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GOE 628 AIRFOIL (goe628-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 628 AIRFOIL (goe628-il)
Reynolds number: 1,000,000
Max Cl/Cd: 111.41 at α=5.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe628-il-1000000.txt
Download as CSV file: xf-goe628-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 628 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
  ------ -------- --------- --------- -------- -------- --------
 -19.750  -0.7381   0.12462   0.12230  -0.0545   1.0000   0.0277
 -19.500  -0.7865   0.11257   0.11009  -0.0618   1.0000   0.0291
 -19.250  -0.8111   0.10497   0.10238  -0.0664   1.0000   0.0300
 -19.000  -0.8235   0.09945   0.09685  -0.0697   1.0000   0.0307
 -18.750  -0.8330   0.09450   0.09185  -0.0725   1.0000   0.0313
 -18.500  -0.8441   0.08936   0.08665  -0.0755   1.0000   0.0320
 -18.250  -0.8572   0.08401   0.08121  -0.0787   1.0000   0.0327
 -18.000  -0.8703   0.07882   0.07593  -0.0818   1.0000   0.0332
 -17.750  -0.8818   0.07389   0.07089  -0.0847   1.0000   0.0337
 -17.500  -0.8882   0.06998   0.06698  -0.0868   1.0000   0.0343
 -17.250  -0.8972   0.06580   0.06276  -0.0891   1.0000   0.0346
 -17.000  -0.9041   0.06201   0.05893  -0.0911   1.0000   0.0349
 -16.750  -0.9098   0.05848   0.05537  -0.0930   1.0000   0.0354
 -16.500  -0.9212   0.05466   0.05150  -0.0948   1.0000   0.0357
 -16.250  -0.9349   0.05082   0.04760  -0.0965   1.0000   0.0360
 -16.000  -0.9489   0.04709   0.04381  -0.0979   1.0000   0.0363
 -15.750  -0.9662   0.04339   0.04006  -0.0989   1.0000   0.0366
 -15.500  -0.9905   0.03965   0.03627  -0.0991   1.0000   0.0368
 -15.250  -1.0039   0.03555   0.03207  -0.1018   0.9991   0.0370
 -15.000  -0.9818   0.03136   0.02774  -0.1102   0.9962   0.0376
 -14.750  -0.9542   0.02768   0.02386  -0.1193   0.9923   0.0380
 -14.500  -0.9394   0.02569   0.02179  -0.1213   0.9862   0.0386
 -14.250  -0.9098   0.02460   0.02068  -0.1237   0.9832   0.0392
 -14.000  -0.8777   0.02382   0.01987  -0.1259   0.9812   0.0397
 -13.750  -0.8490   0.02313   0.01915  -0.1273   0.9779   0.0402
 -13.500  -0.8220   0.02246   0.01842  -0.1282   0.9731   0.0408
 -13.250  -0.7908   0.02177   0.01766  -0.1298   0.9698   0.0414
 -13.000  -0.7553   0.02114   0.01695  -0.1322   0.9675   0.0421
 -12.750  -0.7239   0.02073   0.01645  -0.1335   0.9625   0.0426
 -12.500  -0.6934   0.02020   0.01583  -0.1346   0.9561   0.0430
 -12.250  -0.6644   0.01890   0.01449  -0.1362   0.9500   0.0437
 -12.000  -0.6396   0.01835   0.01391  -0.1361   0.9397   0.0442
 -11.750  -0.6121   0.01793   0.01345  -0.1364   0.9304   0.0447
 -11.500  -0.5871   0.01756   0.01302  -0.1361   0.9192   0.0453
 -11.250  -0.5642   0.01719   0.01258  -0.1353   0.9072   0.0458
 -11.000  -0.5407   0.01684   0.01214  -0.1346   0.8949   0.0463
 -10.750  -0.5178   0.01651   0.01171  -0.1337   0.8812   0.0469
 -10.500  -0.4945   0.01631   0.01142  -0.1328   0.8661   0.0475
 -10.250  -0.4709   0.01613   0.01113  -0.1319   0.8496   0.0479
 -10.000  -0.4487   0.01581   0.01068  -0.1309   0.8314   0.0484
  -9.750  -0.4302   0.01499   0.00979  -0.1294   0.8118   0.0492
  -9.500  -0.4084   0.01462   0.00934  -0.1283   0.7925   0.0498
  -9.250  -0.3857   0.01432   0.00895  -0.1273   0.7754   0.0502
  -9.000  -0.3626   0.01401   0.00856  -0.1263   0.7614   0.0506
  -8.500  -0.3148   0.01340   0.00780  -0.1246   0.7387   0.0514
  -8.250  -0.2907   0.01314   0.00745  -0.1238   0.7290   0.0518
  -8.000  -0.2654   0.01284   0.00710  -0.1232   0.7213   0.0522
