532   0.00905   0.0082   0.1150   1.0000
   9.000   0.9734   0.01560   0.00933   0.0090   0.1123   1.0000
   9.250   0.9953   0.01595   0.00966   0.0099   0.1098   1.0000
   9.500   1.0144   0.01649   0.01017   0.0112   0.1073   1.0000
   9.750   1.0350   0.01692   0.01063   0.0123   0.1056   1.0000
  10.000   1.0567   0.01726   0.01102   0.0132   0.1039   1.0000
  10.250   1.0775   0.01763   0.01142   0.0143   0.1020   1.0000
  10.500   1.0974   0.01803   0.01183   0.0154   0.1001   1.0000
  10.750   1.1151   0.01853   0.01232   0.0167   0.0982   1.0000
  11.000   1.1279   0.01930   0.01306   0.0187   0.0962   1.0000
  11.250   1.1442   0.01969   0.01352   0.0203   0.0950   1.0000
  11.500   1.1586   0.02014   0.01403   0.0222   0.0935   1.0000
  11.750   1.1719   0.02066   0.01459   0.0241   0.0919   1.0000
  12.000   1.1847   0.02124   0.01519   0.0257   0.0901   1.0000
  12.250   1.1948   0.02203   0.01599   0.0275   0.0885   1.0000
  12.500   1.2005   0.02321   0.01715   0.0293   0.0866   1.0000
  12.750   1.2146   0.02394   0.01798   0.0302   0.0853   1.0000
  13.000   1.2270   0.02483   0.01894   0.0311   0.0836   1.0000
  13.250   1.2385   0.02585   0.02001   0.0318   0.0819   1.0000
  13.500   1.2482   0.02707   0.02125   0.0325   0.0801   1.0000
  13.750   1.2532   0.02871   0.02288   0.0332   0.0783   1.0000
  14.000   1.2642   0.02999   0.02426   0.0335   0.0765   1.0000
  14.250   1.2748   0.03136   0.02571   0.0336   0.0746   1.0000
  14.500   1.2835   0.03295   0.02734   0.0337   0.0725   1.0000
  14.750   1.2874   0.03500   0.02939   0.0336   0.0707   1.0000
  15.000   1.2945   0.03685   0.03133   0.0335   0.0686   1.0000
  15.250   1.3023   0.03870   0.03327   0.0332   0.0665   1.0000
  15.500   1.3064   0.04095   0.03554   0.0328   0.0644   1.0000
  15.750   1.3062   0.04363   0.03824   0.0323   0.0626   1.0000
  16.000   1.3114   0.04584   0.04056   0.0318   0.0604   1.0000
  16.250   1.3136   0.04840   0.04316   0.0311   0.0584   1.0000
  16.500   1.3105   0.05152   0.04630   0.0303   0.0569   1.0000
  16.750   1.3102   0.05444   0.04930   0.0294   0.0552   1.0000
  17.000   1.3100   0.05744   0.05238   0.0285   0.0535   1.0000
  17.250   1.3075   0.06078   0.05577   0.0273   0.0522   1.0000
  17.500   1.3015   0.06462   0.05963   0.0258   0.0510   1.0000
  17.750   1.2982   0.06818   0.06327   0.0245   0.0499   1.0000
  18.000   1.2953   0.07180   0.06698   0.0231   0.0488   1.0000
  18.250   1.2909   0.07571   0.07097   0.0214   0.0477   1.0000
  18.500   1.2853   0.07985   0.07517   0.0196   0.0468   1.0000
  18.750   1.2783   0.08424   0.07959   0.0176   0.0460   1.0000
  19.000   1.2704   0.08873   0.08411   0.0156   0.0451   1.0000
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