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GOE 626 AIRFOIL (goe626-il) Xfoil prediction polar at RE=1,000,000 Ncrit=5


Details Polar file
Airfoil: GOE 626 AIRFOIL (goe626-il)
Reynolds number: 1,000,000
Max Cl/Cd: 94.86 at α=4.5°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe626-il-1000000-n5.txt
Download as CSV file: xf-goe626-il-1000000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 626 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 =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.7658   0.09063   0.08729  -0.0690   1.0000   0.0234
 -16.500  -0.7661   0.08773   0.08435  -0.0699   1.0000   0.0235
 -16.250  -0.7667   0.08488   0.08147  -0.0708   1.0000   0.0237
 -16.000  -0.7659   0.08235   0.07891  -0.0713   1.0000   0.0237
 -15.750  -0.7657   0.07980   0.07634  -0.0718   1.0000   0.0239
 -15.500  -0.7651   0.07683   0.07334  -0.0731   0.9999   0.0240
 -15.250  -0.7554   0.07371   0.07017  -0.0762   0.9992   0.0242
 -15.000  -0.7449   0.07081   0.06724  -0.0791   0.9984   0.0243
 -14.750  -0.7343   0.06802   0.06442  -0.0818   0.9974   0.0243
 -14.500  -0.7253   0.06484   0.06119  -0.0850   0.9960   0.0245
 -14.250  -0.7138   0.06202   0.05833  -0.0881   0.9942   0.0246
 -14.000  -0.7037   0.05934   0.05562  -0.0906   0.9919   0.0247
 -13.750  -0.6962   0.05654   0.05279  -0.0930   0.9892   0.0247
 -13.500  -0.6880   0.05361   0.04982  -0.0959   0.9862   0.0249
 -13.250  -0.6770   0.05087   0.04705  -0.0991   0.9833   0.0249
 -12.750  -0.6712   0.04420   0.04030  -0.1060   0.9722   0.0253
 -12.500  -0.6674   0.04033   0.03637  -0.1112   0.9660   0.0254
 -12.000  -0.6486   0.02865   0.02444  -0.1334   0.9434   0.0256
 -11.750  -0.6288   0.02256   0.01813  -0.1446   0.9314   0.0258
 -11.500  -0.6041   0.01936   0.01476  -0.1494   0.9220   0.0260
 -11.250  -0.5815   0.01805   0.01334  -0.1507   0.9131   0.0262
 -11.000  -0.5572   0.01709   0.01228  -0.1515   0.9047   0.0264
 -10.750  -0.5339   0.01632   0.01144  -0.1517   0.8962   0.0266
 -10.500  -0.5097   0.01567   0.01070  -0.1518   0.8879   0.0268
 -10.250  -0.4853   0.01508   0.01004  -0.1518   0.8812   0.0271
 -10.000  -0.4609   0.01456   0.00945  -0.1517   0.8732   0.0273
  -9.750  -0.4358   0.01410   0.00890  -0.1516   0.8650   0.0276
  -9.500  -0.4107   0.01366   0.00840  -0.1513   0.8568   0.0278
  -9.000  -0.3598   0.01292   0.00751  -0.1508   0.8376   0.0283
  -8.750  -0.3343   0.01261   0.00711  -0.1505   0.8269   0.0285
  -8.500  -0.3083   0.01231   0.00675  -0.1502   0.8169   0.0288
  -8.250  -0.2824   0.01199   0.00636  -0.1499   0.8079   0.0292
  -8.000  -0.2563   0.01164   0.00595  -0.1496   0.7981   0.0296
  -7.750  -0.2303   0.01136   0.00560  -0.1492   0.7873   0.0301
  -7.500  -0.2042   0.01111   0.00529  -0.1489   0.7744   0.0305
  -7.250  -0.1782   0.01089   0.00500  -0.1484   0.7587   0.0310
  -7.000  -0.1528   0.01073   0.00473  -0.1478   0.7379   0.0315
  -6.750  -0.1284   0.01063   0.00449  -0.1470   0.7079   0.0320
  -6.500  -0.1049   0.01060   0.00429  -0.1460   0.6718   0.0326
  -6.250  -0.0803   0.01056   0.00411  -0.1452   0.6461   0.0331
