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GOE 692 AIRFOIL (goe692-il) Xfoil prediction polar at RE=1,000,000 Ncrit=9


Details Polar file
Airfoil: GOE 692 AIRFOIL (goe692-il)
Reynolds number: 1,000,000
Max Cl/Cd: 132.64 at α=4.75°
Description: Mach=0 Ncrit=9
Source: Xfoil prediction
Download polar: xf-goe692-il-1000000.txt
Download as CSV file: xf-goe692-il-1000000.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 692 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
  ------ -------- --------- --------- -------- -------- --------
 -16.750  -0.7741   0.08220   0.07956  -0.0884   1.0000   0.0276
 -16.500  -0.8283   0.07153   0.06874  -0.0944   1.0000   0.0276
 -16.250  -0.8778   0.06201   0.05908  -0.0995   1.0000   0.0276
 -16.000  -0.9252   0.05300   0.04993  -0.1040   1.0000   0.0275
 -15.750  -0.9676   0.04489   0.04166  -0.1080   1.0000   0.0275
 -15.500  -0.9745   0.03791   0.03449  -0.1167   0.9981   0.0276
 -15.250  -0.9641   0.03352   0.02993  -0.1238   0.9952   0.0279
 -15.000  -0.9480   0.03069   0.02696  -0.1284   0.9930   0.0281
 -14.750  -0.9336   0.02862   0.02477  -0.1306   0.9880   0.0284
 -14.500  -0.9134   0.02691   0.02295  -0.1327   0.9844   0.0286
 -14.250  -0.8958   0.02558   0.02150  -0.1332   0.9784   0.0288
 -14.000  -0.8778   0.02447   0.02029  -0.1332   0.9711   0.0290
 -13.750  -0.8607   0.02355   0.01927  -0.1326   0.9617   0.0292
 -13.500  -0.8415   0.02273   0.01835  -0.1322   0.9530   0.0293
 -13.250  -0.8298   0.02139   0.01687  -0.1308   0.9413   0.0296
 -13.000  -0.8156   0.02029   0.01567  -0.1295   0.9296   0.0300
 -12.750  -0.7972   0.01950   0.01480  -0.1286   0.9196   0.0304
 -12.500  -0.7766   0.01889   0.01410  -0.1279   0.9101   0.0307
 -12.250  -0.7549   0.01834   0.01349  -0.1273   0.9014   0.0311
 -12.000  -0.7326   0.01782   0.01288  -0.1267   0.8934   0.0315
 -11.750  -0.7097   0.01730   0.01229  -0.1262   0.8865   0.0319
 -11.500  -0.6863   0.01681   0.01171  -0.1257   0.8798   0.0322
 -11.250  -0.6625   0.01636   0.01115  -0.1253   0.8738   0.0326
 -11.000  -0.6380   0.01591   0.01064  -0.1249   0.8682   0.0330
 -10.750  -0.6131   0.01552   0.01016  -0.1246   0.8625   0.0333
 -10.500  -0.5878   0.01518   0.00973  -0.1243   0.8570   0.0335
 -10.250  -0.5653   0.01444   0.00893  -0.1237   0.8521   0.0342
 -10.000  -0.5406   0.01396   0.00842  -0.1234   0.8471   0.0348
  -9.750  -0.5148   0.01360   0.00800  -0.1232   0.8424   0.0355
  -9.500  -0.4884   0.01330   0.00764  -0.1230   0.8380   0.0361
  -9.250  -0.4617   0.01299   0.00730  -0.1229   0.8338   0.0369
  -9.000  -0.4349   0.01270   0.00696  -0.1228   0.8291   0.0375
  -8.750  -0.4079   0.01246   0.00664  -0.1226   0.8244   0.0380
  -8.500  -0.3821   0.01203   0.00617  -0.1224   0.8199   0.0392
  -8.250  -0.3551   0.01171   0.00584  -0.1223   0.8156   0.0403
  -8.000  -0.3277   0.01146   0.00556  -0.1223   0.8112   0.0414
  -7.750  -0.3002   0.01126   0.00530  -0.1222   0.8067   0.0426
  -7.500  -0.2729   0.01099   0.00500  -0.1221   0.8022   0.0443
  -7.250  -0.2453   0.01073   0.00475  -0.1221   0.7977   0.0463
  -7.000  -0.2173   0.01056   0.00454  -0.1221   0.7927   0.0485
  -6.750  -0.1899   0.01033   0.00431  -0.1220   0.7877   0.0519
  -6.500  -0.1616   0.01018   0.00414  -0.1221   0.7832   0.0551