  -7.750  -0.2405   0.01258   0.00678  -0.1225   0.7132   0.0526
  -7.500  -0.2150   0.01233   0.00648  -0.1219   0.7059   0.0530
  -7.250  -0.1893   0.01210   0.00619  -0.1213   0.6979   0.0534
  -7.000  -0.1637   0.01192   0.00594  -0.1207   0.6893   0.0537
  -6.750  -0.1372   0.01174   0.00571  -0.1202   0.6809   0.0540
  -6.500  -0.1132   0.01138   0.00527  -0.1193   0.6724   0.0545
  -6.250  -0.0878   0.01100   0.00487  -0.1187   0.6660   0.0552
  -6.000  -0.0619   0.01073   0.00456  -0.1182   0.6595   0.0559
  -5.750  -0.0360   0.01055   0.00432  -0.1176   0.6526   0.0565
  -5.500  -0.0089   0.01034   0.00409  -0.1173   0.6466   0.0571
  -5.250   0.0179   0.01017   0.00389  -0.1168   0.6402   0.0578
  -5.000   0.0444   0.01004   0.00370  -0.1163   0.6337   0.0585
  -4.750   0.0719   0.00989   0.00352  -0.1160   0.6278   0.0592
  -4.500   0.0991   0.00976   0.00335  -0.1156   0.6208   0.0599
  -4.250   0.1259   0.00969   0.00321  -0.1151   0.6136   0.0604
  -4.000   0.1532   0.00949   0.00300  -0.1148   0.6075   0.0620
  -3.750   0.1801   0.00935   0.00283  -0.1144   0.6007   0.0636
  -3.500   0.2070   0.00925   0.00270  -0.1139   0.5939   0.0651
  -3.250   0.2346   0.00915   0.00258  -0.1136   0.5868   0.0668
  -3.000   0.2613   0.00907   0.00246  -0.1131   0.5790   0.0698
  -2.500   0.3137   0.00860   0.00219  -0.1122   0.5644   0.1272
  -2.250   0.3390   0.00836   0.00210  -0.1116   0.5571   0.1752
  -2.000   0.3661   0.00824   0.00207  -0.1113   0.5498   0.2034
  -1.750   0.3925   0.00822   0.00206  -0.1108   0.5414   0.2225
  -1.500   0.4199   0.00820   0.00206  -0.1105   0.5335   0.2361
  -1.250   0.4464   0.00822   0.00208  -0.1100   0.5243   0.2499
  -1.000   0.4736   0.00823   0.00209  -0.1096   0.5162   0.2600
  -0.750   0.5003   0.00828   0.00211  -0.1092   0.5071   0.2686
  -0.500   0.5272   0.00831   0.00213  -0.1088   0.4987   0.2766
  -0.250   0.5537   0.00836   0.00216  -0.1083   0.4890   0.2845
   0.000   0.5804   0.00843   0.00219  -0.1078   0.4796   0.2908
   0.250   0.6060   0.00851   0.00224  -0.1072   0.4683   0.2995
   0.500   0.6326   0.00858   0.00229  -0.1068   0.4577   0.3073
   0.750   0.6581   0.00867   0.00235  -0.1061   0.4464   0.3159
   1.000   0.6837   0.00877   0.00243  -0.1055   0.4347   0.3245
   1.250   0.7093   0.00887   0.00249  -0.1049   0.4236   0.3321
   1.500   0.7341   0.00899   0.00258  -0.1042   0.4118   0.3400
   1.750   0.7591   0.00913   0.00267  -0.1035   0.3998   0.3466
   2.000   0.7838   0.00924   0.00277  -0.1028   0.3885   0.3557
   2.250   0.8077   0.00941   0.00288  -0.1019   0.3776   0.3641
   2.500   0.8325   0.00952   0.00298  -0.1012   0.3684   0.3717
   2.750   0.8562   0.00967   0.00310  -0.1003   0.3596   0.3795
   3.000   0.8811   0.00979   0.00320  -0.0996   0.3527   0.3861
   3.250   0.9041   0.00994   0.00334  -0.0986   0.3453   0.3954
   3.500   0.9285   0.01005   0.00345  -0.0978   0.3399   0.4045
   3.750   0.9521   0.01016   0.00358  -0.0969   0.3343   0.4150
   4.250   0.9977   0.01043   0.00387  -0.0948   0.3241   0.4384
   4.500   1.0211   0.01051   0.00400  -0.0939   0.3204   0.4547
   4.750   1.0423   0.01062   0.00415  -0.0926   0.3165   0.4753
   5.000   1.0611   0.01073   0.00431  -0.0908   0.3123   0.5039
   5.250   1.0785   0.01077   0.00451  -0.0888   0.3085   0.5695
   5.500   1.1488   0.01032   0.00497  -0.0980   0.3044   1.0000
   5.750   1.1687   0.01049   0.00512  -0.0964   0.3013   1.0000
   6.000   1.1874   0.01069   0.00529  -0.0946   0.2981   1.0000