  -6.000  -0.0542   0.01044   0.00391  -0.1448   0.6303   0.0344
  -5.750  -0.0277   0.01031   0.00372  -0.1444   0.6186   0.0361
  -5.500  -0.0010   0.01016   0.00352  -0.1440   0.6077   0.0396
  -5.250   0.0250   0.00969   0.00316  -0.1438   0.5996   0.0726
  -5.000   0.0524   0.00954   0.00299  -0.1436   0.5919   0.0809
  -4.750   0.0794   0.00940   0.00284  -0.1433   0.5841   0.0894
  -4.500   0.1069   0.00915   0.00263  -0.1432   0.5773   0.1066
  -4.250   0.1337   0.00885   0.00241  -0.1429   0.5699   0.1341
  -4.000   0.1607   0.00862   0.00224  -0.1427   0.5635   0.1609
  -3.750   0.1885   0.00845   0.00213  -0.1426   0.5573   0.1821
  -3.500   0.2159   0.00838   0.00209  -0.1423   0.5492   0.1980
  -3.250   0.2437   0.00836   0.00206  -0.1420   0.5420   0.2099
  -3.000   0.2716   0.00835   0.00206  -0.1418   0.5341   0.2200
  -2.750   0.2992   0.00839   0.00205  -0.1415   0.5262   0.2249
  -2.500   0.3273   0.00839   0.00205  -0.1413   0.5190   0.2294
  -2.250   0.3545   0.00844   0.00207  -0.1409   0.5082   0.2345
  -2.000   0.3819   0.00851   0.00208  -0.1405   0.4953   0.2385
  -1.750   0.4088   0.00858   0.00209  -0.1401   0.4823   0.2412
  -1.500   0.4357   0.00865   0.00211  -0.1396   0.4711   0.2440
  -1.250   0.4633   0.00870   0.00214  -0.1393   0.4625   0.2471
  -1.000   0.4902   0.00879   0.00219  -0.1389   0.4531   0.2504
  -0.750   0.5175   0.00887   0.00222  -0.1385   0.4436   0.2528
  -0.500   0.5439   0.00899   0.00227  -0.1380   0.4324   0.2544
  -0.250   0.5707   0.00907   0.00230  -0.1375   0.4211   0.2566
   0.000   0.5973   0.00914   0.00235  -0.1371   0.4126   0.2589
   0.250   0.6244   0.00920   0.00239  -0.1367   0.4056   0.2607
   0.500   0.6511   0.00929   0.00245  -0.1362   0.3988   0.2622
   0.750   0.6782   0.00935   0.00250  -0.1358   0.3937   0.2640
   1.000   0.7052   0.00942   0.00255  -0.1354   0.3881   0.2654
   1.250   0.7317   0.00951   0.00262  -0.1350   0.3820   0.2667
   1.500   0.7584   0.00959   0.00268  -0.1345   0.3769   0.2679
   1.750   0.7849   0.00968   0.00274  -0.1340   0.3690   0.2690
   2.000   0.8105   0.00981   0.00283  -0.1334   0.3604   0.2700
   2.250   0.8371   0.00989   0.00290  -0.1329   0.3547   0.2708
   2.500   0.8627   0.01001   0.00298  -0.1323   0.3465   0.2723
   2.750   0.8882   0.01013   0.00307  -0.1317   0.3373   0.2743
   3.000   0.9129   0.01029   0.00319  -0.1309   0.3267   0.2760
   3.250   0.9384   0.01040   0.00329  -0.1303   0.3193   0.2776
   3.500   0.9634   0.01054   0.00340  -0.1296   0.3115   0.2792
   3.750   0.9884   0.01067   0.00353  -0.1289   0.3053   0.2808
   4.000   1.0132   0.01081   0.00364  -0.1281   0.2976   0.2824
   4.250   1.0370   0.01099   0.00379  -0.1272   0.2891   0.2839
   4.500   1.0605   0.01118   0.00394  -0.1263   0.2775   0.2853
   4.750   1.0824   0.01145   0.00413  -0.1250   0.2619   0.2866
   5.000   1.1033   0.01171   0.00432  -0.1236   0.2470   0.2877
   5.250   1.1199   0.01213   0.00460  -0.1215   0.2223   0.2889
   5.500   1.1310   0.01278   0.00504  -0.1184   0.1833   0.2910
   5.750   1.1472   0.01321   0.00538  -0.1162   0.1668   0.2934
   6.000   1.1673   0.01347   0.00564  -0.1147   0.1608   0.2957
