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GOE 701 AIRFOIL (goe701-il) Xfoil prediction polar at RE=500,000 Ncrit=5


Details Polar file
Airfoil: GOE 701 AIRFOIL (goe701-il)
Reynolds number: 500,000
Max Cl/Cd: 94.46 at α=3.75°
Description: Mach=0 Ncrit=5
Source: Xfoil prediction
Download polar: xf-goe701-il-500000-n5.txt
Download as CSV file: xf-goe701-il-500000-n5.csv

  
       XFOIL         Version 6.96
  
 Calculated polar for: GOE 701 AIRFOIL                                 
  
 1 1 Reynolds number fixed          Mach number fixed         
  
 xtrf =   1.000 (top)        1.000 (bottom)  
 Mach =   0.000     Re =     0.500 e 6     Ncrit =   5.000
  
   alpha    CL        CD       CDp       CM     Top_Xtr  Bot_Xtr
  ------ -------- --------- --------- -------- -------- --------
 -14.000  -0.9261   0.03156   0.02795  -0.1145   0.9832   0.0251
 -13.750  -0.9158   0.02914   0.02536  -0.1149   0.9778   0.0260
 -13.500  -0.8958   0.02733   0.02336  -0.1161   0.9747   0.0272
 -13.250  -0.8722   0.02576   0.02161  -0.1174   0.9725   0.0283
 -13.000  -0.8469   0.02462   0.02039  -0.1184   0.9704   0.0293
 -12.750  -0.8273   0.02376   0.01944  -0.1178   0.9655   0.0304
 -12.500  -0.8018   0.02283   0.01838  -0.1184   0.9627   0.0315
 -12.250  -0.7734   0.02192   0.01729  -0.1195   0.9605   0.0325
 -12.000  -0.7438   0.02107   0.01636  -0.1207   0.9587   0.0335
 -11.750  -0.7196   0.02050   0.01574  -0.1206   0.9546   0.0344
 -11.500  -0.6951   0.01995   0.01511  -0.1204   0.9499   0.0354
 -11.250  -0.6666   0.01936   0.01441  -0.1210   0.9465   0.0365
 -11.000  -0.6359   0.01876   0.01367  -0.1220   0.9439   0.0375
 -10.750  -0.6134   0.01821   0.01301  -0.1213   0.9380   0.0383
 -10.500  -0.5888   0.01763   0.01239  -0.1210   0.9324   0.0392
 -10.250  -0.5591   0.01714   0.01184  -0.1217   0.9284   0.0401
 -10.000  -0.5347   0.01679   0.01142  -0.1211   0.9219   0.0412
  -9.750  -0.5082   0.01638   0.01093  -0.1210   0.9155   0.0422
  -9.500  -0.4792   0.01600   0.01043  -0.1213   0.9103   0.0434
  -9.250  -0.4548   0.01567   0.00998  -0.1207   0.9021   0.0442
  -9.000  -0.4284   0.01504   0.00928  -0.1206   0.8954   0.0452
  -8.750  -0.4045   0.01461   0.00879  -0.1199   0.8865   0.0460
  -8.500  -0.3773   0.01421   0.00831  -0.1199   0.8790   0.0468
  -8.250  -0.3521   0.01389   0.00791  -0.1193   0.8700   0.0478
  -8.000  -0.3255   0.01356   0.00748  -0.1191   0.8619   0.0488
  -7.750  -0.2999   0.01325   0.00708  -0.1185   0.8528   0.0497
  -7.500  -0.2739   0.01296   0.00667  -0.1181   0.8446   0.0504
  -7.250  -0.2482   0.01270   0.00631  -0.1176   0.8359   0.0511
  -7.000  -0.2230   0.01237   0.00591  -0.1170   0.8280   0.0521
  -6.750  -0.1981   0.01206   0.00554  -0.1164   0.8197   0.0533
  -6.500  -0.1724   0.01182   0.00524  -0.1159   0.8124   0.0546
  -6.250  -0.1468   0.01161   0.00497  -0.1153   0.8047   0.0560
  -6.000  -0.1208   0.01142   0.00470  -0.1148   0.7979   0.0573
  -5.750  -0.0951   0.01123   0.00445  -0.1142   0.7906   0.0586
  -5.500  -0.0691   0.01107   0.00421  -0.1137   0.7839   0.0596
  -5.250  -0.0435   0.01085   0.00397  -0.1132   0.7774   0.0617