  -6.250  -0.1336   0.00997   0.00397  -0.1221   0.7780   0.0591
  -6.000  -0.1054   0.00984   0.00381  -0.1221   0.7725   0.0626
  -5.750  -0.0774   0.00971   0.00366  -0.1222   0.7670   0.0663
  -5.500  -0.0486   0.00962   0.00356  -0.1223   0.7614   0.0690
  -5.250  -0.0208   0.00943   0.00337  -0.1223   0.7552   0.0727
  -5.000   0.0073   0.00934   0.00325  -0.1223   0.7489   0.0758
  -4.750   0.0359   0.00924   0.00313  -0.1224   0.7421   0.0782
  -4.500   0.0635   0.00909   0.00296  -0.1223   0.7346   0.0823
  -4.250   0.0918   0.00899   0.00285  -0.1223   0.7273   0.0854
  -4.000   0.1199   0.00891   0.00272  -0.1223   0.7193   0.0883
  -3.750   0.1478   0.00878   0.00260  -0.1223   0.7119   0.0930
  -3.500   0.1759   0.00870   0.00250  -0.1223   0.7038   0.0970
  -3.250   0.2036   0.00861   0.00241  -0.1223   0.6964   0.1039
  -3.000   0.2318   0.00852   0.00233  -0.1223   0.6888   0.1122
  -2.500   0.2878   0.00839   0.00224  -0.1224   0.6750   0.1373
  -2.250   0.3157   0.00835   0.00222  -0.1224   0.6682   0.1491
  -2.000   0.3437   0.00832   0.00219  -0.1224   0.6622   0.1585
  -1.750   0.3723   0.00830   0.00217  -0.1225   0.6564   0.1660
  -1.500   0.4002   0.00828   0.00215  -0.1225   0.6505   0.1748
  -1.250   0.4283   0.00828   0.00214  -0.1225   0.6452   0.1825
  -1.000   0.4569   0.00824   0.00212  -0.1227   0.6403   0.1910
  -0.750   0.4850   0.00823   0.00212  -0.1227   0.6351   0.1998
  -0.500   0.5125   0.00825   0.00213  -0.1227   0.6296   0.2109
  -0.250   0.5412   0.00820   0.00213  -0.1228   0.6255   0.2238
   0.000   0.5695   0.00817   0.00214  -0.1229   0.6208   0.2406
   0.250   0.5970   0.00813   0.00216  -0.1229   0.6158   0.2646
   0.500   0.6244   0.00809   0.00219  -0.1229   0.6109   0.2999
   0.750   0.6522   0.00791   0.00222  -0.1230   0.6068   0.3670
   1.000   0.6785   0.00763   0.00227  -0.1229   0.6014   0.4846
   1.250   0.7029   0.00734   0.00236  -0.1224   0.5948   0.6360
   1.500   0.7273   0.00700   0.00245  -0.1217   0.5888   0.7777
   1.750   0.7486   0.00684   0.00257  -0.1200   0.5814   0.8842
   2.000   0.7716   0.00687   0.00267  -0.1187   0.5746   0.9411
   2.250   0.8021   0.00693   0.00274  -0.1191   0.5678   0.9682
   2.500   0.8370   0.00706   0.00282  -0.1207   0.5610   0.9835
   2.750   0.8752   0.00716   0.00290  -0.1230   0.5545   0.9933
   3.000   0.9154   0.00729   0.00298  -0.1258   0.5459   0.9972
   3.250   0.9495   0.00741   0.00306  -0.1273   0.5379   1.0000
   3.500   0.9712   0.00750   0.00311  -0.1261   0.5297   1.0000
   3.750   0.9930   0.00761   0.00318  -0.1249   0.5222   1.0000
   4.000   1.0154   0.00771   0.00325  -0.1238   0.5136   1.0000
   4.250   1.0375   0.00785   0.00334  -0.1227   0.5043   1.0000
   4.500   1.0593   0.00801   0.00345  -0.1215   0.4929   1.0000
   4.750   1.0823   0.00816   0.00357  -0.1206   0.4818   1.0000
   5.000   1.1044   0.00836   0.00370  -0.1195   0.4706   1.0000
   5.250   1.1263   0.00857   0.00386  -0.1184   0.4593   1.0000
   5.500   1.1491   0.00875   0.00401  -0.1175   0.4491   1.0000
   5.750   1.1704   0.00899   0.00419  -0.1163   0.4385   1.0000
   6.000   1.1919   0.00921   0.00438  -0.1152   0.4276   1.0000
   6.250   1.2122   0.00944   0.00456  -0.1138   0.4175   1.0000
