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GOE 648 AIRFOIL (goe648-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 648 AIRFOIL (goe648-il)
Reynolds number: 1,000,000
Max Cl/Cd: 104.31 at α=8°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe648-il-1000000.txt
Download as CSV file: xf-goe648-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 648 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
  ------ -------- --------- --------- -------- -------- --------
 -18.750  -0.7536   0.11996   0.11747  -0.0491   1.0000   0.0186
 -18.500  -0.7967   0.10831   0.10566  -0.0556   1.0000   0.0188
 -18.250  -0.8228   0.10026   0.09751  -0.0601   1.0000   0.0188
 -18.000  -0.8524   0.09176   0.08889  -0.0649   1.0000   0.0189
 -17.750  -0.8845   0.08319   0.08019  -0.0699   1.0000   0.0190
 -17.500  -0.9145   0.07540   0.07228  -0.0743   1.0000   0.0190
 -17.250  -0.9449   0.06774   0.06450  -0.0787   1.0000   0.0191
 -17.000  -0.9755   0.06027   0.05690  -0.0830   1.0000   0.0191
 -16.750  -0.9965   0.05405   0.05055  -0.0866   1.0000   0.0191
 -16.500  -1.0217   0.04750   0.04387  -0.0905   1.0000   0.0191
 -16.250  -1.0460   0.04147   0.03770  -0.0939   1.0000   0.0193
 -16.000  -1.0624   0.03691   0.03303  -0.0961   1.0000   0.0194
 -15.750  -1.0781   0.03304   0.02905  -0.0972   1.0000   0.0196
 -15.500  -1.0894   0.03035   0.02629  -0.0968   1.0000   0.0198
 -15.250  -1.0990   0.02846   0.02433  -0.0950   1.0000   0.0200
 -15.000  -1.1137   0.02697   0.02276  -0.0915   1.0000   0.0201
 -14.750  -1.1339   0.02602   0.02175  -0.0856   1.0000   0.0202
 -14.500  -1.1286   0.02527   0.02094  -0.0833   0.9989   0.0205
 -14.250  -1.1018   0.02445   0.02007  -0.0844   0.9969   0.0210
 -14.000  -1.0735   0.02363   0.01919  -0.0857   0.9949   0.0214
 -13.750  -1.0442   0.02285   0.01833  -0.0871   0.9934   0.0219
 -13.500  -1.0175   0.02213   0.01753  -0.0877   0.9912   0.0222
 -13.250  -0.9943   0.02098   0.01631  -0.0881   0.9878   0.0228
 -13.000  -0.9670   0.02008   0.01538  -0.0890   0.9854   0.0233
 -12.750  -0.9364   0.01947   0.01474  -0.0902   0.9837   0.0239
 -12.500  -0.9046   0.01886   0.01410  -0.0915   0.9825   0.0244
 -12.250  -0.8703   0.01832   0.01350  -0.0932   0.9814   0.0251
 -12.000  -0.8443   0.01787   0.01299  -0.0929   0.9768   0.0256
 -11.750  -0.8152   0.01707   0.01214  -0.0938   0.9734   0.0264
 -11.500  -0.7837   0.01637   0.01143  -0.0949   0.9714   0.0272
 -11.250  -0.7503   0.01586   0.01089  -0.0963   0.9699   0.0279
 -11.000  -0.7162   0.01537   0.01037  -0.0977   0.9688   0.0286
 -10.750  -0.6880   0.01496   0.00992  -0.0978   0.9651   0.0293
 -10.500  -0.6603   0.01445   0.00935  -0.0979   0.9606   0.0300
 -10.250  -0.6284   0.01382   0.00872  -0.0990   0.9578   0.0311
 -10.000  -0.5945   0.01339   0.00827  -0.1004   0.9554   0.0320
  -9.750  -0.5607   0.01302   0.00787  -0.1016   0.9522   0.0330
  -9.500  -0.5353   0.01273   0.00753  -0.1010   0.9445   0.0337
  -9.250  -0.5034   0.01215   0.00692  -0.1019   0.9397   0.0349
  -9.000  -0.4766   0.01180   0.00656  -0.1017   0.9312   0.0360
  -8.750  -0.4449   0.01149   0.00621  -0.1024   0.9232   0.0372
  -8.500  -0.4180   0.01127   0.00593  -0.1020   0.9123   0.0383
  -8.250  -0.3912   0.01089   0.00550  -0.1017   0.9024   0.0397
  -8.000  -0.3654   0.01063   0.00520  -0.1011   0.8915   0.0410
  -7.750  -0.3393   0.01044   0.00497  -0.1006   0.8813   0.0426