  -5.000  -0.0177   0.01068   0.00378  -0.1126   0.7706   0.0640
  -4.750   0.0085   0.01054   0.00359  -0.1121   0.7645   0.0666
  -4.500   0.0345   0.01040   0.00343  -0.1116   0.7579   0.0693
  -4.250   0.0605   0.01027   0.00330  -0.1111   0.7515   0.0733
  -4.000   0.0868   0.01018   0.00317  -0.1107   0.7455   0.0776
  -3.750   0.1130   0.01007   0.00308  -0.1102   0.7389   0.0824
  -3.500   0.1393   0.01002   0.00299  -0.1097   0.7329   0.0877
  -3.250   0.1657   0.00994   0.00290  -0.1093   0.7269   0.0922
  -3.000   0.1919   0.00988   0.00283  -0.1088   0.7203   0.0970
  -2.750   0.2183   0.00985   0.00275  -0.1083   0.7142   0.1009
  -2.500   0.2447   0.00981   0.00268  -0.1078   0.7077   0.1033
  -2.250   0.2704   0.00972   0.00259  -0.1073   0.7011   0.1073
  -2.000   0.2965   0.00967   0.00253  -0.1068   0.6949   0.1111
  -1.750   0.3223   0.00963   0.00247  -0.1062   0.6870   0.1146
  -1.500   0.3480   0.00962   0.00241  -0.1056   0.6791   0.1173
  -1.250   0.3732   0.00958   0.00235  -0.1049   0.6693   0.1200
  -1.000   0.3984   0.00954   0.00230  -0.1042   0.6607   0.1240
  -0.750   0.4232   0.00952   0.00226  -0.1034   0.6505   0.1285
  -0.500   0.4480   0.00952   0.00223  -0.1027   0.6391   0.1332
  -0.250   0.4722   0.00952   0.00221  -0.1018   0.6273   0.1388
   0.000   0.4960   0.00953   0.00220  -0.1008   0.6146   0.1453
   0.250   0.5202   0.00955   0.00220  -0.0999   0.6021   0.1530
   0.500   0.5446   0.00956   0.00222  -0.0991   0.5913   0.1627
   0.750   0.5685   0.00959   0.00224  -0.0982   0.5805   0.1740
   1.000   0.5924   0.00963   0.00227  -0.0973   0.5689   0.1849
   1.250   0.6164   0.00967   0.00231  -0.0964   0.5579   0.1962
   1.500   0.6398   0.00971   0.00236  -0.0954   0.5475   0.2075
   1.750   0.6633   0.00977   0.00241  -0.0944   0.5363   0.2192
   2.250   0.7090   0.00988   0.00254  -0.0923   0.5133   0.2517
   2.500   0.7303   0.00993   0.00264  -0.0909   0.5002   0.2834
   2.750   0.7509   0.00992   0.00275  -0.0895   0.4860   0.3482
   3.000   0.7704   0.00985   0.00287  -0.0878   0.4725   0.4379
   3.500   0.8944   0.00949   0.00363  -0.1031   0.4303   0.9958
   3.750   0.9257   0.00980   0.00382  -0.1041   0.4083   1.0000
   4.000   0.9413   0.01007   0.00399  -0.1016   0.3895   1.0000
   4.250   0.9566   0.01035   0.00417  -0.0990   0.3712   1.0000
   4.500   0.9718   0.01063   0.00436  -0.0965   0.3536   1.0000
   4.750   0.9866   0.01092   0.00456  -0.0939   0.3359   1.0000
   5.000   1.0001   0.01123   0.00478  -0.0910   0.3182   1.0000
   5.250   1.0117   0.01155   0.00501  -0.0878   0.3011   1.0000
   5.500   1.0238   0.01187   0.00524  -0.0847   0.2856   1.0000
   5.750   1.0368   0.01220   0.00550  -0.0818   0.2722   1.0000
   6.000   1.0510   0.01252   0.00576  -0.0793   0.2603   1.0000
   6.250   1.0665   0.01282   0.00603  -0.0770   0.2510   1.0000
   6.500   1.0812   0.01319   0.00634  -0.0746   0.2415   1.0000
   6.750   1.0977   0.01350   0.00662  -0.0725   0.2330   1.0000
   7.000   1.1133   0.01387   0.00696  -0.0704   0.2262   1.0000
   7.250   1.1309   0.01417   0.00726  -0.0687   0.2206   1.0000