   6.500   1.2303   0.00973   0.00480  -0.1120   0.4067   1.0000
   6.750   1.2506   0.00997   0.00502  -0.1107   0.3959   1.0000
   7.000   1.2699   0.01027   0.00527  -0.1092   0.3845   1.0000
   7.250   1.2880   0.01063   0.00557  -0.1076   0.3718   1.0000
   7.500   1.3064   0.01099   0.00588  -0.1060   0.3584   1.0000
   7.750   1.3249   0.01136   0.00621  -0.1045   0.3450   1.0000
   8.000   1.3424   0.01178   0.00658  -0.1029   0.3311   1.0000
   8.250   1.3590   0.01226   0.00699  -0.1012   0.3162   1.0000
   8.500   1.3746   0.01280   0.00746  -0.0993   0.3011   1.0000
   8.750   1.3896   0.01338   0.00797  -0.0975   0.2861   1.0000
   9.000   1.4041   0.01400   0.00852  -0.0956   0.2719   1.0000
   9.250   1.4178   0.01468   0.00914  -0.0936   0.2586   1.0000
   9.500   1.4331   0.01530   0.00973  -0.0920   0.2469   1.0000
   9.750   1.4473   0.01600   0.01039  -0.0903   0.2356   1.0000
  10.000   1.4602   0.01679   0.01112  -0.0884   0.2241   1.0000
  10.250   1.4724   0.01764   0.01193  -0.0866   0.2127   1.0000
  10.500   1.4868   0.01840   0.01267  -0.0851   0.2033   1.0000
  10.750   1.4992   0.01929   0.01353  -0.0834   0.1939   1.0000
  11.000   1.5109   0.02025   0.01444  -0.0817   0.1838   1.0000
  11.250   1.5230   0.02120   0.01538  -0.0801   0.1741   1.0000
  11.500   1.5330   0.02232   0.01645  -0.0784   0.1643   1.0000
  11.750   1.5428   0.02347   0.01757  -0.0767   0.1554   1.0000
  12.000   1.5536   0.02457   0.01866  -0.0752   0.1487   1.0000
  12.250   1.5629   0.02580   0.01987  -0.0736   0.1424   1.0000
  12.500   1.5738   0.02696   0.02105  -0.0722   0.1379   1.0000
  12.750   1.5854   0.02810   0.02220  -0.0710   0.1343   1.0000
  13.000   1.5948   0.02940   0.02351  -0.0696   0.1306   1.0000
  13.250   1.6024   0.03088   0.02499  -0.0681   0.1266   1.0000
  13.500   1.6156   0.03195   0.02612  -0.0672   0.1247   1.0000
  13.750   1.6261   0.03326   0.02746  -0.0661   0.1222   1.0000
  14.000   1.6352   0.03469   0.02891  -0.0650   0.1193   1.0000
  14.250   1.6417   0.03639   0.03063  -0.0637   0.1161   1.0000
  14.500   1.6506   0.03790   0.03218  -0.0627   0.1137   1.0000
  14.750   1.6618   0.03924   0.03357  -0.0619   0.1119   1.0000
  15.000   1.6712   0.04076   0.03514  -0.0611   0.1096   1.0000
  15.250   1.6783   0.04251   0.03691  -0.0601   0.1070   1.0000
  15.500   1.6828   0.04454   0.03897  -0.0591   0.1040   1.0000
  15.750   1.6916   0.04617   0.04065  -0.0584   0.1018   1.0000
  16.000   1.7003   0.04785   0.04238  -0.0577   0.0991   1.0000
  16.250   1.7055   0.04986   0.04441  -0.0569   0.0951   1.0000
  16.500   1.7091   0.05206   0.04663  -0.0561   0.0911   1.0000
  16.750   1.7126   0.05431   0.04890  -0.0554   0.0845   1.0000
  17.000   1.7081   0.05739   0.05191  -0.0545   0.0736   1.0000
  17.250   1.6959   0.06130   0.05576  -0.0534   0.0612   1.0000
  17.500   1.6825   0.06547   0.05989  -0.0525   0.0523   1.0000
  17.750   1.6704   0.06961   0.06403  -0.0517   0.0450   1.0000
  18.000   1.6590   0.07373   0.06816  -0.0512   0.0382   1.0000
  18.250   1.6466   0.07808   0.07252  -0.0509   0.0317   1.0000
  18.500   1.6352   0.08241   0.07688  -0.0507   0.0269   1.0000
  18.750   1.6263   0.08652   0.08103  -0.0507   0.0239   1.0000
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