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GOE 692 AIRFOIL (goe692-il) Xfoil prediction polar at RE=200,000 Ncrit=5


Details Polar file
Airfoil: GOE 692 AIRFOIL (goe692-il)
Reynolds number: 200,000
Max Cl/Cd: 73.64 at α=5.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe692-il-200000-n5.txt
Download as CSV file: xf-goe692-il-200000-n5.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 =     0.200 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -12.250  -0.6142   0.04197   0.03685  -0.1278   0.9587   0.0408
 -12.000  -0.6234   0.03840   0.03298  -0.1288   0.9461   0.0411
 -11.750  -0.6203   0.03566   0.02993  -0.1291   0.9374   0.0415
 -11.500  -0.6112   0.03335   0.02731  -0.1292   0.9298   0.0420
 -11.250  -0.5985   0.03137   0.02502  -0.1291   0.9231   0.0426
 -11.000  -0.5825   0.02992   0.02340  -0.1286   0.9160   0.0431
 -10.750  -0.5592   0.02887   0.02228  -0.1290   0.9115   0.0437
 -10.500  -0.5398   0.02802   0.02137  -0.1285   0.9046   0.0443
 -10.250  -0.5185   0.02712   0.02035  -0.1282   0.8988   0.0451
 -10.000  -0.4947   0.02612   0.01919  -0.1284   0.8944   0.0460
  -9.750  -0.4750   0.02519   0.01809  -0.1276   0.8878   0.0470
  -9.500  -0.4533   0.02421   0.01691  -0.1271   0.8819   0.0479
  -9.250  -0.4285   0.02334   0.01591  -0.1271   0.8773   0.0488
  -9.000  -0.4061   0.02274   0.01527  -0.1266   0.8713   0.0497
  -8.750  -0.3826   0.02215   0.01461  -0.1262   0.8656   0.0508
  -8.500  -0.3571   0.02151   0.01385  -0.1261   0.8610   0.0521
  -8.250  -0.3324   0.02089   0.01308  -0.1257   0.8559   0.0538
  -8.000  -0.3089   0.02037   0.01251  -0.1252   0.8496   0.0554
  -7.750  -0.2830   0.01993   0.01202  -0.1251   0.8444   0.0572
  -7.500  -0.2561   0.01946   0.01143  -0.1250   0.8400   0.0595
  -7.250  -0.2323   0.01901   0.01089  -0.1244   0.8338   0.0617
  -7.000  -0.2067   0.01861   0.01047  -0.1242   0.8285   0.0639
  -6.750  -0.1794   0.01821   0.00997  -0.1242   0.8239   0.0668
  -6.500  -0.1541   0.01784   0.00953  -0.1238   0.8181   0.0699
  -6.250  -0.1286   0.01752   0.00919  -0.1234   0.8120   0.0731
  -6.000  -0.1011   0.01721   0.00876  -0.1234   0.8070   0.0770
  -5.750  -0.0747   0.01687   0.00841  -0.1232   0.8021   0.0804
  -5.500  -0.0492   0.01661   0.00812  -0.1229   0.7958   0.0842
  -5.250  -0.0220   0.01633   0.00776  -0.1227   0.7902   0.0882
  -5.000   0.0054   0.01605   0.00747  -0.1227   0.7853   0.0925
  -4.750   0.0311   0.01586   0.00724  -0.1223   0.7786   0.0973
  -4.500   0.0580   0.01562   0.00702  -0.1222   0.7730   0.1025
  -4.250   0.0863   0.01544   0.00676  -0.1222   0.7681   0.1087
  -4.000   0.1118   0.01526   0.00663  -0.1218   0.7611   0.1146
  -3.750   0.1392   0.01510   0.00642  -0.1217   0.7552   0.1217
  -3.500   0.1670   0.01491   0.00623  -0.1217   0.7501   0.1286
  -3.250   0.1931   0.01479   0.00609  -0.1213   0.7430   0.1366