   6.250   1.2051   0.01093   0.00550  -0.0927   0.2945   1.0000
   6.500   1.2235   0.01117   0.00573  -0.0909   0.2915   1.0000
   6.750   1.2454   0.01131   0.00589  -0.0898   0.2897   1.0000
   7.000   1.2668   0.01148   0.00607  -0.0886   0.2873   1.0000
   7.250   1.2871   0.01169   0.00628  -0.0873   0.2846   1.0000
   7.500   1.3066   0.01194   0.00651  -0.0858   0.2818   1.0000
   7.750   1.3248   0.01224   0.00680  -0.0842   0.2786   1.0000
   8.000   1.3421   0.01259   0.00714  -0.0825   0.2751   1.0000
   8.250   1.3651   0.01274   0.00732  -0.0818   0.2727   1.0000
   8.500   1.3863   0.01296   0.00755  -0.0808   0.2698   1.0000
   8.750   1.4060   0.01324   0.00783  -0.0795   0.2666   1.0000
   9.000   1.4247   0.01358   0.00817  -0.0782   0.2640   1.0000
   9.250   1.4414   0.01401   0.00859  -0.0767   0.2608   1.0000
   9.500   1.4601   0.01438   0.00897  -0.0754   0.2585   1.0000
   9.750   1.4812   0.01464   0.00928  -0.0746   0.2566   1.0000
  10.000   1.5015   0.01496   0.00962  -0.0736   0.2545   1.0000
  10.250   1.5208   0.01533   0.01001  -0.0726   0.2519   1.0000
  10.500   1.5386   0.01578   0.01047  -0.0715   0.2492   1.0000
  10.750   1.5551   0.01631   0.01100  -0.0702   0.2463   1.0000
  11.000   1.5696   0.01696   0.01166  -0.0687   0.2432   1.0000
  11.250   1.5902   0.01732   0.01207  -0.0680   0.2416   1.0000
  11.500   1.6096   0.01775   0.01254  -0.0672   0.2393   1.0000
  11.750   1.6273   0.01827   0.01309  -0.0663   0.2366   1.0000
  12.000   1.6435   0.01889   0.01373  -0.0653   0.2337   1.0000
  12.250   1.6565   0.01973   0.01455  -0.0640   0.2298   1.0000
  12.500   1.6732   0.02036   0.01523  -0.0631   0.2263   1.0000
  12.750   1.6907   0.02095   0.01585  -0.0623   0.2222   1.0000
  13.000   1.7044   0.02180   0.01671  -0.0613   0.2181   1.0000
  13.250   1.7143   0.02292   0.01782  -0.0600   0.2136   1.0000
  13.500   1.7306   0.02365   0.01860  -0.0593   0.2107   1.0000
  13.750   1.7448   0.02453   0.01952  -0.0584   0.2069   1.0000
  14.000   1.7539   0.02579   0.02077  -0.0573   0.2015   1.0000
  14.250   1.7639   0.02702   0.02204  -0.0563   0.1979   1.0000
  14.500   1.7767   0.02807   0.02313  -0.0556   0.1939   1.0000
  14.750   1.7850   0.02950   0.02457  -0.0546   0.1889   1.0000
  15.000   1.7905   0.03117   0.02625  -0.0536   0.1836   1.0000
  15.250   1.7996   0.03258   0.02770  -0.0528   0.1792   1.0000
  15.500   1.8010   0.03467   0.02978  -0.0518   0.1726   1.0000
  15.750   1.8070   0.03640   0.03154  -0.0510   0.1675   1.0000
  16.000   1.8081   0.03858   0.03374  -0.0501   0.1616   1.0000
  16.250   1.8081   0.04092   0.03610  -0.0493   0.1561   1.0000
  16.500   1.8097   0.04315   0.03836  -0.0486   0.1511   1.0000
  16.750   1.8041   0.04612   0.04133  -0.0478   0.1448   1.0000
  17.000   1.8037   0.04861   0.04386  -0.0473   0.1399   1.0000
  17.250   1.7952   0.05200   0.04727  -0.0467   0.1343   1.0000
  17.500   1.7903   0.05512   0.05042  -0.0463   0.1290   1.0000
  17.750   1.7810   0.05872   0.05405  -0.0460   0.1242   1.0000
  18.000   1.7734   0.06222   0.05761  -0.0458   0.1207   1.0000
  18.250   1.7682   0.06552   0.06095  -0.0457   0.1170   1.0000
  18.500   1.7558   0.06968   0.06515  -0.0457   0.1130   1.0000
  18.750   1.7451   0.07370   0.06924  -0.0458   0.1099   1.0000
  19.000   1.7365   0.07755   0.07315  -0.0461   0.1068   1.0000
  19.250   1.7224   0.08211   0.07777  -0.0465   0.1034   1.0000
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