  -7.250  -0.2890   0.00999   0.00444  -0.0991   0.8594   0.0463
  -7.000  -0.2634   0.00984   0.00424  -0.0984   0.8492   0.0484
  -6.750  -0.2384   0.00964   0.00402  -0.0976   0.8396   0.0513
  -6.500  -0.2127   0.00951   0.00386  -0.0969   0.8304   0.0542
  -6.250  -0.1877   0.00935   0.00367  -0.0961   0.8200   0.0576
  -6.000  -0.1620   0.00925   0.00355  -0.0954   0.8099   0.0612
  -5.750  -0.1367   0.00913   0.00339  -0.0946   0.7995   0.0650
  -5.500  -0.1110   0.00903   0.00328  -0.0939   0.7887   0.0686
  -5.250  -0.0856   0.00894   0.00314  -0.0932   0.7775   0.0719
  -5.000  -0.0606   0.00882   0.00300  -0.0923   0.7652   0.0755
  -4.750  -0.0348   0.00876   0.00289  -0.0916   0.7523   0.0785
  -4.500  -0.0100   0.00865   0.00274  -0.0908   0.7391   0.0821
  -4.250   0.0147   0.00856   0.00261  -0.0899   0.7245   0.0859
  -4.000   0.0395   0.00853   0.00250  -0.0890   0.7076   0.0887
  -3.750   0.0637   0.00845   0.00237  -0.0880   0.6897   0.0932
  -3.500   0.0881   0.00839   0.00227  -0.0870   0.6722   0.0982
  -3.000   0.1370   0.00828   0.00210  -0.0852   0.6389   0.1156
  -2.750   0.1611   0.00817   0.00203  -0.0842   0.6238   0.1379
  -2.500   0.1848   0.00804   0.00196  -0.0833   0.6091   0.1702
  -2.250   0.2085   0.00792   0.00191  -0.0823   0.5941   0.2058
  -2.000   0.2323   0.00784   0.00188  -0.0813   0.5792   0.2411
  -1.750   0.2564   0.00778   0.00186  -0.0804   0.5646   0.2719
  -1.500   0.2814   0.00772   0.00184  -0.0796   0.5506   0.2997
  -1.250   0.3057   0.00767   0.00183  -0.0787   0.5361   0.3314
  -1.000   0.3295   0.00761   0.00183  -0.0778   0.5207   0.3697
  -0.750   0.3527   0.00754   0.00184  -0.0767   0.5036   0.4169
  -0.500   0.3756   0.00752   0.00187  -0.0756   0.4833   0.4662
  -0.250   0.3978   0.00756   0.00192  -0.0743   0.4581   0.5077
   0.250   0.4415   0.00782   0.00207  -0.0716   0.3970   0.5714
   0.500   0.4633   0.00799   0.00216  -0.0702   0.3701   0.5968
   0.750   0.4858   0.00810   0.00225  -0.0690   0.3529   0.6218
   1.000   0.5088   0.00815   0.00234  -0.0679   0.3416   0.6535
   1.250   0.5306   0.00819   0.00245  -0.0665   0.3320   0.6954
   1.500   0.5534   0.00821   0.00254  -0.0652   0.3252   0.7349
   1.750   0.5756   0.00828   0.00265  -0.0639   0.3181   0.7679
   2.000   0.5978   0.00829   0.00275  -0.0625   0.3134   0.8066
   2.250   0.6196   0.00825   0.00283  -0.0610   0.3094   0.8474
   2.500   0.6518   0.00824   0.00299  -0.0617   0.3041   0.9152
   2.750   0.7292   0.00854   0.00326  -0.0725   0.2970   0.9550
   3.000   0.7821   0.00870   0.00340  -0.0779   0.2930   0.9780
   3.250   0.8181   0.00889   0.00354  -0.0796   0.2887   0.9943
   3.500   0.8594   0.00911   0.00370  -0.0825   0.2839   1.0000
   3.750   0.8792   0.00927   0.00383  -0.0808   0.2803   1.0000
   4.000   0.9015   0.00934   0.00390  -0.0796   0.2782   1.0000
   4.250   0.9234   0.00944   0.00399  -0.0783   0.2755   1.0000
   4.500   0.9450   0.00956   0.00409  -0.0769   0.2721   1.0000
   4.750   0.9659   0.00972   0.00422  -0.0755   0.2689   1.0000
   5.000   0.9859   0.00991   0.00438  -0.0739   0.2649   1.0000
   5.250   1.0079   0.01004   0.00450  -0.0726   0.2624   1.0000
   5.500   1.0304   0.01014   0.00462  -0.0715   0.2601   1.0000
   5.750   1.0524   0.01027   0.00474  -0.0703   0.2570   1.0000
   6.000   1.0734   0.01043   0.00488  -0.0689   0.2534   1.0000
   6.250   1.0919   0.01062   0.00505  -0.0670   0.2499   1.0000