  -3.000   0.2204   0.01462   0.00594  -0.1212   0.7371   0.1450
  -2.750   0.2480   0.01450   0.00577  -0.1211   0.7313   0.1542
  -2.500   0.2743   0.01438   0.00568  -0.1208   0.7243   0.1636
  -2.250   0.3021   0.01426   0.00552  -0.1208   0.7186   0.1733
  -2.000   0.3289   0.01417   0.00544  -0.1206   0.7122   0.1834
  -1.750   0.3557   0.01407   0.00534  -0.1203   0.7057   0.1928
  -1.500   0.3838   0.01399   0.00521  -0.1203   0.7004   0.2036
  -1.250   0.4100   0.01391   0.00518  -0.1201   0.6940   0.2148
  -1.000   0.4371   0.01383   0.00511  -0.1199   0.6880   0.2270
  -0.750   0.4651   0.01376   0.00502  -0.1199   0.6830   0.2414
  -0.500   0.4911   0.01369   0.00503  -0.1196   0.6767   0.2588
  -0.250   0.5178   0.01359   0.00501  -0.1195   0.6709   0.2840
   0.000   0.5451   0.01344   0.00496  -0.1194   0.6660   0.3254
   0.500   0.5935   0.01287   0.00510  -0.1183   0.6544   0.5209
   0.750   0.6161   0.01249   0.00518  -0.1171   0.6495   0.6704
   1.000   0.6372   0.01227   0.00538  -0.1150   0.6440   0.8109
   1.250   0.6718   0.01229   0.00553  -0.1159   0.6381   0.9114
   1.500   0.7132   0.01239   0.00556  -0.1186   0.6328   0.9590
   1.750   0.7531   0.01252   0.00564  -0.1212   0.6271   0.9855
   2.000   0.7913   0.01265   0.00572  -0.1236   0.6209   1.0000
   2.250   0.8148   0.01277   0.00575  -0.1227   0.6155   1.0000
   2.500   0.8375   0.01291   0.00584  -0.1218   0.6097   1.0000
   2.750   0.8597   0.01305   0.00595  -0.1207   0.6033   1.0000
   3.000   0.8838   0.01319   0.00601  -0.1200   0.5973   1.0000
   3.250   0.9056   0.01333   0.00614  -0.1188   0.5893   1.0000
   3.500   0.9280   0.01348   0.00621  -0.1178   0.5805   1.0000
   3.750   0.9497   0.01363   0.00634  -0.1166   0.5716   1.0000
   4.000   0.9723   0.01379   0.00645  -0.1156   0.5635   1.0000
   4.250   0.9949   0.01396   0.00660  -0.1146   0.5561   1.0000
   4.500   1.0167   0.01414   0.00676  -0.1135   0.5476   1.0000
   4.750   1.0384   0.01433   0.00692  -0.1124   0.5389   1.0000
   5.000   1.0590   0.01452   0.00708  -0.1111   0.5288   1.0000
   5.250   1.0794   0.01473   0.00728  -0.1097   0.5188   1.0000
   5.500   1.0996   0.01496   0.00744  -0.1083   0.5091   1.0000
   5.750   1.1186   0.01519   0.00768  -0.1068   0.4981   1.0000
   6.000   1.1372   0.01546   0.00792  -0.1051   0.4874   1.0000
   6.250   1.1537   0.01575   0.00815  -0.1031   0.4761   1.0000
   6.500   1.1691   0.01606   0.00844  -0.1009   0.4643   1.0000
   6.750   1.1842   0.01642   0.00876  -0.0987   0.4527   1.0000
   7.000   1.1990   0.01683   0.00912  -0.0965   0.4417   1.0000
   7.250   1.2149   0.01724   0.00953  -0.0945   0.4303   1.0000
   7.500   1.2299   0.01771   0.00996  -0.0925   0.4191   1.0000
   7.750   1.2435   0.01825   0.01045  -0.0904   0.4076   1.0000
   8.000   1.2581   0.01878   0.01099  -0.0885   0.3955   1.0000