   7.500   1.1477   0.01452   0.00760  -0.0668   0.2147   1.0000
   7.750   1.1635   0.01493   0.00798  -0.0649   0.2089   1.0000
   8.000   1.1814   0.01526   0.00833  -0.0633   0.2036   1.0000
   8.250   1.1981   0.01565   0.00871  -0.0616   0.1985   1.0000
   8.500   1.2137   0.01610   0.00916  -0.0597   0.1939   1.0000
   8.750   1.2319   0.01645   0.00954  -0.0583   0.1898   1.0000
   9.000   1.2487   0.01688   0.00998  -0.0567   0.1845   1.0000
   9.250   1.2636   0.01741   0.01050  -0.0549   0.1790   1.0000
   9.500   1.2809   0.01784   0.01096  -0.0535   0.1736   1.0000
   9.750   1.2963   0.01838   0.01149  -0.0519   0.1672   1.0000
  10.000   1.3115   0.01895   0.01207  -0.0503   0.1613   1.0000
  10.250   1.3253   0.01961   0.01270  -0.0486   0.1520   1.0000
  10.500   1.3392   0.02029   0.01338  -0.0470   0.1434   1.0000
  10.750   1.3512   0.02110   0.01415  -0.0452   0.1335   1.0000
  11.000   1.3619   0.02202   0.01503  -0.0434   0.1230   1.0000
  11.250   1.3717   0.02303   0.01600  -0.0416   0.1120   1.0000
  11.500   1.3803   0.02415   0.01707  -0.0397   0.1008   1.0000
  11.750   1.3898   0.02524   0.01815  -0.0381   0.0925   1.0000
  12.000   1.3966   0.02656   0.01944  -0.0363   0.0822   1.0000
  12.250   1.4025   0.02798   0.02083  -0.0345   0.0712   1.0000
  12.500   1.3925   0.03067   0.02329  -0.0316   0.0393   1.0000
  12.750   1.3941   0.03257   0.02520  -0.0299   0.0327   1.0000
  13.000   1.4001   0.03417   0.02684  -0.0285   0.0299   1.0000
  13.250   1.4062   0.03581   0.02853  -0.0273   0.0281   1.0000
  13.500   1.4107   0.03764   0.03042  -0.0261   0.0263   1.0000
  13.750   1.4185   0.03921   0.03207  -0.0252   0.0253   1.0000
  14.000   1.4242   0.04100   0.03394  -0.0242   0.0240   1.0000
  14.250   1.4286   0.04297   0.03598  -0.0233   0.0230   1.0000
  14.500   1.4314   0.04515   0.03823  -0.0225   0.0221   1.0000
  14.750   1.4356   0.04725   0.04040  -0.0219   0.0212   1.0000
  15.000   1.4400   0.04936   0.04260  -0.0213   0.0203   1.0000
  15.250   1.4426   0.05172   0.04505  -0.0208   0.0198   1.0000
  15.500   1.4439   0.05428   0.04769  -0.0204   0.0190   1.0000
  15.750   1.4438   0.05707   0.05055  -0.0202   0.0184   1.0000
  16.000   1.4410   0.06024   0.05380  -0.0200   0.0178   1.0000
  16.250   1.4415   0.06308   0.05674  -0.0200   0.0174   1.0000
  16.500   1.4400   0.06623   0.05999  -0.0201   0.0169   1.0000
  16.750   1.4380   0.06952   0.06337  -0.0203   0.0164   1.0000
  17.000   1.4341   0.07310   0.06705  -0.0207   0.0159   1.0000
  17.250   1.4292   0.07687   0.07091  -0.0212   0.0155   1.0000
  17.500   1.4220   0.08104   0.07518  -0.0219   0.0152   1.0000
  17.750   1.4136   0.08547   0.07972  -0.0228   0.0149   1.0000
  18.000   1.4032   0.09028   0.08463  -0.0239   0.0147   1.0000
  18.250   1.3935   0.09504   0.08951  -0.0251   0.0143   1.0000
  18.500   1.3846   0.09977   0.09435  -0.0265   0.0141   1.0000
  18.750   1.3732   0.10499   0.09968  -0.0281   0.0139   1.0000
  19.000   1.3618   0.11027   0.10509  -0.0298   0.0137   1.0000
  19.250   1.3511   0.11548   0.11041  -0.0316   0.0133   1.0000
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