   6.500   1.1106   0.01080   0.00521  -0.0652   0.2464   1.0000
   6.750   1.1318   0.01091   0.00534  -0.0638   0.2438   1.0000
   7.000   1.1523   0.01105   0.00548  -0.0624   0.2402   1.0000
   7.250   1.1718   0.01124   0.00565  -0.0608   0.2364   1.0000
   7.500   1.1897   0.01151   0.00588  -0.0589   0.2316   1.0000
   7.750   1.2120   0.01163   0.00603  -0.0579   0.2281   1.0000
   8.000   1.2329   0.01182   0.00621  -0.0566   0.2239   1.0000
   8.250   1.2523   0.01206   0.00643  -0.0552   0.2194   1.0000
   8.500   1.2718   0.01232   0.00668  -0.0538   0.2150   1.0000
   8.750   1.2931   0.01252   0.00690  -0.0527   0.2113   1.0000
   9.000   1.3128   0.01278   0.00715  -0.0513   0.2067   1.0000
   9.250   1.3308   0.01313   0.00747  -0.0498   0.2014   1.0000
   9.500   1.3517   0.01337   0.00773  -0.0487   0.1983   1.0000
   9.750   1.3712   0.01367   0.00803  -0.0475   0.1936   1.0000
  10.000   1.3888   0.01406   0.00839  -0.0460   0.1885   1.0000
  10.250   1.4080   0.01440   0.00874  -0.0448   0.1847   1.0000
  10.500   1.4269   0.01475   0.00910  -0.0436   0.1808   1.0000
  10.750   1.4441   0.01519   0.00953  -0.0422   0.1761   1.0000
  11.000   1.4608   0.01566   0.01000  -0.0408   0.1719   1.0000
  11.250   1.4796   0.01604   0.01041  -0.0396   0.1685   1.0000
  11.500   1.4968   0.01651   0.01088  -0.0384   0.1650   1.0000
  11.750   1.5119   0.01710   0.01146  -0.0369   0.1608   1.0000
  12.000   1.5287   0.01761   0.01200  -0.0357   0.1575   1.0000
  12.250   1.5460   0.01811   0.01253  -0.0346   0.1548   1.0000
  12.500   1.5615   0.01871   0.01314  -0.0333   0.1511   1.0000
  12.750   1.5749   0.01945   0.01388  -0.0319   0.1473   1.0000
  13.000   1.5905   0.02009   0.01454  -0.0307   0.1439   1.0000
  13.250   1.6058   0.02075   0.01523  -0.0296   0.1403   1.0000
  13.500   1.6184   0.02159   0.01608  -0.0283   0.1364   1.0000
  13.750   1.6304   0.02249   0.01700  -0.0270   0.1324   1.0000
  14.000   1.6448   0.02326   0.01780  -0.0261   0.1290   1.0000
  14.250   1.6541   0.02439   0.01891  -0.0247   0.1233   1.0000
  14.500   1.6653   0.02541   0.01997  -0.0236   0.1200   1.0000
  14.750   1.6757   0.02652   0.02110  -0.0225   0.1149   1.0000
  15.000   1.6815   0.02800   0.02257  -0.0212   0.1095   1.0000
  15.250   1.6896   0.02935   0.02394  -0.0201   0.1038   1.0000
  15.500   1.6920   0.03118   0.02576  -0.0189   0.0969   1.0000
  15.750   1.6909   0.03339   0.02795  -0.0176   0.0888   1.0000
  16.000   1.6836   0.03623   0.03075  -0.0164   0.0777   1.0000
  16.250   1.6760   0.03926   0.03378  -0.0154   0.0702   1.0000
  16.500   1.6727   0.04204   0.03660  -0.0149   0.0664   1.0000
  16.750   1.6649   0.04537   0.03996  -0.0145   0.0625   1.0000
  17.000   1.6619   0.04832   0.04298  -0.0143   0.0607   1.0000
  17.250   1.6558   0.05172   0.04645  -0.0144   0.0590   1.0000
  17.500   1.6463   0.05559   0.05039  -0.0146   0.0573   1.0000
  17.750   1.6356   0.05970   0.05458  -0.0150   0.0557   1.0000
  18.000   1.6300   0.06330   0.05828  -0.0155   0.0550   1.0000
  18.250   1.6212   0.06737   0.06245  -0.0162   0.0544   1.0000
  18.500   1.6089   0.07193   0.06712  -0.0171   0.0536   1.0000
  18.750   1.5943   0.07692   0.07220  -0.0182   0.0528   1.0000
  19.000   1.5784   0.08219   0.07758  -0.0196   0.0523   1.0000
  19.250   1.5596   0.08792   0.08342  -0.0212   0.0518   1.0000
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