   6.250   1.1872   0.01374   0.00590  -0.1132   0.1558   0.2978
   6.500   1.2068   0.01403   0.00618  -0.1116   0.1507   0.2998
   6.750   1.2277   0.01424   0.00641  -0.1103   0.1483   0.3019
   7.000   1.2479   0.01450   0.00668  -0.1089   0.1452   0.3038
   7.250   1.2674   0.01479   0.00696  -0.1073   0.1416   0.3055
   7.500   1.2860   0.01511   0.00728  -0.1057   0.1377   0.3071
   7.750   1.3056   0.01537   0.00757  -0.1042   0.1351   0.3104
   8.000   1.3249   0.01565   0.00788  -0.1028   0.1312   0.3138
   8.250   1.3417   0.01605   0.00826  -0.1009   0.1253   0.3168
   8.500   1.3591   0.01642   0.00863  -0.0992   0.1201   0.3201
   8.750   1.3736   0.01694   0.00910  -0.0972   0.1104   0.3230
   9.000   1.3688   0.01838   0.01029  -0.0925   0.0707   0.3249
   9.250   1.3787   0.01914   0.01104  -0.0899   0.0623   0.3299
   9.500   1.3915   0.01977   0.01169  -0.0878   0.0590   0.3354
   9.750   1.4043   0.02043   0.01236  -0.0858   0.0562   0.3411
  10.000   1.4181   0.02103   0.01301  -0.0840   0.0549   0.3476
  10.250   1.4317   0.02167   0.01370  -0.0822   0.0537   0.3571
  10.500   1.4446   0.02236   0.01444  -0.0804   0.0529   0.3672
  11.000   1.4690   0.02387   0.01609  -0.0769   0.0513   0.4070
  11.250   1.4800   0.02472   0.01705  -0.0751   0.0504   0.4433
  11.500   1.4903   0.02563   0.01808  -0.0734   0.0494   0.4909
  11.750   1.5010   0.02636   0.01914  -0.0717   0.0489   0.6366
  12.250   1.5348   0.02789   0.02135  -0.0710   0.0479   1.0000
  12.500   1.5452   0.02903   0.02252  -0.0697   0.0473   1.0000
  12.750   1.5547   0.03027   0.02380  -0.0683   0.0468   1.0000
  13.000   1.5633   0.03164   0.02521  -0.0670   0.0463   1.0000
  13.250   1.5712   0.03311   0.02672  -0.0658   0.0458   1.0000
  13.500   1.5786   0.03467   0.02832  -0.0647   0.0454   1.0000
  13.750   1.5851   0.03637   0.03007  -0.0636   0.0449   1.0000
  14.000   1.5904   0.03827   0.03201  -0.0627   0.0443   1.0000
  14.250   1.5949   0.04031   0.03410  -0.0619   0.0438   1.0000
  14.500   1.5995   0.04243   0.03628  -0.0612   0.0435   1.0000
  14.750   1.6020   0.04482   0.03874  -0.0606   0.0431   1.0000
  15.000   1.6070   0.04703   0.04101  -0.0602   0.0428   1.0000
  15.250   1.6113   0.04937   0.04341  -0.0599   0.0427   1.0000
  15.500   1.6161   0.05169   0.04579  -0.0596   0.0423   1.0000
  15.750   1.6193   0.05421   0.04838  -0.0594   0.0422   1.0000
  16.000   1.6225   0.05677   0.05100  -0.0593   0.0417   1.0000
  16.250   1.6241   0.05957   0.05387  -0.0593   0.0413   1.0000
  16.500   1.6254   0.06245   0.05681  -0.0594   0.0409   1.0000
  16.750   1.6259   0.06546   0.05990  -0.0596   0.0405   1.0000
  17.000   1.6253   0.06868   0.06318  -0.0599   0.0401   1.0000
  17.250   1.6239   0.07206   0.06663  -0.0603   0.0398   1.0000
  17.500   1.6225   0.07551   0.07014  -0.0608   0.0393   1.0000
  17.750   1.6210   0.07901   0.07371  -0.0615   0.0389   1.0000
  18.000   1.6177   0.08282   0.07759  -0.0623   0.0385   1.0000
  18.250   1.6138   0.08680   0.08163  -0.0632   0.0380   1.0000
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