   8.250   1.2719   0.01938   0.01156  -0.0865   0.3838   1.0000
   8.500   1.2844   0.02005   0.01221  -0.0844   0.3721   1.0000
   8.750   1.2971   0.02075   0.01290  -0.0824   0.3597   1.0000
   9.000   1.3094   0.02151   0.01365  -0.0805   0.3472   1.0000
   9.250   1.3204   0.02235   0.01447  -0.0784   0.3348   1.0000
   9.500   1.3301   0.02330   0.01539  -0.0763   0.3222   1.0000
   9.750   1.3395   0.02432   0.01639  -0.0743   0.3094   1.0000
  10.000   1.3492   0.02536   0.01742  -0.0724   0.2969   1.0000
  10.250   1.3578   0.02651   0.01855  -0.0705   0.2852   1.0000
  10.500   1.3648   0.02780   0.01981  -0.0685   0.2743   1.0000
  10.750   1.3734   0.02904   0.02105  -0.0668   0.2635   1.0000
  11.000   1.3812   0.03036   0.02238  -0.0651   0.2540   1.0000
  11.250   1.3875   0.03181   0.02382  -0.0633   0.2448   1.0000
  11.500   1.3958   0.03318   0.02520  -0.0618   0.2365   1.0000
  11.750   1.4015   0.03476   0.02678  -0.0602   0.2284   1.0000
  12.000   1.4095   0.03622   0.02828  -0.0588   0.2208   1.0000
  12.250   1.4149   0.03791   0.02997  -0.0574   0.2133   1.0000
  12.500   1.4222   0.03950   0.03160  -0.0561   0.2067   1.0000
  12.750   1.4290   0.04117   0.03330  -0.0549   0.2002   1.0000
  13.000   1.4335   0.04305   0.03519  -0.0536   0.1948   1.0000
  13.250   1.4427   0.04459   0.03681  -0.0527   0.1894   1.0000
  13.500   1.4488   0.04641   0.03867  -0.0516   0.1842   1.0000
  13.750   1.4532   0.04842   0.04068  -0.0506   0.1798   1.0000
  14.000   1.4617   0.05010   0.04246  -0.0498   0.1749   1.0000
  14.250   1.4671   0.05209   0.04449  -0.0490   0.1701   1.0000
  14.500   1.4700   0.05435   0.04674  -0.0481   0.1657   1.0000
  14.750   1.4772   0.05625   0.04874  -0.0475   0.1606   1.0000
  15.000   1.4806   0.05855   0.05107  -0.0469   0.1555   1.0000
  15.250   1.4828   0.06101   0.05354  -0.0463   0.1511   1.0000
  15.500   1.4888   0.06312   0.05575  -0.0459   0.1466   1.0000
  15.750   1.4918   0.06555   0.05823  -0.0454   0.1425   1.0000
  16.000   1.4928   0.06821   0.06091  -0.0450   0.1391   1.0000
  16.250   1.4983   0.07041   0.06321  -0.0447   0.1358   1.0000
  16.500   1.5021   0.07285   0.06574  -0.0444   0.1322   1.0000
  16.750   1.5036   0.07557   0.06852  -0.0443   0.1286   1.0000
  17.250   1.5068   0.08107   0.07417  -0.0441   0.1218   1.0000
  17.500   1.5082   0.08390   0.07710  -0.0442   0.1182   1.0000
  17.750   1.5073   0.08703   0.08028  -0.0443   0.1149   1.0000
  18.000   1.5064   0.09017   0.08347  -0.0445   0.1121   1.0000
  18.250   1.5091   0.09295   0.08641  -0.0448   0.1088   1.0000
  18.500   1.5090   0.09611   0.08968  -0.0452   0.1053   1.0000
  18.750   1.5058   0.09971   0.09334  -0.0457   0.1019   1.0000
  19.000   1.5053   0.10297   0.09672  -0.0463   0.0984   1.0000
  19.250   1.5042   0.10636   0.10024  -0.0471   0.0938   1.0000
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